发明授权
US08276391B2 Combustor liner cooling at transition duct interface and related method
有权
过渡管道界面的燃烧器衬管冷却及相关方法
- 专利标题: Combustor liner cooling at transition duct interface and related method
- 专利标题(中): 过渡管道界面的燃烧器衬管冷却及相关方法
-
申请号: US12762842申请日: 2010-04-19
-
公开(公告)号: US08276391B2公开(公告)日: 2012-10-02
- 发明人: Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
- 申请人: Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
- 申请人地址: US NY Schenectady
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: US NY Schenectady
- 代理机构: Nixon & Vanderhye, P.C.
- 主分类号: F02C7/18
- IPC分类号: F02C7/18 ; F23R3/46
摘要:
A resilient annular seal structure is disposed radially between an aft end portion of a combustor liner and a forward end portion of a transition piece, the resilient annular seal structure configured to form a first annular cavity radially between the forward end portion of the transition piece and the aft end portion of said combustor. At least one transfer tube radially extends from the second flow sleeve through the second flow annulus to the transition piece, and is arranged to supply compressor discharge cooling air radially from an area outside the first and second substantially axially extending flow annuli directly to the resilient annular seal structure and to the aft end of the combustor liner.
公开/授权文献
信息查询
IPC分类: