发明名称 GAS TURBINE COMBUSTOR
摘要 An internal cylinder which has the opening section from which combustion gas is blown out is inserted into the tail cylinder which becomes a flow path of the combustion gas, and is engaged with the tail cylinder, while securing a clearance between the edge of the opening section and the internal wall surface of the tail cylinder. Air compressed with a compressor is jetted from the clearance along the internal wall surface of the tail cylinder, and a film of cooling air is formed on the internal wall surface of the tail cylinder.
申请公布号 CA2380914(C) 申请公布日期 2007.11.06
申请号 CA20022380914 申请日期 2002.04.05
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 AKAGI, KOUICHI;TOMIMOTO, SOUICHIROU
分类号 F02C7/18;F23R3/02;F23R3/00;F23R3/04;F23R3/42 主分类号 F02C7/18
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