JPS59108054U - Fuel/air premixing device - Google Patents

Fuel/air premixing device

Info

Publication number
JPS59108054U
JPS59108054U JP27283U JP27283U JPS59108054U JP S59108054 U JPS59108054 U JP S59108054U JP 27283 U JP27283 U JP 27283U JP 27283 U JP27283 U JP 27283U JP S59108054 U JPS59108054 U JP S59108054U
Authority
JP
Japan
Prior art keywords
fuel
premixing
air
flow path
premixing device
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
JP27283U
Other languages
Japanese (ja)
Inventor
松井宏
Original Assignee
株式会社東芝
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 株式会社東芝 filed Critical 株式会社東芝
Priority to JP27283U priority Critical patent/JPS59108054U/en
Publication of JPS59108054U publication Critical patent/JPS59108054U/en
Pending legal-status Critical Current

Links

Landscapes

  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

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) [Abstract] 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図は従来におけるガス燃料ノズルの構造を示す断面
図、第2図は第1図における■−■線断面図、第3図は
この考案の一実施例を示す半裁断面図、第4図は第3図
におけるIV−IV線断面図である。 1・・・ガス燃料供給管、2・・・取付フランジ、3・
・・予混合管、4・・・ガス燃料流路、5・・・内側管
壁、6・・・外側管壁、7・・・予混合流路、8・・・
空気取入口、9・・・供給口、10・・・旋回器、11
・・・狭隘部、12・・・燃料噴射孔、13・・・入口
旋回羽根、A・・・燃焼用空気、G・・・ガス燃料、F
・・・予混合気、101・・・旋回器、102・・・取
付フランジ、103・・・嵌合部、104・・・ガス燃
料供給管、105・・・ガス燃料噴射孔、106・・・
旋回羽根、107・・・旋回器内輪、108・・・旋回
器外輪、110・・・ガス燃料、111・・・燃料、1
12・・・燃焼用空気、113・・・燃料・空気混合気
Fig. 1 is a sectional view showing the structure of a conventional gas fuel nozzle, Fig. 2 is a sectional view taken along the line ■-■ in Fig. 1, Fig. 3 is a half-cut sectional view showing an embodiment of this invention, and Fig. 4 is a sectional view taken along the line IV-IV in FIG. 3. 1... Gas fuel supply pipe, 2... Mounting flange, 3...
... Premixing tube, 4... Gas fuel channel, 5... Inner tube wall, 6... Outer tube wall, 7... Premixing channel, 8...
Air intake port, 9... Supply port, 10... Swirl device, 11
...Narrow part, 12...Fuel injection hole, 13...Inlet swirl vane, A...Combustion air, G...Gas fuel, F
... Premixture, 101 ... Swirl device, 102 ... Mounting flange, 103 ... Fitting part, 104 ... Gas fuel supply pipe, 105 ... Gas fuel injection hole, 106 ...・
Swirling vane, 107...Swivel inner ring, 108...Swivel outer ring, 110...Gas fuel, 111...Fuel, 1
12... Combustion air, 113... Fuel/air mixture.

Claims (1)

【実用新案登録請求の範囲】 1 燃料供給管に連通ずる燃料流路の外周に、環状に形
成された空気取入口を後部に、所定のガスタービン燃焼
器へ連通ずる混合気供給口を前部に有する予混合管の予
混合流路を区画形成して二重管構造となし、予混合流路
自体の環状半径または流量面積を縮小することで狭隘部
を予混合流路の中途に形成し、この狭隘部またはその近
傍の燃料流路周囲に燃料噴射孔を開穿配列したことを特
徴とする燃料・空気予混合装置。 2 取入れる空気に旋回速度成分を与える入口旋回羽根
を空気取入口に列設した実用新案登録請求の範囲第1項
記載の燃料・空気予混合装置。 3 燃料噴射孔から混合気供給口までの距離を長くした
実用新案登録請求の範囲第1項記載の燃料・空気予混合
装置。 4 予混合管流路壁面が流線形状になっている実用新案
登録請求の範囲第1項記載の燃料・空気予混合装置。
[Claims for Utility Model Registration] 1. An annularly formed air intake port on the outer periphery of the fuel flow path communicating with the fuel supply pipe at the rear, and a mixture supply port communicating with a predetermined gas turbine combustor at the front. The premixing channel of the premixing tube in the premixing tube is divided into a double pipe structure, and a narrow part is formed in the middle of the premixing channel by reducing the annular radius or flow area of the premixing channel itself. A fuel/air premixing device characterized in that fuel injection holes are arranged around the fuel flow path in or near the narrow portion. 2. The fuel/air premixing device according to claim 1, wherein inlet swirl vanes are arranged in the air intake port to give a swirling speed component to the air taken in. 3. The fuel/air premixing device according to claim 1, in which the distance from the fuel injection hole to the mixture supply port is increased. 4. The fuel/air premixing device according to claim 1, wherein the wall surface of the premixing tube flow path has a streamlined shape.
JP27283U 1983-01-07 1983-01-07 Fuel/air premixing device Pending JPS59108054U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP27283U JPS59108054U (en) 1983-01-07 1983-01-07 Fuel/air premixing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP27283U JPS59108054U (en) 1983-01-07 1983-01-07 Fuel/air premixing device

Publications (1)

Publication Number Publication Date
JPS59108054U true JPS59108054U (en) 1984-07-20

Family

ID=30132033

Family Applications (1)

Application Number Title Priority Date Filing Date
JP27283U Pending JPS59108054U (en) 1983-01-07 1983-01-07 Fuel/air premixing device

Country Status (1)

Country Link
JP (1) JPS59108054U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014115072A (en) * 2012-12-05 2014-06-26 General Electric Co <Ge> Fuel nozzle for combustor of gas turbine engine
JP2021169913A (en) * 2020-04-15 2021-10-28 マーベル−テック・リミテッド Combustion device of gas turbine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014115072A (en) * 2012-12-05 2014-06-26 General Electric Co <Ge> Fuel nozzle for combustor of gas turbine engine
JP2021169913A (en) * 2020-04-15 2021-10-28 マーベル−テック・リミテッド Combustion device of gas turbine

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