JPS5888565U - gas turbine combustor - Google Patents

gas turbine combustor

Info

Publication number
JPS5888565U
JPS5888565U JP18000981U JP18000981U JPS5888565U JP S5888565 U JPS5888565 U JP S5888565U JP 18000981 U JP18000981 U JP 18000981U JP 18000981 U JP18000981 U JP 18000981U JP S5888565 U JPS5888565 U JP S5888565U
Authority
JP
Japan
Prior art keywords
gas turbine
turbine combustor
primary air
combustor
air hole
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
JP18000981U
Other languages
Japanese (ja)
Inventor
「まん」代 重實
満 稲田
佐藤 亘男
Original Assignee
三菱重工業株式会社
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 by 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP18000981U priority Critical patent/JPS5888565U/en
Publication of JPS5888565U publication Critical patent/JPS5888565U/en
Pending legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

第1図は従来のガスタービン燃焼器部分の断面図、第2
図は第1図の燃料ノズル付近の断面図、および第3図は
本考案によるガスタービン燃焼器の燃料ノズル付近の断
面図である。 1・・・・・・ケーシング、2・・・・・・燃焼器、3
・・川・ディフューザ、4・・・・・・燃料ノズル、5
・・曲−次空気孔、6・・・・・・二次空気孔、7・・
・・・・希釈空気孔、8・・曲−次空気通路、9・・・
・・・案内筒。
Figure 1 is a sectional view of a conventional gas turbine combustor section;
These figures are a sectional view of the vicinity of the fuel nozzle in FIG. 1, and FIG. 3 is a sectional view of the vicinity of the fuel nozzle of the gas turbine combustor according to the present invention. 1...Casing, 2...Combustor, 3
...River diffuser, 4...Fuel nozzle, 5
... Curved air hole, 6... Secondary air hole, 7...
...Dilution air hole, 8...Curved air passage, 9...
...Guidance tube.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃料ノズルの外側で燃焼器側壁に設けられた一次空気孔
から一次空気通路を経て一次空気を供給されるガスター
ビン燃焼器において、前記−次空気孔の外側に均一な空
気流を得るための案内筒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 in which primary air is supplied through a primary air passage from a primary air hole provided in a side wall of the combustor outside a fuel nozzle, a guide for obtaining a uniform air flow outside the primary air hole. A gas turbine combustor characterized by having a cylinder.
JP18000981U 1981-12-04 1981-12-04 gas turbine combustor Pending JPS5888565U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18000981U JPS5888565U (en) 1981-12-04 1981-12-04 gas turbine combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18000981U JPS5888565U (en) 1981-12-04 1981-12-04 gas turbine combustor

Publications (1)

Publication Number Publication Date
JPS5888565U true JPS5888565U (en) 1983-06-15

Family

ID=29976216

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18000981U Pending JPS5888565U (en) 1981-12-04 1981-12-04 gas turbine combustor

Country Status (1)

Country Link
JP (1) JPS5888565U (en)

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