JPS63162938U - - Google Patents

Info

Publication number
JPS63162938U
JPS63162938U JP5473487U JP5473487U JPS63162938U JP S63162938 U JPS63162938 U JP S63162938U JP 5473487 U JP5473487 U JP 5473487U JP 5473487 U JP5473487 U JP 5473487U JP S63162938 U JPS63162938 U JP S63162938U
Authority
JP
Japan
Prior art keywords
gas turbine
temperature reducing
gas
reducing device
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.)
Pending
Application number
JP5473487U
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 JP5473487U priority Critical patent/JPS63162938U/ja
Publication of JPS63162938U publication Critical patent/JPS63162938U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Temperature (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Description

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

単一の図は、本考案によるガスタービンの回転
数制御装置の一例を示す系統図である。 1……ガスタービン、2……コンプレツサ、3
……燃焼器、4……燃焼用空気供給ライン、5…
…タービン駆動ガス供給ライン、6……ガス放出
ライン、7……放風弁、8……減温装置、9……
冷却流体供給ライン、10……流量調節器。
A single figure is a system diagram showing an example of a gas turbine rotation speed control device according to the present invention. 1...Gas turbine, 2...Compressor, 3
...Combustor, 4...Combustion air supply line, 5...
... Turbine drive gas supply line, 6 ... Gas discharge line, 7 ... Air discharge valve, 8 ... Temperature reduction device, 9 ...
Cooling fluid supply line, 10...Flow rate regulator.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃焼器からのタービン駆動ガスをガスタービン
へ送るラインの途中に減温装置を設けるとともに
、ガスタービンの回転数変動に応じてこの減温装
置への冷却流体供給量を調節する手段を設けたこ
とを特徴とするガスタービンの回転数制御装置。
A temperature reducing device is provided in the middle of the line that sends the turbine drive gas from the combustor to the gas turbine, and a means is provided to adjust the amount of cooling fluid supplied to the temperature reducing device in accordance with fluctuations in the rotational speed of the gas turbine. A gas turbine rotation speed control device featuring:
JP5473487U 1987-04-13 1987-04-13 Pending JPS63162938U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5473487U JPS63162938U (en) 1987-04-13 1987-04-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5473487U JPS63162938U (en) 1987-04-13 1987-04-13

Publications (1)

Publication Number Publication Date
JPS63162938U true JPS63162938U (en) 1988-10-25

Family

ID=30881998

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5473487U Pending JPS63162938U (en) 1987-04-13 1987-04-13

Country Status (1)

Country Link
JP (1) JPS63162938U (en)

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