发明名称 CERAMIC MATRIX COMPOSITE TURBINE BLADE SQUEALER TIP WITH FLARE
摘要 A method of forming a ceramic matrix composite turbine blade with squealer tip and with tip flare is provided. The tip flare may be located at either or both of the pressure side and the suction side. The method provides a mandrel which is placed in the pre-form tooling to create the cavity and aid in formation of the pressure side flare.
申请公布号 US2016333698(A1) 申请公布日期 2016.11.17
申请号 US201515111033 申请日期 2015.01.07
申请人 GENERAL ELECTRIC COMPANY 发明人 WEAVER Matthew Mark;IZON Paul;ALBERS Kathleen Elizabeth
分类号 F01D5/14;F01D5/28 主分类号 F01D5/14
代理机构 代理人
主权项 1. A method of forming a ceramic matrix composite (CMC) turbine blade having a squealer tip comprising: forming a plurality of two dimensional ply shapes formed of pre-preg tape; laying out a first amount of the plurality of two dimensional ply shapes with a cavity of a tool to form the turbine blade; inserting a mandrel in the tool to form a squealer tip cavity and a tip flare on at least one of a pressure side or a suction side of the blade; laying out a second amount of the plurality of two dimensional ply shapes formed of pre-preg tape; closing the tool; and, inserting the tool in an autoclave to form the turbine blade.
地址 Schenectady NY US