发明名称 SEALS FOR A GAS TURBINE ENGINE
摘要 A sealing assembly may include a support, an engine component, and a seal. The engine component may be mounted relative to the support to define a gap between the engine component and the support. The seal may be arranged between the support and the engine component to block gasses from passing through the gap. The seal may be adapted to compress and expand to fill the gap during expansion and contraction of the adjacent components that occurs during operation of a gas turbine engine including the sealing assembly.
申请公布号 US2016341056(A1) 申请公布日期 2016.11.24
申请号 US201615227333 申请日期 2016.08.03
申请人 Rolls-Royce North American Technologies, Inc. 发明人 Sutterfield David L.;Zeaton Gregory W.
分类号 F01D11/00;F16J15/10;F01D25/28 主分类号 F01D11/00
代理机构 代理人
主权项 1. (canceled)
地址 Indianapolis IN US
您可能感兴趣的专利