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3500-hour durability testing of ceramic materials for automotive gas turbine enginesA two-year durability program was performed by AiResearch Phoenix to evaluate four commercially available ceramic materials under simulated automotive gas turbine combustor discharge conditions. These conditions included extended cyclic thermal exposures up to 2500 F and 3500 hr. The four materials selected for evaluation were Norton NCX-34 hot pressed silicon nitride, AiResearch RBN 101 reaction bonded silicon nitride, Carborundum pressureless sintered alpha-SiC and Pure Carbon Co. (British Nuclear Fuels, Ltd.) Refel reaction sintered silicon carbide. These materials were initially exposed to 350 hr/1750 cycles at 1200 and 1370 C. Subsequent exposures to 1050, 2100 and 3500 hr were performed on those materials maintaining 50% of baseline strength after the initial exposure. Additional evaluations of exposed bars included dimensional and weight changes, dye penetrant, specific damping capacity changes, SEM fractography, and X-ray diffraction.
Document ID
19800051405
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carruthers, W. D.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Richerson, D. W.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Benn, K. W.
(AiResearch Manufacturing Company of Arizona Phoenix, Ariz., United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Subject Category
Nonmetallic Materials
Report/Patent Number
AIRESEARCH-31-3542
Meeting Information
Meeting: International Automotive Propulsion Systems Symposium
Location: Dearborn, MI
Start Date: April 14, 1980
End Date: April 18, 1980
Sponsors: U.S. Department of Energy and NASA
Accession Number
80A35575
Funding Number(s)
CONTRACT_GRANT: DEN3-27
Distribution Limits
Public
Copyright
Other

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