IGTC-111 RESEARCH AND DEVELOPMENT OF TURBOFAN ENGINE FJR710-UPDATING(Session C-8 Aeroengine)

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概要

• 論文の詳細を見る

• A prototype high bypass ratio turbofan engine designated FJR710/600 has been developed in the second phase of National Research and Development Program of the Japanese Government. The engine was designed and manufactured on the technical basis accumulated in the first phase of the program and component researches in universities and laboratories. Extensive running tests according to airworthiness standards were conducted to assure the design goal of high stability, endurance and reliability. General description of the engine and engine running tests will be given along with some component researches.

• 公益社団法人日本ガスタービン学会の論文

著者

• Matsuki M.

  Engineering Research Association For Aero-jet Engines:nippon Institute Of Technology

• Takagi H.

  Nippon Institute of Technology

• Matsuki M.

  Engineering Research Association For Advanced Gas Turbines

関連論文

• IGTC-123 NONCONTACT MEASUREMENT OF ROTATING BLADE VIBRATIONS
• IGTC-123 NONCONTACT MEASUREMENT OF ROTATING BLADE VIBRATIONS(Session C-12 Vibration and Dynamics II)
• IGTC-111 RESEARCH AND DEVELOPMENT OF TURBOFAN ENGINE FJR710-UPDATING(Session C-8 Aeroengine)
• IGTC-99 Development of AGTJ-100A Reheat Gas Turbine(Session C-8 GAS TURBINE DEVELOPMENT)

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