发明名称 THREADED SEAL FOR A GAS TURBINE ENGINE
摘要 <p>A seal assembly includes a first component and a second component of a gas turbine engine. The first component has a threaded portion. The second component interfaces with the threaded portion and together the threaded portion and the second component form a seal that restricts fluid flow between a first cavity and a second cavity of the gas turbine engine.</p>
申请公布号 WO2014039274(A1) 申请公布日期 2014.03.13
申请号 WO2013US56233 申请日期 2013.08.22
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 AMADOR, ARMANDO
分类号 F02C7/28;F02C7/00;F02K3/00 主分类号 F02C7/28
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