NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design and performance of compliant thrust bearing with spiral-groove membranes on resilient supportsNovel thrust bearings with spiral-groove flexible membranes mounted on resilient supports were designed and their performance demonstrated. Advantages of surface compliance were combined with the superior load-capacity of the spiral-groove geometry. Loads of 127-150N were supported on an area 42 sq cm, at speeds of 43,000-45,000 rpm and mean clearances of 15-20 microns. Support-worthiness was proved when tested in conjunction with foil journal-bearings and a 19N rotor, excited in a pitching mode by a total unbalance of 43 micron-N.
Document ID
19810034280
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Licht, L.
(NASA Lewis Research Center Cleveland, OH, United States)
Anderson, W. J.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Doroff, S. W.
(U.S. Navy, Office of Naval Research, Arlington Va., United States)
Date Acquired
August 11, 2013
Publication Date
August 1, 1980
Subject Category
Mechanical Engineering
Report/Patent Number
ASME PAPER 80-C2/LUB-36
Meeting Information
Meeting: Century 2 International Lubrication Conference
Location: San Francisco, CA
Country: US
Start Date: August 18, 1980
End Date: August 21, 1980
Sponsors: American Society of Mechanical Engineers, American Society of Lubrication Engineers
Accession Number
81A18684
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available