Page 260 - Tribology in Machine Design
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Friction, lubrication and wear in higher kinematic pairs  245


                                 where JJ.Q is the lubricant viscosity at the atmospheric pressure and the inlet
                                 surface temperature, V = (Vi + K 2)/2 is the average surface velocity, [m/s],
                                 5 is the lubricant viscosity-temperature coefficient, [ = (l/^)/A/VAT);
                                 °C~ *] and p is the lubricant thermal conductivity.
                                   The viscosity-temperature coefficient, 5, can be adequately estimated
                                 from a temperature viscosity chart of the lubricant. It is necessary to select
                                 two temperatures about 20° apart near the assumed inlet temperature and
                                 divide the viscosity difference by the average viscosity and temperature
                                 difference corresponding to the viscosity difference.
                                   Thermal conductivity, p, is relatively constant for classes of lubricants
                                 based on chemical composition. For mineral oils, suitable values for these
                                 calculations are 0.12-0.15 W/mK. The lower range applies for lower
                                 viscosity either resulting from lower molecular weight or higher tempera-
                                 ture. To illustrate the procedure outlined above the numerical example
                                 solved earlier is used. Thus, assuming that the lubricant is SAE10 mineral
                                                                                           1
                                 oil, inlet temperature is 55 °C, corresponding 5 value is 0.045 °C~  and
                                 lubricant thermal conductivity is 0.12W/mK, eqn (6.29) gives




                                 Then, using eqn (6.28)


                                 Finally, the thermally corrected film thickness is



                                 This means a 20 per cent reduction of the film thickness as a result of the
                                 heating at the inlet zone.


     6.9. Analysis of point      In contrast with the heavily loaded line contacts which have been
     contact lubrication         investigated very fully, the understanding of point contact lubrication is less
                                 advanced. Any analysis of the problem naturally relies to a considerable
                                 extent on a knowledge of the local shape of the contact, which usually is not
                                 known in detail. The foundation of the theoretical solution to the problem
                                 was laid down by Grubin. He proposed that:
                                  (i) the pressure distribution under lubricated conditions was almost
                                    Hertzian;
                                 (ii) the shape of the entry gap was determined by the Hertz pressure alone,
                                    i.e. the fluid pressure at the entry to the contact zone had negligible
                                    effect.
                                 The application of the Grubin approximation is quite simple in the case of
                                 line contacts. The point contact case is far more complex due to side leakage
                                 effects. Figure 6.6 shows the geometry of the point contact. The various
                                 formulae for load, peak pressure, contact radius and surface deformation
                                 can be easily found in any standard textbook on elasticity (see Chapter 3 for
                                 more details). The relationships needed here are as follows:
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