Ceramic matrix composite combustor liner rig test

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 2000, Pages

  Brewer, David ^a   Ojard, Greg ^b   Gibler, Martin ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b PRATT AND WHITNEY   (United States)

^c STRESS ENGINEERING SERVICES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CERAMIC MATERIALS; CERAMIC MATRIX COMPOSITES; COMPOSITE MATERIALS; ENGINES; NASA; OIL WELL CASINGS; RESEARCH AIRCRAFT; SILICON CARBIDE;

CERAMIC MATRIX COMPOSITE COMBUSTORS; COMBUSTOR LINERS; CRITICAL COMPONENT; HIGH SPEED CIVIL TRANSPORTS; MATERIALS AND TECHNOLOGIES; MELT INFILTRATION; OPERATING CONDITION; SIC/SIC COMPOSITES;

COMBUSTORS;

EID: 84955083084     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0670     Document Type: Conference Paper

References (3)

1. Nemets, S.A., Ehlers, R.C., Parrot, E.;"NASA Lewis Research Center's Preheated Combustor and Materials Test Facility", NASA TM-106676, 1995.
2. Brewer, D.;"HSR/EPM Combustor Materials Development Program", Materials Science and Engineering A261 pp. 284-291, 1999.
3. Ojard, G.;"NASA Rich Burn Quick Quench Lean Burn Sector Rig SiC/SiC CMC Testing", American Ceramics Conference, Cocoa Beach, Jan 2000.