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CHRYSLER’S GAS TURBINE CAR - Materials Requirements
ISSN: 0148-7191, e-ISSN: 2688-3627
Published January 01, 1964 by SAE International in United States
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Both conventional and newly developed materials used in unique applications have played an important role in making the Chrysler gas turbine engine a practical powerplant. The new low-cost materials developed by Chrysler Metallurgical Research include, (a) a series of iron-base super alloys having equivalent or superior life to aircraft type alloys, (b) heat resisting iron aluminum alloys for elevated temperature service under low stress application, and (c) long life rubbing seal materials that operate satisfactorily from ambient temperature up to 1200°F and above.
These materials appear to meet all present or immediate high temperature alloy requirements for a competitive mass produced automotive turbine.
CitationRoy, A., Hagen, F., and Belleau, C., "CHRYSLER’S GAS TURBINE CAR - Materials Requirements," SAE Technical Paper 640417, 1964, https://doi.org/10.4271/640417.
- “Premium Quality Magnesium Castings” by Flemings M. C. and Poirier, E. J. Foundry, Oct., 1963.
- “Alloy Digest”
- Transactions, ASME, Larson F. R. and Miller, J. Vol. 74, No. 5, July, 1952, pp. 765–771.