Page 96 - Analysis and Design of Machine Elements
P. 96

Analysis and Design of Machine Elements
                    74
                         According to the force equilibrium and force-deflection relationships, the forces in
                       the bolt and in the clamped members are calculated by
                             {
                               ΔF =Δ  k b
                               F −ΔF =Δ  k
                                           m
                         From these equations, we then have
                                      k b
                             ⎧
                             ⎪ ΔF =       F
                                   k + k
                             ⎪      b   m
                             ⎨
                                         k m
                              F −ΔF =        F
                             ⎪
                                       k + k
                             ⎪
                                        b   m
                             ⎩
                         Therefore, the total load in the bolt is
                                        k b
                             Q = Q +        F                                             (3.18)
                                  p
                                      k + k
                                      b   m
                         The total load in the bolt includes the initial preload due to tightening, and a partial
                       of subsequently applied operating force, which tends to separate the clamped members.
                       And the resultant load in the clamped members is
                                        k m
                              ′
                             Q = Q −         F                                            (3.19)
                              p    p
                                      k + k
                                       b   m

                       where  k b  is the relative stiffness of the joint. Since gaskets are usually inserted at the
                             k b +k m
                       interface between bolted members, the relative stiffness depends on the material of gas-
                       kets. For a metal gasket, it is approximately 0.2–0.3; for leather 0.7; for asbestos, 0.8 and
                       for rubber, 0.9.
                         The total load in the bolt depends greatly on the relative stiffness. If k ≫ k ,wehave
                                                                                      m
                                                                                  b
                       Q ≈ Q + F; while for k ≪ k ,wehave Q ≈ Q . Therefore, when a bolted joint carries a
                                               m
                                                             p
                            p
                                          b
                       relatively large load, high stiffness gaskets should be used.
                         To prevent the separation of joint, the resultant load in the clamped members Q ′ p
                       should be greater than zero, that is,
                              ′
                             Q ≥ 0                                                        (3.20)
                              p
                                                                           ′
                         For ordinary bolted joints subjected to a stable load, select Q = (0.2–0.6) F; for ordi-
                                                                           p
                       nary bolted joints subjected to a variable load, Q ′  = (0.6–1.0) F;for asealing case,
                                                                  p
                                                              ′
                         ′
                       Q = (1.5–1.8) F and for anchor bolt joints, Q ≥ F [8].
                         p                                    p
                         The static strength of a preloaded bolt subjected to a combined preload and static axial
                       loads is then
                                  1.3Q
                                =      ≤ [  ]                                             (3.21)
                              ca  1
                                     d 2 1
                                  4
                       3.5.3.4  Preloaded Tension Bolts Subjected to Combined Preload and Variable Axial
                       Loads
                       When a preloaded tension bolt is subjected to a variable load fluctuating between zero
                       and an upper extreme F, the total load in a bolt varies from Q to Q, as indicated in
                                                                            p
   91   92   93   94   95   96   97   98   99   100   101