JPS58144038U - Gas turbine fuel combustion equipment - Google Patents

Gas turbine fuel combustion equipment

Info

Publication number
JPS58144038U
JPS58144038U JP4100282U JP4100282U JPS58144038U JP S58144038 U JPS58144038 U JP S58144038U JP 4100282 U JP4100282 U JP 4100282U JP 4100282 U JP4100282 U JP 4100282U JP S58144038 U JPS58144038 U JP S58144038U
Authority
JP
Japan
Prior art keywords
gas turbine
fuel combustion
turbine fuel
combustion equipment
combustion
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.)
Granted
Application number
JP4100282U
Other languages
Japanese (ja)
Other versions
JPS6311491Y2 (en
Inventor
重實 萬代
満 稲田
佐藤　亘男
五良　哲雄
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 JP4100282U priority Critical patent/JPS58144038U/en
Publication of JPS58144038U publication Critical patent/JPS58144038U/en
Application granted granted Critical
Publication of JPS6311491Y2 publication Critical patent/JPS6311491Y2/ja
Granted legal-status Critical Current

Links

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の燃料燃焼装置を示す縦断
側面図、第２図は本案のガスタービンの　。 燃料燃焼装置の一実施例を示す縦断側面図、第３図はバ
イパス空気孔の不適例を示す説明図である。 ３・・・燃焼器内筒、５・・・尾筒、’５ａ・・・！曲
部外側、７・・・バイパス空気孔、Ａ・・・バイパス空
気、Ｂ・・・燃焼ガス流。FIG. 1 is a vertical side view showing a conventional gas turbine fuel combustion device, and FIG. 2 is a diagram of the proposed gas turbine. FIG. 3 is a longitudinal sectional side view showing one embodiment of the fuel combustion device, and is an explanatory diagram showing an example of an unsuitable bypass air hole. 3... Combustor inner cylinder, 5... Tail piece, '5a...! Outside the curved portion, 7... Bypass air hole, A... Bypass air, B... Combustion gas flow.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃焼器内筒へ供給した燃料をそこに供給した燃焼用空気
により燃焼させて高温の燃焼ガスとしたのち、尾筒を経
てガスタービンへ導くガスタービンの燃料燃焼装置にお
いて、前記尾筒内を流れる燃焼ガス流に対してバイパス
空気を鋭角で流入させるバイパス空気孔を前記尾筒の彎
曲部外側に設けたことを特徴とするガスタービンの燃料
燃焼装置。In a gas turbine fuel combustion device, the fuel supplied to the combustor inner cylinder is combusted by the combustion air supplied there to produce high-temperature combustion gas, which is then guided to the gas turbine via the transition piece. A fuel combustion device for a gas turbine, characterized in that a bypass air hole for allowing bypass air to flow in at an acute angle with respect to the combustion gas flow is provided on the outside of the curved portion of the transition piece.
JP4100282U 1982-03-25 1982-03-25 Gas turbine fuel combustion equipment Granted JPS58144038U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4100282U JPS58144038U (en) 1982-03-25 1982-03-25 Gas turbine fuel combustion equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4100282U JPS58144038U (en) 1982-03-25 1982-03-25 Gas turbine fuel combustion equipment

Publications (2)

Publication Number Publication Date
JPS58144038U true JPS58144038U (en) 1983-09-28
JPS6311491Y2 JPS6311491Y2 (en) 1988-04-04

Family

ID=30052198

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4100282U Granted JPS58144038U (en) 1982-03-25 1982-03-25 Gas turbine fuel combustion equipment

Country Status (1)

Country Link
JP (1) JPS58144038U (en)

Also Published As

Publication number Publication date
JPS6311491Y2 (en) 1988-04-04

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