JPS61166142U - - Google Patents

Info

Publication number
JPS61166142U
JPS61166142U JP4981385U JP4981385U JPS61166142U JP S61166142 U JPS61166142 U JP S61166142U JP 4981385 U JP4981385 U JP 4981385U JP 4981385 U JP4981385 U JP 4981385U JP S61166142 U JPS61166142 U JP S61166142U
Authority
JP
Japan
Prior art keywords
passage
compressor
auxiliary
turbine
gas 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
JP4981385U
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 JP4981385U priority Critical patent/JPS61166142U/ja
Publication of JPS61166142U publication Critical patent/JPS61166142U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案の実施例を示すフローシート、
第2図に従来例のフローシートである。 1……コンプレツサー、2……ガスタービン、
3……給気路、4……燃料供給用流路、5……燃
焼器、6……排気路、7……アフターバーナ、8
……燃焼用酸素含有ガス供給路、11……分岐路
、12……補助タービン、13……補助コンプレ
ツサー。
FIG. 1 is a flow sheet showing an example of the present invention.
FIG. 2 is a flow sheet of a conventional example. 1...Compressor, 2...Gas turbine,
3...Air supply path, 4...Fuel supply flow path, 5...Combustor, 6...Exhaust path, 7...Afterburner, 8
... Oxygen-containing gas supply path for combustion, 11 ... Branch path, 12 ... Auxiliary turbine, 13 ... Auxiliary compressor.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 空気を加圧供給するコンプレツサー1をガスタ
ービン2に連動連結し、前記コンプレツサー1か
ら前記ガスタービン2への給気路3に燃焼器5を
介装し、前記燃焼器5に燃料を供給する流路4を
設け、前記ガスタービン2からの排気路6をアフ
ターバーナ7の燃焼用酸素含有ガス供給路8に接
続した熱風発生装置であつて、前記排気路6に接
続した分岐路11に補助タービン12を設け、前
記アフターバーナ7に燃焼用空気を加圧供給する
補助コンプレツサー13を、前記補助タービン1
2に連動連結してある熱風発生装置。
A compressor 1 that supplies pressurized air is interlocked and connected to a gas turbine 2, a combustor 5 is interposed in an air supply path 3 from the compressor 1 to the gas turbine 2, and a flow is provided that supplies fuel to the combustor 5. A hot air generator is provided with a passage 4 and an exhaust passage 6 from the gas turbine 2 is connected to a combustion oxygen-containing gas supply passage 8 of an afterburner 7, and an auxiliary turbine is connected to a branch passage 11 connected to the exhaust passage 6. 12, and an auxiliary compressor 13 for supplying combustion air under pressure to the afterburner 7 is connected to the auxiliary turbine 1.
A hot air generator that is interlocked with 2.
JP4981385U 1985-04-03 1985-04-03 Pending JPS61166142U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4981385U JPS61166142U (en) 1985-04-03 1985-04-03

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4981385U JPS61166142U (en) 1985-04-03 1985-04-03

Publications (1)

Publication Number Publication Date
JPS61166142U true JPS61166142U (en) 1986-10-15

Family

ID=30567352

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4981385U Pending JPS61166142U (en) 1985-04-03 1985-04-03

Country Status (1)

Country Link
JP (1) JPS61166142U (en)

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