发明名称 Friction stir welded hollow airfoils and method therefor
摘要 A hollow component for gas turbine engine, for example an outlet guide vane, is assembled from a body having at recessed pocket formed therein, and an aerodynamic cover bonded over the pocket. Both the cover and the body are constructed from materials which are not readily fusion weldable. The cover is attached to the body by a solid state bonding process, for example friction stir welding. The hollow component may also be built up from multiple individual components which are bonded to each other by a solid state bonding process such as friction stir welding.
申请公布号 US2005254955(A1) 申请公布日期 2005.11.17
申请号 US20040846326 申请日期 2004.05.14
申请人 GENERAL ELECTRIC COMPANY 发明人 HELDER EARL C.;TRAPP TIMOTHY J.;KELLEY JOHN R.;TUDOR COURTNEY J.;BUDINGER VICKY S.
分类号 F01D9/02;B23K20/12;B23K103/10;F01D5/14;F02C7/00;F04D29/32;F04D29/54;(IPC1-7):B63H1/26 主分类号 F01D9/02
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