发明名称 Vane assembly and method of forming a vane assembly for a gas turbine engine
摘要 <p>A method of working a vane assembly (10) for a gas turbine engine involves a collar (32) and an engine operated cooling baffle (14). The collar is connected to the cooling baffle and installed into the interior cavity (26) of the vane assembly. A braze is applied to both a portion (46) of the collar that interfaces with the cooling baffle and to a second portion (48) of the collar that interfaces with the vane assembly. In one embodiment, the connection between the replacement collar and both the cooling baffle and vane assembly is accomplished by fitting the cooling baffle into the collar and by slipping a portion of the cooling baffle with a smaller cross-sectional area through the collar, and both portions are brazed in the same operation.</p>
申请公布号 EP2551457(A2) 申请公布日期 2013.01.30
申请号 EP20120178565 申请日期 2012.07.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 VETERE, THOMAS A.;MILLER, MICHAEL L.
分类号 F01D5/18;F01D9/04 主分类号 F01D5/18
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