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公开(公告)号:US10145308B2
公开(公告)日:2018-12-04
申请号:US14611920
申请日:2015-02-02
Applicant: United Technologies Corporation
Inventor: Carson A. Roy Thill , Mark Broomer , Timothy M. Davis , Craig R. McGarrah , Mark J. Rogers , Russell E. Keene , Anthony B. Swift
Abstract: A seal assembly for a gas turbine engine includes an engine static structure. First and second members fluidly separate cavities from one another. A seal assembly is captured by the engine structure. The seal assembly includes a carrier and a seal that engages the first member. The second member is captured by the carrier.