Page 543 - Automotive Engineering Powertrain Chassis System and Vehicle Body
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CHAP TER 1 6. 2       Standard sedan (saloon) – baseline load paths


                                                                    Careful inspection of this equation and of Fig. 16.2-14
                Table 16.2-1 (a)
                                                                  reveals that the coefficients of the Qs must be their
                Edge force   Moment about G Moment arm about G    moment arms r 2 , r 3 , etc., about point G as given in
                                                                  equation (16.2.27). Moment arms r 2 to r 7 are listed in
                Lower A-pillar   Q 2 X      r 2 ¼ X
                                                                  Tables 16.2-1(a) and (b).
                Header (roof rail)  Q 4 ðH  ZÞ  r 4 ¼ H  Z

                Lower C-pillar   Q 6 ðL 5  XÞ  r 6 ¼ L 5  X
                                                                  16.2.3.5 Summary – baseline closed
                Rocker       Q 7 Z          r 7 ¼ Z
                                                                  sedan
                Parcel shelf  Moment about G
                reactions                                         Front and rear inner fenders:
                Front         Q x1 ðh 1  ZÞ  h 1  Z
                                                                    R FT ¼ T=S F     R RT ¼ T=S R ¼ R FT S F =S R
                Rear          Q x2 ðh 2  ZÞ  h 2  Z                 P FT ¼ TL 1 =S F h 1  P RT ¼ TL 2 =S R h 2
                                                                  Parcel shelves:

                                                                    Q X1 ¼ P FT S F =B ¼ TL 1 =h 1 B      (16.2.19)
                                                                    Q X2 ¼ P RT S R =B ¼ TL 2 =h 2 B      (16.2.20)
                 For sideframe equilibrium, all moments acting about
               G will sum to zero (SM ¼ 0):                       Passenger compartment (with some re-arrangements):



















                   Q 2 X þ Q 3 fðh 1   ZÞ sinðq Þþ X cosðq Þg       The input moment is Tand P FT ,P RT ,Q x1 and Q x2 are
                                          A
                                                     A
                                                                  known in terms of T. The remaining seven unknown
                   þ Q ðH   ZÞþQ 5 fðh 2   ZÞ sinðq Þ
                      4
                                              C
                                                                  edge forces (Q 1 to Q 7 ) can be solved using the seven
                   þðL 5   XÞ cosðq Þg   Q 6 ðL 5   XÞþ Q 7 Z     simultaneous equations (16.2.21)–(16.2.27) if T is
                                 C
                     Q X1 ðh 1   ZÞ  Q X2 ðh 2   ZÞ               known. This could be done by hand (the equations are
                                                                  linear and relatively ‘sparse’). Alternatively, if the
                   ¼ 0
                                                                  equations are rearranged slightly and put in matrix
                                                                  form, they become:


















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