发明名称 STATIONARY BLADE SHROUD OF A GAS TURBINE
摘要 A base plate and honeycomb member disposed at the inner circumference side of an inside shroud are fixed to the inside shroud, at a phase deviation in the peripheral direction, with respect to the inside shroud, so as to plug the missing range of seal member, out of gaps between adjacent inside shrouds, and therefore leak of purge air from the missing range of seal member is prevented without adding new constituent members.
申请公布号 CA2366758(A1) 申请公布日期 2002.08.06
申请号 CA20022366758 申请日期 2002.01.07
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 TOMITA, YASUOKI;KUWABARA, MASAMITSU;TORII, SHUNSUKE
分类号 F01D11/02;F01D9/04;F01D11/00;(IPC1-7):F01D25/24;F01D9/02 主分类号 F01D11/02
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