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Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 1
Design and Analysis of High Speed Helical Gear By Using Ansys
A. Sai Bharath*1, T .v .s .r .k. Prasad*2
M.Tech Student (Cad/ Cam) Mechanical Engineering, NCET, Jupudi, Ibrahimpatnam, Vijayawada, Krishna (dt),A.P, India.
Professor, Mechanical Engineering in NCET, Jupudi, Ibrahimpatnam, Vijayawada, Krishna (dt),A.P, India
Email: [email protected]
ABSTRACT
Marine engines are among heavy-duty machineries, which need to be taken care of in the best way during prototype
development stages. These engines are operated at very high speeds which induce large stresses and deflections in the gears as
well as in other rotating components. For the safe functioning of the engine, these stresses and deflections have to be minimized.
In this project, static-structural analysis on a high speed helical gear used in marine engines, have been performed. The
dimensions of the model have been arrived at by theoretical methods. The stresses generated and the deflections of the tooth have
been analyzed for different materials. Finally the results obtained by theoretical analysis and finite element Analysis are
compared to check the correctness. A conclusion has been arrived on the material which is best suited for the marine engines
based on the results. The present used material for helical gears is Mild Steel. In this project, gear is designed using two different
aluminum alloys 7475 and 6061. Theoretical calculations and analysis are done for Helical gear using Mild Steel, Aluminum
alloys 7475 and 6061. Parametric 3D modeling is done in Pro/Engineer and analysis is done in Ansys.
Key words: Gear design, Computer aided analysis, Gear Hobbing, Gear shaving, Structural Analysis.
1. INTRODUCTION
A gear is a rotating machine part having cut teeth, which
mesh with another toothed part in order to transmit torque.
Two or more gears working in tandem are called a
transmission and can produce a mechanical advantage
through a gear ratio and thus may be considered a simple
machine. Geared devices can change the speed, magnitude,
and direction of a power source. The most common
situation is for a gear to mesh with another gear however a
gear can also mesh with a non-rotating toothed part, called
a rack, thereby producing translation instead of rotation.
The gears in a transmission are analogous to the wheels in a
pulley. An advantage of gears is that the teeth of a gear
prevent slipping. When two gears of unequal number of
teeth are combined, a mechanical advantage is produced,
with both the rotational speeds and the torques of the two
gears differing in a simple relationship. In transmissions
which offer multiple gear ratios, such as bicycles and cars,
the term gear, as in first gear, refers to a gear ratio rather
than an actual physical gear. The term is used to describe
similar devices even when gear ratio is continuous rather
than discrete, or when the device does not actually contain
any gears, as in a continuously variable transmission.
2. METHODOLOGY OF SYSTEM
DESIGN
In order to design a helical gear system the following
procedure should be followed; The input conditions are
power, speed, helix angle, gear ratio.
Gear design starts with material selection. Proper
material selection is very important; Aluminum
has been selected as a material. If the material for
gear and pinion is same then the design should be
based since it is weak.
Find out the minimum central distance based on
the surface compression stress is
a≥ (i+1)3√ (0.7/σc) 2 E (Mt) iψ……. [Design
data]
Here Mt=torque transmitted by the
pinion=97420(KW/N)*Kd*K
Where Kd*K=1.3 , ψ=b/a………..[Design data].
Minimum normal modules may e determined as
mn≥1.15Cosβ {Mt/Yv σb ψm Z1} ^1/3..[design data]
Assume Z1=18, ψm=b/mn=10 from ..[design data]
Virtual number of teeth Zv=Z1/cos3β ,
Lewis form factor Yv=0.1540.192/Zv ….[ Design data]
Number of teeth on pinion Z1=2acosβ/mn*(i+1) , Number
of teeth on gear Z2=iZ1
Diameter of pinion D1=mn*Z1/cosβ , Diameter of gear
D2=mn*Z2/cosβ
Centre distance a=D1+D2/2 , Face width b= ψa
checking the calculations:
i): based on the compressive stress,
σc=0.7(i+1)/a*√{(i+1/ib)*E[mt]}
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 2
ii): based on the bending stress, σb=0.7(i+1)
(Mt)/{a.b.mn.Yv}
Here the bending and compressive stress values obtained
are less than the material property values, then the design is
safe.
2.1. Theoretical design calculation The theoretical design calculations are performed using the
input parameters such as power for marine high speed
engine, pinion speed, gear ratio, helix angle, pressure angle
etc. i.e Power P = 9000 KW, Speed of Pinion N = 3500
rpm, Gear Ratio i = 7, Helix Angle, β = 25oMinimum
centre distance based on surface compression strength is
given by
a ≥ (7+1) ]2.x
2.2 Material Selection Let the material for Pinion & Gear is Aluminum Alloy ;
Its design compressive stress & bending stresses are [σc =
25000 kgf/cm2 ], [σb = 3500 kgf/cm2]
2.2.1 Properties for Aluminum Alloy 6061
Speed of the pinion = 2000rpm
Power = p =240KW = 240 W
Gear ratio =6
Center distance = x =
Helix angle = 450 = α
Material used = mild steel
Properties = BHN =30
Minimum tensile strength = 500MPa
Young’s modulus = 68.9GPa=68.9 MPa
Compressive stress =
Bending stress = =392265.9 N/mm2
Module = m = 18
WKT gear ratio = GR =
We have GR =6 and
GR = No of teeth on gear =
Diameter of gear ,
mm
No of teeth on gear =
No of teeth on pinion = =15
Diameter of pinion =
center distance = mm
GR =
Normal pitch
m
m
mm
Normal pressure angle = фN
tan фN = tan ф (ф=20)
tan фN = tan 20
фN =
a) Face width
Usually recommended that the overlap should be 15 percent of the circular pitch
b =
The maximum face width may taken as 12.5 m to 20m
b = 20m = 360mm
Formative or equivalent no of teeth for helical gears =
Equivalent no of teeth on pinion =
Equivalent no of teeth on gear =
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 3
Tooth form factor for pinion for 200 full depth involute
Y1P = 0.154
Tooth form factor for gear for 200 full depth involute
Y1G = 0.154
Properties for helical gears:
Pressure angle ф = 20
Helix angle α = 450
Addendum = 0.8M(maximum) = 14. 4mm
Dedendum = 1M(minimum) = 18mm
Minimum total depth = 1.8m =32.4mm
Minimum clearance 0.2M =3.6mm
Thickness of tooth = 1.5708M =28.2744mm
Strength of helical gears:
b = face width
M = module
Y1 =tooth form factors
Both the pinion and gear are made of the same material the pinion is weaker thus the design will be based upon pinion
The allowable static stress ( ) for steel gears is
approximately one third of the ultimate tensile strength
= ,
Peripheral speed = V
= m/s
The value of velocity factor C depending upon peripheral
velocities greater than 20 m/s is given by
= ( ) Y1P
=
41.333
The dynamic tooth load on the helical gear is given by
Where v, b, c have usual meaning as discussed in spur gears
C = deformation factor =
K =0.111 for 200 full depth involute system
in N/mm2
C= =122.366N/mm
The static tooth load or endurance strength of the tooth for bevel gear is given by
(BHN=30) =flexural
endurance limit
N
DP, b, Q and K have usual meanings as discussed in spur gears in this case
K =load stress factor =
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 4
K=
Q =
b) Design for pinion shaft
Tangential load on pinion
Axial load of pinion
Bending moment of pinion shaft
X = over hang =1296
Bending moment of pinion shaft due to the axial load =
=
Torque transmitted by pinion T =
Equivalent twisting moment
We know that equivalent twisting moment
=
Let us now check for the principle shear stress WKT the shear stress induced
direct stress due to axial load = σ= 0.32
principle shear stress =
the principle shear stress is less than the permissible shear stress of 230 Mpa therefore the design is satisfactory
WKT the diameter of pinion hub =1.8 mm
Length of the hub = 1.25 mm
If the pitch circle diameter of the pinion is less than or equal to 14.7M+60mm = 14.7
c) Design for the gear shaft
Let
We have already calculated that the tangential load =
Axial load =
Bending moment due to the tangential load =
= (x = 1296)
Bending moment due to axial load =
N mm
= 20464606.45
Torque on the gear shaft = T
=torque on the pinion shaft N mm
We Know that equivalent twisting moment =
We also know that equivalent twisting moment
=
=
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 5
Let us know check for the principle shear stress;
We Know that shear stress = τ =
230
Direct stress due to axial load σ =
Principle shear stress =
The principle shear stress is same as the permissible stress of 230 Mpa the design is satisfactory
We Know that diameter of gear hub = 1.8 =138.276mm
Length of hub =1.25 =96.025mm
Length of hub is < face width i.e = 360mm
3. MODEL OF HELICAL GEAR
2D DRAWING
3.1 Analysis Significant Development in analysis of strength
properties of gear transmission follows the achievements in
computation design, simulation of meshing and tooth
contact analysis made by Lewiki,Handschuh.They carried
out 2D analyses using finite element method, boundary
element methods & Compared the results to experimental
ones validated crack simulation based on calculated stress
intensity factors and mixed mode crack angle prediction. In
practice, simplified formulas are usually used in gear
transmission design. They enables estimation of stresses at
tooth root with accuracy acceptable for engineering design.
In every case, strength properties of gear transmissions are
strongly influenced by gear geometry, applied
manufacturing processes, and dimensional accuracy of
manufactured gears.
3.2 Gear Manufacturing
Gears are manufactured by various processes. These are,
casting, stamping, rolling, extruding, and machining. Gears
can also be produced by powder metallurgy. Among the
above said process, machining process in most commonly
used. It is an accurate method. Basically gears are produced
by machining by a) Forming method. b) Generating
method.
3.2.1 Forming Method
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 6
In this method a form cutter is used. The formed cutter
may be single point cutting tool or a multipoint milling
cutter. The cutting edges formed cutter has been finished to
the shape between the gear teeth being cut. Forming
method is used for producing very small number of gears.
Gears produced by forming are less accurate. Forming
process is simple and cheaper. This method is takes more
time.
3.2.2 Gear Generating processes
This method of gear manufacturing is based on the
fact that any two involute gears of the same module will
mesh together. Here one of the meshing gears is made as
the cutter. The other gear rotates and also reciprocates
along the width of the gear blank. Because of the relative
rolling motion between cutter and the blank, gear teeth are
generated on the gear blank. The gear may be generated by
rack cutter, pinion cutter or a hob. Using the generated
method, profile of the gear teeth can be very accurately
produced. The following generating methods used for gear
production are Gear shaping, Gear planning, Gear hobbing.
3.2.3 Gear Hobbing It is a process of generating a gear by means of a
rotating cutter called hob. The hob has helical threads.
Grooves are cut in the threads parallel to the axis. This will
provide the edges. Proper rake and clearance angle are
ground on these cutting edges. The rotating hob acts like a
continuously moving rack as it cuts. The blank is mounted
on a vertical arbour. The hob is mounted in a rotating
arbour. The hob axis is tilted the hob lead angle so that its
teeth are parallel to the axis of the gear blank.
Then = (90º-1).
Where 1 = helix angle of the hob thread. NOTE: (hob lead
angle = 90º-hob helix angle)
The hob is rotated at suitable cutting speed. It is fed across
the blank face. The hob and blank are made to rotate in
correct relationship to each other; they rotate like a worm
and worm gear in mesh. For one relation of the hob, the
blank rotates by one tooth. (In case of single start hob).
For helical gears, the axis of the hob is inclined to
horizontally. Where a= θ + (90º-1).
(If the helix of the hob and the helix of the gear to be cut
are different. One is right and another is left handed.)
a= θ (90º-1)
(if the helix of the hob and the helix of the gear to be cut
are both right handed or both is left handed.)
Where, a = helix angle of the helical gear to be cut.,1 =
helix angle of the hob.
The gear hobbing technique is used for generating spur,
helical and worm gears. Gear hobbing is used in
automobiles, machine tools, various components,
instruments, clocks and other equipment.
In the present the helical gears were produced by gear
hobbing technique and finished by gear shaving operation.
The gear teeth generating process by milling machine is
shown in fig 2.3.1.
Fig.2.3.1. Image showing milling machine
3.2.4 Finishing Process Gears manufactured by different machining processes
will have rough surfaces. The machined gears may have
errors in tooth profiles, concentricity and helix angles. For
quiet and smooth running of gears, these errors and rough
surfaces should be removed. Gear finishing operations are
done for this purpose. The various gear finishing processes
like gear burnishing, gear shaving etc.
3.2.5 Gear Burnishing Is a method of finishing of gear teeth which are not
hardened. This is a cold working process. This method is
used to improve the surface finish of the gear teeth. This
also increases the hardness at the teeth surface. The teeth of
burnishing gears are very hard, smooth and accurate. They
are arranged at 120º position around the work gear. The
gears are rotated in one direction for some period. Then
they are rotated in the reverse direction for the some period.
The pressure is applied by the harder burnishing teeth on
the work gear.
3.2.6 Gear Shaving This is the most common method of gear
finishing. In this method a very hard gear shaving cutter is
used to remove fine chips from the gear teeth. The shaving
cutter may be in the form of a rack or a pinion. The rotary
method using pinion cutter is used on all types of gears.
The rotating cutter will have helical teeth of about 15º helix
angle. The cutter has a number of serrations on its
periphery. These act as cutting edges. In the rotary type of
gear shaving the work gear is held between centres and is
free to rotate. The shaving cutter meshes with the work
gear. The axis of the cutter is inclined to the gear at an
angle equal to the helix angle of the cutter (θ) when the
cutter rotate, the cutter reciprocates in a direction parallel to
the gear axis. The cutting edges of the shaving cutter
remove burrs, nicks and high points on the surface of the
work gear. It can remove from the teeth flank, chips up to
0.1mm thick.
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 7
4. ANALYSIS OF HELICAL GEAR
MATERIAL – ALUMINUM
ALLOY 6061 STRUCTURAL
AND RESULT ANALYSIS
Imported Model from Pro/Engineer
Element Type: Solid 20 node 95
Material Properties: Youngs Modulus (EX)
: 68900N/mm2
Poissons Ratio (PRXY) : 0.33
Density : 0.00000270 kg/mm3
Meshed Model
Loads
Pressure – 0.0084721 N/mm2
Solution
Solution – Solve – Current LS – ok
Displacement Vector Sum
Von Mises Stress
Strain
MODAL ANALYSIS
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 8
Main menu>Preprocessor>Loads>Analysis Type> New
Analysis> Select Modal> Click> OK
Main menu>Preprocessor>Loads>Analysis Type>
Analysis Options> No. Of Modes to Extract: 5 Click> OK
Main menu>Solution>Solve>Current Ls>Ok
RESULTS
Mode 1
Mode 2
Mode
3
Mode 4
Mode 5
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 9
RESULTS TABLE
STRUCTURAL RESULTS
ALUMINUM ALLOY 6061 ALUMINUM ALLOY 7475 MILD STEEL
DISPLACEMENT (mm) 0.898e-04 0.362e-03 0.117e-03
STRESS (N/mm2) 0.050801 0.159783 0.165659
STRAIN 0.745e-06 0.229e-05 0.794e-06
MODAL RESULTS
WEIGHT COMPARISON
MILD STEEL AL ALLOY 6061 AL ALLOY 7475
Kg 5632.034 1932.2 2010.92
5. CONCLUSION
In this project, static-structural analysis on a high speed
helical gear used in marine engines, have been performed.
The dimensions of the model have been arrived at by
theoretical methods. The stresses generated and the
deflections of the tooth have been analyzed for different
materials.The present used material for helical gears is
Mild Steel. In this project, gear is designed using two
different aluminum alloys 7475 and 6061. Theoretical
calculations and analysis are done for helical gear using
Mild Steel, Aluminum alloys 7475 and 6061. While using
Mild Steel for helical gears, the weight is more. By
replacing with aluminum alloys, the weight is reduced.
Parametric 3D modeling is done in Pro/Engineer and
analysis is done in Ansys.
By observing the analysis results, the stress values are less
by using all the 3 materials than their respective yield stress
values. So using aluminum alloys is better for helical gear
used in high speed marine engines. In aluminum alloys,
using aluminum alloy 6061 is better as its weight is less
than aluminum alloy 7475.
ALUMINUM ALLOY
6061
ALUMINUM ALLOY
7475 MILD STEEL
MODE 1 FREQUENCY (Hz) 15.861 15.704 16.551
DISPLACEMENT (mm) 0.3645 0.035725 0.021412
MODE 2 FREQUENCY (Hz) 16.446 16.284 16.839
DISPLACEMENT (mm) 0.052211 0.051179 0.030543
MODE 3 FREQUENCY (Hz) 16.887 14.72 17.284
DISPLACEMENT (mm) 0.066233 0.064924 0.038727
MODE 4 FREQUENCY (Hz) 19.323 19.132 19.754
DISPLACEMENT (mm) 0.053395 0.05234 0.030758
MODE 5 FREQUENCY (Hz) 21.804 21.589 22.663
DISPLACEMENT (mm) 0.056598 0.05234 0.032597
Sai Bharath -International Journal of Computer Science information and Engg., Technologies ISSN 2277-4408 || 01112013-021
IJCSIET-ISSUE3-VOLUME3-SERIES3 Page 10
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