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NASA NTRS ยท 20100025714

Two High-Temperature Foil Journal Bearings

Abstract

An enlarged, high-temperature-compliant foil bearing has been built and tested to demonstrate the feasibility of such bearings for use in aircraft gas turbine engines. Foil bearings are attractive for use in some machines in which (1) speeds of rotation, temperatures, or both exceed maximum allowable values for rolling-element bearings; (2) conventional lubricants decompose at high operating temperatures; and/or (3) it is necessary or desirable not to rely on conventional lubrication systems. In a foil bearing, the lubricant is the working fluid (e.g., air or a mixture of combustion gases) in the space between the journal and the shaft in the machine in which the bearing is installed.

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BibTeXRIS

Zak, Michail. 2006-05-01. Two High-Temperature Foil Journal Bearings. https://ntrs.nasa.gov/citations/20100025714

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