发明名称 PLUG SEAL FOR GAS TURBINE ENGINE
摘要 An example seal includes, among other things, a plug body to limit flow through an axially extending interface between a first component and a second component, the plug body to flow when positioned within both a cavity of the first component and a cavity of the second component.
申请公布号 US2016215642(A1) 申请公布日期 2016.07.28
申请号 US201414916752 申请日期 2014.09.08
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Simonds Mark E.
分类号 F01D11/00;F01D9/04 主分类号 F01D11/00
代理机构 代理人
主权项 1. A seal, comprising: a plug body to limit flow through an axially extending interface between a first component and a second component, the plug body to limit flow when positioned within both a cavity of the first component and a cavity of the second component.
地址 Hartford CT US