| LIU Hong-xia, LIANG Chun-hua, SUN Ming-xia.Progress and Analysis of U.S. Supersonic Turbine Based Combined Cycle Engine[J].航空发动机,2017,43(4):96-102 |
| Progress and Analysis of U.S. Supersonic Turbine Based Combined Cycle Engine |
| DOI： |
| Key Words:supersonic propulsion system TBCC combined ramjet engine aeroengine |
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| Abstract:Aim to provide references for future aerospace power technology investigation and product development, the progress of
Trbine Based Combined Cycle engine 渊TBCC冤and advanced programs on turbine engine for TBCC were overviewed and analyzed. These
programs include the National Aerospace Plane 渊NASP冤, High-Speed Propulsion Assessment 渊HiSPA冤, Falcon Combined Cycle Engine
Technology渊FaCET冤, etc. The analysis results show that TBCC is always key technology for supersonic flight vehicle, the in-service turbine
engine is preferred for TBCC at present, high speed turbine engine and adaptive cycle engine will be selected for TBCC in future, ramjet for
TBCC and mode transition between turbine engine and ramjet need to be researched deeply. |
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