Page 188 - Marks Calculation for Machine Design
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                          January 4, 2005
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                  a solid circular cross section. If other cross sections are of interest, then these expressions
                  should be modified accordingly.  STRENGTH OF MACHINES
                    Also notice that the second term in the third line of Eq. (4.13) is four-thirds the direct
                  shear stress, which is the shear force (V ) divided by the cross-sectional area (A).
                            U.S. Customary                       SI/Metric
                  Example 5. Determine the maximum stresses  Example 5. Determine the maximum stresses
                  on the top element of a solid circular crank arm,  on the top element of a solid circular crank arm,
                  like the one shown in Fig. 4.16, subjected to a  like the one shown in Fig. 4.16, subjected to a
                  downward applied force (P), where  downward applied force (P), where
                      P = 500 lb                        P = 2,250 N
                    L AB = 2ft = 24 in                 L AB = 0.8 m
                    L BC = 1ft = 12 in                 L BC = 0.4 m
                      R = 1.0 in                        R = 2.5 cm = 0.025 m
                  solution                           solution
                  Step 1. Using Eq. (4.6), calculate the bending  Step 1. Using Eq. (4.6), calculate the bending
                  moment (M A ).                     moment (M A ).
                     M A = P × L AB = (500 lb)(24.0in)  M A = P × L AB = (2,250 N)(0.80 m)
                        = 12,000 in · lb                  = 1,800 N · m
                  Step 2.  Using Eq. (4.5), calculate the torque  Step 2.  Using Eq. (4.5), calculate the torque
                  (T AB ).                           (T AB ).
                     T AB = P × L BC = (500 lb)(12.0in)  T AB = P × L BC = (2,250 N)(0.40 m)
                        = 6,000 in · lb                   = 900 N · m
                  Step 3. Substitute the bending moment (M A )  Step 3. Substitute the bending moment (M A )
                  and the radius (R) in Eq. (4.10) to give the  and the radius (R) in Eq. (4.10) to give the
                  normal stress (σ xx ).             normal stress (σ xx ).
                           4M A  4 (12,000 in · lb)            4M A  4 (1,800 N · m)
                      σ xx =  3  =       3                σ xx =  3  =       3
                            πR     π(1.0in)                    πR    π(0.025 m)
                           48,000 in · lb                      7,200 N · m
                         =       3                          =          3
                             3.14 in                           0.0000491 m
                         = 15,279 lb/in 2                   = 146,680,000 N/m 2
                         = 15.3 kpsi                        = 146.7MPa
                  Step 4. Substitute the torque (T AB ) and the  Step 4. Substitute the torque (T AB ) and the
                  radius (R) in Eq. (4.11) to give the shear stress  radius (R) in Eq. (4.11) to give the shear stress
                  (τ xy ).                           (τ xy ).
                           2 T AB  2 (6,000 in · lb)           2 T AB  2 (900 N · m)
                       τ xy =   =                         τ xy =   =
                            πR 3   π(1.0in) 3                  πR  3  π(0.025 m) 3
                           12,000 in · lb                       1,800 N · m
                         =       2                           =         3
                             3.14 in                           0.0000491 m
                         = 3,820 lb/in 2                     = 36,670,000 N/m 2
                         = 3.8 kpsi                          = 36.7MPa
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