Invention Grant
- Patent Title: Ring cooling for a combustion liner and related method
- Patent Title (中): 燃烧衬套的环形冷却及相关方法
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Application No.: US12349173Application Date: 2009-01-06
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Publication No.: US08677759B2Publication Date: 2014-03-25
- Inventor: Karthick Kaleeswaran , Rao Ganesh Pejawar , Sonal Bhojani
- Applicant: Karthick Kaleeswaran , Rao Ganesh Pejawar , Sonal Bhojani
- 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: F23R3/04
- IPC: F23R3/04 ; F23R3/46
Abstract:
A gas turbine combustor includes a liner having a forward end and an aft end; a flow sleeve surrounding the liner, the flow sleeve also having forward and aft ends, the aft end of the flow sleeve supporting an annular ring formed with a plurality of cooling bores and extending through the flow sleeve, at least some of the plurality of cooling bores formed at an acute angle relative to a longitudinal axis of the liner.
Public/Granted literature
- US20100170256A1 RING COOLING FOR A COMBUSTION LINER AND RELATED METHOD Public/Granted day:2010-07-08
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