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Title: Apparatus and method for cooling a combustor cap

Patent ·
OSTI ID:1130307

A combustor includes an end cap having a perforated downstream plate and a combustion chamber downstream of the downstream plate. A plenum is in fluid communication with the downstream plate and supplies a cooling medium to the combustion chamber through the perforations in the downstream plate. A method for cooling a combustor includes flowing a cooling medium into a combustor end cap and impinging the cooling medium on a downstream plate in the combustor end cap. The method further includes flowing the cooling medium into a combustion chamber through perforations in the downstream plate.

Research Organization:
General Electric Co., Schenectady, NY (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
8,707,672
Application Number:
12/879,238
OSTI ID:
1130307
Resource Relation:
Patent File Date: 2010 Sep 10
Country of Publication:
United States
Language:
English

References (9)

Gas burners patent December 1989
Gas turbine combustor of the completely premixed combustion type patent August 1994
Deflecting feeder bowl assembly for a turbojet engine combustion chamber patent August 1999
Gas turbine combustor and operating method thereof patent March 2008
Methods and apparatus for cooling gas turbine engine components patent September 2009
Combustor end cap assembly patent May 2013
Swirled Diffusion Dump Combustor patent-application January 2003
Premixed Direct Injection Disk patent-application September 2010
Dual Fuel Combustor Nozzle for a Turbomachine patent-application March 2011

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Combustor having wake air injection patent December 2014