JPH02133554U - - Google Patents

Info

Publication number
JPH02133554U
JPH02133554U JP3796589U JP3796589U JPH02133554U JP H02133554 U JPH02133554 U JP H02133554U JP 3796589 U JP3796589 U JP 3796589U JP 3796589 U JP3796589 U JP 3796589U JP H02133554 U JPH02133554 U JP H02133554U
Authority
JP
Japan
Prior art keywords
gas turbine
swirler
primary air
combustor
turbine combustor
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
JP3796589U
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 JP3796589U priority Critical patent/JPH02133554U/ja
Publication of JPH02133554U publication Critical patent/JPH02133554U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案によるガスタービン燃焼器の一
例を示す要部の断面図、第2図は従来例を示す図
である。 1……燃料ノズル、2……燃焼器内筒、6……
一次空気流路、7……スワラ、8……内筒支え、
9……一次空気孔、10……二次空気孔、11…
…ノズル冷却空気孔、21……水噴射手段、22
……水供給管、23……水マニホルド管、24…
…水噴射管。
FIG. 1 is a sectional view of essential parts of an example of a gas turbine combustor according to the present invention, and FIG. 2 is a diagram showing a conventional example. 1...Fuel nozzle, 2...Combustor inner cylinder, 6...
Primary air flow path, 7... swirler, 8... inner cylinder support,
9...Primary air hole, 10...Secondary air hole, 11...
... Nozzle cooling air hole, 21 ... Water injection means, 22
...Water supply pipe, 23...Water manifold pipe, 24...
...Water injection tube.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃料ノズルの外周に配設した一次空気流路の先
端にスワラを設け、このスワラを通して一次空気
を燃焼器内へ供給するガスタービン燃焼器におい
て、前記スワラの上流側における一次空気流路の
壁面に向つて水を噴射する水噴射手段を設けたこ
とを特徴とするガスタービン燃焼器。
In a gas turbine combustor, a swirler is provided at the tip of a primary air flow path disposed around the outer periphery of the fuel nozzle, and primary air is supplied into the combustor through this swirler. A gas turbine combustor characterized in that it is provided with a water injection means for injecting water toward the gas turbine.
JP3796589U 1989-04-03 1989-04-03 Pending JPH02133554U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3796589U JPH02133554U (en) 1989-04-03 1989-04-03

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3796589U JPH02133554U (en) 1989-04-03 1989-04-03

Publications (1)

Publication Number Publication Date
JPH02133554U true JPH02133554U (en) 1990-11-06

Family

ID=31545549

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3796589U Pending JPH02133554U (en) 1989-04-03 1989-04-03

Country Status (1)

Country Link
JP (1) JPH02133554U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009069426A1 (en) * 2007-11-29 2009-06-04 Mitsubishi Heavy Industries, Ltd. Combustion burner

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009069426A1 (en) * 2007-11-29 2009-06-04 Mitsubishi Heavy Industries, Ltd. Combustion burner
JP2009133517A (en) * 2007-11-29 2009-06-18 Mitsubishi Heavy Ind Ltd Combustion burner
US8656699B2 (en) 2007-11-29 2014-02-25 Mitsubishi Heavy Industries, Ltd. Combustion burner
US8820047B2 (en) 2007-11-29 2014-09-02 Mitsubishi Heavy Industries, Ltd. Combustion burner
US9562688B2 (en) 2007-11-29 2017-02-07 Mitsubishi Hitachi Power Systems, Ltd. Cooling unit for cooling swirler vane of combustion burner
US9593852B2 (en) 2007-11-29 2017-03-14 Mitsubishi Hitachi Power Systems, Ltd. Cooling unit cooling swirler vane of combustion burner

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