燃料ノズルマニホルド

Japanese Patent JP5523859

B2

A fuel nozzle (100) manifold comprising a flange (102), a stem (103) and a swirler (130) is provided. The flange (102) has a first fluid inlet (171) fluidly connected to a radially extending first flow passage (186), the stem (103) includes at least a first axially extending and only partially circumferentially extending flow channel (181,182), and the swirler (130) has at least a first radially extending premix passage (176). The flange (102) and the stem (103) can comprise a homogeneous component, or two separate components fluidly connecting the first axially extending flow channel (188) to the first flow passage (154), to form a fluid connection between the flange (102) and the stem (103), the swirler (130) comprises another component fitted together with the flange (102) and stem (103) component and fluidly connecting the first premix passage (154) and the first flow channel (182).

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WO/2012/041906	BURNER FOR A GAS TURBINE
WO/2022/182853	HYDROGEN INJECTION FOR ENHANCED COMBUSTION STABILITY IN GAS TURBINE SYSTEMS

Stanley Kevin Widener
Scott Robert Simmons

JP2010024942A

June 18, 2014

February 08, 2010

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GENERAL ELECTRIC COMPANY

F23R3/28; F02C7/232; F23R3/14; F23R3/30

JP2008089298A
JP2008215646A
JP10160164A

US6898937

Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa

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