INTRODUCTION
TILTING PAD THRUST BEARINGS operating at high sliding speeds (in excess of 60 m/s) may fail owing to high pad surface temperatures. The object of the work described in this paper was primarily to investigate the effectiveness of current methods used for the design of high-speed assemblies, and to evaluate improvements. The paper also studies the effects of speed, load, oil quantity, oil pressure, misalignment, and oil flow arrangement on a flood lubricated double thrust bearing. The final section considers the problem of power loss in high-speed tilting pad thrust assemblies and shows how significant savings can be made by using a different system of lubrication (directed lubrication).
EXPERIMENTAL EQUIPMENT
The Orion test rig shown in Fig. 13.1 was used for the majority of the work described. A 124-mm 0.d. double tilting pad thrust bearing assembly was used, in which each thrust ring incorporated eight white-metal faced, steel backed, centre pivoted thrust pads, 28 mm wide. To enable accurate friction torque measurements to be made, the double thrust bearing was supported in a test head mounted on hydrostatic journal bearings with the thrust load applied by means of hydrostatic pistons. The 55-mmtest shaft was driven at speeds up to 15 000 rev/min by a 56-kW variable-speed d.c. motor. Lubricating oil was supplied to the test head from an external circuit which incorporated heate’rs, coolers, pressure and temperature controls, etc., to maintain the lubricant within the required parameters for each test. Shaft speed was measured with an electronic counter, and friction torque by means of a spring balance.
For the early tests the bearing performance was estimated mainly by means of copper-constantan thermocouples embedded within about 0.05 mm of the bearing surface. Later tests used film thickness probes embedded in selected thrust pads. These probes were of the capacitance type with the signal being read on an inductive ratioing instrument (I)+. Up to eight thermocouples were used in some pads, and a typical set of instrumented pads is shown in Fig. 13.2.
For many of the initial tests on the directed lubrication system of oil supply described later in this paper, a relatively simple test rig (Scylla) was used. This rig permitted larger thrust pads (68 mm) to be tested on a 750-mm 0.d. t h m t Cbllar at speeds up to 3000 revlmin, which enabled a mean sliding speed of 100 m/s to be achieved compared with the maximum of 76 m/s that was possible on the Orion rig. To minimize power requirements and to simplify loading arrangements the Scylla rig incorporated two pairs of thrust pads, each pair being hydraulically loaded against opposite sides of the thrust collar so that

there was no resultant axial thrust. Instrumentation consisted of thrust pad temperature thermocouples, oil flow quantity, pressure, temperature, shaft speed, and applied thrust. It was found that results obtained on this simplerig could be subsequently confirmed on the Orion rig.
All the work described in this paper used a mineral oil with a viscosity of 41 cS at 50°C, 8.4 cS at 100°C. The majority of the tests were carried out with an oil inlet temperature of 50°C.