Friction and heat generation in oil-lubricated ball bearings is mainly the
result of sliding in the ball-raceway contacts and agitation of the lubrica
nt in the free space between the balls, cage, and bearing rings. Endurance
of a ball bearing is highly dependent on the thicknesses of the oil films w
hich serve to separate the balls from the raceways in a well-lubricated bea
ring. The film thicknesses, in turn, are dependent upon the lubricant's vis
cous properties. These are functions of bearing temperatures and are determ
ined by the balance between the rates of frictional heat generation and hea
t dissipation. Therefore, in the design of a ball bearing application such
as the high speed rotor and low speed rotor support bearings in an aircraft
gas turbine, it is important to be able to predict the bearing frictional
heat generation rates with reasonable accuracy. This paper presents a metho
d to perform the required calculations considering bearing loading and spee
ds, realistic lubricant rheological properties, and a relatively simple hea
t transfer system between the bearing rings, balls, and lubricant. The resu
lts of the analysis are shown to compare favorably with experimental data.