A. M. Mikula
Research Engineer
Mem.ASME
R. S. Gregory
Vice President and Manager, Research and Development
Assoc. Mem. ASME
Kingsbury, Inc., Philadelphia. Pa. 19154
This paper compares three different lubricant supply methods-pressurized supply
(flooded), spray feed, and leading edge distribution groove-and analyzes their
influence on the performance of tilting pad, equalizing thrust bearings. The paper
presents experimental data on 267 mm (10-½ in.) o.d. bearings, operating at
shaft speeds up to 13,000 rpm with loads ranging up to 3.45 MPa (500 psi). The
data presented demonstrate the effect each lubricant supply method has on bearing
power loss and temperature. Conclusions are drawn, based upon the effectiveness
of each design, to guide the potential user.
Introduction
There are a wide variety of thrust bearing types available to
machinery designers. In addition to initial cost, each type of
thrust bearing has its own unique set of performance
characteristics which serve as the evaluation criteria for
identical operating conditions. The two primary indicators of
bearing performance are power loss and babbitt temperature
of the pads, or "shoes." Rising energy costs have made
bearing power loss a very critical yardstick in the evaluation
of relative performance. The maximum babbitt temperature
effectively gages the degree of bearing operating risk, and can
even limit the bearing's suitability for a specific application.
The approach of this paper will be limited to a thorough
discussion of power loss values and bearing operating temperatures
attained in similar bearings employing three different
lubricant supply methods.
In order to evaluate the three different lubricant supply
methods - pressurized supply, spray feed, and leading edge
distribution groove - each method was tested under identical
conditions of applied load, shaft speed, inlet oil temperature,
and oil viscosity. A detailed description of the test rig can be
found in reference [1]. By reporting the effect of each
lubricant supply method on bearing power loss and babbitt
temperature, it is hoped that this paper will provide the
necessary information for the designer to make a well-reasoned
thrust bearing selection, based upon actual performance
data.
All three bearings were evaluated in comprehensive tests
using a light turbine oil with a viscosity of 0.027 Pa·S @
37.8°C and 0.006 Pa·S @ 98.9°C (150 SSU @ 100°F and 43
SSU @ 210°F) supplied at 46°C (115°F), for applied loads
ranging from 0-3.45 MPa (0-500 psi) and shaft speeds ranging
from 4000-13,000 rpm.
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