An improved long life duration CMC for jet aircraft engine applications

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 4 A, Issue , 2002, Pages 119-125

  Bouillon, Eric ^a   Lamouroux, Franck ^a   Baroumes, Laurent ^a   Cavalier, Jean Claude ^a   Spriet, Patrick ^a   Habarou, Georges ^a  

^a SNECMA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMICAL VAPOR INFILTRATION; JET AIRCRAFT ENGINE; MULTILAYER WOVEN REINFORCEMENT; SELF-SEALING MATRIX COMPOSITE; SELF-SEALING TECHNOLOGY; THERMO-MECHANICAL PROPERTY;

AIRCRAFT ENGINES; CARBON FIBERS; CREEP TESTING; FATIGUE TESTING; JET ENGINES; MICROCRACKS; OXIDATION; RELIABILITY; SILICON CARBIDE; THERMODYNAMIC PROPERTIES;

CERAMIC MATRIX COMPOSITES;

EID: 0036998202     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30625     Document Type: Conference Paper

References (5)

1. Spriet, P., Habarou, G., 1996, "Applications of Continuous Fiber Reinforced Ceramic Composites in Military Turbojet Engines," ASME paper 96-GT-294, presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Birmingham U.K., June 10-13, 1996.
2. Jouin, J. M., Cotteret, J., Christin, F., 1991, "SiC/SiC Interphase: Case History," 2nd European Colloquium, EEC Joint Res.Center, Petten (N.L.), Nov. 11-13, 1991.
3. Bouillon, E., Abbé, F., Goujard, S., Pestourie, E., Habarou, G., Dambrine, B., 2002, "Mechanical and Thermal Properties of a Self-sealing Matrix Composite and Determination of the Lifetime Duration," 24th Annual Conference on Composites, Advanced Ceramics, Materials, and Structures: 21[3], 459-468.
4. Guillaumat L., 1994, "PhD Thesis," Univ. Bordeaux 1, France.
5. John, R., Zawada, L. P., Kroupa, J. L., 1998, "Stresses Due to Temperature Gradients in Ceramic-Matrix-Composite Aerospace Components," J. Am. Ceram. Soc., 82[1], 161-168.