发明名称 TOOL AND METHOD FOR FILLING VOIDS IN TURBINE VANES AND OTHER ARTICLES
摘要 A tool for filling voids of a turbine vane and other components and a method thereof are provided to efficiently fill a hole with alloy paste more than the existing method using an injection needle and to satisfy human body conditions and reduce errors by making the working procedure less boring. A tool for filling voids of a turbine vane and other components comprises at least one pad, that is, a first pad and a second pad having a working surface formed similarly to the shape of a desired area of the component surface having the voids. The pads are combined with each other to cover a corresponding desired area to press paste into the void by the working surface. The component is a turbine engine blade or vane(12) having a suction surface, a pressure surface, and a front end edge connecting the suction surface with the pressure surface. One of the pads is a suction surface pad having a working surface formed similarly to a suction surface desired area; the other is a pressure surface pad having a working surface formed similarly to a pressure surface desired area.
申请公布号 KR20060132478(A) 申请公布日期 2006.12.21
申请号 KR20060054244 申请日期 2006.06.16
申请人 UNITED TECHNOLOGIES CORP. 发明人 D'AMOUR BRIAN E.;THURSTON RAYMOND D.
分类号 B23P15/00;B23P15/02;B23P15/04;B25B33/00 主分类号 B23P15/00
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