发明名称 Repair method for gas turbine engine components
摘要 A method for repairing a gas turbine engine component includes applying a braze slurry to a first portion of the component, applying a pre-sintered preform to a second portion of the component that is different than the first portion, and brazing the component.
申请公布号 US8356409(B2) 申请公布日期 2013.01.22
申请号 US20070933660 申请日期 2007.11.01
申请人 UNITED TECHNOLOGIES CORPORATION;PERRET EDMUNDO J. 发明人 PERRET EDMUNDO J.
分类号 B23P6/00;B23K15/06;B23K31/00 主分类号 B23P6/00
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