发明名称 TURBINE COMBUSTOR WITH CLOSED CIRCUIT COOLING
摘要 PROBLEM TO BE SOLVED: To provide a turbine combustor with a closed circuit cooling including an inside wall and an outside wall demarcating a combustion chamber, where a gap for passing a cooling fluid is formed between the inside wall and the outside wall, a cooling fluid introduction passage is opened to the gap and a cooling fluid discharge passage is provided for discharging the cooling fluid from the gap, improved to have a small radial expanding dimension. SOLUTION: The cooling fluid discharge passage has a duct-like discharge passage structure 8 extending along the axial direction of a combustor, and the discharge passage structure is interrupted by an inlet structure 4 of the cooling fluid introduction passage disposed between the discharge passage structures. COPYRIGHT: (C)2004,JPO&NCIPI
申请公布号 JP2004197748(A) 申请公布日期 2004.07.15
申请号 JP20030421132 申请日期 2003.12.18
申请人 SIEMENS AG 发明人 TIEMANN PETER
分类号 F02C7/18;F02C7/28;F23M7/04;F23R3/00;F23R3/42;(IPC1-7):F02C7/18 主分类号 F02C7/18
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