发明名称 Fan outlet guide vane shroud insert repair
摘要 A method of repairing a turbine engine component that contains a series of lined apertures. The component is removed from the engine, and then at least one of the aperture liners is also removed. The area adjacent the aperture is machined to remove a portion of the parent material of the component. An insert which replaces the material removed by machining is secured adjacent the aperture. The liner about the aperture is then replaced.
申请公布号 US7980813(B2) 申请公布日期 2011.07.19
申请号 US20070891815 申请日期 2007.08.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MEDYNSKI ANDREW W.;ZAPPONE RONALD N.
分类号 F01D5/10 主分类号 F01D5/10
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