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Appendix 5. Mechanical Subsystem 5.1 Mass Budget 5.2 Stability Analysis5.3 Stress Analysis 5.4 Thermal Analysis5.5 Pictures 5.6 Test Plan and Results5.7 Component Specifications5.8 Technical Drawings
Appendix 5. Mechanical Subsystem
Stability Analysis
Thermal Analysis
Results Component Specifications Technical Drawings
5.1 MASS BUDGET The following table summarizes the mass budget for the mechanical components of the design.
PartName Description Mass (g) Material Qty
MAIN Complete Assembly
The complete assembly of all the components of the MAIN payload. Excluding the FISH. 15657.98 N/A 184
Line Guide AssemblySafety mechanism to brake the line, reel up and reel down 139.04 N/A 1
Line Guide Side BlockBlocks that make up the sides of the line guide's cage 13.37 Aluminium 2
Line Guide PinPins that make up the struts of the line guide's cage 10.57 Aluminium 2
Line Guide Shaft
Shafts to fit inside the supporting bearings of the line guide as well as the shaft coupling to the motor 32.35 Steel 2
M6 20mm Flat Head ScrewM6-1mm machine screw with flat head and 20mm length 4.41 Steel 6
Line Guide MountingMounting parts for the Line Guide Assembly 684.6 N/A 1
Line Guide Bearing
Sleeve bearings used to support the Line Guide AssemblyPdyn = 16.6 kN; Pstat = 52 kN 5.13
Steel with coatings of Bronze and PTFE 2
Line Guide Bearing MountCustom parts to support the Line Guide Bearings 307.81 Aluminium 2
Slide Nut M6Slide nut made for the PU25 profiles 5.91 Steel 4
M6 45mm Flat Head ScrewM6-1mm machine screw with flat head and 45mm length 8.77 Steel 4
Line Guide DriveDrive train for the Line Guide Assembly 3322.194 N/A 1
Rigid Shaft CouplerRigid steel parallel shaft coupler for 10mm to 10mm keyed shafts 187.86 Steel 1
Brushless Motor
Brushless DC Geared Motor with 30W output and 1.5 Nm rated torque 3000 N/A 1
Line Guide Motor SupportPlate to mount the Line Guide Motor to the structure 99.39 Aluminium 1
Slide Nut M6Slide nut made for the PU25 profiles 5.91 Steel 2
M6 12mm Flat Head ScrewM6-1mm machine screw with flat head and 12mm length 3.002 Steel 2
M5 30mm Flat Head ScrewM5-0.8mm machine screw with flat head and 20mm length 4.28 Steel 4
MAIN StructureRigid structure of the MAIN payload 4290.56 N/A 1
PU25 400mm w\ HolesUniversal Profile 25x25x400 with holes at the ends 272.01 Aluminium 2
PU25 350mm Universal Profile 25x25x350 241.63 Aluminium 6
PU25 266.488mm Universal Profile 25x25x266.488 183.98 Aluminium 4
PU25 200mm w\ HolesUniversal Profile 25x25x200 with holes at the ends 133.03 Aluminium 4
PU25 150mm Universal Profile 25x25x150 103.56 Aluminium 4
Angle Adaptor
Piece to join the profiles at an angle; 500 N max loadHinge 6 30x30, heavy-duty 28.86 Aluminium 8
Mount Bracket
Custom corner bracket to mount the MAIN on the gondolaAngle Bracket 6 30x30 Zn, white aluminium, similar to RAL 9006 28.1 Steel 4
Slide Nut M6Slide nut made for the PU25 profiles 5.91 Steel 12
M6 10mm Button Head ScrewM6-1mm machine screw with button head and 10mm length 3.12 Steel 8
M6 20mm Button Head ScrewM6-1mm machine screw with button head and 20mm length 4.87 Steel 36
MAIN InsulationInsulation around the MAIN payload 2435.07 N/A 1
Insulation Frame 775mmAluminium frame to support the insulation panels 79.68 Aluminium 4
Insulation Frame 400mmAluminium frame to support the insulation panels 41.13 Aluminium 4
Insulation Side PanelStyrofoam panel to insulate the sides of the MAIN payload 348.78
Low-Density EPS 4
Insulation Top PanelStyrofoam panel to insulate the top of the MAIN payload 156.71
Low-Density EPS 1
Insulation Bottom Fill
Styrofoam panel to insulate the bottom of the MAIN payload and secure the FISH 400
Low-Density EPS 1
Reel Mount Mounting assembly for the reel 1024.01 N/A 1
Spinning ReelDaiwa Saltiga Surf Spinning Reel 6000 530
Magnesium Alloy Body 1
Reel Mount Plate6mm thick mount plate for the reel and bail-flip stopper 312.71 Aluminium 1
Bail-Flip Stopper
Aluminum block to flip the bail back as a turn of the reel is done when the bail is open 103.8 Aluminium 1
M6 20mm Flat Head ScrewM6-1mm machine screw with flat head and 20mm length 4.41 Steel 6
M6 Washer 4mm thick M6 washer 6.85 Steel 4
Slide Nut M6Slide nut made for the PU25 profiles 5.91 Steel 4
Reel Drive Drive assembly for the reel 3342.724 N/A 1
Rigid Shaft CouplerRigid steel parallel shaft coupler for 10mm to 10mm keyed shafts 187.86 Steel 1
Reel Shaft
Rigid steel shaft for the reel, with M5 right-handed end and a 10mm keyed end 33.26 Steel 1
Reel Motor MountPlate to mount the Reel Motor to the structure 98.48 Aluminium 1
Brushless Motor
Geared motor with brake or self-lock and rated at 30W output, 150 to 200 RPM, and 1.5 to 2 Nm 3000 N/A 1
M6 12mm Flat Head ScrewM6-1mm machine screw with flat head and 12mm length 3.002 Steel 2
M5 30mm Flat Head ScrewM5-0.8mm machine screw with flat head and 20mm length 4.28 Steel 4
Bail ReleaseBail release mechanism for the reel 419.78 N/A 1
Servo Motor
FUTABA S3801 (Segelbåtsservo)with 140 degree motion and 4.8 to 6 V input 107 N/A 2
Bail Release ArmArm which extends across the reel to open the bail 25.92 Aluminium 1
Servo Motor Mount Mount plates for the servos 31.48 Aluminium 3
Bail Release LeverLever which extends to hold the Bail Release Arm 15.62 Aluminium 2
M6 10mm Button Head ScrewM6-1mm machine screw with button head and 10mm length 3.12 Steel 6
Slide Nut M6Slide nut made for the PU25 profiles 5.91 Steel 6
FISH 1849.23External Assembly All external structure 658.87
Nose Skin
0.5 mm Aluminium sheet metal machined to form a cone. Attached to the skin 36.87 Aluminium 1
Skin
1mm thick Aluminium Clad cylinder. 325 mm in length with a 160 mm diameter 622
Aluminium/Steel 1
Insulation MainInsulation of the FISH components 68.32
Nose Insulation160 mm diameter, 75 mm height, cone shaped styrofoam 21.49
Low-Density EPS 1
Body Insulation
Side insulation, approximately 25 mm thickness and height of 50 mm 23.57
Low-Density EPS 1
Top Insulation1160 mm diameter, 25 mm height, semicircle styrofoam 11.63
Low-Density EPS 2
Insulation Tail Insulation fo the radio 93.49
Upper Insulation50mm thick insulation, 160 mm diameter, covers Zigbee 46.45
Low-Density EPS 1
Lower Insulation50mm thick insulation, 160 mm diameter, covers Zigbee 46.44
Low-Density EPS 1
Zigbee Radio UnitRadio Unit to communicate with MAIN 0.6 N/A 1
Internal Structure Internal Structure of the FISH 600.81
Base
160mm diameter base, 1mm thick. Attachs all components to it 46.54 Aluminium 1
Stiffener
1.5 mm thick, 60 mm wide, 160 mm long, 20 mm deep, C-shape. Provide stiffness to base 55.89 Aluminium 1
side
3 mm thick, 50 mm height, 20 mm wide side to hold the top and the bottom together 11.54 Aluminium 2
Top Plate
Attachs to I Beam, holds the parachute up. 160 mm diameter disc, 1mm thick 10.1 Aluminium 1
I-beam1
C-shape, 0.5mm thick, 25 mm height, 20 mm wide, 160 mm long. Attachs to line, parachord and skin 9.1 Aluminium 2
Parachord tubesProtect parachord from I beam, 0.5 mm thick 3 Aluminium 2
Processor Unit
Determines FISH velocity and altitude for parachute deployment 162 N/A 1
Control UnitControls the setting of ground altitude 10 N/A 1
Release UnitCuts line when parachute needs to be activated 10 N/A 1
PCB Houses electronics 55 N/A 1Accelerometer 45 N/A 1
Battery HolderHolds the Batteries, 60mm x 60 mm 15 Plasic 1
Battery Provide power 24 N/A 6
Parachute MechanismThe mechanicsm the deploys the parachute 380
Parachute
Parachute to be used for safetly mechanism. Spring loaded, 150 mm diameter 50mm compressed 370
Steel spring, Parachute material 1
Ring10 mm ring to strengthen hole in parachute 10 Steel 1
ParachordAttachs the Structure to the Parachute 10 Parachord 1
Fasteners All Fasteners 47.74
M4 Screw Button head Joint thick structures together 2 Steel 6M4 Nylon lock nut Attach to screw 0.9 Steel Nylon 6M5 Washer Attach to screw 0.39 Steel 6M4 Aluminium Rivet Light attachments 0.5 Aluminium 48
Epoxy Glue Epoxy 1Cable Tie Attach Cypres unit to base 1 Plastic 4
LINE The complete Line assembly 40
SuperBraid0.5 mm thick braided fishing line, 300 m Dyneema 1
Swivel High strength swivel 20 Steel 2
Line tubesProtect line from I beam, 0.5 mm thick 10 Aluminium 2
5.2 STABILITY ANALYSIS
Static Margin Calculations The static margin requires a two calculations.
1. Calculation of the Aerodynamic Centre 2. Calculation of the Centre of Gravity
Centre of Pressure The Centre of Pressure calculation was conducted using a software called JavaFoil (1). This is a program used to analyse the aerodynamic properties of an aerofoil. Before any calculations could be made a diagram of the FISH aerodynamic surfaces had to be produced so to be inputted in to the program. The overall characteristics of the FISH are summarised below. Once these characteristics were placed into the Java foil a slight rotation was placed on the design to simulate a deviation from the normal position. JavaFoil is able to calculate the pressure on each of the surfaces of the capsule and are shown in Figure XX. These pressures were then used to calculate the centre of Pressure via the static force equations. The equation is stated below.
�� =∑(�/�). ���� − ∑(�/�). �������
∑ ���� − ∑ �������= 0.66 = 264 ��
Where x/L is the position of the pressure along the x axis.
75mm 325mm
160mm
Figure 0.1: Surface Pressure of Skin of FISH
CoG Calculation The CoG calculation is conducted through the CAD program Solidworks. The result of the CoG produces
��� = 165�� from the nose.
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1-10
-8
-6
-4
-2
0
2
4
6
8Centre of Pressure Calculation
x/length
Pre
ssur
e
5.3 STRESS ANALYSIS
Critical Force for the FISH Structure Calculations Parachute Opening The most critical force that shall be applied to the FISH is when the parachute is deployed. The parachute characteristics have been described in the main document and are summarized below.
Cd 1.5
Diameter 0.66 m
Surface Area 0.342m2
If the parachute opens at a low altitude when the FISH is at terminal velocity it will create a drag force on the FISH which is assessed to be the largest stress produced during the whole mission. The maximum force that is experienced by the parachute is given by the following equation
���� =2���������
���1 −
������
���������
Ref: (1) Where T = length of time to open chute = 0.5s and g = gravity (1). The initial and finial velocities are calculated using the terminal velocity equation.
� = �2�
�� ��
Thus Where for the initial conditions
Characteristics Initial Final W 1.8x9.81 = 17.66 N Cd 0.2 1.5 ρ 1.2 kg/m3 S 0.082π = 0.02m2 0.332π = 0.342m2 V 85.78 m/s 7.57 m/s
Thus the maximum force on the parachute is
���� = 563.11 � This force will be experienced through the paracord that is attaches the parachute to the FISH’s structure. G’s produced by Gondola One of the design limitations was to make sure the structure can handle 10 g’s . Since the FISH’s total mass is 1.8kg. Thus the maximum force that FISH will experience during typical mission loads is
� = �� = 1.8�� × 10� × 9.81 = 176.58 � This force will be experience through the attachment of the Fishing line to the FISH structure. Summary Thus the critical forces experienced by the FISH is
Force (N) Interface 176.58 Fishing line attached to FISH structure 563.11 Parachord attached to FISH structure
Reel Brake Analysis The brake of the system has been analysed to one of the more important safety components of the system. Thus a larger level of study has gone into this device. In the previous design the reel.SMRT was meant to have a variable brake system with a motor interfacing with the brake and hence being able to control it. Unfortunately due to reel constraints this idea was substituted for a non-variable brake which is preset before launch. This has many advantages and disadvantages, firstly with a variable brake the user is able to control it thus can increase the force if the brake is not strong enough. This is a more adaptive method to unforeseen environmental hazards. The disadvantage with the variable brake is that it increases the complexity of the system and also it is reliant on more systems to work for the brake to function which is a safety risk in itself. Thus it has been decided that a non variable brake is best for the system. The reel brake has a maximum force 300 N which allows for a wide range of braking strength alternatives. In Figure 0.2 it is shown the stopping distances and time for different brake strengths along with the g’s that are experienced by the FISH in Table 1.
Figure 0.2: The FISH's displacement for different Brake Forces
0 0.5 1 1.5 2 2.5-40
-35
-30
-25
-20
-15
-10
-5
0
Time(seconds)
Z D
ispl
acem
ent f
rom
the
poin
t of B
rake
app
lied
(m)
Z Displacement of the FISH at various Brake Forces
Fb = 40Fb = 60Fb = 80Fb = 100Fb = 120Fb = 140Fb = 160
Displacement and G’s Experience by FISH for various Brake Forces
Brake Force (N) 40N 60N 80N 100N 120N 140N 160N G’s 1.27 2.4 3.53 4.66 5.8 6.93 8.06 Max displacement when braking (m)
39.18 20.89 14.34 10.97 8.91 7.53 6.54
Table 1: Characteristics of the FISH at Various Brake Forces
By observation of the G’s experienced by the FISH when the brake is applied, one can see that the larger the brake force, the larger the G’s that are incurred by the FISH. The two defining factors that affect the choice of the brake force is the maximum distance the FISH is allowed to travel before the line is expired and also the maximum number of G’s that the structure or line can withstand. These two values are summarised in the table below Reference Maximum Deceleration Length 50 m Maximum stress 100 N Line Critical Force Appendix 5.3 To satisfy these two conditions a braking force of approximately 100 N has been chosen. To make sure this system is safe and the brake will work every time, the system will be tested under a various mission environmental conditions. How these conditions will affect the brake will be determined in the tests and the brake force will be set accordingly. In conclusion, a non-variable braking system will be used to reduce the velocity of the FISH because it decreases the complexity of the system thus increasing the relative safety of the braking system. This brake shall be pre-set before mission launch to 100 N.
SuperBraid Line Critical Phases It has been assessed that there are two critical phases during the mission that the line has to endure.
• FISH deceleration phase
• Housing of FISH phase
These phases produce critical forces on different sections of the line which need to be analyzed for design purposes. FISH Deceleration Phase The Deceleration Phase starts when the brake is applied to the line and the FISH starts to slow down. The brake force is 100 N (appendix) which is a approximately a 5 g slow down. This will cause the line to experience a 90 N through it.
� = �� = 1.8 × 9.81 × 5 ≅ 90� Since there is only one line that is connected between the FISH and the reel, 100% of this force will be need to be absorbed by it. From the Test M.3 one can see that the braking strength of a single line is 196.2N at its minimum. Thus the FS is 2.6 which is sufficient enough for the flight.
�� =196.2
90= 2.18
A note, if the gondola experiences a vertical motion when the line is being decelerated, these forces will not be experienced by the FISH. The brake of the reel is designed to only place a constant force on the line, when more g’s are experienced by the FISH the brake merely takes longer stop the FISH. Thus the force on the line will never be larger than the braking force. Housing of the FISH Phase During the housing of the FISH the line experiences the largest force during the mission. Stipulated via the BEXUS user manual the FISH needs to withstand 10 g’s (Req.T.M.1) during the mission. Thus the force that will be experience by the line will be 177N.
� = �� = 1.8 × 9.81 × 10 = 176.6� These forces will be taken over the design shown in the figure below.
Thus the maximum force that is placed over the line is
���� =�
2���� + ��
This force is calculated to be F 177N H 400mm b 41.5mm
����� = 88.97 ≅ 90�
For each of the braids that will be attached to the I-beam there will be 5 lines braided thus reducing the risks from any faults in the line, because the stress will be divided across the lines evenly. Thus the maximum force on each of the lines is
���� ���� =����
# �����=
88.875
≅ 18�
Since the maximum strength of the line is 196.2 N, (Test M.3) this is will produce a FS of
�� =196.2
18= 10.9
Thus the FS when the FISH is being housed is 13.9 which is well above the required limits.
F
�2�
��� + ��
b
L
d
H
�2�
��� + ��
Summary of the Critical Phases The critical phases are summarised in table XX. Critical Phases Critical Forces FS FISH deceleration 90 N 2.18 FISH housing 18 N 10.9 These FS are well within the range of the breaking stress of the line
Stress Calculations As shown in the Critical Force Calculations (Appendix 5.3) the maximum stresses the structure will receive is summarized below. Critical Case Force (N) Interface 1 563.11 Parachord attached to FISH
structure 2 176.58 Fishing line attached to FISH
structure Both of these forces will be experienced through the parachord or fishing line, which are both attached to the I-beam situated at the base of the parachute. I Beam Properties and 2nd moment of Inertia The I beam is 160 mm long with a cross sectional area shown in Figure XX. All dimensions are in mm’s.
The 2nd moment of area for this I beam needs to be calculated so the future stress calculations can be made. This has been calculated like such.
The local 2nd moment of inertia for beams 1, 2, and 3 are
���� =���
12= ����, ���� =
2���
12
With the local CoG distances from the global CoG as such
Member Local CoG from Global CoG
1 �� = � + �
2
2 �� = 0 3 �� = −
� + �2
1
0.5
0.5
30 160
25
L
T
T
2
1
3
H
2T
Using the parallel axis theorem where
�� = � �� ����� + ���
Thus
��� = ��� =���
12+ �� �
� + �2 �
�
��� =2���
12
Hence
�� = 2���
12+ 2�� �
� + �2 �
�+
2���
12
Where Distance (mm) L 30 H 24 T 0.5
Therefore
�� = 4553.8��� Area of Beam The Area of the Beam is
� = 2�� + 2�� = 54�� Bending Moment Analysis For critical case 1 the position of the paracord to the I beam is shown in the diagram along with the forces that are applied The force balance diagram for this beam is Shear Force Balance
�2
F
�2
d d
H
d
�2
�2
�2
�2
d
Shear Stress Bending Moments Thus the maximum bending moment is
�� =��2
Horizontal Force Balance Compressive/ Tensile Force Thus maximum Compressive/ Tensile Force
���� =��2�
The maximum stress for this beam is then
���� =�����
��+
��
−�2
�2
−��2
d
��2�
��2�
d
��2�
��2�
−��2�
��2�
http://physics.uwstout.edu/StatStr/statics/Beams/beam41.htm Critical Case 1 For critical case 1 the parameters for calculating the maximum stress is
F 563.11 N d 20 mm H 1000 mm L 160 mm Y 12.5 mm A 54 mm Ix 4553.8 mm4
The maximum axial force is
���� =��2�
= 5.63 �
The maximum bending moment
���� =��2
= 5631.1 ���
The maximum stress calculated
���� =�����
��+
��
= 15.46 + 0.10 = 15.56�
��� = 15.56���
The Factor of safety is
�� =110
15.56= 7.07
Critical Case 2
F 176.58 N d 80 mm H 30 mm L 160 mm Y 12.5 mm A 54 mm Ix 4553.8 mm4
Note: that there is only one line attached to this beam, but the bending moments are still the same if d is half the length of the beam. The maximum axial force is
���� = 0 � The maximum bending moment
�� =��2
= 7063.2 ���
The maximum stress calculated
���� =�����
��+
��
= 19.39 = 19.39 �
��� = 19.39���
The Factor of safety for the yield tensile strength of aluminum as 110 MPa
�� =110
19.35= 5.67
The Summary table of the Maximum stresses and Factors of Safety for the two critical cases
Critical Case Maximum stress (MPa) FS 1 15.56 7.07 2 19.39 5.67
Base Insert analysis As shown in the Critical Force Calculations (Appendix 5.3) the maximum stresses the structure will receive is summarized below.
Critical Case Force (N) Interface 1 563.11 Connected to I beam
Translating this force into the force the Base will experience will be needed to be done via calculation of the acceleration.
� =�
�����=
563.111.8
= 312.9 �/��
This acceleration will be translated to all components on the base which are the battery and holder, the pcb, accelerometer, and the Cypres unit. The forces have been calculated in table XX
Component Mass (kg) Force (N) Cypress unit 0.183 F1 = 57.26 Battery and Holder 0.164 F2 = 51.52 PCB 0.055 F3 = 17.21 Accelerometer 0.045 F4 = 14.08
Thus the force balance equation is Thus the forces equate to
�� + �� = �1 + �2 + �3 + �4 And
Fb Fa
F1 F2
F4
F3
D1
D2
D3
L
�� =�1 × �1 + (�2 + �3) × �2 + �1 × �3
�
Where
F1 57.26 N D1 41 mm F2 51.52 N D2 80 mm F3 17.21 N D3 95 mm F4 14.08 N L 160 mm
Thus Fa 82.67 N Fb 57.4 N
I Beam Properties and 2nd moment of Inertia The I beam is 160 mm long with a cross sectional area shown in the figure below. The length of the stringers are actually 16mm long but for the analysis have been reduced because the corners at the end are smaller. If this beam is able to withstand the bending moments that the forces above produce then the actual beam should as well. All dimensions are in mm’s. The 2nd moment of area for this I beam needs to be calculated so the future stress calculations can be made. This has been calculated like such. CoG, is locate calculated as such
� =�2
� = � × �� + �2
× �� =��� + 1
2 ���
2�� + ��
60 160
10
1
t
L
CoG
d1
d2 1
2
3 H
4
The local 2nd moment of inertia for beams 1, 2, and 3 are
���� =���
12= ����, ���� =
���
12
Using the parallel axis theorem where
�� = � �� ����� + ���
Thus
��� = ��� =���
12+ ��(�2)�
��� =���
12+ ��(�1)�
Hence
�� =���
12+ ��(�2)� +
���
12+ ��(�1)�
Thus since
t 1.5 mm L 58 mm H 15 mm
Then the centre of gravity is along this the distance to the local CoG’s
X 30 mm Y 3.05 mm from base d1 2.55 d2 4.45
Therefore
�� = 1446.2��� Area of Beam The Area of the Beam is
� = �� + 2�� = 78�� Bending Moment Analysis The force balance diagram for this beam is
Fb Fa
F1 F2
F4
F3
D1
D2
D3
L
Shear Stress Bending Moments Thus the maximum bending moment is
�� = �� × �1 + (�� − �1) × (�2 − �1) The maximum stress for this beam is then
���� =�����
��
Critical Case For critical case 1 the parameters for calculating the maximum stress is
Fa 82.67 N F1 57.26 N D1 41 mm N D2 80 mm Y 15 mm
The maximum bending moment
���� = �� × �1 + (�� − �1) × (�2 − �1) = 4340.46 ��� The maximum stress calculated
���� =�����
��= 45.02
���� = 45.02���
Fa
Fb
Fa-F1
Fa-F1-F2
Fa*D1 + (Fa-F1)*D2)
Fa*D1
The Factor of safety is
�� =110
45.02= 2.44
The Summary table of the Maximum stresses and Factors of Safety for the two critical cases
Critical Case Maximum stress (MPa) FS 1 45.02 2.44
Stress Analysis of the Line Guide Mechanism It was determined through dynamics analysis that the maximum force exerted on the line guide pins will be of 100 N per pin. However, due to the complexity of the analysis, not shown for sake of conciseness, the load is assumed to be of 200 N per pin. By performing a finite-element analysis of the pin, using Cosmos, with the following boundary conditions: - Fixed ends in the middle of the screws - Distributed load of 200 N on the pin’s outer surface The safety factor for aluminium was found to be 35. Figure 0.3 shows the Von Mises stress distribution in the pin on a magnified displacement field.
Figure 0.3 Line Guide Pin's FEA Results - Von Mises Stress
The side blocks, on which the line guide pins are fixed were analysed with the same loading conditions as the pins, i.e. a 100 N force on each end of the block, due to the fact that the reaction load on either side of the pins are half the total load on the pins. The finite-element analysis was performed, using Cosmos, with the following boundary conditions: - Fixed at the fastening point to the line guide shaft, where the screw is attached
- Distributed loads on the fastening points of the pins of 100 N on either side The safety factor for aluminium was found to be 5. Figure 0.4 shows the Von Mises stress distribution in the side block on a magnified displacement field.
Figure 0.4 Line Guide Side Block's FEA Results - Von Mises Stress
Stress Analysis of the Reel Mount Plate In order to analyse the stress on the reel mount plate, the load have been identified to consist of 100 N attributable to a 5 G acceleration given to the FISH of 1.8 kg, rounded up, in addition to a 50 N attributable to 10 G acceleration, inherent to the BEXUS flight, applied on the reel itself of 0.5 kg, rounded up. In total, a force of 150 N is applied to the mount plate, however, it is important to notice that the force is applied through the center-line of the reel, approximately, which is offset from the plate by 10 cm which result in a moment applied to the plate of 15 Nm. Finite-element analysis, using Cosmos, shows that the safety factor is 3 for a 6 mm thick steel plate, see Figure 0.5, loaded under the following conditions: - Fixed at the four mounting screws - Load is applied as distributed inside the mounting slots of the base of the reel Although the factor of safety is not great, one can see that the regions of higher stress are only present near the mounting holes and the slots. The stress concentrations are most probably due to the hard boundary conditions present at those areas which will not be so hard in reality.
Figure 0.5 Reel Mount Plate FEA Results - Factor of Safety > 3
Stress Analysis of the Reel Motor Mount Similar to the analysis of the reel mount plate, the reel motor mount has been analysed for the loading of the 200 N which comes from a 10 G acceleration on the motor. The finite-element analysis, using Cosmos, was performed with the boundary conditions below and a factor of safety of 3 was also obtained for similar reasons as for the reel mount plate, as shown in Figure 0.6. - Fixed at the mounting holes - Distributed load of 200 N applied to the mounting holes of the motor
Figure 0.6 Reel Motor Mount FEA Results - Factor of Safety > 3
Stress Analysis of the Servo Mounts A final critical part in the assembly is the servo motor mount which are subject mainly to the fairly good torque that the servos can produce, i.e. 1.4 Nm. The servos are 70 mm of height, that is, 70 mm between the top and bottom mounting holes. For reacting to a moment of 1.4 Nm with a moment arm of 70 mm one easily obtains a load of about 20 N, sideways. Finite-element analysis, using Cosmos, with the boundary conditions below has given a factor of safety of 32, as shown in Figure 0.7 by the Von Mises stress on a magnified displacement field. - Fixed at the mounting holes - Distributed load of 20 N on the mounting holes of the servos
Figure 0.7 Servo Motor Mount FEA Results - Von Mises Stress
Stress Analysis of the Aluminium Profile Structure The aluminium profiles used for the structure of the MAIN payload are so-called PU25 from Solectro which are specified by the manufacturer and by previous analyses done at the IRV in cooperation with ESRANGE experts to be: � = 70 ��� ������ = 270 ��� � = 14.3 ∙ 10�� �� � = 12.5 �� = 0.0125 � � = �
�= 1.144 ∙ 10�� ��
The above leads to the determination of the maximum axial load on the sections of PU25 which are limited by the yield stress as opposed to buckling loads for lengths under about 40 cm. This is the
case for all the segments of the MAIN payload’s structure. As seen from the MAIN payload structure in Figure 0.8, the main segments under load are the two-force members making up the bottom pyramid structure and their base supporting beams. The middle square of PU25 segments also carried a bending load but it is smaller than the bending load on the bottom segments. Consequently, the only elements that near to be analysed are the two-force members of 266.5 mm length and the bottom long beams of 400 mm length. The maximum axial loading is specified as 68.8 kN and the maximum bending load on the bottom beam can be obtained from Euler-Bernouilli beam theory. The end conditions used here are simple supports although in reality the ends are fixed to some extent, but since the simple supported case is more restrictive on the maximum load it is just an additional factor of safety in case the end are not properly conditioned at assembly time. One can follow these simple calculations to find the maximum load for bending conditions, for a point load applied at the centre of the beam:
���� = ����
� ��������,����� = ��������
�= �∙�.���∙������∙���∙�����
�.��= 3088.8 �
Now that the maximum loading conditions are established, one can identify the expected loads on the MAIN payload.
Figure 0.8 MAIN Payload's Structure
If one assumes that the upper rectangular “cage” is a rigid body which supports all the loads of the structure, consisting of the weight of all components except the bottom segments under 10 G of upward acceleration. First, the weight of the upper “cage” is calculated as ����� = ������ − ������ �������� = 16.2 �� − 4.2 �� = 12 �� ����� � 1200 � ����� 10 � ������������ ������� Simple statics analysis will show that the axial load on the two-force members, at an angle of 18.7 degrees from the vertical, will be about of 315 N which is far below the maximal axial load of the PU25 sections, with a factor of safety of 218. However, it must be noticed here that the PU25 attached to the remaining structure via angle adaptor from Item which are specified at a maximum load of 1000 N under fixed conditions. This reduces the factor of safety to 3.17 which is still a good
Pload
figure. Now for the bending loads, it is clear that the axial load of the two-force members have to be reacted upon by the ends, i.e. the beam segments of the lower square structure. As calculated above, the maximum bending load is 3088.8 N which, under 315 N of load, correspond to a factor of safety of 9.8 which is well within reasonable limits. As a final note, one could remark that there are additional components (electronics and batteries) which were not taken into consideration in the analysis as well as the mass of the lower segments of the structure. However, given the obtained factors of safety, one can, with confidence, assume these additional loads not to drive the stresses above the yielding limits and, in fact, still conserve a significant margin of safety. Another final issue, elaborated in the thermal analysis, is the likelihood of adding an insulation section at the interface between the lower angle adaptors and the two-force members which could have repercussions on the loading at those interfaces. However, the structural strength of EPS material is good and most of the load will be taken by the joining screws which are rated at more than 20 kN of axial load (for M6 steel screws of length of 60 mm), as specified by McMaster-Carr’s industrial ratings of ISO 7380 for class 10.9 screws.
5.4 THERMAL ANALYSIS Thermal Analysis of the MAIN Payload The stratospheric environment poses some challenges and some advantages in terms of thermal considerations. The challenge is that the temperature ranges experienced in the BEXUS flight include a passage of the tropopause at temperatures -70 degrees Celsius to a rise in the stratosphere up to temperatures of -30 degrees at the altitude of the BEXUS’ steady flight period. The advantage is that the convective heat transfer can be neglected from the dual effect of extreme low pressure ambient air and the shielding that the gondola provides to an extent from winds or natural convection. The thermal problem can be stated as the problem to maintain inside temperatures to levels at which the components can operate while handling the heat generated by those same components during operations. First to identify thermal loads: Thermal Heat Sources:
• Heat generated from the reel motor, estimated at 30 W
• Heat generated from the line guide motor, estimated at 30 W
• Heat generated from the batteries, estimated at 5 W
• Heat generated from the electronics, estimated at 2 W
Then to identify the heat sinks, one can remark that in the absence of convection, the main heat sink is through the interfaces to the gondola and possibly by radiation. The radiation will first be neglected and the efforts will be concentrated on the interface to the gondola. Assuming the gondola is in thermal equilibrium with the environment and that its size, in terms of thermal capacity, is much larger than the MAIN payload, the gondola can be considered as a heat reservoir, i.e. with constant temperature and infinite heat capacity. The strategy will be to maintain the temperature in a selected portion of the MAIN payload by designing the thermal interfaces to the outside. The goal is to impede the flow of heat to the outside in order to keep the temperature inside within operating ranges without needing too much power during the non-operating phases of the mission. Then during the operating phases of the mission, the heat generated from the sources needs to be evacuated or stored in the bulk of the MAIN payload. Let us first concentrate on the non-operating phases of the mission. As seen in Figure 0.9, the payload bulk is set against the gondola’s heat reservoir via aluminium profiles which will act as heat pipes since all other thermal conduction processes are negligible compared to these heat pipes. Since all components of the MAIN payload are attached to the upper “cage” structure, it is essential to maintain the temperature of this section within operating ranges of the components. Except for the electronics, all components only require temperatures above -20 degrees Celsius in order to guarantee good operations. The electronics for their part can be treated as a separate thermal problem, one which poses no challenge and will not be considered here. A second property of the MAIN payload bulk is the fact that it is almost entirely built of aluminium which is a remarkable heat conductor and makes the temperature quasi uniform in that section.
Figure 0.9 MAIN Payload's Thermal Sections
In the light of the aforementioned assumptions, one can realise that the problem can be reduced to finding how much heat will flow through the heat pipes in order to maintain a temperature of -20 degrees Celsius in the bulk when the reservoir is at -30 degrees at steady state and -70 degrees for a short period. It is clear that aluminium is a good conductor and that much heat will be able to flow from the bulk to the reservoir. For that reason, the heat pipes will be terminated by a layer of insulating polystyrene (EPS). Structurally, EPS is almost as strong as aluminium in compression which may come to a surprise but is a known fact. Nevertheless, the mounting of the ends of those two-force members will be accomplished with M6 steel screws which are by far strong enough to hold the structural loads. And hence, a 50 mm thick section of EPS will be terminating the heat pipes. This leads to the following analysis:
�
����= �
���+ �
�����������
Where the C stands for thermal conductance in W/K. It remains to obtain the conductance of the aluminium heat pipes, the screw and the EPS section.
��� = ���
=��� �
�� ∙ �.������ ��
�.���� �= 0.2791 �
�
������ = ���
=�� �
�� ∙ �.��������� ��
�.�� �= 0.01636 �
�
���� = ��
� = 0.68 ����
∙ 0.000255 �� = 0.000425 ��
From the above, we obtain an overall heat conduction of 0.01583 W/K for one member. As there are four members in the structure, this number is multiplied by 4 and we obtain a thermal conductance between the bulk and the reservoir of 0.06332 W/K. This means effectively, that the thermal insulation provided at the interface to the gondola can keep a temperature difference of almost 16 degrees Celsius with only 1 W of heating power, which is provided by the electronics easily. Of course, during the ascent, the tropopause will impose a temperature difference of 50 degrees Celsius between the bulk and the reservoir which will demand about 3.3 W of power from the heaters and the electronics combined, and only for a fairly short amount of time, less than 1 hour. Additionally, some small heaters will be required from specialised items such as the batteries and the reel if our tests find that these are necessary.
Now the remaining issue is the operating phases of the mission in which to much heat is generated and needs to be handled. In classical thermal analysis, it would be advisable to evacuate the heat from the payload at the same rate as it is being generated. However, in this case, the operating phase of the mission is at most 2 hours due to the flight characteristics. The strategy employed to is to hold the heat within the bulk of the MAIN payload. One can calculate the heat capacity of the bulk by summing the aluminium and steel components of the bulk, which comes up to 3654 g of aluminium and 4900 g of steel. One then obtains the thermal capacity: ��� = ��� ∙ ��� + ��� ∙ ��� ��� = 0.896 �
�� ∙ 3654 � + 0.46 �
�� ∙ 4900 � = 5528 �
�
����� ∙ � = ��� ∙ ∆� = 5528 ��
∙ 70 � = 386.96 ��
Where C refer to the total heat capacity. Here, the temperature difference is taken as 70 degrees Celsius because after the non-operating phase, the temperature is kept at -20 degrees and the maximum operating temperature of the limiting components is 50 degrees Celsius, as seen in Figure 0.10. If one considers the operating condition that one motor is operated at full capacity, generating 30 W of heat, along with the heat of the batteries and the electronics of at most 10 W, one obtains the following operating time:
� = ������ ��� �
= 9674 � = 161 ������� = 2 ℎ���� 41 �������
The above clearly shows that the MAIN payload can operate under full duty cycle for the whole time of the experiment without over-heating. Furthermore, some heat evacuation will be done via radiation by simply painting the inside of the MAIN payload in black and leaving the outside surface white, limiting the heat input from radiation while evacuating heat when the inside is hot and not so much when it is cold.
Figure 0.10 Thermal Data Table for MAIN Payload
5.5 PICTURES
Figure 0.11 Showcase of Purchased Hardware
Figure 0.12 Mikael Persson in First Step of Assembly
Figure 0.13 Line Tied to the Reel with Locked Half Blood Knot
Figure 0.14 The Saltiga Surf Spinning Reel 6000 with 200m of Braided Line
5.6 TEST PLAN AND RESULTS The tests are planned according to the table on the following pages.
Test No Test ObjectiveRisks Assessedor Requirements Description
Mechanical Tests
M.1 Reel strength Test - Normal
Confirm that the reel can withstand the accelerations of the gondola and support the FISH Risk.M – M 07
The reel will have to succesfully support an oversized weight with vibrations
M.2 Reel strength Test - Mission temp
Confirm that the reel can withstand the accelerations of the gondola and support the FISH at mission temperature Risk.M – M 07
The reel will have to succesfully support an oversized weight with vibrations at mission temperature
M.3 Line Strength Test - Normal Test the line strength until it breaksRisk.M – M 08Risk.M – M 09
The line will be pulled tension until it breaks
M.4 Line Strength Test - Mission tempTest the line strength until it breaks at mission temperature
Risk.M – M 08Risk.M – M 09
The line will be pulled tension until it breaks at mission temperature
M.5 Brake strength Test - Normal
Confirm that the reel brake can withstand the shock of the braking of the FISH
Risk.M – M 01Risk.M – M 03Risk.M – M 04
The line will be dropped with a mass to various heights and brought to a stop
M.6 Brake strength Test - Mission temp
Confirm that the reel brake can withstand the shock of the braking of the FISH at mission temperature
Risk.M – M 01Risk.M – M 03Risk.M – M 04
The line will be dropped with a mass to various heights and brought to a stop, under cold conditions
M.7 Reliability of Bail Mechanism TestConfirm the repeatability of the bail mechanism under various conditions Req.F.2
The bail release system will be tested under all possible conditions and repeated to obtain confidence in the repeatability of the mechanism
M.8 Parachute deployment Test Test to see if the Parachute deploys Req.O.3The FISH will be dropped from a tall building and the parachute deployed
M.9 Line guide strength test
Test that the line guide is strong enough to withstand the shock of braking the FISH Risk.M – M 06
The line guide will have to succesfully support an oversized weight with vibrations
M.10 Line guide functionality - NormalTest that the line guide's operating principles are appropriate Risk.M – M 06
The line will be dropped with a mass to various heights, brought to a stop and reeled back by the line guide
M.11Line guide functionality - Mission temp
Test that the line guide's operating principles are appropriate under mission temperature Risk.M – M 06
The line will be dropped with a mass to various heights, brought to a stop and reeled back by the line guide at mission temperature
M.12 Line Interface Test - Normal
Test to see the line interface and withstand the mission loads + factor of safety
Risk.M – M 08Risk.M – M 09
The Reel line and fish will be placed in tension to test if it can handle mission load with FS
M.13 Line Interface Test - Mission Temp
Test to see the line interface and withstand the mission loads + factor of safety at mission temp
Risk.M – M 08Risk.M – M 09
The Reel line and fish will be placed in tension to test if it can handle mission load with FS at mission temperature
M.14 Mounting structure testTest that the structure can withstand all loads and vibrations Risk.M – M 07
The structure will have to succesfully support an oversized weight with vibrations
M.15 Reel functionality - Normal Test the functional principles of the reel Req.F.2
The line will be dropped by the reel with a mass to various heights, brought to a stop and reeled back by the reel
M.16Reel functionality - Mission Temperature
Test the functional principles of the reel under mission temperature Req.F.2
The line will be dropped by the reel with a mass to various heights, brought to a stop and reeled back by the reel under mission temperatures
M.17 Reel functionality - Mission PressureTest the functional principles of the reel under mission pressure Req.F.2
The line will be released to the experimental fixture by the reel with a mass to various heights, brought to a stop and reeled back by the reel under mission pressures
M.18 Center of Gravity TestTo locate the center of Gravity of the Fish Req.F.1
The FISH will be place on multiple weight scales to find the x, y, z center of gravity
M.19 FISH aerodynamic Stability TestTo test the Aerodynamic Stability of the FISH Req.F.1
Place a line at the center of gravity and spin the FISH around in a circle, Observe any major movements of the FISH
M.20FISH insulation Thermal Test - Mission Temp
To test if the internal environment of the FISH is at the correct temperature during mission temperature Req.F.7
Place the outer structure and Thermal insulation in a thermal chamber for the mission length and monior the internal temperature
M.21FISH insulation Thermal Test - Mission Temp and Pressure
To test if the internal environment of the FISH is at the correct temperature during mission conditions Req.F.7
Place the outer structure and Thermal insulation in a thermal chamber for the mission length and monior the internal temperature
M.22 Fish Aerodynamic testTo calculate the Cl and Cd of the FISH with respect to its angle of attack Req.F.1
Place the FISH in the wind tunnel and calculate the Cl's and Cd's at various angles of attach
M.23 Reel tether testTo test the over all functionallity of the reel and tether mechanism Req.F.1
The Reel along with the motors will be attached to the test rig and a complete simulation of the system will be conducted
Test No Test Conditions Test Location Required Resources Dates Reliant on Responsibility Participants
M.1 Sea Level conditions Kiruna Large masses May Reel and line present Mikael Campbell, Mikael
M.2 Mission Temperature KirunaLarge massesThermal Chamber June Reel and line present Mikael Campbell, Mikael
M.3 Sea Level conditions Kiruna Force Gauge May Line present Campbell Campbell, Mikael
M.4 Mission Temperature KirunaThermal Chamber Force Gauge May
Line present and thermal chamber times Campbell Campbell, Mikael
M.5 Sea Level conditions Kiruna
Mounting fixtureForce GaugeSufficient drop heightLarge masses May
Reel and line presentTests M.1 & M.3 completed Mikael Campbell, Mikael
M.6 Mission Temperature Kiruna
Mounting fixtureForce GaugeSufficient drop heightLarge massesThermal Chamber or cooling system June
Reel and line presentTests M.2 & M.4 completed Mikael Campbell, Mikael
M.7 Sea Level conditions KirunaLarge massesSufficient drop height August
Structure and Bail release mechanism built Mikael Campbell, Mikael
M.8 Sea Level conditions Kiruna Tall Building August FISH Constructed Campbell Campbell, Mikael
M.9 Sea Level conditions Kiruna Large masses JuneLine Guide BuiltLine present Mikael Campbell, Mikael
M.10 Sea Level conditions Kiruna
Mounting fixtureForce GaugeSufficient drop heightLarge masses
JulyAugust
Line presentStructure and line guide mechanism builtTest M.3 & M.9 completed Mikael Campbell, Mikael
M.11 Mission Temperature Kiruna
Mounting fixtureForce GaugeSufficient drop heightLarge massesThermal Chamber or cooling system
JulyAugust
Line presentStructure and line guide mechanism builtTest M.4 & M.9 completed Mikael Campbell, Mikael
M.12 Sea Level conditions Kiruna Force Gauge JuneLine, Reel and Fish interface constructed Campbell Campbell, Mikael
M.13 Mission Temperature KirunaThermal Chamber Force Gauge June
Line, Reel and Fish interface constructed Campbell Campbell, Mikael
M.14 Sea Level conditions Kiruna Large masses June Structure built Mikael Campbell, Mikael
M.15 Sea Level conditions Kiruna
Mounting fixtureForce GaugeSufficient drop heightLarge masses August
Line and Reel presentReel mechanism builtBail mechanism builtTests M.1, M.3, M.5, & M.7 completed Mikael
Campbell, Mikael, Mikulas
M.16 Mission Temperature Kiruna
Mounting fixtureForce GaugeSufficient drop heightLarge massesThermal Chamber or cooling system August
Line and Reel presentReel mechanism builtBail mechanism builtTests M.2, M.4, M.6, & M.7 completed Mikael
Campbell, Mikael, Mikulas
M.17Mission Temperature and Pressure Kiruna
Mounting fixtureForce GaugeTest fixtureVacuum Chamber August
Line and Reel presentReel mechanism builtBail mechanism builtTests M.1, M.3, M.5, & M.7 completed Mikael
Campbell, Mikael, Mikulas
M.18 Sea Level conditions Kiruna 4 scales, minimum 2 August Fish Constructed Campbell Campbell, Mikael
M.19 Sea Level conditions Kiruna
Line, a place to attach the line to the FISH at the center of Gravity August Fish Constructed Campbell Campbell, Mikael
M.20 Mission Temperature KirunaTemperature sensors, Thermal Chamber June
Structure and Insulation of the FISH constructured Campbell Campbell, Mikael
M.21Mission Temperature and Pressure Kiruna
Temperature sensors, Thermal and presure Chamber June
Structure and Insulation of the FISH constructured Campbell Campbell, Mikael
M.22Mission Temperature and Pressure Lulea Wind Tunnel August Fish Structure Built Campbell Campbell, Mikael
M.23 Sea Level conditionsLeiden Netherlands Delta Utec August
Reel and interfaces are connected Campbell Campbell, Mikael
TEST M.1: Aim Method Results and Discussion Conclusion
TEST M.2: Aim Method Results and Discussion Conclusion
TEST M.3 : Line Strength Test at Room Temperature Aim To verify requirement XXX by determining the braking force of the Superbraid line. Method The line was fed through two carabina’s, which were both attached to a weights machine. This machine is designed for the gym but is easy to use and easy to change the weight that can be placed on the line. The carabina’s was attached to two points that will experience the complete force of the weight once the machine is in used. Specific weights can only be used ranging from 5 – 100 kg moving in 5 kg steps. This experiment was repeated on 5 different pieces of Superbraid so the average braking force could be calculated along with the reliability of the results can be increased. Result and Discussion The results of this experiment are shown in Table 2 Weight (kg) Force (N) Line 1 Line 2 Line 3 Line 4 Line 5 5 49.05 No No No No No 10 98.1 No No No No No 15 147.15 No No No No No 20 196.2 No No No No No 25 245.25 Yes Yes Yes Yes Yes 30 294.3 Yes Yes Yes Yes Yes
Table 2: The Results from the room temperature line strength test
As can be seen the line continuously broke when the weight was 25kg and above, thus is can be assumed that the maximum stress the line can withstand is 196.2N Conclusion
The result show that the maximum force the line can withstand is 196.2 N at room temperature. This verifies the breaking force of the line as stipulated by risk M – M08 and M – M09. To improve the lines characteristics the line will have to be tested at different temperatures.
TEST M.4: Aim Method Results and Discussion Conclusion
TEST M.5: Aim Method Results and Discussion Conclusion
TEST M.6: Aim Method Results and Discussion Conclusion
TEST M.7: Aim Method Results and Discussion Conclusion
TEST M.8: Aim Method
Results and Discussion Conclusion
TEST M.9: Aim Method Results and Discussion Conclusion
TEST M.10: Aim Method Results and Discussion Conclusion
TEST M.11: Aim Method Results and Discussion Conclusion
TEST M.12: Aim Method Results and Discussion Conclusion
TEST M.13: Aim
Method Results and Discussion Conclusion
TEST M.14: Aim Method Results and Discussion Conclusion
TEST M.15: Aim Method Results and Discussion Conclusion
TEST M.16: Aim Method Results and Discussion Conclusion
TEST M.17: Aim Method Results and Discussion Conclusion
TEST M.18: Aim
Method Results and Discussion Conclusion
TEST M.19: Aim Method Results and Discussion Conclusion
TEST M.20: Aim Method Results and Discussion Conclusion
TEST M.21: Aim Method Results and Discussion Conclusion
TEST M.22: Aim Method Results and Discussion Conclusion
TEST M.23:
Aim Method Results and Discussion Conclusion
5.7 COMPONENT SPECIFICATIONS
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Built to Saltiga standards, they are specifically designed for optimum surf fishing performance with today’s braided lines. click here for the perfect performance match to Saltiga Surf spinning reels. Saltiga Surf Features:
Lightweight “Air Metal” Magnesium body treated to prevent saltwater corrosion.
Seven ball bearings, including CRBB anti-corrosion bearings, plus roller bearing
Digigear™ digitally designed and machined gears
Dual, selectable Infinite Anti-Reverse
Tubular stainless Air Bail® Ultra-reliable, manual bail closure Bail lock prevents handle and rotor
turning during a cast Washable design with sealed drag
system Dual CRBB ball bearing line roller Silent Oscillation (with worm gear
levelwind) Lifetime™ Bail Spring Machined aluminum spool and
handle
SASURF5000
Digigear® Digital gear design ensures a perfect mesh.
CRBB Super Corrosion Resistant Ball Bearings.
For optimum performance, use Saltiga® Surf braided
Page 1 of 2Daiwa | Saltiga Surf
01/04/2009http://www.daiwa.com/Reel/detail.aspx?ID=199
line.
CRBB = Super Corrosion Resistant Ball Bearing, BB = Stainless Steel Ball Bearing, RB Roller Bearing
Model Number
Action FW/SW Bearings Gear
Ratio Line Per Handle
Turn Wt. (oz.)
Line Capacity (Lb. Test/Yards)
Drag Max
Surf Spinning Reels
SASURF4500 -/M 4CRBB,3BB, 1RB
4.1 : 1 32.7" 18.00
12/350, 14/300, 17/220 BRAID: 15/620, 20/520,30/330
33.0
SASURF5000 -/MH 4CRBB,3BB, 1RB
4.1 : 1 32.7" 18.00
14/400, 17/310, 20/24030/490 BRAID: 15/910, 20/760,30/490
33.0
SASURF5500 -/H 4CRBB,3BB, 1RB 3.6:1 28.0” 18.70
20/290, 25/230, 30/190 BRAID: 15/1080, 20/900,
30/580 33.0
SASURF6000 -/XH 4CRBB,3BB, 1RB 3.6:1 28.0” 18.70
25/280, 30/230, 40/170 BRAID: 15/1350, 20/1130,
30/730 33.0
© 2009 Daiwa Corporation. Daiwa Corporation believes the specifications in this site to be correct. However, Daiwa reserves the right to make changes in specifications without prior notice. Daiwa prices and programs are subject to change without prior notice. Daiwa reserves the right to make changes without obligation. Site designed and maintained by Dean Mitchell Design
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Measurements are in millimeters. To convert millimeters to inches, insert specs below:
Millimeters: Inches: Convert
Page 1 of 1Futaba® Servo Specs
19/05/2009http://www.futabarc.com/servos/specs-lineart/specs-futm0038.html
Hinge 6 30x30, heavy-duty // Order No.: 0.0.419.80
For connecting profiles at various angles up to 180° and for use as heavy-duty hinges (adjustment range ± 90°). When used in conjunction with the spacer rings, they can be used as freely movable hinges. If the spacer rings are removed, they can be used as rigid angle elements, e.g. bracing, and can also be pinned. The Hinges with Clamp Lever can be locked in position or released. Particularly suitable for adjustable holders, swivel-type arms for Parts Containers and other similar equipment.
Page 1 of 5Hinge 6 30x30, heavy-duty
24/05/2009http://catalog.item-international.com/Onlinekatalog/web/EN/print/artikelinfo/Hinges_hea...
Calculation of the strut length L:
Page 2 of 5Hinge 6 30x30, heavy-duty
24/05/2009http://catalog.item-international.com/Onlinekatalog/web/EN/print/artikelinfo/Hinges_hea...
Page 3 of 5Hinge 6 30x30, heavy-duty
24/05/2009http://catalog.item-international.com/Onlinekatalog/web/EN/print/artikelinfo/Hinges_hea...
Click here to find our CAD data.
Extensive product descriptions and/or fitting instructions are available for this product
Page 4 of 5Hinge 6 30x30, heavy-duty
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Print this page for your records or for later reference.
Page 5 of 5Hinge 6 30x30, heavy-duty
24/05/2009http://catalog.item-international.com/Onlinekatalog/web/EN/print/artikelinfo/Hinges_hea...
Oriental Motor U.S.A. Corp.1001 Knox St.Torrance, CA 90502Tel: 800-418-7903 Fax: 800-309-7999www.orientalmotor.com
Item # AXH230KC-15, Brushless Speed Control System$336.00
Brushless Speed Control SystemBrushless speed control system provides space savings and high power output in an easy to use solution.● Compact board-level driver● Compact, high power motor● Superior speed stability● Constant torque over a wide speed range
SPECIFICATIONS · FEATURES · MULTI-SPEED SETTING METHOD
SPECIFICATIONS
Product Line VEXTA ®
Motor Type Brushless
Motor Frame Size 2.36 in. sq.
Output Power HP (W) 1/25 HP (30W)
Power Supply 24 VDC
Gear Ratio (X:1) 15 :1
Gear/ Shaft Type Parallel Shaft
Rated Torque (lb-in) 14.1
Variable Speed Range (r/min) 6.7 ~ 167
Permissible Load Inertia 77 oz-in2
Type Cable
Available to Ship Same Day (if ordered by 12pm PST) (1-10 pcs)
Components GFH2G15 (Gearhead)AXHM230KC-GFH (Motor)
AXHD30K (Driver)
RoHS Compliant No
Safety Standards ULCSACE
3/7/2009 | Page 1 of 2
CE Marking EMC Directives
Control System Any one of the following methods: 1. By built in potentiometer (1 piece) 2. By externalpotentiometer (20 k Ω 1/4 W) 3. By DC voltage control (0 ~ 5 VDC)
Insulation Class Class E [248°F (120°C)]
Insulation Resistance [Motor] 100 M Ω or more when 500 VDC megger is applied between the windings and theframe after rated motor operation under normal ambient temperature and humidity.
[Driver] 100 M Ω or more when 500 VDC megger between the power supply input terminaland the frame after 1 minute continuous operation under normal ambient temperature and
humidity.
Dielectric Strength [Motor] Sufficient to withstand 0.5 kVAC at 50 Hz applied between the windings and theframe for 1 minute after continuous operation under normal ambient temperature and
humidity.[Driver] Sufficient to withstand 0.5 kVAC at 50 Hz applied between the power supply input
terminal and the frame for 1 minute after continuous operation under normal ambienttemperature and humidity.
Ambient Temperature Range [Motor] 14°F ~ 104°F (-10°C ~ 40°C)14°F ~ 122°F (-10°C ~ 50°C) for 100/200 VAC, nonfreezing
[Driver] 32°F ~ 122°F (0°C ~ 50°C), nonfreezing
Ambient Humidity 85% maximum (noncondensing)
Operating Atmosphere No corrosive gases or dust
Degree of Protection [Driver] IP00[Motor] IP65
FEATURES
Speed Control Method (Select one of the following) Internal potentiometerExternal DC Voltage (0~5VDC)
External potentiometer (20kΩ, 1/4W)
Number of Speed Settings 2
Multi-Speed Setting Method Switching between 2 speedsOne speed is set by the internal potentiometer (1 pc), while another speed is set by an
external potentiometer (optional PAVR-20KZ) or by external DC voltage (0~5 VDC).
Instantaneous Stop Yes
Multi-Axes Control Yes
Alarm Output Yes
Position Control Mode No
Torque Limit Control No
Vertical Drive (Gravitational Operation) No
Max. Extension Length (m) 2
MULTI-SPEED SETTING METHODSwitching between 2 speedsOne speed is set by the internal potentiometer (1 pc), while another speed is set by an external potentiometer (optional PAVR-20KZ) or by external DCvoltage (0~5 VDC).
3/7/2009 | Page 2 of 2
mec
han
ics
MECHANICS Aluminium Profiles
Aluminium Profiles
Universal Profiles PU-Profiles
Features
• for fast and easy assembly of hou-sings, tables and frames
• aluminium, anodized• made according to DIN 17615• light, compact, solid• universally applicable• high stress-resistance• with our fast-clamped connections
very firm, stress, reversion and ben-ding resistant profile connections areproduced by means of profile bore holes and clamping pieces
• cut to size on request
Technical Data
Dimension Drawings
B8
PU 25 PU 50
dimensions (W x H) 25 x 25 mm 50 x 25 mm
length up to 3 m (special lenghts upon request)
weight 690 g/m 1,270 g/m
4 T-groove indentions for slide nuts M6hollow indention, Ø 5.5 mm for M6
4 T-groove indentions for slide nuts M62 hollow indentions, Ø 5.5 mm for M6
inertia moment IX 1.43 cm4 10.99 cm4
inertia moment IY 1.43 cm4 2.81 cm4
moment of resistance WX 1.14 cm3 4.40 cm3
moment of resistance WY 1.14 cm3 2.25 cm3
1725
6.5
10.5
28
R 5
R 7.
5
5.5
4
PU 25
6.5
10.5
1725 5.5
4
28
R 5254250
Ø 15
10.5
PU 50
profile designationArt. No: L = 1000Art. No: L = 3000
PU 25W 25 x H 25 mm
200 001 1000200 001 3000
PU 50W 50 x H 25 mm
200 002 1000200 002 3000
Ordering Data
mec
han
ics
MECHANICS Aluminium Profiles
Aluminium Profiles
B14
Accessory
Threaded Strips
Slide Nuts
Threaded Strip M6• 13 x 6 mm• galvanized• M6 grid 50 • 3 pieces à 1 m • suitable for PT / RE 40, 65 / PGItem no.: 209 010
Threaded Strip M6• 10 x 4 mm• galvanized• M6 grid 50• 3 pieces à 1 m • suitable for PT / RE 40, 65 / SP / PGItem no.: 209 011
Slide Nut M6 (fig. 1)• L 25 x W 10 x H 3,5 • galvanized• 100 pieces• for all except PT / RE 40, 65 / PS 50 / SP / PG
Item no.: 209 001 0005
Slide Nut M6 (fig. 1)• L 25 x W 13 x H 5• galvanized• 50 pieces • suitable for PT / RE 40, 65 / PGItem no.: 209 004 0001
Slide Nut 2 x M6 (fig. 2)• L 45 x W 10 x H 3,5 • galvanized• 50 pieces• for all except PT / RE 40, 65 / SP / PGItem no.: 209 002 0004
Slide Nut 2 x M6 (fig. 2)• L 45 x W 13 x H 6• galvanized• 2 x M6 grid 25 mm • 25 pieces• suitable for PT / RE 40, 65 / PGItem no.: 209 005 0001
Slide Nut M5• L 25 x W 10 x H 3,5• galvanized• 20 piecesItem no.: 209 006 0001
Angular Slide Nut 2 x M6 (fig. 3)
•galvanized• 25 pieces• for all except PT / RE 40, 65 / SP / PGItem no.: 209 021 0003
Special Slide Nut3 x M6 (fig. 4)
•galvanized• 25 pieces• for all except PT / RE 40, 65 / SP / PGItem no.: 209 022 0003
T-Groove Blocks
T-Groove Block M6•DIN 508• hardened• 20 pieces• suitable for PT / RE 40, 65 / PGItem no.: 209 119 0003
Clamping Vices
Clamping Vice 1 (see figure)
•L 152 x W 130 x H 45 mm • grid 100 •suitable for RE / PTItem no.: 290 055
Clamping Vice 2 (without figure)
•L 215 x W 175 x H 75 mm• grid 125 • suitable for RE / PTItem no.: 290 056
Clamping Blocks
Clamping Block SE•with adjustable screw M6• 2 pieces• suitable for all except PP / PT / PM / SPitem no.: 290 051
Clamping Devices
Hand Lever Clamping Device SH 1• for all except PP / PT / RE 40, 65 / SP / PGItem no.: 290 001
Hand Lever Clamping Device SH 2
• for all except SPItem no.: 290 002
Pneumatic Clamping Device SP 1•lift 10 mm• L 65 x W 10 x H 10 mm• grid 50• suitable for PT / REItem no.: 290 010
Pneumatic Clamping Device SP 2• lift 5 mm• L 65 x W 12 x H 50 mm• grid 50 • suitable for PT / REItem no.: 290 011
Stop Rails
Stop Rail • W 20 x H 10• grid 50• 2 pieces + mounting material • suitable for all except SP
L 125 mmItem no.: 290 021 0125
L 175 mmItem no.: 290 021 0175
L 225 mmItem no.: 290 021 0225
mech
anics
MECHANICSAluminium Profiles
Aluminium Profiles
B15
Accessory
Panel Guide Strips/Profiles
Panel Guide Strip black1-part• for Plates 3 - 6 mm• 1 piece à 10 m • suitable for all except PT / SP / PGItem no.: 209 202 0001
Panel Guide Profile black2-part • for Plates 3 - 6 mm• 1 piece à 3 m • suitable for all exceptPT / SP / PGItem no.: 209 212 3000
Profile Connecting Cubes
Profile Connecting Cubeblack•10 pieces + mounting material• suitable for PU 252-fold
Item no.: 209 104 00023-fold
Item no.: 209 103 0002
Profile Connecting Cubeblack•10 pieces + mounting material• suitable for PU 253-fold
Item no.: 209 106 00024-fold
Item no.: 209 107 0002
Profile Connecting Cubeblack•10 pieces + mounting material• suitable for PU 254-fold
Item no.: 209 108 00025-fold
Item no.: 209 109 0002
Profile Coverings
Profile Coveringsblack•PU 25 - 25 x
Item no.: 209 105 0003•PU 50 - 25 x
Item no.: 209 126 0003•PL 40 - 20 x
Item no.: 209 127 0003•PL 80 - 20 x
Item no.: 209 128 0003•PS 50 - 25 x
Item no.: 209 129 0003•PS 80 - 20 x
Item no.: 209 130 0003•PS 140 - 10 x
Item no.: 209 130 1001•PG 200 - 10 x
Item no.: 209 130 2000
Aluminium Cast Pedestals• 2 pieces + mounting material • suitable for PGanthracite
Item no.: 248 700 1000light grey
Item no.: 248 700 2000
Aluminium Cast Pedestals
Plastic Rollers
Plastic Rollers Ø 50black (M6)• 4 pieces• 2 with and 2 without locks for PU 25
Item no.: 209 040 0012for PU 50
Item no.: 209 040 0011
Ruberized Steering Rollers Ø 75(M10)• 4 pieces• 2 with and 2 without locks • for PL 40 / PS 50Item no.: 209 043 0011
Steering Rollers
mec
han
ics
MECHANICS Aluminium Profiles
Aluminium Profiles
Accessory
B16
Plastic Pedestals
Plastic Pedestals with rubber plate• 4 pieces + adjusting screws• black
for PU 25• Ø 40• adjusting screws M6 x 15 mm
Item no.: 209 029 0003
for PL 40 / PS 50• Ø 60• adjusting screws M10 x 45
Item no.: 209 032 0003
for PL 40 / PS 50• Ø 80• adjusting screws M10 x 45
Item no.: 209 031 0013
for PL 80 / PS 80• Ø 80• adjusting screws M12 x 45
Item no.: 209 034 0001
for PL 80 / PS 80• Ø 120• adjusting screws M12 x 45
Item no.: 209 033 0003
Aluminium Pedestals
Aluminium Pedestals with rubber plate•4 pieces + adjusting screws
for PU 50• Ø 50• adjusting screws M16 x 30• natural
Art.-Nr.: 209 030 0000
for PS 100 / 140• Ø 170• adjusting screws M16 x 100• black
Art.-Nr.: 209 035 0001
T-Groove Coverings
T-Groove Covering• 30 m • (turquoise = similar RAL 5018)• for all except PT / RE 40, 65 / SP / PG
black
Item no.: 209 201 0004turquoise
Item no.: 209 201 0003
AluminiumCorner Connection
Aluminium Corner Connection• L 25 x W 25 x H 15• 10 pieces + mounting material • suitable for RE / PU / PS 50
natural
Item no.: 209 114 0101black
Item no.: 209 114 0111
Aluminium Corner Connection• L 40 x W 40 x H 22• 10 pieces + mounting material • suitable for PP / PL / PS 80 / PS 140
natural
Item no.: 209 115 0101black
Item no.: 209 115 0111
Aluminium Corner Connection• L 50 x W 50 x H 15• 10 pieces + mounting material • suitable for RE / PM / PU / PS 50
naturalItem no.: 209 116 0101
black
Item no.: 209 116 0111
Aluminium Corner Connection• L 80 x W 80 x H 22• 10 pieces + mounting material • suitable for PP / PL / PM / PS
natural
Item no.: 209 117 0101black
Item no.: 209 117 0111
AluminiumFloor Mounting
Aluminium Floor Mounting• L 120 x W 40 x H 75 • 2 bore holes Ø 11, grid 90 mm • suitable for PL / PGItem no.: 209 300 0002
Cross Member out of PP 50
Cross Member out of PP 50• L 490 mm• miter sawed• bore holes M6• for all except PT / RE 40, 65 / SP / PGItem no.: 209 300 0000
Plastic Strap Hinge• L 65 x W 40• 10 pieces + mounting material• grid 43 x 20• suitable for PLItem no.: 209 050 0012
Aluminium Strap Hinge• L 40 x W 40 mm• 10 pieces + mounting material• grid 25 x 25• for all except PT / RE 40, 65 / SP / PGItem no.: 209 050 0011
Strap Hinge
mech
anics
MECHANICSAluminium Profiles
Aluminium Profiles
Accessory
B17
Strap Hinge• L 80 x W 40 mm• zinc diecast• 2 pieces• grid 24 x 53 mm• for all except PT / RE 40, 65 / SP / PGItem no.: 209 050 0021
AluminiumMounting Angle
Aluminium Mounting Angle•2 pieces• Angle of gradient adjustable• suitable for RE / PGItem no.: 209 300 0004
Mounting Bracket
Mounting Bracket for pedestal / rollers • steel galvanized• 2 pieces• H 33 mm• suitable for all except SPItem no.: 209 300 0003
Application Sample
Clamping set
mm
X
ru
dilgi
®X
4.1
Inch
iglidur® X – The High TechProblem Solver
Temperature resistant from -100°C to+250°C in continuous operation
Universal resistance to chemicals
High compressive strength
Very low moisture absorption
Great wear resistance through the entiretemperature range
Colly Components AB. Box 76, 164 94 Kista. Tel 08-703 01 00. Fax 08-703 98 41. www.colly.se
X
+ 250º
- 100º
ru
dilgi
®X
4.2
When to use iglidur® X plain bearings:
•when especially high temperature
resistance is necessary
•For pressure loads
up to 150 MPa
•For linear movements with stainless steel
•For linear movements, especially at
high temperatures
•when universal resistance to
chemicals is required
When not to use the iglidur® X plain bearings:
•For very low wear at high loads
iglidur® Q, Z
•For underwater applications
iglidur® H, H370
•For edge pressure
iglidur® Z
Price Index
3 Styles
> 566 Dimensions
Ø 2 - 75 mm
High Tech Problem Solver
temperature resistant from -100°C to +250°C (short term to + 315°C)
universal resitance to chemicals
high compressive strength
very low moisture absorption
high wear resistance over the entire temperature range
Picture 4.1: Intake control device
Picture 4.2: Battery decanting
mm
X
4.3
0,001 0,01 0,1 1 1 00,1
1
10
100
1000
Inch
Material Table
Table 4.1: Material Data
General Properties Unit iglidur® X Testing Method
Density g/cm3 1,44
Colour black
Max. moisture absorption at 23°C / 50% r.F. % weight 0.1 DIN 53495
Max. moisture absorption % weight 0.5
Coefficient of sliding friction, dynamic against steel µ 0.09 - 0.27
p x v-value, max. (dry) MPa x m/s 1.32
Mechanical Properties
Modulus of elasticity MPa 8,100 DIN 53457
Tensile strength at 20°C MPa 170 DIN 53452
Compressive strength MPa 100
Permissible static surface pressure (20°C) MPa 150
Shore D hardness 85 DIN 53505
Physical and Thermal Properties
Max. long term application temperature °C 250
Max. short term application temperature °C 315
Min. application temperature °C -100
Thermal conductivity W/m x K 0.6 ASTM C 177
Coefficient of thermal expansion (to 23°C) K-1 x 10-5 5 DIN 53752
Electrical Properties
Specific volume resistance ? cm < 105 DIN IEC 93
Surface resistance ? < 103 DIN 53482
Graph. 4.1: Permissible p x v - values for iglidur® X running dry against a steel shaft, at 20°C
Surface Speed [m/s]
]aP
M[ da
oL
Picture 4.3: Flaps, valves
Picture 4.4: Catering equipment
X
ru
dilgi
®X
4.4
0 25 50 75 100
0
1
2
3
4
5
6
7
8
0 25 50 75 100 125 150 175 200 225 2500
30
60
90
120
150
180
23 °C60 °C
m/sec Rotaring Oscilating Linear
Continuous 1.5 3 5
Short term 3.5 4 6
iglidur® X Application Temperature
Minimum - 100 °C
Max., long term + 250 °C
Max., short term + 315 °C
Table 4.2: Maximum surface speeds
Table 4.3: Temperature limits for iglidur® X
Picture 4.5: Application on an
outboard engine
Graph 4.3: Recommended maximum permissible static sur-
face pressure of iglidur® X as a function of temperature
Temperature in °C
]aP
M[ da
oL
iglidur® X is defined by its combination of
high temperature resistance with com-
pressive strength, along with high resistance
to chemicals.
Compressive Strength
Graph 4.2 shows how iglidur® X plain bea-
rings deform elastically under load. Graph
4.1 on the preceding page shows the maxi-
mum p x v values at room temperature. In
this case, the compressive strength of igli-
dur® X even measures up to that of steel.
Graph 4.3 shows the special compression
resistance of iglidur® X at very high tempe-
ratures. Even at the highest long term appli-
cation temperature of 250°C iglidur® X plain
bearings still withstand a static surface pres-
sure of approximately 30 MPa.
Graph 4.2
Compressive Strength, Page 1.12
Permissible Surface Speeds
iglidur® X is designed for higher speeds than
other iglidur® bearings. This is due to its high
temperature resistance and excellent heat
conductivity. These benefits are readily
apparent in the pxv values of max.
1.32 MPa x m/s.
However, only the smallest radial loads may
act on the bearings. At the given speeds,
friction can cause a temperature increase
to maximum permissible levels.
Surface Speed, Page 1.14
p x v Value, Page 1.16
Temperature
In terms of temperature resistance iglidur®
X has also taken on a leading position.
Having a permissible long term application
temperature of 250°C iglidur® X will even
withstand 315°C for the short term.
As in all thermoplastics, the compression
resistance of iglidur® X decreases with
increasing temperature. However, the wear
drops considerably when used within the
observed temperature range of 23°C to
150°C In certain cases, relaxation of the
Graph 4.2: Deformation under load and temperature
% ni
noita
mrofe
D
Load [MPa]
e
X
mm
ru
dilgi
®X
4.5
0
1
2
3
4
5
6
7
87,1
2,2
0,05 0,10 0,15 0,20 0,25 0,30 0,35
0,1
0,2
0,3
0,4
0 10 20 30 40 50 60 70 80 900,00
0,05
0,10
0,15
0,20
0,25
0,30
0,35
23 °C 150 °C
Inch
Table 4.4: Coefficient of friction for igli-
dur® X against steel (Ra = 1µm, 50 HRC)
iglidur®X Dry Grease Oil Water
C.o.f. [µ] 0.09 - 0.27 0.09 0.04 0.04
Graph 4.4: Wear of iglidur® X, Rotation with p = 0.75 MPa,
v = 0.5 m/s, shaft made of Cold Rolled Steel
Graph 4.6: Coefficient of friction for iglidur® X as a function of
the load, v = 0.01 m/s
Graph 4.5: Coefficient of friction for iglidur® X as a function of
the surface speed; p = 0.75 MPa, shaft Cold Rolled Steel
Temperature in °C
Surface Speed [m/s]
µ n
oitcirf fo t
neiciff eo
Cµ
noi tc ir f f
o tneiciffe
oC
Load [MPa]
W]
mk/m
µ[ rae
bearing can even occur at temperatures of
greater than 170°C. This leads, after re-
cooling, to the bearing moving out of the
housing. At temperatures over 170°C the
axial security of the bearing in the housing
needs to be tested. If necessary, secondary
measures must be taken to mechanically
secure the bearing. Please contact us if you
have questions on bearing use.
Graph 4.3 and 4.4
Application Temperatures, Page 1.17
Friction and Wear
Similar to wear resistance, the coefficient
of friction also changes with the load.The
coefficient of friction increases with an
increase in surface speed. On the other
hand, an increased load has an inverse
effect: the coefficient of friction decreases
(see Graph 4.5 and 4.6). This explains the
excellent performance of iglidur® X plain
bearings for high loads.
Friction and wear are also, dependent to a
large degree on the shaft material. Shafts
that are too smooth increase the coefficient
of friction of the bearing. Ground surfaces
with an average roughness Ra of 0.6 to 0.8.
are ideal.
Graph 4.5 to 4.7
Coefficients of friction and surfaces,
Page 1.19
Wear resistance, Page 1.20
Shaft Materials
Graph 4.7 and 4.8 show results of testing
different shaft materials with plain bearings
made of iglidur® X. For low loads in rotating
operation, the best wear values are found
with 303 Stainless and HR Carbon Steel
shafts. However, above a load of 2 MPa the
bearing wear greatly increases with these
two shaft materials. For the higher load
range, hard chromed shafts or Cold Rolled
Steel shafts are advantageous. In oscilla-
ting operation at low loads, similar wear
values for cold rolled Steel and 303 stain-
less steel shafts occur The wear is somewhat
higher than during rotational movements.
X
ru
dilgi
®X
4.6
0,1 0,4 0,7 1,0 1,3 1,6
0,20
0,30
0,40
0,50
0,60
0
2,0
4,0
6,0
8,0
10,0
12,0
3,5
5,1
7,0 7,1 7,88,6
9,310,0
0 1 2 3 4 5
0
20
40
60
80
100
120
140
160
180
0
5
10
15
20
25
18,3
21,7
12,8
20,5
If the shaft material you plan to use is not
contained in this list, please contact us.
Graph 4.8 to 4.10
Shaft Materials, Page 1.22
Installation Tolerances
iglidur® X plain bearings are meant to be
oversized before pressfit. After proper instal-
lation into a recommended housing bore,
the inner diameter adjusts to meet our spe-
cified tolerances.
Please adhere to the catalogue specifica-
tions for housing bore and recommended
shaft sizes. This will help to ensure optimal
performance of iglidur® plain bearings.
Please contact an iglidur® technical expert
if you have any question.
Testing Methods, Page 1.27
Chemical Resistance
iglidur® X plain bearings are close to uni-
versally resistant to chemicals.
They are only attacked by concentrated
nitric acid and by sulphuric acid with acidi-
ty levels over 65%. The list at the end of
this catalogue provides more comprehen-
sive detailed information.
Graph 4.11
Chemicals Table, Page 35.1
Graph 4.10: Wear for oscillating and rotating applications with
different shaft materials
Material
W]
mk/m
µ[ rae
Oscillating, p = 2 MPa Rotating, p = 2 MPa
303 Stainless SteelCold Rolled Steel
Graph 4.9: Wear of iglidur® X with different shaft materials
Load [MPa]
W]
mk/m
µ[ rae
Hard chromedCF53 HRCS 303 S. Steel
Graph 4.8: Wear of iglidur® X with different shaft materials,
p = 0.75 MPa, v = 0.5 m/s
Shaft Materials
W]
mk/m
µ[ rae
Drill Rod H. A. Aluminium
304 S. SteelHard chromed
CRS
SS HSS
HRCS
Graph 4.7: Coefficients of friction as a function of the shaft
surface (shaft Cold Rolled Steel)
µ n
oitcirf fo t
neiciffeo
C
Shaft Roughness Ra [µm]
X
mm
ru
dilgi
®X
4.7
0,0 0,1 0,2 0,3 0,4 0,50,00
0,02
0,04
0,06
0,08
0,10
Inch
Table 4.6: Chemical resistance of iglidur® X
iglidur® X
Specificvolume resistance < 105 ? cmSurface resistance < 103 ?
Graph 4.11: Effect of moisture absorption on iglidur®X plain
bearings
Table 4.5: Essential tolerances for igli-
dur® X plain bearings
Table 4.7: Electrical properties of
iglidur® X
Medium Resistance
Alcohols Resistant
Chlorinated hydrocarbons Resistant
Ester Resistant
Greases, oils Resistant
Ketone Resistant
Fuels Resistant
Weak acids Resistant
Strong acids Conditionally resistant
Weak alkalines Resistant
Strong alkalines Resistant
Picture 4.6: iglidur® X plain bearing in
valve applications
Diameter Shaft h9 iglidur® Xd1 [mm] [mm] F10 [mm]
up to 3 0 - 0.025 +0.006 + 0.046
> 3 to 6 0 - 0.030 +0.010 + 0.058
> 6 to 10 0 - 0.036 +0.013 + 0.071
> 10 to 18 0 - 0.043 +0.016 + 0.086
> 18 to 30 0 - 0.052 +0.020 + 0.104
> 30 to 50 0 - 0.062 +0.025 + 0.125
> 50 to 80 0 - 0.074 +0.030 + 0.150
Moisture absorption [weight %]
]%[ rete
maid re
nn i e
h t fo
noitc
ude
R
Radiation Resistance
Plain bearings made from iglidur® X are resi-
stant to radiation up to an intensity of 1x105
Gy iglidur® X is the most radioactive resi-
stant material of the iglidur® product line igli-
dur® X is extremely resistant to hard gamma
radiation and withstands a radiation dose
of 1000 Mrad without detectable change in
its properties. The material also withstands
an alpha or beta radiation of 10,000 Mrad
with practically no damage.
UV Resistance
The excellent material properties of iglidur®
X do not change under UV radiation and
other weathering effects.
Vacuum
In a vacuum environment iglidur® X plain
bearings can be used virtually without
restrictions. Outgassing takes place to a
very limited extent.
Electrical Properties
iglidur® X plain bearings are electrically con-
ductive.
Application Example
X
4.8
XSM-0203-03 2.0 +0.006 +0.046 3.5 3.0XSM-0304-03 3.0 +0.006 +0.046 4.5 3.0XSM-0304-06 3.0 +0.006 +0.046 4.5 6.0XSM-0405-04 4.0 +0.010 +0.058 5.5 4.0XSM-0507-035 5.0 +0.010 +0.058 7.0 3.5XSM-0507-05 5.0 +0.010 +0.058 7.0 5.0XSM-0507-08 5.0 +0.010 +0.058 7.0 8.0XSM-0608-06 6.0 +0.010 +0.058 8.0 6.0XSM-0608-08 6.0 +0.010 +0.058 8.0 8.0XSM-0608-10 6.0 +0.010 +0.058 8.0 10.0XSM-0608-13 6.0 +0.010 +0.058 8.0 13.8XSM-0709-10 7.0 +0.013 +0.071 9.0 10.0XSM-0709-12 7.0 +0.013 +0.071 9.0 12.0XSM-0810-10 8.0 +0.013 +0.071 10.0 10.0XSM-0810-15 8.0 +0.013 +0.071 10.0 15.0XSM-1012-06 10.0 +0.013 +0.071 12.0 6.0XSM-1012-08 10.0 +0.013 +0.071 12.0 8.0XSM-1012-10 10.0 +0.013 +0.071 12.0 10.0XSM-1012-12 10.0 +0.013 +0.071 12.0 12.0XSM-1012-20 10.0 +0.013 +0.071 12.0 20.0XSM-1214-06 12.0 +0.016 +0.086 14.0 6.0XSM-1214-08 12.0 +0.016 +0.086 14.0 8.0XSM-1214-10 12.0 +0.016 +0.086 14.0 10.0XSM-1214-15 12.0 +0.016 +0.086 14.0 15.0XSM-1214-20 12.0 +0.016 +0.086 14.0 20.0XSM-1416-12 14.0 +0.016 +0.086 16.0 12.0XSM-1416-15 14.0 +0.016 +0.086 16.0 15.0XSM-1416-20 14.0 +0.016 +0.086 16.0 20.0XSM-1517-15 15.0 +0.016 +0.086 17.0 15.0XSM-1517-20 15.0 +0.016 +0.086 17.0 20.0XSM-1618-15 16.0 +0.016 +0.086 18.0 15.0XSM-1618-20 16.0 +0.016 +0.086 18.0 20.0XSM-1618-35 16.0 +0.016 +0.086 18.0 35.0XSM-1820-15 18.0 +0.016 +0.086 20.0 15.0XSM-1820-20 18.0 +0.016 +0.086 20.0 20.0
XSM-2022-14 20.0 +0.020 +0.104 22.0 14.0XSM-2022-18 20.0 +0.020 +0.104 22.0 18.0XSM-2022-20 20.0 +0.020 +0.104 22.0 20.0XSM-2023-15 20.0 +0.020 +0.104 23.0 15.0XSM-2023-20 20.0 +0.020 +0.104 23.0 20.0XSM-2023-25 20.0 +0.020 +0.104 23.0 25.0XSM-2023-30 20.0 +0.020 +0.104 23.0 30.0XSM-2225-15 22.0 +0.020 +0.104 25.0 15.0XSM-2225-20 22.0 +0.020 +0.104 25.0 20.0XSM-2427-20 24.0 +0.020 +0.104 27.0 20.0XSM-2528-13 25.0 +0.020 +0.104 28.0 13.0XSM-2528-20 25.0 +0.020 +0.104 28.0 20.0XSM-2528-30 25.0 +0.020 +0.104 28.0 30.0XSM-2730-05 27.0 +0.020 +0.104 30.0 5.7XSM-2832-20 28.0 +0.020 +0.104 32.0 20.0XSM-2832-30 28.0 +0.020 +0.104 32.0 30.0XSM-3034-20 30.0 +0.020 +0.104 34.0 20.0XSM-3034-25 30.0 +0.020 +0.104 34.0 25.0XSM-3034-30 30.0 +0.020 +0.104 34.0 30.0XSM-3034-40 30.0 +0.020 +0.104 34.0 40.0XSM-3236-30 32.0 +0.025 +0.125 36.0 30.0XSM-3539-20 35.0 +0.025 +0.125 39.0 20.0XSM-3539-30 35.0 +0.025 +0.125 39.0 30.0XSM-3539-40 35.0 +0.025 +0.125 39.0 40.0XSM-4044-30 40.0 +0.025 +0.125 44.0 30.0XSM-4044-40 40.0 +0.025 +0.125 44.0 40.0XSM-4044-50 40.0 +0.025 +0.125 44.0 50.0XSM-4550-50 45.0 +0.025 +0.125 50.0 50.0XSM-5055-30 50.0 +0.025 +0.125 55.0 30.0XSM-5055-40 50.0 +0.025 +0.125 55.0 40.0XSM-5055-60 50.0 +0.025 +0.125 55.0 60.0XSM-5560-50 55.0 +0.030 +0.150 60.0 50.0XSM-6065-60 60.0 +0.030 +0.150 65.0 60.0XSM-6570-50 65.0 +0.030 +0.150 70.0 50.0
X S M - 0 2 0 3 - 0 3
d1 d2 b1
Part Number d1 d1-Tolerance d2 b1after Pressfit in Ø H7 h13
Part Number d1 d1-Tolerance d2 b1after Pressfit in Ø H7 h13
Structure of the Part Number:
(Data in mm)
Metric dimension
Type
Material
iglidur® X – Sleeve Bearing, mm
Dimensions according to ISO 3547-1 and special dimensions
mm
ru
d ilg i
®S e
py T – X
X
mm
4.9
XFM-0304-05 3.0 +0.006 +0.046 4.5 7.5 5.0 0.75XFM-0405-04 4.0 +0.010 +0.058 5.5 9.5 4.0 0.75XFM-0405-06 4.0 +0.010 +0.058 5.5 9.5 6.0 0.75XFM-040508-06 4.0 +0.010 +0.058 5.5 8.0 6.0 0.75XFM-0507-05 5.0 +0.010 +0.058 7.0 11.0 5.0 1.0XFM-0608-08 6.0 +0.010 +0.058 8.0 12.0 8.0 1.0XFM-0608-10 6.0 +0.010 +0.058 8.0 12.0 10.0 1.0XFM-0810-075 8.0 +0.013 +0.071 10.0 15.0 7.5 1.0XFM-0810-09 8.0 +0.013 +0.071 10.0 15.0 9.0 1.0XFM-1012-06 10.0 +0.013 +0.071 12.0 18.0 6.0 1.0XFM-1012-08 10.0 +0.013 +0.071 12.0 15.0 8.0 1.0XFM-1012-09 10.0 +0.013 +0.071 12.0 18.0 9.0 1.0XFM-1012-15 10.0 +0.013 +0.071 12.0 18.0 15.0 1.0XFM-1012-18 10.0 +0.013 +0.071 12.0 18.0 18.0 1.0XFM-1214-09 12.0 +0.016 +0.086 14.0 20.0 9.0 1.0XFM-1214-12 12.0 +0.016 +0.086 14.0 20.0 12.0 1.0XFM-1214-15 12.0 +0.016 +0.086 14.0 20.0 15.0 1.0XFM-1416-12 14.0 +0.016 +0.086 16.0 22.0 12.0 1.0XFM-1416-17 14.0 +0.016 +0.086 16.0 22.0 17.0 1.0XFM-1517-12 15.0 +0.016 +0.086 17.0 23.0 12.0 1.0XFM-1517-17 15.0 +0.016 +0.086 17.0 23.0 17.0 1.0XFM-1618-12 16.0 +0.016 +0.086 18.0 24.0 12.0 1.0XFM-1618-17 16.0 +0.016 +0.086 18.0 24.0 17.0 1.0XFM-1820-12 18.0 +0.016 +0.086 20.0 26.0 12.0 1.0XFM-1820-17 18.0 +0.016 +0.086 20.0 26.0 17.0 1.0XFM-2023-11 20.0 +0.020 +0.104 23.0 30.0 11.0 1.5XFM-2023-21 20.0 +0.020 +0.104 23.0 30.0 21.5 1.5XFM-2528-21 25.0 +0.020 +0.104 28.0 35.0 21.0 1.5XFM-2730-20 27.0 +0.020 +0.104 30.0 38.0 20.0 1.5XFM-3034-16 30.0 +0.020 +0.104 34.0 42.0 16.0 2.0XFM-3034-26 30.0 +0.020 +0.104 34.0 42.0 26.0 2.0XFM-3034-40 30.0 +0.020 +0.104 34.0 42.0 40.0 2.0XFM-3236-15 32.0 +0.025 +0.125 36.0 45.0 15.0 2.0XFM-3236-26 32.0 +0.025 +0.125 36.0 45.0 26.0 2.0XFM-3539-26 35.0 +0.025 +0.125 39.0 47.0 26.0 2.0XFM-4044-30 40.0 +0.025 +0.125 44.0 52.0 30.0 2.0XFM-4044-40 40.0 +0.025 +0.125 44.0 52.0 40.0 2.0XFM-4550-50 45.0 +0.025 +0.125 50.0 58.0 50.0 2.0XFM-5055-40 50.0 +0.025 +0.125 55.0 63.0 40.0 2.0
X F M - 0 3 0 4 - 0 5
d1 d2 b1
Inch
Part Number d1 d1-Tolerance d2 d3 b1 b2after Pressfit in Ø H7 d13 h13 -0.14
Structure of the Part Number:
(Data in mm)
Metric dimension
Type
Material
ru
dilgi
®F e
py T – X
mm
iglidur® X – Flange Bearing, mm
Dimensions according to ISO 3547-1 and special dimensions
X
4.10
XFM-6065-40 60.0 +0.030 +0.150 65.0 73.0 40.0 2.0XFM-7075-40 70.0 +0.030 +0.150 75.0 83.0 40.0 2.0XFM-7580-50 75.0 +0.030 +0.150 80.0 88.0 50.0 2.0
X F M - 6 0 6 5 - 4 0
d1 d2 b1
Part Number d1 d1-Tolerance d2 d3 b1 b2after Pressfit in Ø H7 d13 h13 -0.14
Structure of the Part Number:
(Data in mm)
Metric dimension
Type
Material
iglidur® X – Flange Bearing, mm
Dimensions according to ISO 3547-1 and special dimensions
mm
ru
d ilg i
®F e
pyT – X
mm
X
4.11
XTM-0620-015 6.0 20.0 1.5 13.0 1.5 1.0 20.0XTM-0818-015 8.0 18.0 1.5 13.0 1.5 1.0 18.0XTM-1018-010 10.0 18.0 1.0 * * 0.7 18.0XTM-1224-015 12.0 24.0 1.5 18.0 1.5 1.0 24.0XTM-1426-015 14.0 26.0 1.5 20.0 2.0 1.0 26.0XTM-1524-015 15.0 24.0 1.5 19.5 1.5 1.0 24.0XTM-1630-015 16.0 30.0 1.5 22.0 2.0 1.0 30.0XTM-1832-015 18.0 32.0 1.5 25.0 2.0 1.0 32.0XTM-2036-015 20.0 36.0 1.5 28.0 3.0 1.0 36.0XTM-2238-015 22.0 38.0 1.5 30.0 3.0 1.0 38.0XTM-2442-015 24.0 42.0 1.5 33.0 3.0 1.0 42.0XTM-2644-015 26.0 44.0 1.5 35.0 3.0 1.0 44.0XTM-3254-015 32.0 54.0 1.5 38.0 4.0 1.0 54.0XTM-3862-015 38.0 62.0 1.5 50.0 4.0 1.0 62.0XTM-4266-015 42.0 66.0 1.5 84.0 4.0 1.0 66.0XTM-4874-020 48.0 74.0 2.0 61.0 4.0 1.5 74.0XTM-5278-020 52.0 78.0 2.0 65.0 4.0 1.5 78.0XTM-6290-020 62.0 90.0 2.0 76.0 4.0 1.5 90.0
X T M - 0 6 2 0 - 0 1 5
d1 d2 s
* Design without fixation bore
Inch
Part Number d1 d2 s d4 d5 h d6 +0.25 -0.25 -0.05 -0.12 +0.375 +0.2 +0.12
+0.12 +0.125 -0.2
Structure of the Part Number:
(Data in mm)
Metric dimension
Type
Material
iglidur® X – Thrust Washer, mm
Dimensions according to ISO 3547-1 and special dimensions
ru
dilgi
®T e
py T – X
mm
X
4.12
TSI-0203-03 1/8 3/16 3/16 .1269 .1251 .1878 .1873 .1243 .1236TSI-0203-05 1/8 3/16 5/16 .1269 .1251 .1878 .1873 .1243 .1236TSI-0203-06 1/8 3/16 3/8 .1269 .1251 .1878 .1873 .1243 .1236TSI-0304-03 3/16 1/4 3/16 .1892 .1873 .2503 .2497 .1865 .1858TSI-0304-04 3/16 1/4 1/4 .1892 .1873 .2503 .2497 .1865 .1858TSI-0304-06 3/16 1/4 3/8 .1892 .1873 .2503 .2497 .1865 .1858TSI-0304-08 3/16 1/4 1/2 .1892 .1873 .2503 .2497 .1865 .1858TSI-0405-04 1/4 5/16 1/4 .2521 .2498 .3128 .3122 .2490 .2481TSI-0405-06 1/4 5/16 3/8 .2521 .2498 .3128 .3122 .2490 .2481TSI-0405-08 1/4 5/16 1/2 .2521 .2498 .3128 .3122 .2490 .2481TSI-0506-04 5/16 3/8 1/4 .3148 .3125 .3753 .3747 .3115 .3106TSI-0506-06 5/16 3/8 3/8 .3148 .3125 .3753 .3747 .3115 .3106TSI-0506-08 5/16 3/8 1/2 .3148 .3125 .3753 .3747 .3115 .3106TSI-0607-04 3/8 15/32 1/4 .3773 .3750 .4691 .4684 .3740 .3731TSI-0607-05 3/8 15/32 5/16 .3773 .3750 .4691 .4684 .3740 .3731TSI-0607-06 3/8 15/32 3/8 .3773 .3750 .4691 .4684 .3740 .3731TSI-0607-08 3/8 15/32 1/2 .3773 .3750 .4691 .4684 .3740 .3731TSI-0607-10 3/8 15/32 5/8 .3773 .3750 .4691 .4684 .3740 .3731TSI-0708-04 7/16 17/32 1/4 .4406 .4379 .5316 .5309 .4365 .4355TSI-0708-08 7/16 17/32 1/2 .4406 .4379 .5316 .5309 .4365 .4355TSI-0708-10 7/16 17/32 5/8 .4406 .4379 .5316 .5309 .4365 .4355TSI-0708-12 7/16 17/32 3/4 .4406 .4379 .5316 .5309 .4365 .4355TSI-0809-04 1/2 19/32 1/4 .5030 .5003 .5941 .5934 .4990 .4980TSI-0809-06 1/2 19/32 3/8 .5030 .5003 .5941 .5934 .4990 .4980TSI-0809-08 1/2 19/32 1/2 .5030 .5003 .5941 .5934 .4990 .4980TSI-0809-10 1/2 19/32 5/8 .5030 .5003 .5941 .5934 .4990 .4980TSI-0809-12 1/2 19/32 3/4 .5030 .5003 .5941 .5934 .4990 .4980TSI-0809-16 1/2 19/32 1 .5030 .5003 .5941 .5934 .4990 .4980TSI-0910-08 9/16 21/32 1/2 .5655 .5627 .6566 .6559 .5615 .5605TSI-0910-12 9/16 21/32 3/4 .5655 .5627 .6566 .6559 .5615 .5605TSI-1011-04 5/8 23/32 1/4 .6280 .6253 .7192 .7184 .6240 .6230TSI-1011-06 5/8 23/32 3/8 .6280 .6253 .7192 .7184 .6240 .6230TSI-1011-08 5/8 23/32 1/2 .6280 .6253 .7192 .7184 .6240 .6230TSI-1011-10 5/8 23/32 5/8 .6280 .6253 .7192 .7184 .6240 .6230TSI-1011-12 5/8 23/32 3/4 .6280 .6253 .7192 .7184 .6240 .6230TSI-1011-16 5/8 23/32 1 .6280 .6253 .7192 .7184 .6240 .6230TSI-1112-14 11/16 25/32 7/8 .6906 .6879 .7817 .7809 .6865 .6855TSI-1214-06 3/4 7/8 3/8 .7541 .7507 .8755 .8747 .7491 .7479TSI-1214-08 3/4 7/8 1/2 .7541 .7507 .8755 .8747 .7491 .7479
T S I - 0 2 0 3 - 0 3
d1 d2 b1
Part Number d1 d2 b1 I.D.after Pressfit Housing bore Shaft Sizemax. min. max. min. max. min.
iglidur® X – Sleeve Bearing, inch
Structure of the Part Number:
(Data in inch)
Inch dimension
Type
Material
in mm
hc
ni
ru
dilgi
®S e
pyT – X
X
mm
4.13
TSI-1214-12 3/4 7/8 7/8 .7541 .7507 .8755 .8747 .7491 .7479TSI-1214-16 3/4 7/8 1 .7541 .7507 .8755 .8747 .7491 .7479TSI-1416-12 7/8 1 3/4 .8791 .8757 1.0005 .9997 .8741 .8729TSI-1416-16 7/8 1 1 .8791 .8757 1.0005 .9997 .8741 .8729TSI-1618-08 1 1 1/8 1/2 1.0041 1.0007 1.1255 1.1247 .9991 .9979TSI-1618-12 1 1 1/8 3/4 1.0041 1.0007 1.1255 1.1247 .9991 .9979TSI-1618-16 1 1 1/8 1 1.0041 1.0007 1.1255 1.1247 .9991 .9979TSI-1618-24 1 1 1/8 1 1/2 1.0041 1.0007 1.1255 1.1247 .9991 .9979TSI-1820-12 1 1/8 1 9/32 3/4 1.1288 1.1254 1.2818 1.2808 1.1238 1.1226TSI-2022-10 1 1/4 1 13/32 5/8 1.2548 1.2508 1.4068 1.4058 1.2488 1.2472TSI-2022-20 1 1/4 1 13/32 1 1/4 1.2548 1.2508 1.4068 1.4058 1.2488 1.2472TSI-2426-12 1 1/2 1 21/32 3/4 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TSI-2426-16 1 1/2 1 21/32 1 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TSI-2426-24 1 1/2 1 21/32 1 1/2 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TSI-2629-20 1 25/32 1 13/16 1 1/4 1.6297 1.6258 1.7818 1.7808 1.6238 1.6222TSI-2831-16 1 3/4 1 15/16 1 1.7547 1.7507 1.9381 1.9371 1.7487 1.7471TSI-3235-24 2 2 3/16 1 1/2 2.0057 2.0011 2.1883 2.1871 1.9981 1.9969TSI-3235-32 2 2 3/16 2 2.0057 2.0011 2.1883 2.1871 1.9981 1.9969TSI-3639-32 2 1/4 2 7/16 2 2.2577 2.2531 2.4377 2.4365 2.2507 2.2489TSI-4447-32 2 3/4 2 15/16 2 2.7570 2.7523 2.9370 2.9358 2.7500 2.7490
T S I - 1 2 1 4 - 1 2
d1 d2 b1
Inch
Part Number d1 d2 b1 I.D. after Pressfit Housing Bore Shaft Sizemax. min. max. min. max. min.
iglidur® X – Sleeve Bearing, inch
Structure of the Part Number:
(Data in inch)
Inch dimension
Type
Material
in mm
ru
d ilg i
®S e
py T – X
hc
ni
X
4.14
TFI-0203-03 1/8 3/16 3/16 .312 .032 .1269 .1251 .1878 .1873 .1243 .1236TFI-0203-06 1/8 3/16 3/8 .312 .032 .1269 .1251 .1878 .1873 .1243 .1236TFI-0304-04 3/16 1/4 1/4 .375 .032 .1892 .1873 .2503 .2497 .1865 .1858TFI-0304-06 3/16 1/4 3/8 .375 .032 .1892 .1873 .2503 .2497 .1865 .1858TFI-0304-08 3/16 1/4 1/2 .375 .032 .1892 .1873 .2503 .2497 .1865 .1858TFI-0405-03 1/4 5/16 3/16 .500 .032 .2521 .2498 .3128 .3122 .2490 .2481TFI-0405-04 1/4 5/16 1/4 .500 .032 .2521 .2498 .3128 .3122 .2490 .2481TFI-0405-06 1/4 5/16 3/8 .500 .032 .2521 .2498 .3128 .3122 .2490 .2481TFI-0405-08 1/4 5/16 1/2 .500 .032 .2521 .2498 .3128 .3122 .2490 .2481TFI-0405-12 1/4 5/16 3/4 .500 .032 .2521 .2498 .3128 .3122 .2490 .2481TFI-0506-04 5/16 3/8 1/4 .562 .032 .3148 .3125 .3753 .3747 .3115 .3106TFI-0506-06 5/16 3/8 3/8 .562 .032 .3148 .3125 .3753 .3747 .3115 .3106TFI-0506-08 5/16 3/8 1/2 .562 .032 .3148 .3125 .3753 .3747 .3115 .3106TFI-0607-04 3/8 15/32 1/4 .687 .046 .3773 .3750 .4691 .4684 .3740 .3731TFI-0607-06 3/8 15/32 3/8 .687 .046 .3773 .3750 .4691 .4684 .3740 .3731TFI-0607-08 3/8 15/32 1/2 .687 .046 .3773 .3750 .4691 .4684 .3740 .3731TFI-0607-12 3/8 15/32 3/4 .687 .046 .3773 .3750 .4691 .4684 .3740 .3731TFI-0708-08 7/16 17/32 1/2 .750 .046 .4406 .4379 .5316 .5309 .4365 .4355TFI-0809-04 1/2 19/32 1/4 .875 .046 .5030 .5003 .5941 .5934 .4990 .4980TFI-0809-06 1/2 19/32 3/8 .875 .046 .5030 .5003 .5941 .5934 .4990 .4980TFI-0809-08 1/2 19/32 1/2 .875 .046 .5030 .5003 .5941 .5934 .4990 .4980TFI-0809-12 1/2 19/32 3/4 .875 .046 .5030 .5003 .5941 .5934 .4990 .4980TFI-0809-16 1/2 19/32 1 .875 .046 .5030 .5003 .5941 .5934 .4990 .4980TFI-1011-08 5/8 23/32 1/2 .937 .046 .6280 .6253 .7192 .7184 .6240 .6230TFI-1011-12 5/8 23/32 3/4 .937 .046 .6280 .6253 .7192 .7184 .6240 .6230TFI-1011-16 5/8 23/32 1 .937 .046 .6280 .6253 .7192 .7184 .6240 .6230TFI-1011-24 5/8 23/32 1 1/2 .937 .046 .6280 .6253 .7192 .7184 .6240 .6230TFI-1214-08 3/4 7/8 1/2 1.125 .062 .7541 .7507 .8755 .8747 .7491 .7479TFI-1214-12 3/4 7/8 3/4 1.125 .062 .7541 .7507 .8755 .8747 .7491 .7479TFI-1214-16 3/4 7/8 1 1.125 .062 .7541 .7507 .8755 .8747 .7491 .7479TFI-1214-28 3/4 7/8 1 3/4 1.125 .062 .7541 .7507 .8755 .8747 .7491 .7479TFI-1416-12 7/8 1 3/4 1.250 .062 .8791 .8757 1.0005 .9997 .8741 .8729TFI-1416-16 7/8 1 1 1.250 .062 .8791 .8757 1.0005 .9997 .8741 .8729TFI-1618-08 1 1 1/8 1/2 1.375 .062 1.0041 1.0007 1.1255 1.1247 .9991 .9979TFI-1618-12 1 1 1/8 3/4 1.375 .062 1.0041 1.0007 1.1255 1.1247 .9991 .9979TFI-1618-16 1 1 1/8 1 1.375 .062 1.0041 1.0007 1.1255 1.1247 .9991 .9979TFI-1618-24 1 1 1/8 1 1/2 1.375 .062 1.0041 1.0007 1.1255 1.1247 .9991 .9979TFI-1820-12 1 1/8 1 9/32 3/4 1.562 .078 1.1288 1.1254 1.2818 1.2808 1.1238 1.1226TFI-2022-20 1 1/4 1 13/32 1 1/4 1.687 .078 1.2548 1.2508 1.4068 1.4058 1.2488 1.2472
T F I - 0 2 0 3 - 0 3
d1 d2 b1
Part Number d1 d2 b1 d3 b2 I.D. after Pressfit Housing Bore Shaft Sizemax. min. max. min. max. min.
Structure of the Part Number:
(Data in inch)
Inch dimension
Type
Material
iglidur®X – Flange Bearing, inch
in mm hc
ni
ru
dilgi
®F e
pyT – X
mm
X
4.15
Référence d1 d2 b1 d3 b2 d1 après emmanchement Alésage Arbremax. min. max. min. max. min.
TFI-2022-32 1 1/4 1 13/32 2 1.687 .078 1.2548 1.2508 1.4068 1.4058 1.2488 1.2472TFI-2426-12 1 1/2 1 21/32 3/4 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2426-16 1 1/2 1 21/32 1 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2426-24 1 1/2 1 21/32 1 1/2 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2426-26 1 1/2 1 21/32 1 5/8 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2831-16 1 3/4 1 15/16 1 2.375 .093 1.7547 1.7507 1.9381 1.9371 1.7487 1.7471TFI-3235-32 2 2 3/16 2 2.625 .093 2.0057 2.0011 2.1883 2.1871 1.9981 1.9969TFI-4447-32 2 3/4 2 15/16 2 3.375 .093 2.7570 2.7523 2.9370 2.9358 2.7500 2.7490
TFI-2022-32 1 1/4 1 13/32 2 1.687 .078 1.2548 1.2508 1.4068 1.4058 1.2488 1.2472TFI-2426-12 1 1/2 1 21/32 3/4 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2426-16 1 1/2 1 21/32 1 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2426-24 1 1/2 1 21/32 1 1/2 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2426-26 1 1/2 1 21/32 1 5/8 2.000 .078 1.5048 1.5008 1.6568 1.6558 1.4988 1.4972TFI-2831-16 1 3/4 1 15/16 1 2.375 .093 1.7547 1.7507 1.9381 1.9371 1.7487 1.7471TFI-3235-32 2 2 3/16 2 2.625 .093 2.0057 2.0011 2.1883 2.1871 1.9981 1.9969TFI-4447-32 2 3/4 2 15/16 2 3.375 .093 2.7570 2.7523 2.9370 2.9358 2.7500 2.7490
T F I - 2 0 2 2 - 3 2
d1 d2 b1
Inch
Part Number d1 d2 b1 d3 b2 I.D.after Pressfit Housing Bore Shaft Sizemax. min. max. min. max. min.
ru
dilgi
®F e
pyT – X
hc
ni
Structure of the Part Number:
(Data in inch)
Inch dimension
Type
Material
iglidur® X – Flange Bearing, inch
in mm
X
4.16
TTI-0814-01 .500 .875 .0585 .692 .067 .040 .875TTI-1018-01 .625 1.125 .0585 .880 .099 .040 1.125TTI-1220-01 .750 1.250 .0585 1.005 .099 .040 1.250TTI-1424-01 .875 1.500 .0585 1.192 .130 .040 1.500TTI-1628-01 1.000 1.750 .0585 1.380 .130 .040 1.750TTI-1826-01 1.125 1.625 .0585 – – .040 1.625TTI-2034-01 1.250 2.125 .0585 1.692 .161 .040 2.125TTI-2440-01 1.500 2.500 .0585 2.005 .192 .040 2.500TTI-2844-01 1.750 2.750 .0585 2.255 .192 .040 2.750TTI-3248-01 2.000 3.000 .0895 2.505 .192 .070 3.000
T T I - 0 8 1 4 - 0 1
d1 d2 s
Structure of the Part Number:
(Data in inch)
Inch dimension
Type
Material
Part Number d1 d2 s d4 d5 h d6 +.010 -.010 -.0020 +-.005 .015 +.005 +.008 +.005
iglidur® X – Thrust Washer, inchh
cni
ru
d ilg i
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Colly Components AB. Box 76, 164 94 Kista. Tel 08-703 01 00. Fax 08-703 98 41. www.colly.se
13 21 00/ZERBuyLine 0678www.zeroloc.com
Fiberglass Reinforced Plastic (FRP)
may be factory-bonded to the
steel skins of the Zero-Loc
EPS insulated panels, offering
increased scratch and dent
resistance. FRP protects panels from
the frequent rigorous
cleaning that is required in maintain-
ing a sanitary environment.
Food Processing
The finished Zero-Loc insulated
system is sanitary, energy efficient
and durable.
Cold Storage Warehouses
Ideally suited for low temperature
facilities, Zero-Loc EPS “R” value
performance increases as the
temperature decreases.
Walk-on Suspended Ceiling System
Constructed with Zero-Loc EPS
insulated panels, the finished
Zero-Loc walk-on suspended
ceiling system is energy efficient
and durable and is ideally suited for
low temperature, food processing and
controlled environment applications.
factory applied FRP
Expanded Polystyrene (EPS) Insulated Panel Systems
food processing plants cold storage warehouses walk-on suspended ceiling systems
Technical Specifications
5202-272nd St, Langley, BC Canada V4W 1S3 T: 604-607-1101 F: 604-607-1142
28 Plant Farm Blvd, Brantford, ON Canada N3S 7W3 T: 519-754-4500 F: 519-754-4214
119-9757 Juanita Dr N.E., Kirkland, WA USA 98033 T: 425-823-4588 F: 425-820-9749
Expanded Polystyrene (EPS) Insulated Panel Systems
9. Gasket: a. Hinged Door and Manual Sliding Door gaskets shall designed for heavy-duty applications, and shall be resistant to oils, grease and/or fats. Door gasket shall create a positive seal at all contact points between door leaf and frame, and door leaf and floor. Level floor surface required for positive gasket seal shall be provided by others. 10. Hinged Door Hardware: a. Overlap-type hinged doors shall be equipped with Kason #1398 Heavy-Duty Cam Rise hinges. b. Infitting-type hinged doors shall be equipped with Kason #1245 Reversible Cam-Rise Hinges. c. Hinged doors shall be equipped with Kason K56 Standard Latches complete with strike assemblies and Kason 481 inside Release Handles. 11. Sliding Door Hardware : a. Sliding door track shall consist of heavy gauge anodized alumi- num. Door leaf hanger assembly to be fabricated from: 1) 10 gauge (3.416 mm) 304 2B stainless steel to match door leaf trim finish and faceplate frame finish. 2) G90 galvanized steel to match door leaf trim finish and face plate frame finish. b. Hanger wheels shall be 4 inches (102 mm) in diameter and made from “Delrin” plastic. The 10 gauge (3.416 mm) hanger assembly shall also serve as the cover for the hanger assem bly. 12. Freezer Doors : a. Freezer doors shall be equipped with CSA/UL rated anti-frost heat trace in both door leaf and faceplate frame for heavy-duty hinged and sliding freezer doors and in door leaf or faceplate frame only for hinged and sliding freezer doors in lighter-duty commercial applications. Heat trace shall be factory-wired to a ground-fault circuit interrupter.
2.3 FABRICATION A. Corners: 1. Corner panel connections shall be butt or mitered, flashed, and finished by installation crew on-site. 2. Where specified, corner panel connections shall be a single unit corner panel with a continuous metal skin on the outer bend. B. Offset: Maximum offset from true alignment between two identical members abutting end-to-end: 1/8 inch (3 mm).
PART 3 EXECUTION3.1 EXAMINATION A. Verification of Conditions: Examine areas and conditions under which Work is to be performed and identify conditions detrimental to proper or timely completion. 1. Panel installer to verify that structural steel supports for wall panels are within tolerances in the AISC Code of Standard Practice, Section 7 and supplement modification controlling Section 7.11.3, adjustable items. Limit maximum deviation of steel alignment to plus or minus 3/16 inch(4 mm) from the control with a 1/8 inch (3 mm) maximum change in deviation for any member for any 10 feet (3 m) length of panel. 2. Do not proceed until unsatisfactory conditions have been corrected. B. If support system preparation is the responsibility of another installer, notify Architect of unsatisfactory preparation before proceeding.
3.2 INSTALLATION A. Install in accordance with manufacturer’s instructions.
3.3 TOLERANCES A. Variation: Maximum variation from vertical or horizontal plane, 1/4 inch (6 mm) in 12 feet (3658 mm) length section or 1/2 inch (13 mm) over total length.
B. Offset: Maximum offset from true alignment between two identical members abutting end-to-end: 1/8 inch (3 mm).
3.4 FIELD QUALITY CONTROL A. Manufacturer’s Field Services: Manufacturer shall make periodic inspec tions and issue report to Architect regarding compliance with manufactur ers installation recommendations developed for the Project.
3.5 ADJUSTING A. Repair damage caused during construction. 1. Touch-up mars, scratches, and cut edges to match original finish. 2. If repairs cannot be made to comply with Architect’s requirements, remove damage and install new materials.
Company Profile. Since our establishment in 1969, ZERO-LOC
has grown to become a major worldwide producer of Insulated Panel
and Door Systems. This achievement has been made possible by the
dedication of our employees and the belief that giving greater service
and value to our customers is essential to success.
For design assistance, structural details,
AutoCAD disks, product specifications and
other technical information, please contact
your nearest Zero-Loc representative.
www.zeroloc.com13 21 00/ZERBuyLine 0678
A Wide Range of Applications
• Exterior / Interior EPS insulated build-ing panels for warehouses, and food processing plants
• Standard & specialty insulated doors
• Walk-on suspended ceiling systems
• Storage freezers & coolers
• Blast/Spiral/IQF Freezer Tunnels & Enclosures
• Federally inspected food processing areas
• Environment/atmosphere control rooms
• Factory-Laminated Fiberglass Reinforced Plastic (FRP)
INSULATED PANEL SYSTEMS
PART 1 GENERAL1.1 SECTION INCLUDES
A. Expanded polystyrene (EPS) insulated metal wall and ceiling panels with related accessories.
1.2 RELATED SECTIONS A. Section 03300 - Concrete: Foundations. B. Section 05120 - Structural Steel: Primary structure. C. Section 05500 - Steel Fabrication: Supporting structure.
1.3 REFERENCES
A. American Society for Testing and Materials (ASTM) E96: Standard Test Methods for Water Vapor Transmission of Materials. B. American Society for Testing and Materials (ASTM) E283: Standard Test Method for Rate of Air Leakage through Exterior Windows, Curtain Walls, and Doors. C. Underwriters’ Laboratories of Canada (ULC/ORD-C376-1995): Fire Growth of Foamed Plastic Insulated Building Panels in a Full-Scale Room configuration.
1.4 SYSTEM DESCRIPTION A. General: Construct panel system to provide for expansion and contrac tion of component materials without causing buckling, failure of joint seals, undue stress on fasteners, or other detrimental effects to the panel system or adjacent building systems, or warping of faces of panel system. B. Performance Requirements: Design and construct panels to meet requirements as indicated. 1. Design panel composition to resist wind load mandated by code, with deflection limit of L/180. a. No permanent damage to panels or connections when sub jected to 1.5 times the design wind pressures for both inward and outward. 2. Air leakage: Not greater than .06 cfm per square foot when tested in compliance with ASTM E283 at 1.56 pounds per square foot.
1.5 SUBMITTALS A. Submit under provisions of Section 01300. B. [Product Data]: Manufacturer’s data sheets on each product to be used, including: 1. Preparation instructions and recommendations. 2. Storage and handling requirements and recommendations. 3. Detailed specification of construction and fabrication. 4. Manufacturer’s installation instructions. 5. Certified test reports indicating compliance with specified perfor- mance requirements.
C. Shop Drawings: Indicate dimensions, description of materials and fin ishes, general construction, specific modifications, component connec- tions, anchorage methods, hardware, and installation procedures, including specific requirements indicated. 1. Profile and gauge of both exterior and interior sheet. 2. Metal finish. 3. Relationship to other work. 4. Fully show details and connections to and locations of supporting steel indicating control points. D. Selection Samples: For each finish product specified, two complete sets of color chips representing manufacturer’s full range of available colors and patterns. E. Verification Samples: For each finish product specified, two samples, minimum size 6 inches (150 mm) square, representing actual product, color, and patterns. F. Quality Control Submittals: 1. Statement of qualifications. 2. Design data. 3. Test reports.
1.6 QUALITY ASSURANCE A. Manufacturer/installer shall be responsible for fabrication and installa- tion of panel and support framing as specified in this section to comply with the following: 1. Wind load engineering to comply with code requirements. B. Manufacturer’s Qualifications: Not less than 5 years experience in the actual production of specified products. 1. Comply with rigid factory Quality Control program which includes quarterly unannounced inspections from UL, and independent test ing laboratories providing reports directly to code authority. 2. Successfully completed not less than 100 comparable scale projects using this system. C. Installer’s Qualifications: Firm experienced in installation of systems similar in complexity to those required for this Project, including specific requirements indicated. 1. Acceptable to or licensed by manufacturer. 2. Not less than 3 years experience with systems. 3. Successfully completed not less than 5 comparable scale projects using this system. D. Product Requirements: 1. Metal members (prone to rust) and wood or wood by-products (prone to moisture absorption and rot), shall not be permitted within the panel connection system. 2. Panel joints connection system, tested in accordance with ASTM E283 “Air Leakage Rate Testing” and ASTM E96 “Water Vapor Per meance Rate Testing” shall have an air leakage rate at 75 Pa OF 0.00m3/h-m2 (0.00cfm/sq.ft.) and a water vapor permeance rate of 0.00 perms. 3. Insulated panels, related accessories, and construction details shall be in accordance with the following regulatory agencies, where required: a. Canadian Food Inspection Agency (CFIA) b. United States Department of Agriculture (USDA) 4. Wall and ceiling panels, insulated with Type 1 Expanded Polysty- rene (EPS) manufactured to EPS Type 1 standards, shall be listed in accordance with ULC/ORD-C376-1995, “Fire Growth of Foamed Plastic Insulated Building Panels in a Full-Scale Room Configura tion”, in compliance with Part 3.1.5.12 of the 2005 National Build Code of Canada (Combustible Insulation and its Protection). a. ICC-ES Legacy Report No. 96-43.
E. Mock-Up: Provide a mock-up for evaluation of surface preparation tech niques and application workmanship. 1. Finish areas designated by Architect. 2. Do not proceed with remaining work until workmanship, color, and sheen are approved by Architect. 3. Refinish mock-up area as required to produce acceptable work.
1.7 DELIVERY, STORAGE, AND HANDLING A. Store products in per manufacturer’s recommendation until ready for installation. B. Store and dispose of solvent-based materials, and materials used with solvent-based materials, in accordance with requirements of local authorities having jurisdiction.
1.8 PROJECT CONDITIONS A. Maintain environmental conditions (temperature, humidity, and ventila tion) within limits recommended by manufacturer for optimum results. Do not install products under environmental conditions outside manufacturer’s absolute limits.
1.9 WARRANTY A. Provide manufacturer’s standard limited warranty.
PART 2 PRODUCTS2.1 MANUFACTURERS A. Acceptable Manufacturer: Zero-Loc, Enterprises Ltd.; 5202 272nd Street, Langley, BC, Canada V4W 1S3. ASD. Tel: (604) 607-1101. Fax: (604) 607-1142. Email: [email protected]. Web: www.zeroloc.com. B. Substitutions: Not permitted. C. Requests for substitutions will be considered in accordance with provisions of Section 01600.
2.2 MATERIALS A. Panel General Requirements: Roll-formed exterior and interior steel sheet faces laminated to panel grade type 1 expanded polystyrene (EPS) foam core. EPS foam core shall not contain CFC’s, HCFC’s or HFC’s. Insulated wall and ceiling panels shall be supplied in 46 inches (1168 mm) widths. Panel lengths shall be factory-sized to meet required site dimensions. 1. Panel Thickness: a. 2 inches (50 mm). b. 4 inches (100 mm). c. 6 inches (150 mm). d. 8 inches (200 mm). e. 10 inches (250 mm) 2. Interior wall and ceiling panels shall be clad on all exposed areas with 26 gauge (0.455 mm) pre-painted G90 galvanized steel (USDA & CFIA accepted). a. High gloss white (QC5216 White Appliance Polyester) b. Approved alternate. 3. Exterior insulated panels shall be clad on the weather-exposed side with 26 gauge (0.455 mm) pre-painted stucco embossed G90 galvanized steel. a. 8000 series (QC8317) white. b. USDA white. c. Approved alternate. 4. Concealed areas of panels (ie. top of ceiling panels) shall be clad with 28 gauge (0.378 mm) plain G90 galvanized steel. 5. Metal skins shall be thermal-set to the Type 1 EPS insulation. Insu- lated panels shall be manufactured individually laminated, ensuring uniform adhesion between metal skins and EPS insulation.
6. Panel edges shall be fabricated with a tongue-in groove type panel connection system (sleeve joint). 7. Sleeve-Joints shall be sealed internally by running continuous beads of butyloid caulking (or approved alternate) along the inside edges of the female sides of the panel joints. 8. Sleeve-Joints shall be externally caulked for USDA and Canadian Food Inspection Agency (CFIA) inspected areas only, or as speci- fied, with Tremco Proglaze White silicone (or approved alternate).
B. Wall and Ceiling Panel Insulation: 1. Wall panels and ceiling panels shall consist of Type 1 Expanded Polystyrene (EPS) insulation. 2. Finished panels shall have an R-value of 4.17 per inch at 75 de- grees F (23.8 degrees C). Insulation thickness of panels shall be adjusted in accordance with design R-value requirements. 3. Insulation shall not contain CFCs or HCFCs, or other expanding agents. 4. EPS Type 1 shall be manufactured with BASF KF262 bead size (or approved alternate), ensuring uniform densities throughout the insulation. 5. EPS Type 1 panel grade insulation shall meet or exceed federal standards for Type 1 EPS.
C. Panel Protection: 1. Manufacturer shall factory-bond 0.090 inch (2.3 mm) Fiberglass Re inforced Plastic (FRP) a minimum of 4 feet (1219 mm) high on the wall panels or as indicated. Refer to Room Finish Schedule.
D. Insulated Freezer Floor: 1. Insulated freezer floors shall be insulated with Zelsius EPS Type 2 high density insulation, complete with a minimum 10 mil (0.254 mm) polyethylene vapor barrier. a. Type 2 EPS shall meet or exceed federal standards for Type 2 EPS. E. Insulated Doors: 1. Hinged doors. 2. Manually operated horizontal sliding doors. 3. Door leafs shall be insulated with 4 inches (102 mm) of Type 1 ex- panded polystyrene (EPS) insulation. Type 1 EPS shall meet or exceed federal standards for Type 1 EPS. 4. Door leafs shall be finished as follows: a. FRP 0.090 inch (2.3 mm) thickness fiberglass reinforced plas tic factory-laminated (using a high-pressure heat-bonding process) to 28 gauge (0.378 mm) galvanized metal skins. b. 26 gauge (0.455 mm) stainless steel (304 2B) finish. c. 26 gauge (0.455 mm) prepainted white (QC5216 or approved alternate) G90 galvanized steel. 5. Door finishes shall be factory laminated (using a high-pressure heat-bonding process) to the Type 1 EPS insulation core. 6. Door leafs shall contain no wood or wood by-products. 7. Perimeter of door leafs shall be trimmed as follows: a. 18 gauge (1.214 mm) #304 2B stainless steel channel. b. 18 gauge (1.214 mm) G90 galvanized steel channel. c. 26 gauge (0.455 mm) prepainted white channel to match door leaf. 8. Doorframe Component: The Zero-Loc standard door frame com- ponent consists of a faceplate frame to which the door leaf is mounted, door jamb channel up to 8 inches (204 mm) thick for the perimeter of the door opening, and nuts, washers, through-bolts, reverse-side bolt plates and a snap-cap style sheet metal finishing channel to match wall finish. a. The faceplate component shall be fabricated from the following: 1) 16 gauge (1.897 mm) (minimum) #304 2B stainless steel. 2) 16 gauge ( 1.897 mm) (minimum) G90 galvanized steel. 3) 26 gauge (0.455 mm) prepainted white G90 galvanized steel clad overtop 16 gauge G90 galvanized steel. b. Door jambs to be capped with the following: 1) 18 gauge (1.214 mm) 304 2B stainless steel to match stain less steel faceplate. 2) 18 gauge (1.214 mm) G90 galvanized steel to match galva- nized steel faceplate. 3) 26 gauge (0.455 mm) prepainted white steel to match white faceplate. c. The frame component supplied by Zero-Loc also includes 3/8 inch (9.5 mm) nuts, washers and through-bolts and for up to an 8 inches (204 mm) thick wall. Reverse side of faceplate shall include 16 gauge (1.519 mm) bolt plates for bolts and sheet metal snap-cap finish flashing to match wall panel finish.
Technical Data Table
Insulation Tickness of Panels (Zelsius EPS)Inches (mm) 2 (50) 4 (100) 6 (150) 8 (200) 10 (250)
Insulation Type (Zelsius EPS) Type 1 Type 1 Type 1 Type 1 Type 1
Thermal Conductance ASTM C518-19 @ 75ºF (23.8ºC)Imperial Units [BTU/(ft2.hr.ºF) 0.12 0.06 0.04 0.03 0.024SI Units [w/(m2.ºC] 0.68 0.34 0.23 0.17 0.14
Thermal Conductance ASTM C518-19 @ -25ºF (-31.66ºC)*Imperial Units [BTU/(ft2.hr.ºF) 0.096 0.048 0.032 0.024 0.019SI Units [w/(m2.ºC] 0.55 0.27 0.18 0.14 0.11
Total Thermal Resistance ASTM C518-19 @ 75ºF (23.8ºC)RT [(ºF.ft2.hr.)/(BTU.in.)] 8.34 16.68 25.02 33.4 41.7RSI [(m2.ºC)/W] 1.47 2.94 4.4 5.88 7.34
Total Thermal Resistance ASTM C518-19 @ -25ºF (31.66ºC)*RT [(ºF.ft2.hr.)/(BTU.in.)] 10.34 20.68 31.02 41.36 51.7RSI [(m2.ºC)/W] 1.82 3.64 5.46 7.28 9.1
Panel Weight Per Sq.Ft.Foam density Approx. 1#/cu/ft 1#/cu/ft 1#/cu/ft) 1#/cu/ft 1#/cu/ftSheet Steel, 26 gauge,
galvanized & painted 2.16 lb 2.33 lb 2.5 lb 2.66 lb 2.83 lb
Bond Strength Metal to Polystyrene (EPS)When tested to ASTM C-297 Tension test of flat sandwich construction in a flat wise plane
29 psi (200kPa) [Styrene failure]
Max. Girt Spacing for a Max Deflection L/180For exterior wall panels: Interior Skin 26 gauge/Exterior Skin 26 gauge/ Uniform Load = 25PSF**
N/A 16’ 20’ 24’ 27’
Max. Spans in Ceiling Panels (Uniform Load 25PSF**)Walk-on ceiling. Single Span. No ceiling Suspension Hangers.
N/A 16’ 20’ 24’ 27’Walk-on ceiling. Multi Span. With ceiling Suspension Hangers.
N/A 12’ 12’ 12’ 12’Non walk-on ceiling - Single Span
N/A 23’ 28’ 32’ 32’Non walk-on ceiling - Multi Span
N/A 23’ 28’ 30’ 30’
Zero-Loc EPS Insulated Panel System
*Value at -25ºF (-33.66ºC) are for reference only, indicating the increased efficiency of EPS at lower temperature. All design loads should be calculated using the values at 75ºF (23.8ºC).
**Zero-Loc is not responsible for determining the implications of loads applied to a structure by either the wind loading of exterior wall panels or the live and dead of the ceiling system.
Company Profile. Since our establishment in 1969, ZERO-LOC
has grown to become a major worldwide producer of Insulated Panel
and Door Systems. This achievement has been made possible by the
dedication of our employees and the belief that giving greater service
and value to our customers is essential to success.
For design assistance, structural details,
AutoCAD disks, product specifications and
other technical information, please contact
your nearest Zero-Loc representative.
www.zeroloc.com13 21 00/ZERBuyLine 0678
A Wide Range of Applications
• Exterior / Interior EPS insulated build-ing panels for warehouses, and food processing plants
• Standard & specialty insulated doors
• Walk-on suspended ceiling systems
• Storage freezers & coolers
• Blast/Spiral/IQF Freezer Tunnels & Enclosures
• Federally inspected food processing areas
• Environment/atmosphere control rooms
• Factory-Laminated Fiberglass Reinforced Plastic (FRP)
INSULATED PANEL SYSTEMS
PART 1 GENERAL1.1 SECTION INCLUDES
A. Expanded polystyrene (EPS) insulated metal wall and ceiling panels with related accessories.
1.2 RELATED SECTIONS A. Section 03300 - Concrete: Foundations. B. Section 05120 - Structural Steel: Primary structure. C. Section 05500 - Steel Fabrication: Supporting structure.
1.3 REFERENCES
A. American Society for Testing and Materials (ASTM) E96: Standard Test Methods for Water Vapor Transmission of Materials. B. American Society for Testing and Materials (ASTM) E283: Standard Test Method for Rate of Air Leakage through Exterior Windows, Curtain Walls, and Doors. C. Underwriters’ Laboratories of Canada (ULC/ORD-C376-1995): Fire Growth of Foamed Plastic Insulated Building Panels in a Full-Scale Room configuration.
1.4 SYSTEM DESCRIPTION A. General: Construct panel system to provide for expansion and contrac tion of component materials without causing buckling, failure of joint seals, undue stress on fasteners, or other detrimental effects to the panel system or adjacent building systems, or warping of faces of panel system. B. Performance Requirements: Design and construct panels to meet requirements as indicated. 1. Design panel composition to resist wind load mandated by code, with deflection limit of L/180. a. No permanent damage to panels or connections when sub jected to 1.5 times the design wind pressures for both inward and outward. 2. Air leakage: Not greater than .06 cfm per square foot when tested in compliance with ASTM E283 at 1.56 pounds per square foot.
1.5 SUBMITTALS A. Submit under provisions of Section 01300. B. [Product Data]: Manufacturer’s data sheets on each product to be used, including: 1. Preparation instructions and recommendations. 2. Storage and handling requirements and recommendations. 3. Detailed specification of construction and fabrication. 4. Manufacturer’s installation instructions. 5. Certified test reports indicating compliance with specified perfor- mance requirements.
C. Shop Drawings: Indicate dimensions, description of materials and fin ishes, general construction, specific modifications, component connec- tions, anchorage methods, hardware, and installation procedures, including specific requirements indicated. 1. Profile and gauge of both exterior and interior sheet. 2. Metal finish. 3. Relationship to other work. 4. Fully show details and connections to and locations of supporting steel indicating control points. D. Selection Samples: For each finish product specified, two complete sets of color chips representing manufacturer’s full range of available colors and patterns. E. Verification Samples: For each finish product specified, two samples, minimum size 6 inches (150 mm) square, representing actual product, color, and patterns. F. Quality Control Submittals: 1. Statement of qualifications. 2. Design data. 3. Test reports.
1.6 QUALITY ASSURANCE A. Manufacturer/installer shall be responsible for fabrication and installa- tion of panel and support framing as specified in this section to comply with the following: 1. Wind load engineering to comply with code requirements. B. Manufacturer’s Qualifications: Not less than 5 years experience in the actual production of specified products. 1. Comply with rigid factory Quality Control program which includes quarterly unannounced inspections from UL, and independent test ing laboratories providing reports directly to code authority. 2. Successfully completed not less than 100 comparable scale projects using this system. C. Installer’s Qualifications: Firm experienced in installation of systems similar in complexity to those required for this Project, including specific requirements indicated. 1. Acceptable to or licensed by manufacturer. 2. Not less than 3 years experience with systems. 3. Successfully completed not less than 5 comparable scale projects using this system. D. Product Requirements: 1. Metal members (prone to rust) and wood or wood by-products (prone to moisture absorption and rot), shall not be permitted within the panel connection system. 2. Panel joints connection system, tested in accordance with ASTM E283 “Air Leakage Rate Testing” and ASTM E96 “Water Vapor Per meance Rate Testing” shall have an air leakage rate at 75 Pa OF 0.00m3/h-m2 (0.00cfm/sq.ft.) and a water vapor permeance rate of 0.00 perms. 3. Insulated panels, related accessories, and construction details shall be in accordance with the following regulatory agencies, where required: a. Canadian Food Inspection Agency (CFIA) b. United States Department of Agriculture (USDA) 4. Wall and ceiling panels, insulated with Type 1 Expanded Polysty- rene (EPS) manufactured to EPS Type 1 standards, shall be listed in accordance with ULC/ORD-C376-1995, “Fire Growth of Foamed Plastic Insulated Building Panels in a Full-Scale Room Configura tion”, in compliance with Part 3.1.5.12 of the 2005 National Build Code of Canada (Combustible Insulation and its Protection). a. ICC-ES Legacy Report No. 96-43.
E. Mock-Up: Provide a mock-up for evaluation of surface preparation tech niques and application workmanship. 1. Finish areas designated by Architect. 2. Do not proceed with remaining work until workmanship, color, and sheen are approved by Architect. 3. Refinish mock-up area as required to produce acceptable work.
1.7 DELIVERY, STORAGE, AND HANDLING A. Store products in per manufacturer’s recommendation until ready for installation. B. Store and dispose of solvent-based materials, and materials used with solvent-based materials, in accordance with requirements of local authorities having jurisdiction.
1.8 PROJECT CONDITIONS A. Maintain environmental conditions (temperature, humidity, and ventila tion) within limits recommended by manufacturer for optimum results. Do not install products under environmental conditions outside manufacturer’s absolute limits.
1.9 WARRANTY A. Provide manufacturer’s standard limited warranty.
PART 2 PRODUCTS2.1 MANUFACTURERS A. Acceptable Manufacturer: Zero-Loc, Enterprises Ltd.; 5202 272nd Street, Langley, BC, Canada V4W 1S3. ASD. Tel: (604) 607-1101. Fax: (604) 607-1142. Email: [email protected]. Web: www.zeroloc.com. B. Substitutions: Not permitted. C. Requests for substitutions will be considered in accordance with provisions of Section 01600.
2.2 MATERIALS A. Panel General Requirements: Roll-formed exterior and interior steel sheet faces laminated to panel grade type 1 expanded polystyrene (EPS) foam core. EPS foam core shall not contain CFC’s, HCFC’s or HFC’s. Insulated wall and ceiling panels shall be supplied in 46 inches (1168 mm) widths. Panel lengths shall be factory-sized to meet required site dimensions. 1. Panel Thickness: a. 2 inches (50 mm). b. 4 inches (100 mm). c. 6 inches (150 mm). d. 8 inches (200 mm). e. 10 inches (250 mm) 2. Interior wall and ceiling panels shall be clad on all exposed areas with 26 gauge (0.455 mm) pre-painted G90 galvanized steel (USDA & CFIA accepted). a. High gloss white (QC5216 White Appliance Polyester) b. Approved alternate. 3. Exterior insulated panels shall be clad on the weather-exposed side with 26 gauge (0.455 mm) pre-painted stucco embossed G90 galvanized steel. a. 8000 series (QC8317) white. b. USDA white. c. Approved alternate. 4. Concealed areas of panels (ie. top of ceiling panels) shall be clad with 28 gauge (0.378 mm) plain G90 galvanized steel. 5. Metal skins shall be thermal-set to the Type 1 EPS insulation. Insu- lated panels shall be manufactured individually laminated, ensuring uniform adhesion between metal skins and EPS insulation.
6. Panel edges shall be fabricated with a tongue-in groove type panel connection system (sleeve joint). 7. Sleeve-Joints shall be sealed internally by running continuous beads of butyloid caulking (or approved alternate) along the inside edges of the female sides of the panel joints. 8. Sleeve-Joints shall be externally caulked for USDA and Canadian Food Inspection Agency (CFIA) inspected areas only, or as speci- fied, with Tremco Proglaze White silicone (or approved alternate).
B. Wall and Ceiling Panel Insulation: 1. Wall panels and ceiling panels shall consist of Type 1 Expanded Polystyrene (EPS) insulation. 2. Finished panels shall have an R-value of 4.17 per inch at 75 de- grees F (23.8 degrees C). Insulation thickness of panels shall be adjusted in accordance with design R-value requirements. 3. Insulation shall not contain CFCs or HCFCs, or other expanding agents. 4. EPS Type 1 shall be manufactured with BASF KF262 bead size (or approved alternate), ensuring uniform densities throughout the insulation. 5. EPS Type 1 panel grade insulation shall meet or exceed federal standards for Type 1 EPS.
C. Panel Protection: 1. Manufacturer shall factory-bond 0.090 inch (2.3 mm) Fiberglass Re inforced Plastic (FRP) a minimum of 4 feet (1219 mm) high on the wall panels or as indicated. Refer to Room Finish Schedule.
D. Insulated Freezer Floor: 1. Insulated freezer floors shall be insulated with Zelsius EPS Type 2 high density insulation, complete with a minimum 10 mil (0.254 mm) polyethylene vapor barrier. a. Type 2 EPS shall meet or exceed federal standards for Type 2 EPS. E. Insulated Doors: 1. Hinged doors. 2. Manually operated horizontal sliding doors. 3. Door leafs shall be insulated with 4 inches (102 mm) of Type 1 ex- panded polystyrene (EPS) insulation. Type 1 EPS shall meet or exceed federal standards for Type 1 EPS. 4. Door leafs shall be finished as follows: a. FRP 0.090 inch (2.3 mm) thickness fiberglass reinforced plas tic factory-laminated (using a high-pressure heat-bonding process) to 28 gauge (0.378 mm) galvanized metal skins. b. 26 gauge (0.455 mm) stainless steel (304 2B) finish. c. 26 gauge (0.455 mm) prepainted white (QC5216 or approved alternate) G90 galvanized steel. 5. Door finishes shall be factory laminated (using a high-pressure heat-bonding process) to the Type 1 EPS insulation core. 6. Door leafs shall contain no wood or wood by-products. 7. Perimeter of door leafs shall be trimmed as follows: a. 18 gauge (1.214 mm) #304 2B stainless steel channel. b. 18 gauge (1.214 mm) G90 galvanized steel channel. c. 26 gauge (0.455 mm) prepainted white channel to match door leaf. 8. Doorframe Component: The Zero-Loc standard door frame com- ponent consists of a faceplate frame to which the door leaf is mounted, door jamb channel up to 8 inches (204 mm) thick for the perimeter of the door opening, and nuts, washers, through-bolts, reverse-side bolt plates and a snap-cap style sheet metal finishing channel to match wall finish. a. The faceplate component shall be fabricated from the following: 1) 16 gauge (1.897 mm) (minimum) #304 2B stainless steel. 2) 16 gauge ( 1.897 mm) (minimum) G90 galvanized steel. 3) 26 gauge (0.455 mm) prepainted white G90 galvanized steel clad overtop 16 gauge G90 galvanized steel. b. Door jambs to be capped with the following: 1) 18 gauge (1.214 mm) 304 2B stainless steel to match stain less steel faceplate. 2) 18 gauge (1.214 mm) G90 galvanized steel to match galva- nized steel faceplate. 3) 26 gauge (0.455 mm) prepainted white steel to match white faceplate. c. The frame component supplied by Zero-Loc also includes 3/8 inch (9.5 mm) nuts, washers and through-bolts and for up to an 8 inches (204 mm) thick wall. Reverse side of faceplate shall include 16 gauge (1.519 mm) bolt plates for bolts and sheet metal snap-cap finish flashing to match wall panel finish.
Technical Data Table
Insulation Tickness of Panels (Zelsius EPS)Inches (mm) 2 (50) 4 (100) 6 (150) 8 (200) 10 (250)
Insulation Type (Zelsius EPS) Type 1 Type 1 Type 1 Type 1 Type 1
Thermal Conductance ASTM C518-19 @ 75ºF (23.8ºC)Imperial Units [BTU/(ft2.hr.ºF) 0.12 0.06 0.04 0.03 0.024SI Units [w/(m2.ºC] 0.68 0.34 0.23 0.17 0.14
Thermal Conductance ASTM C518-19 @ -25ºF (-31.66ºC)*Imperial Units [BTU/(ft2.hr.ºF) 0.096 0.048 0.032 0.024 0.019SI Units [w/(m2.ºC] 0.55 0.27 0.18 0.14 0.11
Total Thermal Resistance ASTM C518-19 @ 75ºF (23.8ºC)RT [(ºF.ft2.hr.)/(BTU.in.)] 8.34 16.68 25.02 33.4 41.7RSI [(m2.ºC)/W] 1.47 2.94 4.4 5.88 7.34
Total Thermal Resistance ASTM C518-19 @ -25ºF (31.66ºC)*RT [(ºF.ft2.hr.)/(BTU.in.)] 10.34 20.68 31.02 41.36 51.7RSI [(m2.ºC)/W] 1.82 3.64 5.46 7.28 9.1
Panel Weight Per Sq.Ft.Foam density Approx. 1#/cu/ft 1#/cu/ft 1#/cu/ft) 1#/cu/ft 1#/cu/ftSheet Steel, 26 gauge,
galvanized & painted 2.16 lb 2.33 lb 2.5 lb 2.66 lb 2.83 lb
Bond Strength Metal to Polystyrene (EPS)When tested to ASTM C-297 Tension test of flat sandwich construction in a flat wise plane
29 psi (200kPa) [Styrene failure]
Max. Girt Spacing for a Max Deflection L/180For exterior wall panels: Interior Skin 26 gauge/Exterior Skin 26 gauge/ Uniform Load = 25PSF**
N/A 16’ 20’ 24’ 27’
Max. Spans in Ceiling Panels (Uniform Load 25PSF**)Walk-on ceiling. Single Span. No ceiling Suspension Hangers.
N/A 16’ 20’ 24’ 27’Walk-on ceiling. Multi Span. With ceiling Suspension Hangers.
N/A 12’ 12’ 12’ 12’Non walk-on ceiling - Single Span
N/A 23’ 28’ 32’ 32’Non walk-on ceiling - Multi Span
N/A 23’ 28’ 30’ 30’
Zero-Loc EPS Insulated Panel System
*Value at -25ºF (-33.66ºC) are for reference only, indicating the increased efficiency of EPS at lower temperature. All design loads should be calculated using the values at 75ºF (23.8ºC).
**Zero-Loc is not responsible for determining the implications of loads applied to a structure by either the wind loading of exterior wall panels or the live and dead of the ceiling system.
13 21 00/ZERBuyLine 0678www.zeroloc.com
Fiberglass Reinforced Plastic (FRP)
may be factory-bonded to the
steel skins of the Zero-Loc
EPS insulated panels, offering
increased scratch and dent
resistance. FRP protects panels from
the frequent rigorous
cleaning that is required in maintain-
ing a sanitary environment.
Food Processing
The finished Zero-Loc insulated
system is sanitary, energy efficient
and durable.
Cold Storage Warehouses
Ideally suited for low temperature
facilities, Zero-Loc EPS “R” value
performance increases as the
temperature decreases.
Walk-on Suspended Ceiling System
Constructed with Zero-Loc EPS
insulated panels, the finished
Zero-Loc walk-on suspended
ceiling system is energy efficient
and durable and is ideally suited for
low temperature, food processing and
controlled environment applications.
factory applied FRP
Expanded Polystyrene (EPS) Insulated Panel Systems
food processing plants cold storage warehouses walk-on suspended ceiling systems
Technical Specifications
5202-272nd St, Langley, BC Canada V4W 1S3 T: 604-607-1101 F: 604-607-1142
28 Plant Farm Blvd, Brantford, ON Canada N3S 7W3 T: 519-754-4500 F: 519-754-4214
119-9757 Juanita Dr N.E., Kirkland, WA USA 98033 T: 425-823-4588 F: 425-820-9749
Expanded Polystyrene (EPS) Insulated Panel Systems
9. Gasket: a. Hinged Door and Manual Sliding Door gaskets shall designed for heavy-duty applications, and shall be resistant to oils, grease and/or fats. Door gasket shall create a positive seal at all contact points between door leaf and frame, and door leaf and floor. Level floor surface required for positive gasket seal shall be provided by others. 10. Hinged Door Hardware: a. Overlap-type hinged doors shall be equipped with Kason #1398 Heavy-Duty Cam Rise hinges. b. Infitting-type hinged doors shall be equipped with Kason #1245 Reversible Cam-Rise Hinges. c. Hinged doors shall be equipped with Kason K56 Standard Latches complete with strike assemblies and Kason 481 inside Release Handles. 11. Sliding Door Hardware : a. Sliding door track shall consist of heavy gauge anodized alumi- num. Door leaf hanger assembly to be fabricated from: 1) 10 gauge (3.416 mm) 304 2B stainless steel to match door leaf trim finish and faceplate frame finish. 2) G90 galvanized steel to match door leaf trim finish and face plate frame finish. b. Hanger wheels shall be 4 inches (102 mm) in diameter and made from “Delrin” plastic. The 10 gauge (3.416 mm) hanger assembly shall also serve as the cover for the hanger assem bly. 12. Freezer Doors : a. Freezer doors shall be equipped with CSA/UL rated anti-frost heat trace in both door leaf and faceplate frame for heavy-duty hinged and sliding freezer doors and in door leaf or faceplate frame only for hinged and sliding freezer doors in lighter-duty commercial applications. Heat trace shall be factory-wired to a ground-fault circuit interrupter.
2.3 FABRICATION A. Corners: 1. Corner panel connections shall be butt or mitered, flashed, and finished by installation crew on-site. 2. Where specified, corner panel connections shall be a single unit corner panel with a continuous metal skin on the outer bend. B. Offset: Maximum offset from true alignment between two identical members abutting end-to-end: 1/8 inch (3 mm).
PART 3 EXECUTION3.1 EXAMINATION A. Verification of Conditions: Examine areas and conditions under which Work is to be performed and identify conditions detrimental to proper or timely completion. 1. Panel installer to verify that structural steel supports for wall panels are within tolerances in the AISC Code of Standard Practice, Section 7 and supplement modification controlling Section 7.11.3, adjustable items. Limit maximum deviation of steel alignment to plus or minus 3/16 inch(4 mm) from the control with a 1/8 inch (3 mm) maximum change in deviation for any member for any 10 feet (3 m) length of panel. 2. Do not proceed until unsatisfactory conditions have been corrected. B. If support system preparation is the responsibility of another installer, notify Architect of unsatisfactory preparation before proceeding.
3.2 INSTALLATION A. Install in accordance with manufacturer’s instructions.
3.3 TOLERANCES A. Variation: Maximum variation from vertical or horizontal plane, 1/4 inch (6 mm) in 12 feet (3658 mm) length section or 1/2 inch (13 mm) over total length.
B. Offset: Maximum offset from true alignment between two identical members abutting end-to-end: 1/8 inch (3 mm).
3.4 FIELD QUALITY CONTROL A. Manufacturer’s Field Services: Manufacturer shall make periodic inspec tions and issue report to Architect regarding compliance with manufactur ers installation recommendations developed for the Project.
3.5 ADJUSTING A. Repair damage caused during construction. 1. Touch-up mars, scratches, and cut edges to match original finish. 2. If repairs cannot be made to comply with Architect’s requirements, remove damage and install new materials.
5.8 TECHNICAL DRAWINGS
5
6
7
2
1
3
8
4
Line Guide AssemblyLine Guide MountingLine Guide DriveMAIN StructureMAIN InsulationReel MountReel DriveBail Release
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11111111
MAIN Complete Assembly
MCA AD01VARIOUSVARIOUS
QUANTITY: 1
15.7 kg
EXPLODED VIEWSCALE: 1:12
ISOMETRIC VIEWSCALE: 1:16
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
NO. PART NAME Qty
3
1
2
1
4
4
4
4
4
4
2
3
1234
LGA01 - Line Guide Side BlockLGA02 - Line Guide PinLGA03 - Line Guide ShaftM6 20mm Flat Head Screw
2226
Line Guide Assembly
LGAxx AD01VARIOUSVARIOUS
QUANTITY: 1
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 22/04/09
NO. PART NAME Qty
16
12.50 12.50
20
R1 Filed
90.00°M6 FLAT HEAD
90.00°M6 FLAT HEAD
40
14
6.60M6
CLEAR
6.60M6
CLEAR
6.60M6
CLEAR
3 3
3
Aluminium 6061
0.1
SMOOTH
Line Guide Side Block
Quantity: 2LGA01 MD01
13.37 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 2:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 22/04/09
M6x1.0 Tapped Hole
15 151212
40
12
0.1
Aluminium 6061Polished
Line Guide Pin
LGA02 MD01
10.57 g
QUANTITY: 2
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 2:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 22/04/09
14
10
M6x1.0 Tapped Hole
16 26
MD01
42
1512
Steel 4150 QUANTITY: 2SMOOTH
LGA03
Line Guide Shaft0.04
32.35 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 2:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 22/04/09
4
4
4
1
3
3
3
2
2
4
3
4
1
Line Guide Mounting
LGMxx AD01QUANTITY: 1VARIOUSVARIOUS
Line Guide BearingLine Guide Bearing MountSlide Nut M6M6 45mm Flat Head Screw
1234
224
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 20/05/09
NO. PART NAME Qty
200100
16BORE THRU
90.00° 90.00°15
40
17512.50 12.50
6.60M6 FIT THRU
6.60M6 FIT THRU
12.60M6 FLAT HEAD
12.60M6 FLAT HEAD
7.50
Line Guide Bearing Mount
LGM01 MD01QUANTITY: 2Aluminium 6061Rough
0.1
308 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 20/05/09
1
4
4
6
6
6
6
3
2
5
5
Line Guide Drive
LGDxx AD01QUANTITY: 1VARIOUSVARIOUS
Rigid Shaft CouplerBrushless MotorLine Guide Motor SuppoerSlide Nut M6M6 12mm Flat Head ScrewM5 30mm Flat Head Screw
111224
123456
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
TENTATIVE DRAWINGM.P. 20/05/09
NO. PART NAME Qty
5.50M5 FIT THRUFOR ALL
6.60M6 FIT THRUFOR ALL
12.60M6 FLAT HEADFOR ALL
3517.50 17.50
28DRILL THRU
10.40M5 FLAT HEADFOR ALL
100
90.00°
90.00°
90.00°
20.25
45
55
49.50
30.25
12.50
6
70
49.5035 35
Line Guide Motor Support
LGD01 MD01QUANTITY: 1Aluminium 6061
ROUGH
0.1
99.4 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
TENTATIVE DRAWINGM.P. 20/05/09
10
4
4 5
5
2
4510
10
4
53
2
1
1
2
7
7
7
108
9
9
6 6
6
6
6
6
2
MAIN Structure
MSxx AD01QUANTITY: 1VARIOUSVARIOUS
PU25 400mm with HolesPU25 350mmPU25 266.488mmPU25 200mm with HolesPU25 150mmAngle AdaptorMount BracketSlide Nut M6M6 10mm Button Head Scr.M6 20mm Button Head Scr.
12345678910
264448412836
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:8 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
NO. PART NAME Qty
2525
20
R5.50M6 BUTTON HEAD FIT20 DEEP
R5.50M6 BUTTON HEAD FIT20 DEEP
400 375
12.50
12.50
MACHINED FROM PU25 SOLECTRO ALUMINIUM PROFILES
AluminiumROUGH
MS01 MD01
PU25 400mm with Holes
QUANTITY: 2
0.1
272 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:5 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
5M6 BOTTOM TAP20 DEEP
5M6 BOTTOM TAP
20 DEEP
350
PU25 350mm
MS02 MD01QUANTITY: 6AluminiumROUGH
0.1
MACHINED FROM PU25 SOLECTRO ALUMINIUM PROFILES
242 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:5 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
5M6 BOTTOM TAP20 DEEP
5M6 BOTTOM TAP
20 DEEP
266.49
PU25 266.488mm
MS03 MD01QUANTITY: 4AluminiumROUGH
0.1
MACHINED FROM PU25 SOLECTRO ALUMINIUM PROFILES
184 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:5 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
25
25
R5.50M6 BUTTON HEAD FIT20 DEEP
R5.50M6 BUTTON HEAD FIT20 DEEP
17512.50 12.50
200
R5.50M6 BUTTON HEAD FIT
20 DEEP
R5.50M6 BUTTON HEAD FIT
20 DEEP
175
12.50
12.50
PU25 200mm with Holes
MS04 MD01QUANTITY: 4AluminiumROUGH
0.1
MACHINED FROM PU25 SOLECTRO ALUMINIUM PROFILES
133 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
2525
5M6 BOTTOM TAP20 DEEP
5M6 BOTTOM TAP
20 DEEP
150
MACHINED FROM PU25 SOLECTRO ALUMINIUM PROFILES
PU25 150mm
MS05 MD01QUANTITY: 4AluminiumROUGH
0.1
104 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
31
1
3
3
3
1
1
2
2
2
2
4
MAIN Insulation
MIxx AD01QUANTITY: 1VARIOUSVARIOUS
Insulation Frame 775mmInsulation Frame 400mmInsulation Side PanelInsulation Top PanelInsulation Bottom Fill
1234x
44411
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:12 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL PARTIAL DRAWINGM.P. 21/05/09
NO. PART NAME Qty
825
Insulation Frame 775mm
MI01 MD01QUANTITY: 4Aluminium 6061ROUGH
0.1
80 g
MACHINED FROM ALUMINIUM CORNER SECTION OF 20 x 20 mm
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:10 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
400
Insulation Frame 400mm
Mi02 MD01QUANTITY: 4Aluminium 6061
ROUGH
0.1
41 g
MACHINED FROM ALUMINIUM Corner Section 20 x 20 mm
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:5 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
396
823 90.00°
50
90.00°
Insulation Side Panel
MI03 MD01QUANTITY: 4Low-dens. EPSROUGH
350 g
1
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:10 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
396
396 90.00°
50
90.00°
Insulation Top Panel
MI04 MD01
150 g
QUANTITY: 1Low-dens. EPS
ROUGH
1
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:5 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
AD01QUANTITY: 1VARIOUSVARIOUS
12345
4
4
44
4
4
2
5
5
6
6
5
5
6
6
3
1 Reel Mount
RMxx
Spinning ReelReel Mount PlateBail Flip StopperM6 20mm Flat Head ScrewM6 Washer - 4mm thickSlide Nut M66
111644
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
NO. PART NAME Qty
100
6.60M6 FIT THRUFOR ALL
12.60M6 FLAT HEAD FITFOR ALL
24
16
16
204
6
90.00°
90.00°75
12.50
32.50
20017545
12.50
77.50
12.50
77.50
Reel Mount Plate
RM01 MD01QUANTITY: 1Aluminium 6061
ROUGH
0.1
313 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
60
30
M6x1.0 Tapped Hole
7.50
R10POLISHED FINISH
R15
15 DEEPBOTTOM TAP
7.50
50
7.50
15
Bail Flip Stopper
RM02 MD01QUANTITY: 1Aluminium 6061ROUGH
0.1
104 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
123456
2
1
6
6
6
6
3
5
5
4
Reel Drive
RDxx AD01QUANTITY: 1VARIOUSVARIOUS
Rigid Shaft CouplerReel ShaftReel Motor MountBrushless MotorM6 12mm Flat Head ScrewM5 30mm Flat Head Screw
111124
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
TENTATIVE DRAWINGM.P. 21/05/09
NO. PART NAME Qty
10
5M5 THREADED
50 20
70
Reel Shaft
RD01 MD01QUANTITY: 1Steel
SMOOTH
0.05
33 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
100
70
28 DRILL THRU
5.50M5 FIT THRUFOR FOUR HOLES
5.505.50
5.50
6.60M6 FIT THRUFOR TWO HOLES6.60
12.60M6 FLAT HEAD FIT
10.40M5 FLAT HEAD FIT
6M6 FIT THRU
6M6 FIT THRU
35
49.50
20.25
30.25
12.50
3.30
45
6
90.00°
90.00°
90.00°
10.25
17.5023.10
10.25
17.5029.90
Reel Motor Mount
RD02 MD01QUANTITY: 1Aluminium 6061
ROUGH
0.1
99 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
TENTATIVE DRAWINGM.P. 21/05/09
123456
1
1
2
4
46
6
6
6
6
5
5
3
3
6
5
5
3
55
Bail Release
BRxx AD01QUANTITY: 1VARIOUSVARIOUS
Servo MotorBail Release ArmServo Motor MountBail Release LeverM6 10mm Button Head Scr.Slide Nut M6
213266
DO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:3 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
NO. PART NAME Qty
3
20160
Bail Release Arm
BR01 MD01QUANTITY: 1Aluminium 6061SMOOTH
0.1
26 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:2 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
200
20
6M6 FIT THRU
6M6 FIT THRU
6M6 FIT THRU
6M6 FIT THRU
ODD:
20
200
6M6 FIT THRU
6M6 FIT THRU
6M6 FIT THRU
6M6 FIT THRU
4.50
15.50
10
3
12.50 69.80 17 88.20 12.50
12.50 88.20 17 69.80 12.50
4.50
15.50
10
3
EVEN:
Servo Motor Mount
BR02 MD01QUANTITY: 2 EVEN 1 ODD
Aluminium 6061ROUGH
0.1
32 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
FINAL DRAWINGM.P. 21/05/09
3100
20
3
8.50
8.5024
Bail Release Lever
BR03 MD01QUANTITY: 2Aluminium 6061
ROUGH
0.1
16 gDO NOT SCALE DRAWING SHEET 1 OF 1
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
ASIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN MMTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFLTU and reel.SMRT Design Team. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OFLTU and reel.SMRT Design Team IS PROHIBITED.
5 4 3 2 1
INCOMPLETE DRAWINGM.P. 21/05/09