NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Comparison of experimental and predicted performance of 150-millimeter-bore solid and drilled ball bearings to 3 million DNSeven 150-millimeter-bore ball bearings were run under 8900-newton (2000-lbf) thrust load at speeds from 6670 to 20,000 rpm (1 million to 3 million DN). Four of the bearings had conventional solid balls, and three bearings had drilled (cylindrically hollow) balls with 50-percent mass reduction. The bearings were under-race cooled and slot lubricated with a type 2 ester oil at flow rates from 4.35 x 0.001 to 5.94 x 0.001 cubic meter/min (1.15 to 1.57 gal/min). Friction torque and temperature were measured on all bearings. While there was considerable spread in the temperature data, the drilled ball bearings tended to run slightly cooler than the solid ball bearings at higher speeds. No significant difference in torque was noted, however, between the solid and drilled ball bearings. One bearing of each type was rerun at 17,800-newton (4000-lbf) thrust load. The solid ball bearings performed satisfactorily at 3 million DN. However, at about 2 million DN the drilled ball bearing experienced a broken ball, and cracks appeared in other balls as a result of flexure fatigue. Metallurgical examination of the cracked balls indicated a brittle structure in the bore of the drilled balls.
Document ID
19740021820
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Scibbe, H. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Munson, H. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-TN-D-7737
E-7722
Accession Number
74N29933
Funding Number(s)
PROJECT: RTOP 502-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available