发明名称 FLEXIBLE CAVITY SEAL FOR GAS TURBINE ENGINES
摘要 A seal assembly, comprising a first segment, a second segment, and a seal incorporated between the first segment and the second segment, the seal comprising a mesh. The first segment may comprise a blade outer air seal and the second segment may comprise a vane. In various embodiments, the first segment and the second segment may define a gap, and the seal may seal the gap. The seal may have a first member and a second member that enmeshes the first member. The seal may comprise a member that enmeshes a non-metallic member. The seal may comprise a ceramic fiber enmeshed by a member. The seal may comprise a non-metallic member enmeshed by a metallic member. The seal may comprise a plurality of annular connecting members, each annular connecting member extending about the seal. The seal may comprise a single annular member.
申请公布号 WO2015116399(A1) 申请公布日期 2015.08.06
申请号 WO2015US11567 申请日期 2015.01.15
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 DAVIS, TIMOTHY
分类号 F01D9/00;F01D11/02;F02C7/28 主分类号 F01D9/00
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