发明名称 Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention
摘要 An impingement insert sleeve is provided that is adapted to be disposed in a coolant cavity defined through a stator vane. The insert has a generally open inlet end and first and second pairs of diametrically opposed side walls, and at least one fail-safe tab defined at a longitudinal end of the insert for limiting radial displacement of the insert with respect to the stator vane.
申请公布号 US6561757(B2) 申请公布日期 2003.05.13
申请号 US20010682195 申请日期 2001.08.03
申请人 GENERAL ELECTRIC COMPANY 发明人 BURDGICK STEVEN SEBASTIAN;KELLOCK IAIN ROBERTSON
分类号 F01D5/18;F01D9/02;F01D9/06;F01D11/00;F01D25/12;(IPC1-7):F01D9/06 主分类号 F01D5/18
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