Development of a high pressure ratio centrifugal compressor for 300kW-Class ceramic gas turbine

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Sakai, T ^a   Tohbe, Y ^a   Fujii, T ^a   Tatsumi, T ^b  

^a Akashi Technical Inst   (Japan)

^b KAWASAKI HEAVY INDUSTRIES LTD   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; CENTRIFUGAL COMPRESSORS; CENTRIFUGATION; CERAMIC MATERIALS; COMPRESSIBILITY OF GASES; EFFICIENCY; ENGINES; GAS COMPRESSORS; GAS GENERATORS; GASES; IMPELLERS; INTERNATIONAL TRADE; MARINE ENGINES;

ADIABATIC EFFICIENCY; FLOW DISTRIBUTION; HIGH PRESSURE RATIO; HIGH-EFFICIENCY; IMPELLER INLETS; RESEARCH AND DEVELOPMENT; THERMAL EFFICIENCY; TURBINE INLET TEMPERATURE;

GAS TURBINES;

EID: 84973664452     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-480     Document Type: Conference Paper

References (3)

1. Y. Ichikawa et al., 1997, "Current Status of CGT302 (Progressing to final phase)", ASME 97-OT.
2. D Eckardt, "Instantaneous Measurements in the Jet-Wake Discharge Flow of a Centrifugal Compressor Impeller", Journal of Engineering for Power, TransASME, Series A, Vol.97, No.3, July 1975, pp.337-346.
3. J. D. Denton and U. K Singh, "Time Marching Methods for Turbomachinery Flow Calculation", VICI Lecture Series on Transonic Flows for Turbomachinery. 1979.