发明授权
- 专利标题: Gas turbine engine combustor surge retention
- 专利标题(中): 燃气轮机发动机燃烧器浪涌保持
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申请号: US13460998申请日: 2012-05-01
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公开(公告)号: US09297536B2公开(公告)日: 2016-03-29
- 发明人: Jonathan Jeffery Eastwood , Kevin Joseph Low
- 申请人: Jonathan Jeffery Eastwood , Kevin Joseph Low
- 申请人地址: US CT Hartford
- 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 Hartford
- 代理机构: Carlson, Gaskey & Olds, P.C.
- 主分类号: F23R3/50
- IPC分类号: F23R3/50 ; F23R3/60 ; F02C7/20 ; F23R3/00 ; F01D25/24
摘要:
A combustor assembly for a gas turbine engine includes a static structure and an annular combustor extending around a central axis and located radially inwards of the static structure. The annular combustor includes an annular outer shell and an annular inner shell that define an annular combustion chamber there between. The annular combustor is free of any rigid attachments directly between the static structure and the annular outer shell. The annular outer shell includes a radially-outwardly extending flange. A stop member is rigidly connected with the static structure and is located adjacent the radially-outwardly extending flange such that axial-forward movement of the annular combustor is limited.
公开/授权文献
- US20130291544A1 GAS TURBINE ENGINE COMBUSTOR SURGE RETENTION 公开/授权日:2013-11-07
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