OS-501 Research and Development of Low Pressure Components(Organized Session 5: HYPR-HST/SST Propulsion System)

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概要

• 論文の詳細を見る

• The design and rig test results of a two-stage transonic axial-flow fan and a single-stage low pressure turbine with the variable vane of turbofan engine for Super/Hyper-sonic Transport propulsion system under HYPR Project are described in this paper. Engine tests were conducted with Mach 2.5-3 flight conditions and the test results are also presented.

• 公益社団法人日本ガスタービン学会の論文
• 1999-11-14

著者

• Tobita Akihiro

  Mitsubishi Heavy Industries Ltd.

• SHIMIZU Kunihiro

  Mitsubishi Heavy Industries, Ltd.

• Kishi Kimihiro

  Mitsubishi Heavy Industries Ltd.

• Hirota Masashi

  Mitsubishi Heavy Industries Ltd.

• NOGAMI Ryouma

  Mitsubishi Heavy Industries, Ltd.

• Nogami Ryouma

  Mitsubishi Heavy Industries Ltd.

• Shimizu Kunihiro

  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)
• OS-501 Research and Development of Low Pressure Components(Organized Session 5: HYPR-HST/SST Propulsion System)

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