IGTC-21 RESEARCH AND DEVELOPMENT ON COMBUSTORS FOR ADVANCED REHEAT GAS TURBINE(Session A-6 Combustion I (Combustor Development))

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概要

• 論文の詳細を見る

• An outline of the reserch and development on the combustors for the advanced reheat gas turbine is presented. According to the R & D progam, the original combustors-the high pressure combustor and the reheat combustor-have been developed along the planned schedule and are ready for operation at the factory. R & D tests such as the flow visualization test, the near atmospheric pressure combustion test and the pressurized combustion test are stated.

• 公益社団法人日本ガスタービン学会の論文

著者

• Kitajima J.

  Technical Institute Kawasaki Heavy Industries Ltd.

• Mori K.

  Technical Institute, Kawasaki Heavy Industries, Ltd.

• Kimura T.

  Technical Institute, Kawasaki Heavy Industries, Ltd.

• Enzaki Y.

  Engineering Div., Engineering Research Association for Advanced Gas Turbines

• Enzaki Y.

  Engineering Div. Engineering Research Association For Advanced Gas Turbines

関連論文

• IGTC-21 RESEARCH AND DEVELOPMENT ON COMBUSTORS FOR ADVANCED REHEAT GAS TURBINE
• IGTC-21 RESEARCH AND DEVELOPMENT ON COMBUSTORS FOR ADVANCED REHEAT GAS TURBINE(Session A-6 Combustion I (Combustor Development))

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