OS-507 R & D and Simulated Altitude Testing of HYPER Combined Cycle Engine(Organized Session 5: HYPR-HST/SST Propulsion System)

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概要

• 論文の詳細を見る

• The Hypersonic Transport Propulsion System Research Project (HYPR) was launched in 1989 to develop technologies for the propulsion system of a Mach 5 hypersonic transport (HST) airplane. The engine being studied is the combined cycle engine composed of a turbo jet engine which can operate from take-off to Mach 3 and a ram jet engine which can operate over Mach 2.5 up to Mach 5. The mode transition from turbo to ram and reverse transition are assumed in the range of Mach 2.5 and 3. The combined cycle engine demonstrator was designed and manufactured in 1997. The first combined cycle engine test was carried out in February, 1998. Then the altitude test was performed to demonstrate turbo-ram mode transition capability from December, 1998 to March, 1999. This paper describes the design features and ATF test results of the combined cycle engine demonstrator focusing on turbo-ram mode transition.

• 社団法人日本ガスタービン学会の論文
• 1999-11-14

著者

• Wells Gray

  P & W

• Kimura Hideo

  Kawasaki Hi

• MITSUOKA Takeo

  IHI

• NAKATA Yasushi

  IHI

• MIYAGI Hiroyuki

  IHI

• KISHI Kimihiro

  Mitsubishi HI

• CABE Jerry

  GE

• YANAGI Ryoji

  NAL

• MITSUOKA Takeo

  Ishikawajima-Harima Heavy Industries, Co., Ltd.

• NAKATA Yasushi

  Ishikawajima-Harima Heavy Industries, Co., Ltd.

• MIYAGI Hiroyuki

  Ishikawajima-Harima Heavy Industries, Co., Ltd.

• WELLS Gary

  United Technologies Pratt & Whitney

• CABE Jerry

  GE Aircraft Engines

• YANAGI Ryoji

  National Aerospace Laboratory

• Kishi Kimihiro

  Mitsubishi Heavy Industries Ltd.

関連論文

• R&D and Simulated Altitude Testing of HYPER Combined Cycle Engine
• OS-507 R & D and Simulated Altitude Testing of HYPER Combined Cycle Engine(Organized Session 5: HYPR-HST/SST Propulsion System)
• OS-504 Research and Development of High Temperature Core Engine(Organized Session 5: HYPR-HST/SST Propulsion System)
• Velocity Field Image of Free Jet using Doppler Global Velocimetry
• OS-503 Research of Mach 5 Ramjet Propulsion System(Organized Session 5: HYPR-HST/SST Propulsion System)
• OS-501 Research and Development of Low Pressure Components(Organized Session 5: HYPR-HST/SST Propulsion System)

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