Development of a combustor liner composed of ceramic matrix composite (CMC)

Journal of Engineering for Gas Turbines and Power

Volumn 121, Issue 1, 1999, Pages 12-17

  Nishio, K ^a   Igashira, K I ^a   Take, K ^a   Suemitsu, T ^b  

^a Res Inst Adv Mat Gas Generator   (Japan)

^b KAWASAKI HEAVY INDUSTRIES LTD   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; FIBER REINFORCED MATERIALS; FILAMENT WINDING; FORMABILITY; GAS GENERATORS; IMPREGNATION; MECHANICAL PROPERTIES; PYROLYSIS; STRESS ANALYSIS; THERMODYNAMIC STABILITY;

NONCOOLING COMBUSTION TEST;

CERAMIC MATRIX COMPOSITES;

EID: 0032663783     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2816300     Document Type: Article

References (4)

1. Yoshida, T., 1993, “The Progress and Future of Cooling Technology of High Temperature Gas Turbines,” Journal of the Japan Gas Turbine Society, Vol. 20, No. 80, p. 4.
2. Petrasek, D. W., McDaniels, D. L., Westfall, L. J., and Stephens, J. R., 1986, “Fiber-Reinforced Superalloy Composites Provide an Added Performance Edge,” Metal Progress, Vol. 130, No. 2, p. 27.
3. Hiromatsu, M., Yamamura, T., Chikata, T., Sekido, T., Ohama, S., Miyagawa, H., Murakami, I., and Seki, S., 1995, “Research and Development Status of Advanced Material Gas-Generator (AMG) Project,” ASME95-GT-287.
4. Nishio, K., Igashira, K., Take, K., Suemitsu, T., 1997, “Development of Combustor Liner Composed of Ceramic Matrix Composite (CMC),” Journal of the Japan Gas Turbine Society, Vol. 25. No. 98, p. 94.