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178  Tribology in machine design


                                 equation. Equation (5.7) transformed into the cylindrical coordinates is








                                 where the velocities of the two surfaces are R  l and R 2 in the radial direction,
                                 T! and T 2 in the tangential direction, and V l and V 2 in the axial direction
                                 across the film. For most bearings many of the terms may be dropped, and
                                 particularly those which imply a stretching of the surfaces.

     5.2. Hydrostatic            Figure 5.4 shows the principle of a hydrostatic bearing action. Lubricant
     bearings                    from a constant displacement pump is forced into a central recess and then
                                 flows outwards between the bearing surfaces, developing pressure and
                                 separation and returning to a sump for recirculation. The surfaces may be
                                 cylindrical, spherical or flat with circular or rectangular boundaries. If the
                                 surfaces are flat they are usually guided so that the film thickness h is
                                 uniform, giving zero values to dh/dx and dh/dr, dh/d& in the Reynolds'
                                 equations. These appear in, and cancel out, the terms containing the surface
                                 velocities, an indication that the latter do not contribute to the development
                                 of pressure. Hence, with u considered constant, Reynolds' equation, eqn
                                 (5.7), is reduced to




                                 If the pad is circular as shown in Fig. 5.4 and the flow is radial, then
                                dp/d&=0 from symmetry, and eqn (5.8) is reduced to




                                Equation (5.10) is readily integrated, and together with the boundary
                                conditions of Fig. 5.4, namely p = 0 at r — D/2 and p = p 0 at r = d/2, the result
                                ic



                                The variation of pressure over the entire circle is illustrated in Fig. 5.4, case
                                (b), from which an integral expression for the total load P may be written
                                and the following expression obtained for p 0




                                An equation for the radial flow velocity u r may be obtained by substituting r
                                for x and 17 1 = U 2 =0 in eqn (4.2a)


     Figure 5.4
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