Page 56 - Tribology in Machine Design
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Basic principles of tribology  43
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                                 Because Q = T /16K and therefore T= (16QR)\ Substituting the expression
                                 for T into eqn (2.100) and rearranging gives






                                 and finally,










                                 and C 2 is a constant of integration. Equation (2.102) gives the dependence
                                 of Q on L. The dependence of Q on the other parameters of the system is
                                 contained in the quantities C t and C 2 of eqn (2.102).
                                   Equation (2.102) implicitly defines the allowed ranges of certain
                                 parameters. In using this equation these parameters cannot be allowed to
                                 assume values for which the assumptions made in obtaining eqn (2.102) are
                                 invalid.
                                   One way of determining C l and C 2 in eqn (2.102), is to perform a series of
                                 controlled experiments, in which Q is determined for two different numbers
                                 of operations for various values and combinations of the parameters of
                                 interest. These values of Q for different values of L enable Ci and C 2 to be
                                 determined. In certain cases, however, C t and C 2 can be determined on an
                                 analytical basis. One analytical approach is for the case in which there is a
                                 period of at least 2000 passes of what may be called zero wear before the
                                 wear has progressed to beyond the surface finish. This is done by taking C 2
                                 to be zero and determining C t from the model for zero wear. C t is
                                 determined by first finding the maximum number L l of operations for
                                 which there will be zero wear for the load, geometry etc. of interest. L t is
                                 then given by:





                                 where t max is the maximum shear stress computed using the unworn
                                 geometry, t y is the yield point in shear of the weaker material and y R is a
                                 quantity characteristic of the mode of lubrication. The geometry of the wear
                                 scar produced during the number L 1 of passes, is taken to be a scar of the
                                 profile assumed in deriving eqn (2.102) and of a depth equal to one-half of
                                 the peak-to-peak surface roughness of the material of the pin. In the
                                 particular case under consideration it is assumed that

                                        7^=0.20    (fatigue mode of wear),
                                         f—Q.26    (coefficient of friction).
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