JPH0188157U - - Google Patents

Info

Publication number
JPH0188157U
JPH0188157U JP18434287U JP18434287U JPH0188157U JP H0188157 U JPH0188157 U JP H0188157U JP 18434287 U JP18434287 U JP 18434287U JP 18434287 U JP18434287 U JP 18434287U JP H0188157 U JPH0188157 U JP H0188157U
Authority
JP
Japan
Prior art keywords
combustor
gas turbine
fuel nozzle
steam injection
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
JP18434287U
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 JP18434287U priority Critical patent/JPH0188157U/ja
Publication of JPH0188157U publication Critical patent/JPH0188157U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案によるガスタービン用燃焼器の
一例を示す要部構造拡大断面図であり、第2図は
その水蒸気噴射によるNOx低減効果を示す図で
ある。第3図は従来のガスタービン用燃焼器を示
す概略断面図であり、第4図はその要部拡大断面
図であり、第5図はその他の例を示す要部拡大断
面図である。 1……燃料ノズル本体、2……燃料ノズル孔、
2′……混合孔、3……水蒸気噴射孔、3′……
水蒸気噴射流路。
FIG. 1 is an enlarged cross-sectional view of a main part structure of an example of a gas turbine combustor according to the present invention, and FIG. 2 is a diagram showing the NOx reduction effect of steam injection. FIG. 3 is a schematic sectional view showing a conventional gas turbine combustor, FIG. 4 is an enlarged sectional view of the main part thereof, and FIG. 5 is an enlarged sectional view of the main part showing another example. 1...Fuel nozzle body, 2...Fuel nozzle hole,
2'...Mixing hole, 3...Steam injection hole, 3'...
Steam injection channel.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃焼器内に水蒸気を噴射してNOx排出量を低
減するガスタービン用燃焼器において、水蒸気噴
射流路を水蒸気噴射孔を介して燃料ノズル本体に
開口した燃料ノズル孔の途中に接続する構造とし
たことを特徴とするガスタービン用燃焼器。
In a gas turbine combustor that injects steam into the combustor to reduce NOx emissions, the steam injection flow path is connected to the middle of a fuel nozzle hole that opens into the fuel nozzle body via a steam injection hole. A combustor for a gas turbine characterized by the following.
JP18434287U 1987-12-04 1987-12-04 Pending JPH0188157U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18434287U JPH0188157U (en) 1987-12-04 1987-12-04

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18434287U JPH0188157U (en) 1987-12-04 1987-12-04

Publications (1)

Publication Number Publication Date
JPH0188157U true JPH0188157U (en) 1989-06-09

Family

ID=31475713

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18434287U Pending JPH0188157U (en) 1987-12-04 1987-12-04

Country Status (1)

Country Link
JP (1) JPH0188157U (en)

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