发明名称 MOUNT WITH DEFLECTABLE TABS
摘要 An assembly for a gas turbine engine includes a first component, a second component, and a first mount. The first mount includes an annular body that is connected to the first component and a plurality of circumferentially spaced tabs extending from the body. The tabs are connected to the second component and are deflectable to allow the second component to move relative to the first component.
申请公布号 US2015345399(A1) 申请公布日期 2015.12.03
申请号 US201314655571 申请日期 2013.12.19
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Budnick Matthew
分类号 F02C7/20;F01D25/24;F02C7/24 主分类号 F02C7/20
代理机构 代理人
主权项 1. An assembly comprising: a first component of a gas turbine engine; a second component of a gas turbine engine; and a first mount including an annular body connected to the first component and a plurality of circumferentially spaced tabs extending from the body, wherein the tabs are connected to the second component and are deflectable to allow the second component to move relative to the first component.
地址 Hartford CT US