Conceptual design of the cooling system for 1700°cclass, hydrogen-fueled combustion gas turbines

Journal of Engineering for Gas Turbines and Power

Volumn 121, Issue 1, 1999, Pages 108-115

  Kizuka, N ^a   Sagae, K ^a   Anzai, S ^a   Marushima, S ^a   Ikeguchi, T ^a   Kawaike, K ^a  

^a HITACHI LTD   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COOLANTS; COOLING SYSTEMS; COPPER ALLOYS; HYDROGEN FUELS; NOZZLES; TURBOMACHINE BLADES;

OPEN-CIRCUIT COOLING SYSTEMS;

GAS TURBINES;

EID: 0032664442     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2816296     Document Type: Article

References (11)

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3. Geiling, D. W., Klompas, N., and Zeman, K. P., 1983, “Water Cooled Gas Turbine Nozzle Technology Demonstration at Ultra-High Firing Temperature,” ASME Paper 83-GT-15.
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8. Kawaike, K., Anzai, S., and Sasada, T., 1992, “Integrated CAE System for Cooled Turbine Blade Design and Verification Tests of Analytical Codes,” Heat Transfer in Turbomachinery, R. J. Goldstein, et al., Proceedings of International Symposium Heat Transfer in Turbomachinery, International Center for Heat and Mass Transfer, eds., Begeh House, Inc., New York, pp. 73-84.
9. Kawaike, K., Anzai, S., Takehara, I., Sasada, T., and Matsuzaki, H., 1993, “Advanced Cooling Design of Turbine Blades With Serpentine Cooling Passages,” CIMAC, G12.
10. Kukreja, R. T., Lau, S. C, and Mcmillin, R. D., 1991, “Effects of Length and Configuration of Transverse Discrete Ribs on Heat Transfer and Friction for Turbulent Flow in a Square Channel,” ASME/JSME Thermal Engineering Proceeding, Vol. 3, pp. 213-218.
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