Page 102 - Marks Calculation for Machine Design
P. 102

P1: Sanjay
                          January 4, 2005
                 Brown˙C02
        Brown.cls
                  84
                            U.S. Customary 16:18  STRENGTH OF MACHINES  SI/Metric
                  Step 2. From Fig. 2.62, this maximum shear  Step 2. Figure 2.62 shows that this maximum
                  force (V max ) occurs at the roller support.  shear force (V max ) occurs at the roller support.
                  Step 3. Calculate the maximum bending  Step 3. Calculate the maximum bending
                  moment (M max ) from Eq. (2.45) as  moment (M max ) from Eq. (2.45) as
                             w                               w
                                    2
                                                                     2
                      M max =  (L + a) (L − a) 2      M max =   (L + a) (L − a) 2
                            8 L  2                          8 L  2
                            (113 lb/ft)                     (1,540 N/m)
                          =                               =
                             8 (3ft) 2                        8 (1m) 2
                                                                       2
                                    2
                            ×(3ft + 1ft) (3ft − 1ft) 2      ×(1m + 0.3m) (1m − 0.3m) 2
                            (113 lb/ft)  2  2               (1,540 N/m)     2    2
                          =        × (4ft) (2ft)          =          × (1.3m) (0.7m)
                                                                 2
                                2
                             (72 ft )                         (8m )


                             1.57 lb  2    2                 192.5N      2      2
                          =        (16 ft )(4ft )         =     3   (1.69 m )(0.49 m )
                              ft 3                             m
                          = 100 ft · lb                   = 159 N · m
                  Step 4. The maximum bending moment  Step 4. This maximum bending moment
                  (M max ) occurs at the location shown in Fig. 2.63  (M max ) occurs at the location shown in Fig. 2.63
                  and given by Eq. (2.46).           and given by Eq. (2.46).
                         L     a  2                            L     a 2
                  x M max  =  1 −                        x M max  =  1 −
                         2     L 2                             2     L  2
                         3ft     (1ft) 2                       1m     (0.3m) 2
                       =     1 −                             =     1 −
                          2    (3ft) 2                          2      (1m) 2
                                                                            2
                                 1ft 2        8                         0.09 m
                       = (1.5ft) 1 −  = (1.5ft)              = (0.5m) 1 −  2
                                 9ft 2        9                          1m
                                                             = (0.5m)(0.91) = 0.455 m
                       = 1.33 ft
                                                                        w
                                                             B
                            A
                                                                 ∆      C
                                             L                    a
                            FIGURE 2.64  Beam deflection diagram.
                  Deflection. For this loading configuration, the deflection ( ) along the beam is shown in
                  Fig. 2.64, and given by Eq. (2.47a) for values of the distance (x) from the left end of the
                  beam to the roller at point B, and given by Eq. (2.47b) for values of the distance (x) from
                  the roller to the free end.
                              wx    4    2 2    3    2 2    2 2
                           =      (L − 2L x + Lx − 2a L + 2a x ) ↑   0 ≤ x ≤ L (2.47a)
                             24EIL
                             wx 1  2     3    2      2   3
                           =     (4a L − L + 6a x 1 − 4ax + x ) ↑  L ≤ x ≤ L + a  (2.47b)
                                                         1
                                                     1
                             24EI
                  where   = deflection of beam
                       w = uniform distributed load
   97   98   99   100   101   102   103   104   105   106   107