发明名称 Endwall Countouring Trench
摘要 A gas turbine engine component comprises a casing, and a component fixed to the casing to extend from a first edge to a second edge. The component has a first side and a second side. A trench is formed within the casing adjacent the second side of the component. The trench has a maximum depth that is positioned at or aft of the first edge.
申请公布号 US2016237837(A1) 申请公布日期 2016.08.18
申请号 US201415027562 申请日期 2014.10.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Bennington Matthew A.
分类号 F01D9/04;F01D25/24;F02C3/04 主分类号 F01D9/04
代理机构 代理人
主权项 1. A gas turbine engine component comprising: a casing; a component fixed to the casing to extend from a first edge to a second edge, the component having a first side and a second side; and a trench formed within the casing adjacent the second side of the component, the trench having a maximum depth that is positioned at or aft of the first edge.
地址 Hartford CT US