公开(公告)号：US20150226132A1

公开(公告)日：2015-08-13

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

IPC: F02C7/28 ,  F01D25/24 ,  F02C3/04

CPC classification number: F02C7/28 ,  F01D11/005 ,  F01D25/24 ,  F01D25/246 ,  F02C3/04 ,  F05D2240/56 ,  F05D2240/58 ,  F05D2260/30 ,  F16J15/0887

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.

Abstract translation: 用于燃气涡轮发动机的密封组件包括发动机静止结构。 第一和第二构件将空腔彼此流体地分开。 密封组件由发动机结构捕获。 密封组件包括承载件和接合第一构件的密封件。 第二个成员由承运人捕获。