Invention Grant
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
- Patent Title: Combustor liner cooling at transition duct interface and related method
- Patent Title (中): 过渡管道界面的燃烧器衬管冷却及相关方法
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Application No.: US12762842Application Date: 2010-04-19
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Publication No.: US08276391B2Publication Date: 2012-10-02
- Inventor: Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
- Applicant: Jonathan Dwight Berry , Kara Johnston Edwards , Heath Michael Ostebee
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye, P.C.
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F23R3/46

Abstract:
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.
Public/Granted literature
- US20110252805A1 COMBUSTOR LINER COOLING AT TRANSITION DUCT INTERFACE AND RELATED METHOD Public/Granted day:2011-10-20
Information query
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