• 검색 결과가 없습니다.

A Study of A Nonlinear Viscoelastic Model for Elastomeric Bushing in Radial Mode

N/A
N/A
Protected

Academic year: 2021

Share "A Study of A Nonlinear Viscoelastic Model for Elastomeric Bushing in Radial Mode"

Copied!
5
0
0

로드 중.... (전체 텍스트 보기)

전체 글

(1)

     



A Study of A Nonlinear Viscoelastic Model for Elastomeric Bushing in Radial Mode

Seong Beom Lee

Key Words : Elastomeric bushing( ), Pipkin-Rogers model( -  ), Nonlinear viscoelastic incompressible material(   )

Abstract

An elastomeric bushing is a device used in automotive suspension systems to reduce the load transmitted from the wheel to the frame of the vehicle. A bushing is an elastomeric hollow cylinder which is bonded to a solid steel shaft at its inner surface and a steel sleeve at its outer surface. The relation between the load applied to the shaft or sleeve and the relative deformation of elastomeric bushing is nonlinear and exhibits features of viscoelasticity. A load-displacement relation for elastomeric bushing is important for dynamic numerical simulations. A boundary value problem for the bushing response leads to the load-displacement relation which requires complex calculations. Therefore, by modifying the constitutive equation for a nonlinear viscoelastic incompressible material developed by Lianis, the data for the elastomeric bushing material was obtained and this data was used to derive the new load-displacement for radial response of the bushing. After the load relaxation function for the bushing is obtained from the step displacement control test, Pipkin-Rogers model was developed. Solutions were allowed for comparison between the results of Modified Lianis model and those of the proposed model. It is shown that the proposed Pipkin-Rogers model is in very good agreement with Modified Lianis model.

1.  

    

    ,    !

" #$% &'  ()* +,* - ./ 01 234, 567 89:; <=

> (sleeve)? @7 89:; A B C1, DE FGC1 89: ;HI JK. L MNO1 ,    PQR S"T UV W" XT? S" -T "Y%

Z[ \- C1 F]; WS" F^A" _Y

`1 W% -.0a WS"b (1,2) % 5cde

MNI Jf0gK.

F]; WS" ZhMN CGO, =Ui1

jk -lmn-oI pR q 8r% s0 a Lianis constitutive equation (3,4,5,6) % P"0gK.

L MNO1, I pR Lianis model % 5c de ^;H 0tu ;vu w)xy Modified Lianis model % z@0gd4,  Modified Lianis model  { +|}$ ~

zG Z8r(one-dimensional radial steep displacement control simulation)% €f0a 2R

‚ƒ E„I …†d4,  E„I 5cde

‡eD F]; WS" Zhy Pipkin-Rogers model (7) % P"0gK.

 ‡eD F]; WS" Zh% P"R

ˆ1 , ‰Š„I p0a R  ‹R

{ +|}$ zG Z8r (one-

†    

E-mail : [email protected]

TEL : (055)320-3667 FAX : (055)324-1723

(2)

dimensional radial displacement control simulation)%

€f0g- , ‘‡e P"Œ x’u ‘‚ Žp

b}% pR x’ ‘uI F’0gd4, [

‘u {01 “” •O –— ˜™š

G , L MN ›œžy +|}$Z, ‹R

  F]; WS" Zh P

"š†K .

Ÿ  ‡e P"Œ Pipkin-Rogers model 

 F]; WS" ZheO, a¡ ¢€ £¤

‰Š„I p0a N\  š\¥, P"Œ

‚Lx 0tu  ¦§w)xde b Z8r ¦§ p¨ € C1 W%

\- CK.

2.   

2.1 Modified Lianis model

Lianis model Žu ;v© w)I ª

«0- I 5cde ¬zI ‘0a ­  

ŒK . ®¯}$Z,? A}$Z, MN‘u

(8,9,10) I -.0a ° , Žu ;v °±`

²}ªx ;HI \  š4, ³ Z, C GO , 0tu ;vu w) XBW% p 0a Modified Lianis model % z@0gd4, I s0a ‚ƒ E„I …†K.

*©% t , +|% r e ´dµ, +|}$ 

;v k ( t r , ) ? ^;H 0t F (t )  w)y Modified Lianis model x (1)u – ªŒK.

[ ] [ ][ ]

[ ][ ]

[ ]

[ ] [ ]

[ ]

[ ]

[ ]

+ + + +

+ +

 

 

− ∂ +

+ −

 

 

− ∂ +

+

 

 

− ∂

− +

 

 

− ∂ +

 +

 

 + + +

 

 

− ∂ +

 

 

− ∂ +

+ +

+ +

 

 

 + + +

+ +

=

+ +

+

t t t t

t t

s s ds r s k t t Q r k

t r k

s s ds r s k r k s t t Q r k

t r k

s s ds r s k t P t r k

s s ds r s k r k s t P t r k

t r k t r k r t k r k

t t Q P r k

s s ds r s k t Q t r k

s s ds r s k t P

t Q t r k t P r k

t r k t r k t r dk c

t r k t r dk c t r t k

r k a b t F

0 1

2 2 2

0 1

2 2

0 1

2

0 1

2 2 2 1 1

0 0

2

0 0

2 0 0

2 2

2 2 2

2

) , ) ( ) (

, ( 1

) , ( 2

) , ) ( , ( ) ) (

, ( 1

) , ( 2

) , ) ( ( ) , ( 2

) , ) ( , ( ) ( ) , ( 2

) , ( ) , ( ) 0 , ( ) 2 , ( 1

) ) ( ( ) 0, (

) , ) ( ( ) , ( 2

) , ) ( ( 2

) ( ) , ( ) ( ) 0 , ( 2

) , ( ) , ( 2 ) , (

) , ( ) , ( ) , ( ) 3 , ( ) 1

(

(1) a‚O P 0 ( t ), Q 0 ( t ), P 1 ( t ), Q 1 ( t ), a , b , c , d 1 _Y

 !"de, Fig. 1  ­l­ CK.

Fig. 1 Material properties for styrene-butadiene rubber

¶R , +|}$  u ( t r , ) ? ;v k ( t r , )

 w)1 K—u –K.

r t r t u r

k ∂

= ∂ ( , ) )

,

( (2)

2.2 Z8r% sR F]; WS" Zh·

L MNO  DE FGC1 89 :e ªšG w" o*0gd4, +|}$

;¥% -.0a {s¸ž) ( r θ , , z ) I Bp0 gK . ¶R,  t < 0 O1 ; ¹d4,

0

t O1 +|}$ ^;H 0t F (t ) I º— »`  567 <=> ‹0a +|}$ 1 u ( t r , ) 4 , ¡R  +

|}$ Z,1 Fig. 2  ­l•†K.

Fig. 2 Bushing in radial mode

 ¼ L •+| R ? +| i

R  F0a, End effect I o* ¥½ ¼K- o

ªRK . |)¾¿de •+| r = R i O

+|}$ I u ( R i , t ) = 0 de ´-, +

| r = R o O +|}$  u ( R , t )

o ? 

O ^ {de ÀG\1 0t F (t ) ? w

)I N0a I ƒ‚ E„e pRK. 

(3)

∑ =

5

1 ( ) 3 3

) 1 ( )

( , ) ( ) ( ) ( )

( {

α

α α

α

a a

a u G t u G t

t u H

5 2 5 )

( ) ( )}

( u α G t a

+| •+| ‹R F1 3 de -ª0 gd4 , 1  ;¢ 5Á »` |

Â0K . ^ {de ÀG\1 0t F (t ) ? +|}$  u ( t r , ) 1 o{Ã0a Bp0 gd4 , *© Ä1 ƒ(sec.)I Bp0gK. ¶ R *© t < 0 O1 ÀGJ 0tÅ ¹d4, 

Å ÆÇ0\ È1 Éde ª0gK.

Modified Lianis model % p0a *© t .

sec 60

0 ≤ t ≤  , u ( R , t ) = 0 . ,1 0 . 2 , 0 . ,3 0 . 4 , 0 . ,5

o

0 . 1 , 9 . 0 , 8 . 0 , 7 . 0 , 6 .

0  ‹R ~zG8r

? 0t‘u1 Fig. 3 u Fig. 4  ­l­ C K .

Fig. 3 Displacement input

Fig. 4 Load output

Fig. 4 O 0tPâ(load relaxation phenomena)% ° € Cd4, 0t F (t ) 1

0 . 1 , 9 . 0 ,8 . 0 , 7 . 0 , 6 . 0 ,5 . 0 , 4 . 0 ,3 . 0 , 2 . 0 ,1 . 0 ) , ( R t =

u o 

³³ ‹R 0tPÃʀ(load relaxation function) )

, ( t u

H š4, 1 +|O +|}$

y u ( R , t )

o  ˀ ÌÍzΤ Ïde

ž¨ € CdÐe, H ( t u , ) 1 K—u – ž

š†K .

) ( ) ( ) ( ) ,

( u t uG 1 t u 3 G 3 t u 5 G 5 t

H = + + (3) .

sec 60

0 ≤ t a ≤  ‹0a,

% ›3Ã01 ]; ›3% p0g-, ÑMÒR E„y G 1 ( t a ), G 3 ( t a ), G 5 ( t a ) I N0a Fig. 5  ­l•†K.

Fig. 5 Coefficients of H ( t u , )

¶R , *© t a ( a = ,1 2 , ,3 L , 601 )  ‹R )

( ), ( ),

( 3 5

1 t a G t a G t a

G 1 x (4)? – \€Ê€

Ïde Œ ʀe ž¨ € CK.

5 , 3 ,1 )

( 1 2

2

3

3

=

+ +

=

i

e C e C C t

G

i

t

i

t i i i

i τ τ

(4)

)€ C ij ? τ ij I N0‚ 0a F]; ›3

 (Nonlinear least square method)% p0g d4 , P"Œ MÒʀ G 1 ( t ), G 3 ( t ), G 5 ( t )  Ó

Ô1 Fig. 6  ­l•†K.

Fig. 6 Coefficients of H ( t u , )

Ó=- G i (t ) ? G i ( t a ) I F’0‚ 0a, )

(t

G i  G i ( t a )  ‹R ¢‹“I 2-norm ÕÖ

% Ř0a K—u – ª 0gK.

 

 

⋅⋅

=

=

= −

. 601 , , 3 , 2 ,1

5 , 3 ,1

) (

) ( ) ) ( (

2 2

a i

t G

t G t t G G of Error

a i

a i i i

(5)

)

1 ( t

G  G 1 a ( t )  ‹R ¢‹“1 0.13%, )

3 ( t

G  G 3 a ( t )  ‹R ¢‹“1 1.36%, G 5 ( t )

 G 5 a ( t )  ‹R ¢‹“1 1.36%4, F];

(4)

WS" Zh% +|}$Z, ‹0a P"R Pipkin-Rogers model K—u –K.

ds ds s R du s R u

s t s R u H

t R u H t F

t o

o o

o ( , )

) , ( , ), ) (

( ) ), 0 , ( ( ) (

∫ 0 ∂

− + ∂

=

(6)

{ } { } 5

52 51

33 3 32

31

13 12

11

) , ( ) (

) , ( ) (

) , ( ) (

) ), , ( (

52

33 32

13 12

t R u e C C

t R u e C e

C C

t R u e C e C C

t t R u H

t o

t o t

t o t

o

τ τ τ

τ τ

− −

+ +

+ +

+

+ +

=

. 5 ,

0042 . 0 ,

0093 . 0

, 03 . 0 ,

2 . 6

, 0032 . 0 ,

0169 . 0 ,

0410 . 0

, 43 . 2 ,

22

, 0706 . 0 ,

0536 . 0 ,

3770 . 0

52 52

51

33 32

33 32

31

13 12

13 12

11

=

=

=

=

=

=

=

=

=

=

=

=

=

τ τ τ

τ τ

C C

C C

C

C C

C

3. Modified Lianis model  Pipkin-Rogers model    

Modified Lianis model  Pipkin-Rogers model 

 ,     F (t )

  ,   . , )

, ( R t

u o    ! "#

$ %&', Modified Lianis model  Pipkin- Rogers model   u ( R , t )

o $ 

( .

. sec 60 10 ,

0

. sec 10 5 ), 10 ( 2 . 0

. sec 5 0 ,

2 . 0 ) , (

=

=

=

t t t

t t

t R u o

(7)

Fig. 7 ) * (7) , Modified Lianis model +  ,-  F (t )  ,./0 1.

Fig. 7 Load output (ML model)

2 , * (7) 3   

 Pipkin-Rogers model 4 56 $ Fig. 8

 70 1.

Fig. 8 Load output (PR model)

8 9:+ ; F (t )  < ,

=>? E @ A0, B(2-norm)4 56,

2

2



ML 



 ML 



PR  −  C+.

Fig. 7  Fig. 8 ', =>?; E $ 3.27%, Modified Lianis model 4 56 D  

 EFG HI9:(Pipkin-Rogers model)5 JK  70 1$ L4 M N 1.

Rise time 4 % O', Modified Lianis model  Pipkin-Rogers model   HI+

PHQ%'+ u ( R o , t ) $  (.

. sec 60 20 ,

0

. sec 20 10 ), 20 ( 1 . 0

. sec 10 0 ,

1 . 0 ) , (

=

=

=

t t t

t t

t R u o

(8)

Fig. 9 $ * (8)4 56 Modified Lianis model +  ,-  F (t )  ,./0 1

 .

Fig. 9 Load output (ML model)

2 , * (8) 3   

 Pipkin-Rogers model 4 56 $ Fig. 10

 70 1.

(5)

Fig. 10 Load output (PR model)

8 9:+ ; F (t )  < ,

=>? E  R ST+ OU (5 B(2-norm) + C+ 56 VWX, =>? E $ 1.1%, Modified Lianis model 4 56 YZ;

[6\] ^_   EFG HI 9: (Pipkin-Rogers model)5 `& JK 

70 1$ L4 a N 1.

2 , 8 b ' c rise time   9 + de 1' f  

rise time 5 g4Nh =>? i L4 7

$D , 5$ + jk l  =

 >? m3 no $ L4 pqZ. r, 9+de 1',  + !s  l tNh    >? m$

L4 au0 1.

4.  

Q% ^v+   wxy+ 

  zV a{7$D 1', '  c 8b+ 9:5 |}~. Modified Lianis model 4 56 <€+ [6\]^_4 56

*)  z*‚5 ƒN „… ;

 \] 9+de †K 56~<$  u‡5 1. QX, ˆ |!‰  E FG 9:; Pipkin-Rogers model ) Š =N ‹

‚+ VWC5 Œq 75<$ ,,  C 5 Ž 56 Ql~, 56<

u‡5 ‘4 ’ {“@, ”G‰ <• *) 

 + †KzV* \] 9+de

 †K 56– N 1$ —E4 b0 1.

• „+ ˜) Q%^v 9™  

 EFG 9:4 ”G$ L5š, Modified Lianis model  Pipkin-Rogers model + $ 5%

›œ+ >? /' ž0 14 a N 1 . 5$ Pipkin-Rogers model 5 Modified Lianis model 4 žŸ N 1$ L4   0 1¡ , HI  ˆ¢  EFG9

:' Pipkin-Rogers model 4 £6Ÿ N 1$ J

¤ |! .

¥ , Pipkin-Rogers model ) <€+ ¦^

v9™U §¨^v9™'U (5 Q%^v9

™'© HI+  EFG 9:' 6 5 ª L4 a N 1.

 

• „$ «]¬­ ˜<®„(2000-1- 30400-024-1)b¯ N°~.



(1) Boltzmann, L., 1876, "Zur Theorie der Elastischen Nachwirkung," Pogg. Ann. Physik, Vol. 7, 624 (2) Gross, B., 1953, Mathematical Structures of the

Theories of Viscoelasticity, Paris:Hermann and Co.

(3) Goldberg, W., Bernstein, B. and Lianis, G., 1967,

"The Exponential Extension Ratio History, Comparison of Theory with Experiment," Purdue University Report AA&ES 67-1.

(4) McGuirt, C. W. and Lianis, G., 1967, "The Constant Stretch Rate history, Comparison of Theory with Experiment," Purdue University Report AA&ES 67-2.

(5) Goldberg, W. and Lianis, G., 1967, "Behavior of Viscoelastic Media Under Small Sinusoidal Oscillations Superposed on Finite Strain," Purdue University Report AA&ES 67-3.

(6) McGuirt, C. W. and Lianis, G., 1970, "Constitutive Equations for Viscoelastic Solids under Finite Uniaxial and Biaxial Deformations," Transactions of the Society of Rheology, Vol. 14:2, pp. 117~134.

(7) Pipkin, A. C. and Rogers, T. G., 1968, "A Non- Linear Integral Representation for Viscoelastic behavior," J. of the Mechanics and Physics of Solids, Vol. 16, pp. 59~72.

(8) Lee, S., 1997, A Study of A Non-linear Viscoelastic Model of Elastomeric Bushing Response, Ph. D. Thesis, The University of Michigan, Ann Arbor.

(9) Lee, S. and Wineman, A. S., 1999, "A model for non-linear viscoelastic torsional response of an elastomeric bushing," Acta Mechanica, Vol. 135, No.

3-4, pp. 199~218.

(10) Lee, S. and Wineman, A. S., 1999, "A model for

non-linear viscoelastic axial response of an

elastomeric bushing," International Journal of Non-

Linear Mechanics, Vol. 34, No. 5, pp. 779~793.

수치

Fig. 1  Material properties for styrene-butadiene  rubber  ¶R ,  +|}$    u ( tr, ) ?   ;v  k ( tr, )    w)1  K—u  –K
Fig.  4 O  0tPâ(load  relaxation  phenomena)%  °  €  Cd4,  0t  F (t ) 1 0.1,9.0,8.0,7.0,6.0,5.0,4.0,3.0,2.0,1.0),(Rt=u o 
Fig. 8  Load output (PR model)
Fig. 10 Load output (PR model)

참조

관련 문서

the material balance for a reaction component must be made for a differential element of volume dV.. For constant-volume reaction.. The integral can be evaluated in any

with the experimental C versus t data. If the fit is unsatisfactory, another rate equation is guessed and tested. Integral method is especially useful for fitting simple

• For the continuous random variable Y the probability density function f ( y ) can be represented by an equation , which can be described graphically by a curve. •

Walker, D. A naturalistic model for curriculum development. Guidelines for better staff development.. A Study on the Development of Early Childhood Parental

In order to simulate a thermo-mechanical behavior in the vicinity of the deposited region by a LENS process, a finite element (FE) model with a moving heat flux is developed

Step 1 Setting up a mathematical model (a differential equation) of the physical process.. By the physical law : The initial condition : Step

In this study, the usage of most common cement for the ground material was highly reduced, and developed a solidifying agent for organic and inorganic

For irrotational flow of ideal incompressible fluid, the Bernoulli’s equation applies over the whole flow field with a single energy line. Exact velocity field