Three decades of research by U.S. industry and government laboratories have produced a vast array of data related to the use of ceramic rolling-element bearings and bearing components for aircraft gas turbine engines. Materials such as alumina, silicon carbide, titanium carbide, silicon nitride, and a crystallized glass ceramic have been investigated. Rolling-element endurance tests and analysis of full-complement bearings have been performed. Materials and bearing design methods have improved continuously over the years. This paper reviews a wide range of data and analyses with emphasis on how early NASA contributions as well as more recent data can enable the engineer or metallurgist to determine just where ceramic bearings are most applicable for gas turbines.
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January 1989
Research Papers
Ceramic Bearings for Use in Gas Turbine Engines
E. V. Zaretsky
E. V. Zaretsky
NASA Lewis Research Center, Cleveland, OH 44135
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E. V. Zaretsky
NASA Lewis Research Center, Cleveland, OH 44135
J. Eng. Gas Turbines Power. Jan 1989, 111(1): 146-154 (9 pages)
Published Online: January 1, 1989
Article history
Received:
January 15, 1988
Online:
October 15, 2009
Citation
Zaretsky, E. V. (January 1, 1989). "Ceramic Bearings for Use in Gas Turbine Engines." ASME. J. Eng. Gas Turbines Power. January 1989; 111(1): 146–154. https://doi.org/10.1115/1.3240213
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