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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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