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                                                                                                                                               2009-01-0770

          Load Path Analysis of Vehicle Body Structures under Eigenmode Deformation
                                                                 of Bending Vibration

                                                            Yasuhisa Okano, Takuya Matsunaga and Shinichi Maruyama
                                                                                                                                         Nissan Motor Co., Ltd.

                                                                                                Masashi Hanazato and Kunihiro Takahashi
                                                                                                                                                Keio University

    Copyright © 2009 SAE International




    ABSTRACT                                                                                  index is introduced that is also applicable to distributed
                                                                                              loads through the use of complementary energy. This
    The load path U* analysis is an effective tool for                                        new index makes it possible to analyze load paths under
    investigating the load paths in body structures. In the                                   distributed load conditions that reproduce the natural
    present study, a new index U** is introduced to                                           modes of the vehicle body. The U** index was applied to
    investigate structures under distributed loading. The new                                 study measures for improving the low-order natural
    parameter U** is a complementary concept of U*.                                           frequencies of the body framework. Examples of
    Although the conventional index U* cannot be applied to                                   improvement measures devised for this purpose are
    cases of distributed loading conditions, the new index                                    presented along with an interpretation of the shape
    U** can be applied to those cases.                                                        optimization results thus obtained in terms of the
                                                                                              concept of load paths.
    This paper describes the application of a load path U**
    analysis to improve efficiently the first eigenvalue of the                               THEORY OF CONVENTIONAL U* INDEX[1,2]
    vertical bending mode in a vehicle body structure model.
    It also explains how target parts for shape optimization                                  U* INDEX FOR EXPRESSING LOAD TRANSFER
    are interpreted on the basis of a load path U** analysis
    when a load is applied to reproduce the first vertical                                    A brief explanation is given here of the theory of the
    bending mode.                                                                             conventional U* index based on previous studies. An
                                                                                              elastic structure is modeled in terms of internal stiffness
    INTRODUCTION                                                                              in Fig. 1(a). Point A in the figure is the loading point,
                                                                                              point B is the support point and point C is any arbitrary
    Any study of vehicle body structures today must                                           point. The relationship between the load and
    consider measures for achieving high stiffness, high                                      displacement at the three points is given by Eq. (1),
    strength and weight savings, among other attributes. A                                    using internal stiffness expressed by subscripted K.
    critical issue in satisfying these various performance                                    Subscripted p is the load and d is a column vector
    requirements simultaneously is to identify accurately the                                 expressing displacement.
    transfer of force through the body structures. As a new
    method for accomplishing that, the U* index has been                                            ­ pA ½          ª K AA    K AB   K AC º ­d A ½
                                                                                                    ° °             «K                      ° °
                                                                                                                                     K BC » ®d B ¾
    proposed for expressing the concept of load paths in
    terms of internal stiffness[1,2]. However, the                                                  ® pB ¾          « BA
                                                                                                                              K BB
                                                                                                                                          »                 (1)
    conventional U* index has the drawback of being                                                 °p °            « K CA           K CC » °d C °
    applicable only to a concentrated load condition and not                                        ¯ C¿            ¬         K CB        ¼¯ ¿
    to a distributed load condition. In this study, a new U**

The Engineering Meetings Board has approved this paper for publication. It has successfully completed SAE’s peer review process under the supervision of the
session organizer. This process requires a minimum of three (3) reviews by industry experts.
All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means, electronic,
mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.
ISSN 0148-7191
Positions and opinions advanced in this paper are those of the author(s) and not necessarily those of SAE. The author is solely responsible for the content of
the paper.
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                                                       Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
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Licensed to Tsinghua University
                                                      Licensed from the SAE Digital Library Copyright 2009 SAE International
                                                                E-mailing, copying and internet posting are prohibited
                                                                Downloaded Sunday, September 27, 2009 8:47:05 AM

The energy U stored in the structure in Fig. 1(a) is given
by Eq. (2).                                                                                                                        A




                                                                                                           U**
         1                   1
    U      pA ˜ d A            K AAd A  K AC d C
˜ d A                     (2)
                                                                                                                                                                         A
         2                   2                                                                                                                          B
This expression takes into account that point B is fixed.                                                                  0                            1                    S2
                                                                                                                                             s/ l
Tensor and vector notation are used for the product                                                                                    (a) Uniformity
notation. Next, the energy U' stored in the structure is




                                                                                                            Curvature of U**
                                                                                                                                                                    S1
found when point C is fixed and the same displacement                                                                          1
dA as in (a) is applied, as shown in Fig. 1(b). Using the
ratio between U and U' thus obtained, U* is defined as                                                                                                  B           B
shown in Eq. (3).                                                                                                                  A                            (c) Consistency of
                                                                                                                                                                     load path
                         1                                        1                                                          0             s/l            1
             §U c ·                 §      2U                  ·
    U* { 1  ¨ ¸                    ¨1 
                                    ¨ (K d ) ˜ d               ¸
                                                               ¸
                                                                                                                                       (b) Continuity
             ©U ¹                   ©    AC C    A             ¹
                                                                              (3)
                                                                                                          Fig. 3 Three indexes of desirable structures
As is indicated in this expression, U* is a value that is
dependent on KAC, which expresses the strength of the                                          The notation s is the distance along the path and l is the
coupling between the loading point and the arbitrary                                           total length of the path. The index of consistency in Fig.
point. With the U* index that expresses the quantified                                         3(c) requires that the two load paths denoted as S1 and
strength of the coupling between these two points, it is                                       S2 be consistent. The former path is for loading at point
possible to identify the condition of load transfer through                                    A with point B fixed and the latter path is for loading at
the structure.                                                                                 point B with point A fixed. In other words, consistency
                                                                                               signifies that the places where U* is high from the
LOAD PATHS                                                                                     direction of the loading point A, i.e., the places stiffly
                                                                                               coupled with the loading point, have the possibility of
A load path U* distribution like that shown in Fig. 2 can                                      improving stiffness if they are also simultaneously
be expressed by calculating U* successively at each                                            coupled stiffly with the support point. The reader is
point in the structure. It is assumed that the applied load                                    referred to reference [1] for a more detailed description
is transferred through the places where there is a strong                                      of these three indexes.
coupling between the loading point and the support point.
Accordingly, the ridgeline that is formed when                                                 INTRODUCTION OF A NEW U** INDEX
generating contours can be defined as the load path S in
a U* distribution[1,2]. On the basis of U*, the transfer of                                    DIFFERENCES WITH THE CONVENTIONAL U* INDEX
force in a structure can be identified globally and also
examined locally along the load path.                                                          The U* index is applicable in the case of a concentrated
                                                                                               load, but it cannot be used to treat a distributed load. In
THREE INDEXES OF STRUCTURAL DESIGN                                                             this study, the U** index described here was introduced
                                                                                               in order to treat cases involving a distributed load.
The three indexes of uniformity, continuity and                                                Although the U** index has already been discussed
consistency, as proposed in reference [1], are applied as                                      elsewhere[3], a detailed explanation of the index is given
the criteria for evaluating a structure in a load path                                         below.
analysis based on U*. According to these indexes, a
structure is deemed desirable when the solid lines in Fig.                                     CONCEPT OF THE U** INDEX[3]
3(a), (b) and (c) are in the direction indicated by the
arrows [1] .                                                                                   The U* index always applies the same displacement to
                                                                                               the loading point A, whereas the U** index always
                                                                                               applies an identical load to point A. In calculating the U*
              pA , d A              pA' , d A        A                                         index, a forced displacement is applied to the loading
        A                     A                                                                point. This gives rise to a contradiction in that a point is
                                                                                               first fixed and then the point is displaced. Because the
                                                         S                                     U** index applies a load to the loading point, it does not
               C                     C                                                         cause a contradiction like what occurs in calculating the
                                                                                               U* index. For that reason, the U** index is also
    B                    B                       B                                             applicable to a distributed load condition.
                                                          0         U*       1
        (a)                   (b)
                                                                                               In addition, U* is defined in terms of the work done by
  Fig. 1 Internal stiffness                     Fig. 2 Load path                               the load because the displacement is the variable. In
                                                                                               contrast, U** is defined in terms of the complementary

                                                     Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
Licensed to Tsinghua University
                                                   Licensed from the SAE Digital Library Copyright 2009 SAE International
                                                             E-mailing, copying and internet posting are prohibited
                                                             Downloaded Sunday, September 27, 2009 8:47:05 AM

                         pA ,d A                     p A , d A'                             distribution     was     calculated  using   customized
                    A                        A                                              MSC.Nastran by DMAP. As the first step, a natural
                                                                                            frequency analysis was conducted using a body-in-white
                                                                                            (BIW) model of a rear-wheel-drive passenger vehicle
                         C                            C                                     with the four shock absorbers supported by a simple
                                                                                            structure as shown in Fig. 5. The modes obtained in this
               B                                                                            frequency analysis at all of the body nodes were then
                                         B
                                                                                            applied to the body as forced displacements, and the
                   (a)                       (b)                                            resultant reaction forces were found. The reaction forces
                   Fig. 4 Internal compliance                                               thus obtained were applied as the inputs to reproduce
                                                                                            the first-order vertical bending mode.
work done by the load because the applied load is the
variable. Since a linearly elastic structure is being                                       U** VALUE CALCULATION AND IDENTIFICATION OF
treated here, work and complementary work have the                                          LOAD PATHS
same values. However, the respective equations differ
as noted below because different variables are adopted.                                     Figure 6 shows the U** distribution of the force
                                                                                            inputs for reproducing the first-order vertical
Figure 4 shows the same elastic structure as that in Fig.                                   bending mode. It is seen in the figure that the U**
1. What is different from Fig. 1 is that a forced load pA is                                value decreases toward the support point from the
applied instead of the forced displacement dA.                                              point of its maximum value at the rear of the body.
                                                                                            The major load paths identified are shown in Fig. 7
The relationship between the displacement and load is                                       and are explained below.
given by Eq. (4), using internal compliance expressed by
subscripted C.                                                                              Load path (1): This path transfers the load from the
                                                                                            rear of the body through the rear side member and
                                                                                            the top of the rear wheel housing to the rear shock
     ­d A ½    ªC AA       C AC º ­ p A ½                                                   absorber.
     ® ¾       «C                 ® ¾
     ¯d C ¿    ¬ CA        C CC » ¯ pC ¿
                                ¼                                          (4)
                                                                                            Load path (2): This path transfers the load from the
Because the displacement at the support point B is zero,                                    rear of the body through the rear side member and
the elements pertaining to point B are omitted here. The                                    the bottom of the rear wheel housing to the rear
complementary energy Ucom stored in the structure in Fig.                                   shock absorber.
4(a) is given by Eq. (5).

                   1               1
       U com         d A ˜ pA        C AA pA
˜ pA
                   2               2                                       (5)

Next, the complimentary energy U'com stored in the
structure is found when the same load pA is applied with
point C fixed, as shown in Fig. 4(b). Using the ratio
between Ucom and U'com thus obtained, U** is defined as                                                    Fig. 5 First-order vertical bending mode
expressed in Eq. (6).

                                           1
                 U'                d C ˜ C CC d C
      U * * { 1  com
                 U com                   2U                                (6)

LOAD PATHS IN U** INDEX

Under a distributed load condition, the ridgeline
from the point of maximum U** to the support point                                                                                              max value
is defined as the load path.

APPLICATION OF U** ANALYSIS TO VEHICLE
BODY STRUCTURES

ANALYSIS CONDITIONS                                                                                                min                  U**           max
In order to identify the load paths of the first-order
vertical bending mode, a U** analysis was conducted
                                                                                                                            Fig. 6 U** distribution
under input conditions reproducing this mode. U**
                                               Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
Licensed to Tsinghua University
                                                  Licensed from the SAE Digital Library Copyright 2009 SAE International
                                                            E-mailing, copying and internet posting are prohibited
                                                            Downloaded Sunday, September 27, 2009 8:47:05 AM

Load path (3): This path transfers the load from the
rear of the body through the rear side member and
the rear spring attachment point to the shock
absorber.

In the graph in Fig. 8, the distance s from the point
of the maximum U** value has been
nondimensionalized by the total load path length l
and is shown along the horizontal axis of the graph,
with the value of U** shown along the vertical axis.
The results indicate that all three load paths are
desirable in terms of uniformity and continuity.

EXAMINATION OF LOAD PATH CONSISTENCY

The consistency of the load paths was then
                                                                                                           min                       U*             max
examined. Figure 9 shows the U* distribution when
forced displacements were applied to the four shock
absorbers, with the rear body supported where the                                                                          Fig. 9 U* distribution
maximum U** value was distributed in relation to the
forces applied to reproduce the first-order vertical
bending mode. The sign of the forced
displacements applied to the four shock absorbers
was reversed from positive to negative with respect
to the displacement at the rear body location of the                                                                                         Path
maximum U** distribution in the first-order vertical
bending mode. The major load paths identified are                                                             Path
shown in Fig. 10 and are explained below.

                                                                                                                                   Path

                                            Path

                                                                                                                      Fig. 10 Major load paths
                                Path
                                                                                           Load path (1): This path transfers the load from the
                                                                                           rear shock absorber through the rear wheel housing
                                                                                           and the rear portion of the rear side member to the
                                                                                           rear of the body.
                 Path
                                                                                           Load path (2): This path transfers the load from the
                                                                                           rear shock absorber through the rear wheel housing
                                                                                           and the front part of the rear side member to the
                                                                                           rear seat cross member.
                      Fig. 7 Major load paths
                                                                                           Load path (3): This path transfers the load from the
    1.0                                                                                    rear shock absorber through the rear wheel housing,
                                             Path                                          the front part of the rear side member and the side
    0.8                                      Path                                          sill to the rear seat cross member.

    0.6
                                             Path
                                                                                           In the graph in Fig. 11, the distance s from the loading
  U**




                                                                                           point has been nondimensionalized by the total load
    0.4                                                                                    path length l and is shown along the horizontal axis, with
                                                                                           the value of U* shown along the vertical axis. The results
    0.2
                                                                                           suggest that load paths (2) and (3) are more desirable
    0.0
                                                                                           than load path (1) with respect to uniformity and
                                                                                           continuity. Load path (1) in Fig. 10 and load path (2) in
          0     0.2       0.4         0.6   0.8          1
                                                                                           Fig. 7 are more desirable in terms of consistency.
                                s/l                                                        However, it is also seen that there are no load paths in
        Fig. 8 Uniformity and continuity of load paths                                     Fig. 7 corresponding to load paths (2) and (3) in Fig. 10.

                                              Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210

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2009-01-0770

  • 1. Licensed to Tsinghua University Licensed from the SAE Digital Library Copyright 2009 SAE International E-mailing, copying and internet posting are prohibited Downloaded Sunday, September 27, 2009 8:47:05 AM 2009-01-0770 Load Path Analysis of Vehicle Body Structures under Eigenmode Deformation of Bending Vibration Yasuhisa Okano, Takuya Matsunaga and Shinichi Maruyama Nissan Motor Co., Ltd. Masashi Hanazato and Kunihiro Takahashi Keio University Copyright © 2009 SAE International ABSTRACT index is introduced that is also applicable to distributed loads through the use of complementary energy. This The load path U* analysis is an effective tool for new index makes it possible to analyze load paths under investigating the load paths in body structures. In the distributed load conditions that reproduce the natural present study, a new index U** is introduced to modes of the vehicle body. The U** index was applied to investigate structures under distributed loading. The new study measures for improving the low-order natural parameter U** is a complementary concept of U*. frequencies of the body framework. Examples of Although the conventional index U* cannot be applied to improvement measures devised for this purpose are cases of distributed loading conditions, the new index presented along with an interpretation of the shape U** can be applied to those cases. optimization results thus obtained in terms of the concept of load paths. This paper describes the application of a load path U** analysis to improve efficiently the first eigenvalue of the THEORY OF CONVENTIONAL U* INDEX[1,2] vertical bending mode in a vehicle body structure model. It also explains how target parts for shape optimization U* INDEX FOR EXPRESSING LOAD TRANSFER are interpreted on the basis of a load path U** analysis when a load is applied to reproduce the first vertical A brief explanation is given here of the theory of the bending mode. conventional U* index based on previous studies. An elastic structure is modeled in terms of internal stiffness INTRODUCTION in Fig. 1(a). Point A in the figure is the loading point, point B is the support point and point C is any arbitrary Any study of vehicle body structures today must point. The relationship between the load and consider measures for achieving high stiffness, high displacement at the three points is given by Eq. (1), strength and weight savings, among other attributes. A using internal stiffness expressed by subscripted K. critical issue in satisfying these various performance Subscripted p is the load and d is a column vector requirements simultaneously is to identify accurately the expressing displacement. transfer of force through the body structures. As a new method for accomplishing that, the U* index has been ­ pA ½ ª K AA K AB K AC º ­d A ½ ° ° «K ° ° K BC » ®d B ¾ proposed for expressing the concept of load paths in terms of internal stiffness[1,2]. However, the ® pB ¾ « BA K BB » (1) conventional U* index has the drawback of being °p ° « K CA K CC » °d C ° applicable only to a concentrated load condition and not ¯ C¿ ¬ K CB ¼¯ ¿ to a distributed load condition. In this study, a new U** The Engineering Meetings Board has approved this paper for publication. It has successfully completed SAE’s peer review process under the supervision of the session organizer. This process requires a minimum of three (3) reviews by industry experts. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. ISSN 0148-7191 Positions and opinions advanced in this paper are those of the author(s) and not necessarily those of SAE. The author is solely responsible for the content of the paper. SAE Customer Service: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerService@sae.org SAE Web Address: http://www.sae.org *9-2009-01-0770* Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210 Printed in USA
  • 2. Licensed to Tsinghua University Licensed from the SAE Digital Library Copyright 2009 SAE International E-mailing, copying and internet posting are prohibited Downloaded Sunday, September 27, 2009 8:47:05 AM The energy U stored in the structure in Fig. 1(a) is given by Eq. (2). A U** 1 1 U pA ˜ d A K AAd A K AC d C
  • 3. ˜ d A (2) A 2 2 B This expression takes into account that point B is fixed. 0 1 S2 s/ l Tensor and vector notation are used for the product (a) Uniformity notation. Next, the energy U' stored in the structure is Curvature of U** S1 found when point C is fixed and the same displacement 1 dA as in (a) is applied, as shown in Fig. 1(b). Using the ratio between U and U' thus obtained, U* is defined as B B shown in Eq. (3). A (c) Consistency of load path 1 1 0 s/l 1 §U c · § 2U · U* { 1 ¨ ¸ ¨1 ¨ (K d ) ˜ d ¸ ¸ (b) Continuity ©U ¹ © AC C A ¹ (3) Fig. 3 Three indexes of desirable structures As is indicated in this expression, U* is a value that is dependent on KAC, which expresses the strength of the The notation s is the distance along the path and l is the coupling between the loading point and the arbitrary total length of the path. The index of consistency in Fig. point. With the U* index that expresses the quantified 3(c) requires that the two load paths denoted as S1 and strength of the coupling between these two points, it is S2 be consistent. The former path is for loading at point possible to identify the condition of load transfer through A with point B fixed and the latter path is for loading at the structure. point B with point A fixed. In other words, consistency signifies that the places where U* is high from the LOAD PATHS direction of the loading point A, i.e., the places stiffly coupled with the loading point, have the possibility of A load path U* distribution like that shown in Fig. 2 can improving stiffness if they are also simultaneously be expressed by calculating U* successively at each coupled stiffly with the support point. The reader is point in the structure. It is assumed that the applied load referred to reference [1] for a more detailed description is transferred through the places where there is a strong of these three indexes. coupling between the loading point and the support point. Accordingly, the ridgeline that is formed when INTRODUCTION OF A NEW U** INDEX generating contours can be defined as the load path S in a U* distribution[1,2]. On the basis of U*, the transfer of DIFFERENCES WITH THE CONVENTIONAL U* INDEX force in a structure can be identified globally and also examined locally along the load path. The U* index is applicable in the case of a concentrated load, but it cannot be used to treat a distributed load. In THREE INDEXES OF STRUCTURAL DESIGN this study, the U** index described here was introduced in order to treat cases involving a distributed load. The three indexes of uniformity, continuity and Although the U** index has already been discussed consistency, as proposed in reference [1], are applied as elsewhere[3], a detailed explanation of the index is given the criteria for evaluating a structure in a load path below. analysis based on U*. According to these indexes, a structure is deemed desirable when the solid lines in Fig. CONCEPT OF THE U** INDEX[3] 3(a), (b) and (c) are in the direction indicated by the arrows [1] . The U* index always applies the same displacement to the loading point A, whereas the U** index always applies an identical load to point A. In calculating the U* pA , d A pA' , d A A index, a forced displacement is applied to the loading A A point. This gives rise to a contradiction in that a point is first fixed and then the point is displaced. Because the S U** index applies a load to the loading point, it does not C C cause a contradiction like what occurs in calculating the U* index. For that reason, the U** index is also B B B applicable to a distributed load condition. 0 U* 1 (a) (b) In addition, U* is defined in terms of the work done by Fig. 1 Internal stiffness Fig. 2 Load path the load because the displacement is the variable. In contrast, U** is defined in terms of the complementary Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
  • 4. Licensed to Tsinghua University Licensed from the SAE Digital Library Copyright 2009 SAE International E-mailing, copying and internet posting are prohibited Downloaded Sunday, September 27, 2009 8:47:05 AM pA ,d A p A , d A' distribution was calculated using customized A A MSC.Nastran by DMAP. As the first step, a natural frequency analysis was conducted using a body-in-white (BIW) model of a rear-wheel-drive passenger vehicle C C with the four shock absorbers supported by a simple structure as shown in Fig. 5. The modes obtained in this B frequency analysis at all of the body nodes were then B applied to the body as forced displacements, and the (a) (b) resultant reaction forces were found. The reaction forces Fig. 4 Internal compliance thus obtained were applied as the inputs to reproduce the first-order vertical bending mode. work done by the load because the applied load is the variable. Since a linearly elastic structure is being U** VALUE CALCULATION AND IDENTIFICATION OF treated here, work and complementary work have the LOAD PATHS same values. However, the respective equations differ as noted below because different variables are adopted. Figure 6 shows the U** distribution of the force inputs for reproducing the first-order vertical Figure 4 shows the same elastic structure as that in Fig. bending mode. It is seen in the figure that the U** 1. What is different from Fig. 1 is that a forced load pA is value decreases toward the support point from the applied instead of the forced displacement dA. point of its maximum value at the rear of the body. The major load paths identified are shown in Fig. 7 The relationship between the displacement and load is and are explained below. given by Eq. (4), using internal compliance expressed by subscripted C. Load path (1): This path transfers the load from the rear of the body through the rear side member and the top of the rear wheel housing to the rear shock ­d A ½ ªC AA C AC º ­ p A ½ absorber. ® ¾ «C ® ¾ ¯d C ¿ ¬ CA C CC » ¯ pC ¿ ¼ (4) Load path (2): This path transfers the load from the Because the displacement at the support point B is zero, rear of the body through the rear side member and the elements pertaining to point B are omitted here. The the bottom of the rear wheel housing to the rear complementary energy Ucom stored in the structure in Fig. shock absorber. 4(a) is given by Eq. (5). 1 1 U com d A ˜ pA C AA pA
  • 5. ˜ pA 2 2 (5) Next, the complimentary energy U'com stored in the structure is found when the same load pA is applied with point C fixed, as shown in Fig. 4(b). Using the ratio between Ucom and U'com thus obtained, U** is defined as Fig. 5 First-order vertical bending mode expressed in Eq. (6). 1 U' d C ˜ C CC d C U * * { 1 com U com 2U (6) LOAD PATHS IN U** INDEX Under a distributed load condition, the ridgeline from the point of maximum U** to the support point max value is defined as the load path. APPLICATION OF U** ANALYSIS TO VEHICLE BODY STRUCTURES ANALYSIS CONDITIONS min U** max In order to identify the load paths of the first-order vertical bending mode, a U** analysis was conducted Fig. 6 U** distribution under input conditions reproducing this mode. U** Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
  • 6. Licensed to Tsinghua University Licensed from the SAE Digital Library Copyright 2009 SAE International E-mailing, copying and internet posting are prohibited Downloaded Sunday, September 27, 2009 8:47:05 AM Load path (3): This path transfers the load from the rear of the body through the rear side member and the rear spring attachment point to the shock absorber. In the graph in Fig. 8, the distance s from the point of the maximum U** value has been nondimensionalized by the total load path length l and is shown along the horizontal axis of the graph, with the value of U** shown along the vertical axis. The results indicate that all three load paths are desirable in terms of uniformity and continuity. EXAMINATION OF LOAD PATH CONSISTENCY The consistency of the load paths was then min U* max examined. Figure 9 shows the U* distribution when forced displacements were applied to the four shock absorbers, with the rear body supported where the Fig. 9 U* distribution maximum U** value was distributed in relation to the forces applied to reproduce the first-order vertical bending mode. The sign of the forced displacements applied to the four shock absorbers was reversed from positive to negative with respect to the displacement at the rear body location of the Path maximum U** distribution in the first-order vertical bending mode. The major load paths identified are Path shown in Fig. 10 and are explained below. Path Path Fig. 10 Major load paths Path Load path (1): This path transfers the load from the rear shock absorber through the rear wheel housing and the rear portion of the rear side member to the rear of the body. Path Load path (2): This path transfers the load from the rear shock absorber through the rear wheel housing and the front part of the rear side member to the rear seat cross member. Fig. 7 Major load paths Load path (3): This path transfers the load from the 1.0 rear shock absorber through the rear wheel housing, Path the front part of the rear side member and the side 0.8 Path sill to the rear seat cross member. 0.6 Path In the graph in Fig. 11, the distance s from the loading U** point has been nondimensionalized by the total load 0.4 path length l and is shown along the horizontal axis, with the value of U* shown along the vertical axis. The results 0.2 suggest that load paths (2) and (3) are more desirable 0.0 than load path (1) with respect to uniformity and continuity. Load path (1) in Fig. 10 and load path (2) in 0 0.2 0.4 0.6 0.8 1 Fig. 7 are more desirable in terms of consistency. s/l However, it is also seen that there are no load paths in Fig. 8 Uniformity and continuity of load paths Fig. 7 corresponding to load paths (2) and (3) in Fig. 10. Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
  • 7. Licensed to Tsinghua University Licensed from the SAE Digital Library Copyright 2009 SAE International E-mailing, copying and internet posting are prohibited Downloaded Sunday, September 27, 2009 8:47:05 AM 1.0 COMPARISON WITH ANALYSIS RESULTS FOR IMPROVEMENT OF NATURAL VIBRATION 0.8 FREQUENCY BY SHAPE OPTIMIZATION 0.6 EXPLANATION OF MODEL U* 0.4 Path Path The vehicle body structure was investigated using 0.2 Path the traction method in the OPTISHAPE-TS[5] program for shape optimization, with the aim of 0.0 improving the natural frequencies of the body 0 0.2 0.4 0.6 0.8 1 framework efficiently. The initial model used in the s/l shape optimization exercise is shown in Fig. 13. Fig. 11 Uniformity and continuity of load paths This model was created by applying solid elements 30 mm in thickness to the rear floor panel and the INVESTIGATION OF MEASURES FOR wheel housing of the BIW model of a rear-wheel- IMPROVING NATURAL FREQUENCY OF FIRST- drive passenger vehicle mentioned earlier. The solid ORDER VERTICAL BENDING MODE elements were coupled to these body parts at shared nodes. An investigation was made of the three indexes that a desirable structure should satisfy, as described in ANALYSIS CONDITIONS section before. Because the results in Fig. 8 indicated that the load paths were desirable with respect to In the shape optimization exercise, maximization of uniformity and continuity, only consistency was the natural frequency of the first-order vertical examined here. From the results in Figs. 6 and 9, it was bending mode was set as the objective functional assumed that the consistency of the load paths would be under the constraint that the volume of the solid improved by providing reinforcements connecting the elements, which were the target of the optimal places having large U** and U* values, respectively. For design, should be reduced from the present level. example, providing stiffness elements connecting the rear shock absorbers and the front and rear ends of the SHAPE OPTIMIZATION RESULTS rear side members would presumably be effective for that purpose. These reinforcements are respectively The shape optimization results are shown in Fig. 14. denoted as and in Fig. 12. The resultant Reinforcements and for connecting the rear improvement in the natural frequency of the first-order shock absorbers and the front and rear ends of the vertical bending mode is shown in Table 1. rear side members are newly represented in the results. With regard to the solid elements of the spare tire pan and the rear floor panel, the thickness of these parts was reduced from the original specification. However, it is clear that applying improvement measures to these parts has little effect on improving the natural frequency of the first- order vertical bending mode. Fig. 12 Reinforced model Table 1 Effects of reinforcement Specification of Change in natural frequency of model first-order vertical bending mode Original model 0 Hz Reinforced model +4.2 Hz Fig. 13 Initial model Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210
  • 8. Licensed to Tsinghua University Licensed from the SAE Digital Library Copyright 2009 SAE International E-mailing, copying and internet posting are prohibited Downloaded Sunday, September 27, 2009 8:47:05 AM (3) A comparison of the shape optimization results and the results of the structural changes based on U** confirmed that both sets of results displayed the same tendencies. In addition, it was found that the shape optimization results were explainable in terms of the improved consistency of the load paths. REFERENCES [1] Takahashi, K., Conditions for desirable Fig. 14 Calculated optimal model structures based on a concept of load transfer courses, Proceedings of the First International Table 2 Results of optimization Structural Engineering and Construction Conference, 2001, pp. 699-702. Specification of Change in natural frequency of model first-order vertical bending mode [2] Sakurai, T., et al., Load Path Optimization and Original model 0 Hz U* Structural Analysis for Passenger Car Compartments under Frontal Collision, Calculated optimal +3.5 Hz Preprints of International Body Engineering model Conference, 2003, pp. 181-186. [3] Wang, Enyang., Zhang, Xiaoguang., Takahashi, Table 2 shows the change in the natural frequency of K., Load Path U* Analysis of Square Pipe the first-order vertical bending mode between the initial under Collision, Society of Automotive model before shape optimization and the shape Engineers of Japan Spring Conference, 2007, optimized model. Compared with the initial model, the No. 17-07. natural frequency of the first-order vertical bending mode of the shape optimized model increased by 3.5 Hz. [4] Sakurai, T., Takahashi, K., Kawakami, H., Abe, M., Reduction of Calculation Time for Load INTERPRETATION OF SHAPE OPTIMIZATION Path U* Analysis of Structures, Journal of Solid RESULTS Mechanics and Materials Engineering, 2007, Vol. 1, No. 11, pp. 1322-1330. Good agreement was seen between the reinforcements provided to improve the consistency of the load paths [5] http://www.quint.co.jp/eng/pro/ots/index.htm (Fig. 12) and the shape optimization results presented in Fig. 14. This agreement can be interpreted as indicating that the shape optimization results in Fig. 14 show the CONTACT improved consistency of the load paths. It is clear from the results in Fig. 7 that the spare tire pan and rear floor Yasuhisa Okano panel did not serve as load paths. That can be E-mail: yasu-okano@mail.nissan.co.jp understood as the reason why the solid elements Phone:+81-50-2029-1327 provided at these locations became thinner in the shape Address:1-1, Morinosatoaoyama, Atsugi-shi, Kanagawa, optimization results in Fig. 14. 243-0123, Japan CONCLUSIONS In this study, a body-in-white (BIW) model was subjected to a load path analysis and shape optimization, with the aim of improving the low-order natural frequencies of the body framework. The following results were obtained. (1) A new U** index was introduced to treat the low- frequency dynamic problems of the BIW. (2) The structural changes made on the basis of the results calculated for U** concerning the vertical bending mode of the BIW showed that dynamic stiffness can be improved efficiently. Author:Gilligan-SID:13330-GUID:23758887-59.66.116.210