- 专利标题: Ceramic matrix composite turbine exhaust assembly for a gas turbine engine
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申请号: US15424930申请日: 2017-02-06
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公开(公告)号: US11118481B2公开(公告)日: 2021-09-14
- 发明人: Gabriel L. Suciu , Brian Merry , Ioannis Alvanos
- 申请人: United Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: United Technologies Corporation
- 当前专利权人: United Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 代理机构: Carlson, Gaskey & Olds, P.C.
- 主分类号: F01D25/30
- IPC分类号: F01D25/30 ; F02K1/04 ; F02K3/06 ; F02K1/48 ; F02K1/38 ; F01D9/02 ; F02C3/04
摘要:
A turbine exhaust assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a turbine exhaust case comprised of CMC material and attachable to a turbine case, a tail cone comprised of CMC material that has a leading edge and a trailing edge, and an exhaust mixer comprised of CMC material and coupled to the turbine exhaust case. The exhaust mixer has a plurality of lobes arranged about the tail cone to define an exhaust flow path. A plurality of struts extend from the tail cone to support the exhaust mixer at a location aft of the leading edge of the tail cone. A method of assembling a propulsion system is also disclosed.
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