JPS593166U - Air bypass structure in gas turbine - Google Patents

Air bypass structure in gas turbine

Info

Publication number
JPS593166U
JPS593166U JP9434682U JP9434682U JPS593166U JP S593166 U JPS593166 U JP S593166U JP 9434682 U JP9434682 U JP 9434682U JP 9434682 U JP9434682 U JP 9434682U JP S593166 U JPS593166 U JP S593166U
Authority
JP
Japan
Prior art keywords
air bypass
gas turbine
bypass structure
pipe
turbine
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
JP9434682U
Other languages
Japanese (ja)
Other versions
JPS6143106Y2 (en
Inventor
重実 萬代
昌彦 森
池上 保彦
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP9434682U priority Critical patent/JPS593166U/en
Publication of JPS593166U publication Critical patent/JPS593166U/en
Application granted granted Critical
Publication of JPS6143106Y2 publication Critical patent/JPS6143106Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (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) [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 drawings]

第1図は従来のガスタービン燃焼器部を示す概略図、第
2図は本考案のガスタービン燃焼器部を示す概略図であ
る。 101.202・・・圧縮機、102,202・・・燃
焼器、103,203・・・尾筒、104,204・・
・タービン、105,205・・・空気バイパス管、1
06.206・・・バイパス弁、107,108゜10
9・・・バイパス管つけ根部、207・・・熱遮蔽管。
FIG. 1 is a schematic diagram showing a conventional gas turbine combustor section, and FIG. 2 is a schematic diagram showing a gas turbine combustor section according to the present invention. 101.202... Compressor, 102,202... Combustor, 103,203... Transition piece, 104,204...
・Turbine, 105, 205... Air bypass pipe, 1
06.206...Bypass valve, 107,108°10
9... Base of bypass pipe, 207... Heat shielding pipe.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 高温燃焼ガスを燃焼器からタービンまで導く間に、空気
バイパス管を設けたガスタービンにおいて、前記空気バ
イパス管内部に熱遮蔽管を設けたことを特徴とするガス
タービンにおける空気バイパス構造。
An air bypass structure for a gas turbine, characterized in that an air bypass pipe is provided while guiding high temperature combustion gas from the combustor to the turbine, and a heat shielding pipe is provided inside the air bypass pipe.
JP9434682U 1982-06-25 1982-06-25 Air bypass structure in gas turbine Granted JPS593166U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9434682U JPS593166U (en) 1982-06-25 1982-06-25 Air bypass structure in gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9434682U JPS593166U (en) 1982-06-25 1982-06-25 Air bypass structure in gas turbine

Publications (2)

Publication Number Publication Date
JPS593166U true JPS593166U (en) 1984-01-10
JPS6143106Y2 JPS6143106Y2 (en) 1986-12-05

Family

ID=30225875

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9434682U Granted JPS593166U (en) 1982-06-25 1982-06-25 Air bypass structure in gas turbine

Country Status (1)

Country Link
JP (1) JPS593166U (en)

Also Published As

Publication number Publication date
JPS6143106Y2 (en) 1986-12-05

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