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Title:
燃焼器ノズル、燃焼器及びガスタービン
Document Type and Number:
Japanese Patent JP6883464
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide a combustor nozzle capable of preventing flashback from occurring, a combustor, and a gas turbine.SOLUTION: The combustor nozzle comprises an axis body 51M having a main outer peripheral face Pm extending along an axial line A1 and a radially converging outer peripheral face Ps with a diameter gradually shrinking from the main outer peripheral face Pm toward the front side in the direction of the axial line A1, a plurality of swirl vanes 60 outwardly extending in the radial direction from the main outer peripheral face Pm and disposed with a gap apart from each other in the circumferential direction of the axial line A1, each having fuel ejection holes H1 formed on the surface thereof for ejecting fuel, and a flow-pass forming cylinder 51T having a first cylinder part T1 that surrounds the main outer peripheral face Pm from the outer circumference side and a second cylinder part T2 continuous from the first cylinder part T1 to surround the radially converging outer peripheral face Ps from the outer circumference side with a diameter gradually shrinking toward the front side thereof in the direction of the axial line A1.SELECTED DRAWING: Figure 4

Inventors:
Kenji Miyamoto
Kei Inoue
Katano Hikaru
Application Number:
JP2017090792A
Publication Date:
June 09, 2021
Filing Date:
April 28, 2017
Export Citation:
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Assignee:
Mitsubishi Power, Ltd.
International Classes:
F23R3/14; F23R3/28; F23R3/30; F23R3/32
Domestic Patent References:
JP2010223577A
JP2016061506A
JP2006336996A
Attorney, Agent or Firm:
Yasushi Matsunuma
Eisuke Ito
Hiroyuki Hashimoto
Satoshi Koto
Koichiro Kamata
Taichi Hasegawa
Ryuichiro Mori
Masatake Shiga
Tadashi Takahashi
Tetsuo Yamazaki



 
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