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Orynyak I.V., Radchenko S.A.
IPS NASUIPS NASU
Pisarenko’ Institute for Problems of Strength , Kyiv, Ukraine National Academy of Sciences of Ukraine
Pisarenko’ Institute for Problems of Strength , Kyiv, Ukraine National Academy of Sciences of Ukraine
STRESS STATE CALCULATION OF COMPLEX PIPING SYSTEMS AT STATIC AND DYNAMIC LOADINGS
STRESS STATE CALCULATION OF COMPLEX PIPING SYSTEMS AT STATIC AND DYNAMIC LOADINGS
1th Hungarian-Ukrainian Joint Conference on
Safety-Reliability and Risk Engineering Plants and Components
11,12 April 2006, Miskolc, Hungary
IPS NASUIPS NASU
3D model of pipeline system of RBMK Chernobyl NPP3D model of pipeline system of RBMK Chernobyl NPP
Problem statementProblem statement
Calculation
designis executed according to currently standards
doesn’t require high accuracy
uses high safety factors
uses old design solution
fitness for service
requires high accuracy
requires determination of
local distribution of stress: for calculation of defects for application of systems of
monitoring for application of strength
criteria
IPS NASUIPS NASUProblems of calculation pipe bend
A
C
B
D
A
C
B
D
zKzK
1d
0d
B
O
R
BR
BtR2
- parameter of flexibility - parameter of flexibility
- parameter of curvature
EI
sMK
ds
d
bendpipeforf
pipesraightforK
1,
1
1. Pipe bend as BEAM element in a piping 1. Pipe bend as BEAM element in a piping
2. The local stress-displacement fields of a SHELL 2. The local stress-displacement fields of a SHELL
• Saint Venant’s task;
• Geometrical non-linearity - internal pressure;
• End-effect; -3
-2
-1
0
1
2
3
0 30 60 90 120 150 180
end-effect
Saint Venant'ssolution
z
x
k
2
IPS NASUIPS NASU
Software “InfoPipeMaster” - Software “InfoPipeMaster” - information and calculating programinformation and calculating program
1. Gathering and storage the information about pipeline:
2. Calculation of the stress strain state:
static calculation static calculation
computer portrait, schemas, drawings and photos;
databases Materials, Soils, Objects and Defects;
results of technical inspection;
results of calculation
3. Comparative analysis of the results of the inspections executed during the different period of time .
4. Preparation of reports about a condition of object according to results of observation
dynamic analysis dynamic analysis
calculation of defects calculation of defects
IPS NASUIPS NASUDatabases structureDatabases structure
«Object location»
«Geometry» «Calculation results»«Loads»• object type
• dimensions
• schemas, photos, drawings
• object label
• coordinates
• pressure
• temperature
• distribution forces
• weight
• displacements and angles
• forces and moments
• stresses
«Defect location»
«Geometry» «Calculation results»«Loads»• defect type
• dimensions• defect label
• element number
• coordinates
• pressure
• axial force
• bending moments
• stress intensity factor
• reference stress
• safety factor
DB «Objects»
DB «Defects»
IPS NASUIPS NASU The features of calculation modules The features of calculation modules • Pipelines are considered as beam structure where characteristics of cross sections are determined from theory of shells
• The calculation method is based on a method of initial parameters
• The continuity of the solution at transition from dynamics to a statics is provided
• Analytical solution for pipe bend are used
• Large library of elements with taking into account environment influence
• Accounting nonlinear supports and soil characteristics
• Convenient system for building and editing
• Abilities for data export – import with other software
IPS NASUIPS NASU
Equilibrium equationsEquilibrium equations
000
B
K
dBdK yx
yzxy mQ
BK
dB
dK
00
zyz mQ
dBdK
0
zz q
dBdQ
0
y
допy q
BN
dB
dQ
00
xy
доп
qB
Q
dBdN
00
000 2
21EtBPR
EFBN
EIKK
dBdθ доп
zin
z
GIK
B
θ
dBd xy
200
EI
KK
BdB
d yout
y 00
The equations for displacementsThe equations for displacements
0
2
0 2GIBRKK
dBd x
кр
yz w
zy
Bu
dB
d
00
w
122
21
0
2
00 EIBRKK
EFsN
EhRP
TBdB
du zinдоп
Tyw
The equations for curved beamThe equations for curved beam
The equations for angles of cross-section center The equations for angles of cross-section center
IPS NASUIPS NASUAnalytical solution for axial displacementAnalytical solution for axial displacement
.sin
221
4sincossin
4sincos
2sin
2sincos
4sin5cos8cos8
4cos54sinsin9
2sin3cos2
2sincos22
cos12
sin2
21
cos1sincos
0
2
0
2
000
220
220
000
2
000
020
00
0
00
00
0
00
00
EtPR
TBBq
BqQNEFB
BqBq
BNBQ
BmtBPR
FBN
K
IK
EIBK
Buu
y
xyдоп
xy
допy
z
доп
inz
in
zyw
IPS NASUIPS NASU Static calculation. Pipe bend - SHELLStatic calculation. Pipe bend - SHELL
r
R
O
B
O1
t
x
y
z
v u
w
Equilibrium equations:Equilibrium equations:
PS
NQS
SQRSR
Nxx
sin11
0cos11
SNL
SR
QSN
RSx
0sin1 2
xx Q
NLS
RS
0cos1
xx M
MSM
RSQ
01 2
x
xxM
MSRS
SQ
HN
HNx
12H
L
HM
HM x
21 H
M x
Physical equations:Physical equations:
IPS NASUIPS NASU
Swvu
S
sincos1
Rwv
R
1
v
SSuu
R1cos1
RS
wv
S
wvw
S
cossinsincos1
22
2
2
22
2
2
1
R
ww
R
w
S
wRSSR
vSS
uuR 2
2 cos22sin11cos1
- strains- strains
- curvatures- curvatures
Geometric equations:Geometric equations:
Solution methodsSolution methods
Complete - 8-th order Simplified - 4-th order- semianalytical - semianalytical
- analytical
2
z
x
k
zk
2
Stress distribution on outside surface for in-plane bending of 900 bend having rigid flanges
Stress distribution on outside surface for in-plane bending of 900 bend having rigid flanges
Example: bend radius ; inside radius ; thickness . Example: bend radius ; inside radius ; thickness .
Circumferential stress factorCircumferential stress factorLongitudinal stress factorLongitudinal stress factor-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
0 30 60 90 120 150 180
analytical solutionexperimentnumerical solution 4numerical solution 8ADINAP
-2.5
-2
-1.5
-1
-0.5
0
0.5
1
1.5
2
0 30 60 90 120 150 180
analytical solutionexperimentnumerical solution 4numerical solution 8ADINAP
mmB 3750 mmR 125 mmt 5.12
IPS NASUIPS NASU
Flexibility factor for in-plane bending of 900 bend having rigid flanges
Flexibility factor for in-plane bending of 900 bend having rigid flanges
mmt 5.12mmR 125
0
2
4
6
8
10
12
200 250 300 350 400 450 500
Saint Venant's solutionour resultsexperimentADINAP
K
0B
IPS NASUIPS NASUThe calculation of multi-branched 3D piping
Pump station view
IPS NASUIPS NASUPump station calculation model
Table of element
Calculation results
displacements
angles
forcesmoment
s
geometry
IPS NASUIPS NASU Dynamic analysisDynamic analysis
1. Determination of own frequencies and forms of vibrations of the piping. 2. Calculation forced vibrations of system.3. Restoration of value of external force by the measured displacements of the piping.
Tasks:Tasks:
Problems:Problems:1. Choice of the optimal method of the solution of statically indefinite beam system. 2. Determination of a local flexibility of curved beam by dynamic loading.Solution methods:Solution methods:1. Dynamic stiffness method for a case of harmonious loading. 2. A method of dynamic analysis for a case of non-stationary loading.
Advantages:Advantages:1. Accurate analytical solutions are used. 2. The continuity of the solution at transition from dynamics to a statics is provided.
IPS NASUIPS NASU
Harmonious vibrations. Harmonious vibrations. Dynamic stiffness methodDynamic stiffness method
1. Straight beam.1. Straight beam.
02
4
4
yz
yW
EI
F
dx
Wd z
y
dx
dW
z
zz
EI
K
dx
d
y
z Qdx
dK
- the equations of movement at cross vibrations:- the equations of movement at cross vibrations:
inertial member - frequency of vibrations- frequency of vibrations
x
y
dx
X0X1
01 XKX
stiffness matrix
IPS NASUIPS NASU
- the constraint equation :- the constraint equation :
xkYkEI
QxkY
kEI
KxkY
kxkYWW y
yz
y
yyz
z
yy
z
yyy 433221000
0
xkYWkxkYkEI
QxkY
kEI
KxkY yyyy
yz
yy
yz
zyzz 43221 0
00
0
xkYEIkxkYEIkWxkYk
QxkYKK yzyzyzyyy
y
yyzz 43
221 00
0
0
xkYkKxkYEIkxkYEIkWxkYQQ yyzyzyzyzyyyyy 432
23
1 0000
zy EI
Fk
24
2. Curved beam.2. Curved beam.
1
1
2
2
3
3
4
4 5
1
;,1,e
izb
iz
;sincos,1, ieii
eiy
biy
;sincos ,1 ie
iyiei
bi
;sincos,1 ieii
eiy
biy, UWW
;1eiz,
biz, WW
.sincos1 ieiy,i
ei
bi WUU
The transition matrixThe transition matrix
Harmonious vibrations. Harmonious vibrations. Dynamic stiffness methodDynamic stiffness method
IPS NASUIPS NASU
zy
x
w
EI
M
xzz
yz Q
x
M
2
2
t
wFq
x
Q yy
y
acceleration
iy
iy
iy
iy
iy
iy A
wwwwlt
w
22
21
2
2
2
;24384
124192
1696
1248
124
14
12
41
4
2
31
30
2
221
20
2
31
02
41
0
xkA
lk
EI
xqxlk
EI
xQxlk
EI
xKlxkx
xkww i
yy
iy
izi
ziy
iy
;6384
166144
1248
112
13
12
41
3
2
31
02
31
20
2
2210
2
31
0
xkA
lk
EI
xqxkw
xlk
EI
xQxlk
EI
xKlxk iy
yiy
iy
izi
ziz
;2384
124296
116
12
02
41
2
2
20
02
20
02
31
02
2210 xm
Alkxqlxmxm
wxlk
xQxlk
EI
KK i
yyi
ziy
iy
izi
z
02
41
2
210
20
020
02
31
0 3841
82481 mA
lkxq
xlkEIKlxmxm
wxlk
QQ iyy
izi
ziy
iy
iy
23844882 2
4
2
30
2
20
20
20 l
AEI
lq
EI
lQ
EIlKlw i
yy
iy
iz
iz
iy
EI
xq
EI
xQ
EI
xKxww y
iy
izi
ziy
iy 2462
430
20
00
Non-stationary vibrations. Non-stationary vibrations. Method of dynamic analysisMethod of dynamic analysis
- the equations of movement at cross vibrations:- the equations of movement at cross vibrations:
- the constraint equation :- the constraint equation :
IPS NASUIPS NASUExamples – dynamic stiffness methodExamples – dynamic stiffness method
P
A B
l
W
х
thtglPl
M
820 4
42
2
1
EI
lF
tPtP cos0
-4
-3
-2
-1
0
1
2
3
4
0 50 100 150 200 250 300
M(l /2)
frequency, rad/s
Е = 2∙106 МPа; G = 8∙105 МPа; = 0.3; = 8000 kg/m3; l = 5 m; R = 0.1 m; h = 0.005 m.
1. The diagram of the bending moment in a middle point of articulate beam
srad136
1.25
2. The restoration of value of exciting force by known displacement
P0, H
-4,E+07
-3,E+07
-2,E+07
-1,E+07
0,E+00
1,E+07
2,E+07
3,E+07
4,E+07
5,E+07
6,E+07
0 500 1000 1500
frequency , rad/s
1
10 P10 W
2. The restoration of value of exciting force by known displacement
1. The diagram of the bending moment in a middle point of articulate beam
IPS NASUIPS NASU
1. The frequency of vibrations is lower than first own frequency
-1,4E-06
-1,0E-06
-6,0E-07
-2,0E-07
2,0E-07
6,0E-07
1,0E-06
1,4E-06
0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0 1,1 1,2 1,3 1,4
numerical solution theoretical solution
w , m
t , s
ttP 68sin
Examples – method of dynamic analysisExamples – method of dynamic analysis
IPS NASUIPS NASU
2. The frequency of vibrations is higher than first own frequency ttP 300sin
-7,E-07
-3,E-07
1,E-07
5,E-07
0,0 0,2 0,4 0,6 0,8 1,0 1,2 1,4 1,6 1,8 2,0
numerical solution theoretical solution
w, m
t , s
Examples – method of dynamic analysisExamples – method of dynamic analysis
IPS NASUIPS NASUThe determination of dynamic flexibility
of pipe bendThe determination of dynamic flexibility
of pipe bend- flexibility factor by harmonious vibrations
B
BABBABAK
2
10607241167211672 2
B
BCBABBCBA
B
BCBAK
iiii
4
151060721632212144
4
32212144 2
2
22
22 )1( A
0
2
4
6
8
10
0 50 100 150 200
K
B
2
EhR
B 2
242 )1(12
BhR2
- flexibility factor by non-stationary vibrations
IPS NASUIPS NASUExampleExample
200
600
1000
1400
1800
2200
2600
1,2s 2,2s 3.2s 1,1s
mode of vibrations (m, n)
fre
qu
en
cy ,
Hz
experiment
FEM
K=1
Saint Venant's solution
our results
L. Salley and J. Pan. A study of the modal characteristics of curved pipes // Applied Acoustics. – 2002. – V.63. – pp. 189-202.
Е = 2.07∙106 МPа; = 0.3; = 8000 kg/m3; R = 0.0806 m; h = 0.00711 m;В = 0.457 m; l=0.2 m;
l
l
Rh
B
IPS NASUIPS NASUThe calculation of defects The calculation of defects
cracks
corrosion
defects of form
IPS NASUIPS NASUPressure calculation modelPressure calculation model
altitude of the pipelineoperating pressure
IPS NASUIPS NASUStrength analysis of defectsStrength analysis of defects
dangerous zone
conditionally dangerous zone
safety zone
defect state
IPS NASUIPS NASUApplication of software “InfoPipeMaster” Application of software “InfoPipeMaster”
Chernobyl NPP
Zaporozhye NPP
South-Ukrainian NPP
Ammoniac pipeline «Togliatti-Odessa»
System oil pipelines JSC«Ukrtransnafta»
System gas pipelines DE«Ukrtransgas»