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JPH0473706U - - Google Patents

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Publication number
JPH0473706U
JPH0473706U JP11216090U JP11216090U JPH0473706U JP H0473706 U JPH0473706 U JP H0473706U JP 11216090 U JP11216090 U JP 11216090U JP 11216090 U JP11216090 U JP 11216090U JP H0473706 U JPH0473706 U JP H0473706U
Authority
JP
Japan
Prior art keywords
gas turbine
spray nozzle
fuel
atomization type
slit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP11216090U
Other languages
Japanese (ja)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP11216090U priority Critical patent/JPH0473706U/ja
Publication of JPH0473706U publication Critical patent/JPH0473706U/ja
Pending legal-status Critical Current

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Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は考案の1実施例に係る気流微粒化式燃
料噴霧ノズルの基本構造図であり、第2図は第1
図の切断線A−Aに沿う本考案の断面図であり、
第3図は本考案のガスタービン環状型燃焼器への
適用例であり、第4図は気流微粒化式燃料噴霧ノ
ズルの基本構造図であり、第5図は第4図の切断
線C−Cに沿う従来型の断面図であり、第6図は
従来型のガスタービン環状型燃焼器への適用例で
ある。 1……ボデイ、2……ピントール、3……燃焼
器内筒、4……燃焼器外筒。
FIG. 1 is a basic structural diagram of an air flow atomization type fuel spray nozzle according to one embodiment of the invention, and FIG.
1 is a cross-sectional view of the present invention along section line A-A in the figure;
FIG. 3 shows an example of the application of the present invention to a gas turbine annular combustor, FIG. 4 is a basic structural diagram of an air flow atomization type fuel spray nozzle, and FIG. 5 is a section line C-- FIG. 6 is a cross-sectional view of the conventional type along line C, and FIG. 6 is an example of application to a conventional gas turbine annular combustor. 1...Body, 2...Pintor, 3...Combustor inner cylinder, 4...Combustor outer cylinder.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ガスタービンエンジンに用いられる気流微粒化
式燃料噴霧ノズルにおいて、燃料分布に偏流を持
たせるために燃料供給通路にスリツトを設けたこ
とを特徴とする気流微粒化式燃料噴霧ノズル。
An airflow atomization type fuel spray nozzle for use in a gas turbine engine, characterized in that a slit is provided in a fuel supply passage in order to provide uneven fuel distribution.
JP11216090U 1990-10-29 1990-10-29 Pending JPH0473706U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11216090U JPH0473706U (en) 1990-10-29 1990-10-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11216090U JPH0473706U (en) 1990-10-29 1990-10-29

Publications (1)

Publication Number Publication Date
JPH0473706U true JPH0473706U (en) 1992-06-29

Family

ID=31859661

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11216090U Pending JPH0473706U (en) 1990-10-29 1990-10-29

Country Status (1)

Country Link
JP (1) JPH0473706U (en)

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