Page 39 - Marks Calculation for Machine Design
P. 39

P1: Shibu
                          January 4, 2005
                                      12:26
        Brown.cls
                 Brown˙C01
                              U.S. Customary  FUNDAMENTAL LOADINGS  SI/Metric      21
                    Step 3. Using this value for the polar moment  Step 3. Using this value for the polar moment
                    ofinertia(J),andthemaximumallowableshear  ofinertia(J),andthemaximumallowableshear
                    stress (τ max ), substitute in the equation devel-  stress (τ max ), substitute into the equation deter-
                    oped in Step 1.                    mined in Step 1.
                             τ max J                         τ max J
                        T max =                        T max =
                               R                               R
                                                                                  4
                                             4
                                                                       2
                                                                   8
                                      2
                             (60,000 lb/in )(127.2in )       (4.1 × 10 N/m )(4.97 × 10 −5  m )
                           =                               =
                                    (3in)                            (0.075 m)
                             7,632,000 lb · in 2             20,377 N · m 2
                           =                               =
                                  3in                          0.075 m
                           = 2,544,000 in · lb             = 271,693 N · m
                           = 212 ft · kip                  = 272 kN · m
                    Step 4. For a maximum angle of twist (φ max ),  Step 4. For a maximum angle of twist (φ max ),
                    solve for the maximum torque (T max ) in Eq.  solve for the maximum torque (T max ) in Eq.
                    (1.29) to give                     (1.29) to give
                              φ max GJ  φ max                    φ max GJ  φ max
                         T max =    =     × GJ             T max =     =    × GJ
                                L      L                           L      L
                    where the quantity (GJ) is called the torsional  where the quantity (GJ) is called the torsional
                    stiffness.                         stiffness.
                    Step 5. Using the polar moment of inertia (J)  Step 5. Using the polar moment of inertia (J)
                    calculated earlier and the shear modulus of elas-  calculated earlier and the shear modulus of elas-
                    ticity (G), calculate the torsional stiffness.  ticity (G), calculate the torsional stiffness.
                                  6
                                             4
                                                                   9
                                                                       2
                                      2
                                                                                  4
                       GJ = (4.1 × 10 lb/in )(127.2in )  GJ = (26.7 × 10 N/m )(4.97 × 10 −5  m )
                                 8
                                                                  6
                          = 5.2 × 10 lb · in 2            = 1.3 × 10 N · m 2
                    Step 6. Substitute the given maximum allow-  Step 6. Substitute the given maximum allow-
                    able angle of twist (φ max ), the torsional stiffness  able angle of twist (φ max ), the torsional stiffness
                    (GJ) just calculated, and the length (L) in the  (GJ) just calculated, and the length (L) into the
                    equation of Step 4 to give         equation of Step 4 to give
                          φ max                              φ max
                    T max =   × GJ                     T max =  × GJ
                           L                                  L
                          (0.026 rad)   8   2                (0.026 rad)  6    2
                        =        (5.2 × 10 lb · in )       =        (1.3 × 10 N · m )
                           (36 in)                            (1m)
                                   1                                 1
                                                                              6
                                                2
                                                                                   2
                                           8
                        =  7.2 × 10 −4  (5.2 × 10 lb · in )  =  2.6 × 10 −2  (1.3 × 10 N · m )
                                  in                                 m
                        = 374,400 in · lb                  = 33,800 N · m
                        = 31 ft · kip                      = 34 kN · m
                    Step 7. As the maximum torque (T max ) associ-  Step 7. As the maximum torque (T max ) associ-
                    ated with the maximum angle of twist (φ max ) is  ated with the maximum angle of twist (φ max ) is
                    smaller than that for the maximum shear stress  smaller than that for the maximum shear stress
                    (τ max ), angle of twist governs, so  (τ max ), angle of twist governs, so
                             T max = 31 ft · kip                T max = 34 kN · m
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