Title:
A burner assembly object for turbine engines, and a method of assembling for the same
Document Type and Number:
Japanese Patent JP6001854
Kind Code:
B2
Abstract:
A method of assembling a combustor assembly for use in a turbine engine is provided. A combustor liner that defines a combustion chamber therein is provided. The liner includes a forward end and an aft end, wherein the aft end includes at least one channel extending therethrough. The channel is aligned obliquely with respect to a centerline extending through the aft end. A plurality of fuel nozzles are coupled to the forward end such that the fuel nozzles extend through the forward end. An annular sleeve that includes at least one opening extending radially therethrough is coupled to the aft end, wherein the sleeve substantially circumscribes the aft end such that a cavity is defined therebetween and such that a fluid channeled through the at least one opening impinges against a surface of the aft end prior to the fluid being channeled into the combustion chamber.
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Inventors:
David William Chiral
Ronald James Chira
Mart Ennis Berkman
Ronald James Chira
Mart Ennis Berkman
Application Number:
JP2011284835A
Publication Date:
October 05, 2016
Filing Date:
December 27, 2011
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F02C7/20; F23R3/00; F23R3/06; F23R3/28; F23R3/42
Domestic Patent References:
| JP2010209912A | ||||
| JP2007155312A | ||||
| JP2002267161A | ||||
| JP2003114023A |
Foreign References:
| US5598697 | ||||
| US20090120096 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka