发明名称 Blade outer air seal and repair method
摘要 An article of manufacture has a body formed in part of a first metal alloy and in part of a second metal alloy, the second metal alloy having a thermal coefficient of expansion that is less than the thermal coefficient of expansion of the first metal alloy. A BOAS segment for a gas turbine engine is disclosed wherein the formation of cracks due to thermal mechanical fatigue in the body of the disclosed BOAS segment is minimized, if not eliminated, through a unique construction of the disclosed BOAS segment, whether original equipment manufacture or a repaired blade outer air seal. A method for manufacture of a BOAS segment and a method for modifying a BOAS segment are disclosed.
申请公布号 US8613590(B2) 申请公布日期 2013.12.24
申请号 US20100844344 申请日期 2010.07.27
申请人 BELANGER PHILIP R.;THOLEN SUSAN M.;UNITED TECHNOLOGIES CORPORATION 发明人 BELANGER PHILIP R.;THOLEN SUSAN M.
分类号 F04D29/08 主分类号 F04D29/08
代理机构 代理人
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