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NASA NTRS · 19780018045

Ceramic regenerator systems development program

Abstract

Ceramic regenerator cores are considered that can be used in passenger car gas turbine engines, Stirling engines, and industrial/truck gas turbine engines. Improved materials and design concepts aimed at reducing or eliminating chemical attack were placed on durability test in Ford 707 industrial gas turbine engines. The results of 19,600 hours of turbine engine durability testing are described. Two materials, aluminum silicate and magnesium aluminum silicate, continue to show promise toward achieving the durability objectives of this program. A regenerator core made from aluminum silicate showed minimal evidence of chemical attack damage after 6935 hours of engine test at 800 C and another showed little distress after 3510 hours at 982 C. Results obtained in ceramic material screening tests, aerothermodynamic performance tests, stress analysis, cost studies, and material specifications are also included.

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BibTeXRIS

Cook, J. A., Fucinari, C. A., Lingscheit, J. N., Rahnke, C. J.. 1977-12-01. Ceramic regenerator systems development program. https://ntrs.nasa.gov/citations/19780018045

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