发明名称 COATING METHOD FOR GAS TURBINE TAIL CYLINDER AND FILLING TAP
摘要 PROBLEM TO BE SOLVED: To perform efficient work for applying a coating of a heat insulating film to the inner face of the tail cylinder of a gas turbine without causing the fouling of air outlets or functional troubles. SOLUTION: The method of forming the heat insulating film 40 on the inner face of the tail cylinder 10 of the gas turbine comprises a step (a) of filling a number of air outlets 18 opening to the inner face of the tail cylinder 10 with a filling tap 50 of a heat resistant material, a step (b) of applying a coating of the heat insulating film 40 to the inner face of the tail cylinder 10 with plasma spray coating, and a step (c) of removing the filling tap 50.
申请公布号 JP2003090229(A) 申请公布日期 2003.03.28
申请号 JP20010285046 申请日期 2001.09.19
申请人 AMAGASAKI TOKUZAIKEN:KK 发明人 TAKEUCHI JUN
分类号 F02C7/00;F02C7/18;(IPC1-7):F02C7/00 主分类号 F02C7/00
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