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Experimental evaluation of foil-supported resilient-pad gas-lubricated thrust bearing

Author
Nemeth, Z. N.
Published
Sep 1, 1977.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary
A new type of resilient-pad gas thrust bearing was tested to determine the feasibility of the design. The bearing consists of carbon graphite pads mounted asymmetrically on foil beams. Two bearing configurations were tested at thrust loads from 27 to 80 newtons at speeds to 9000 rpm. The outside diameter of the bearing was 8.9 centimeters.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19770024558.
Accession ID: 77N31502.
E-9061.
NASA-TP-1030.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15731310