发明名称 Cooled gas turbine engine vane
摘要 A cooled gas turbine vane includes a cast part and a longitudinal sleeve obtained by shaping metal sheet The cast part includes a longitudinal body provided with a longitudinal cavity having a first opening and a second opening at the ends The sleeve is mounted in the cavity by being firmly affixed to the wall of the first opening, and one end part of which being free to slide in the second opening forming a guide. The end part includes a part having constricted dimensions relative to the transverse dimensions of the guide.
申请公布号 US7204675(B2) 申请公布日期 2007.04.17
申请号 US20040916435 申请日期 2004.08.12
申请人 SNECMA MOTEURS 发明人 TEXIER CHRISTOPHE
分类号 F01D5/18;F01D9/02;F02C7/18 主分类号 F01D5/18
代理机构 代理人
主权项
地址