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Title:
COMBUSTION LINER COOLING
Document Type and Number:
Japanese Patent JP2017166485
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a combustor (16) having an annularly shaped liner (42) that at least partially defines a hot gas path of the combustor (16).SOLUTION: A flow sleeve (54) circumferentially surrounds at least a portion of the liner (42). The flow sleeve (54) is radially separated from the liner (42) to form a cooling flow annulus (56) therebetween. A bluff body (58) extends radially between the flow sleeve (54) and the liner (42) in the cooling flow annulus (56). A guide vane (68) is disposed within the cooling flow annulus (56) and extends between the flow sleeve (54) and the liner (42) proximately to the bluff body (58).SELECTED DRAWING: Figure 2

Inventors:
ANDREW GRADY GODFREY
WILLIS CHRISTOPHER PAUL
CIHLAR DAVID WILLIAM
DAVID PHILIP PORZIO
Application Number:
JP2017038875A
Publication Date:
September 21, 2017
Filing Date:
March 02, 2017
Export Citation:
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Assignee:
GENERAL ELECTRIC CO GE
International Classes:
F23R3/28; F02C7/18; F23R3/34; F23R3/42
Domestic Patent References:
JPS5960127A1984-04-06
JPS6218569U1987-02-04
JPS56168038A1981-12-24
Foreign References:
US20120297784A12012-11-29
US20120297783A12012-11-29
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka