Page 360 - Marks Calculation for Machine Design
P. 360

P1: Sanjay
                          January 4, 2005
                 Brown˙C08
        Brown.cls
                  342
                            U.S. Customary 15:14  APPLICATION TO MACHINES  SI/Metric
                        A T E steel                       A T E steel
                    k T =                             k T =
                          L T                               L T
                                                                                 2
                                                                            9
                                         6
                                  2
                                                                     2
                                             2
                        (2.26 × 10 −1  in )(30 × 10 lb/in )  (1.57 × 10 −4  m )(207 × 10 N/m )
                      =                                 =
                                (1.0625 in)                        (0.027 m)
                                                                9
                              6
                      = 6.38 × 10 lb/in                 = 1.20 × 10 N/m
                  Step 5. As the thicknesses (t 1 ) and (t 2 ) are not  Step 5. As the thicknesses (t 1 ) and (t 2 ) are not
                  equal, a third thickness (t middle ) is found from  equal, a third thickness (t middle ) is found from
                  Eq. (8.64) as                      Eq. (8.64) as

                             L grip                             L grip
                     t middle =  − h                     t middle =  − h
                              2                                  2
                             1.0625 in                          0.027 m

                         =           − (0.3125 in)           =         − (0.008 m)
                               2                                  2
                         = 0.219 in                          = 0.0055 m
                  Step 6. Using the third thickness (t middle )  Step 6. Using the third thickness (t middle )
                  found in step 5 in Eq. (8.66), calculate the  found in step 5 in Eq. (8.66), calculate the
                  special diameter (D*) as           special diameter (D*) as
                      ∗
                                                         ∗
                     D = 1.5 d + 2 h tan 30 ◦           D = 1.5 d + 2 h tan 30 ◦
                       = (1.5)(0.625 in)                  = (1.5)(0.016 m)
                         + (2)(0.3125 in)(0.577)            + (2)(0.008 m)(0.577)
                       = (0.9375 in) + (0.625 in) (0.577)  = (0.024 m) + (0.016 m) (0.577)
                       = 1.30 in                          = 0.033 m
                  Step 7. Substitute the special diameter (D*)  Step 7. Substitute the special diameter (D*)
                  found in step 6, the third thickness (t middle )  found in step 6, the third thickness (t middle )
                  found in step 5, and the given cone angle (α)  found in step 5, and the given cone angle (α)
                  and modulus of elasticity (E steel ), in Eq. (8.20)  and modulus of elasticity (E steel ), in Eq. (8.20)
                  to find the stiffness (k middle ) as  to find the stiffness (k middle ) as
                                (π tan α) Ed                       (π tan α) Ed
                   k middle =                        k middle =
                             (2 t tan α + D − d)(D + d)        (2 t tan α + D − d)(D + d)
                          ln                                ln
                             (2 t tan α + D + d)(D − d)        (2 t tan α + D + d)(D − d)
                               ◦                                  ◦
                          (π tan 30 ) E steel d bolt        (π tan 30 ) E steel d bolt
                        =                                 =
                                 C 1                               C 1
                              ln                                 ln
                                 C 2                               C 2
                  where                              where
                     C 1 = (2 t tan α + D − d)(D + d)   C 1 = (2 t tan α + D − d)(D + d)
                        = (2 t middle tan 30 + D − d bolt )  = (2 t middle tan 30 + D − d bolt )
                                       ∗
                                                                          ∗
                                                                      ◦
                                   ◦
                                                               ∗
                             ∗
                          ×(D + d bolt )                    ×(D + d bolt )

                           (2)(0.219 in)(0.577)               (2)(0.0055 m)(0.577)
                        =                                 =
                           +(1.30 in) − (0.625 in)            +(0.033 m) − (0.016 m)
                          × ((1.30 in) + (0.625 in))        × ((0.033 m) + (0.016 m))
                        = (0.928 in)(1.925 in)            = (0.023 m)(0.049 m)
                        = 1.79 in 2                       = 0.00113 m 2
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