JPS608432U - Multi-stage compression type gas turbine drive device - Google Patents

Multi-stage compression type gas turbine drive device

Info

Publication number
JPS608432U
JPS608432U JP1983100446U JP10044683U JPS608432U JP S608432 U JPS608432 U JP S608432U JP 1983100446 U JP1983100446 U JP 1983100446U JP 10044683 U JP10044683 U JP 10044683U JP S608432 U JPS608432 U JP S608432U
Authority
JP
Japan
Prior art keywords
gas turbine
compressors
drive device
stage compression
compression type
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
JP1983100446U
Other languages
Japanese (ja)
Inventor
赤木　功典
平野　茂樹
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.)
Osaka Gas Co Ltd
Original Assignee
Osaka Gas Co 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 Osaka Gas Co Ltd filed Critical Osaka Gas Co Ltd
Priority to JP1983100446U priority Critical patent/JPS608432U/en
Publication of JPS608432U publication Critical patent/JPS608432U/en
Pending legal-status Critical Current

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Control Of Positive-Displacement Air Blowers (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図は本考案の実施例を示すフローシートであり、第
２図は従来例のフローシートである。 ｌａ’、　　Ｉｂ、　　ｌｃ・・・・・・コンプレッサ
ー、２・・・・・・ガスタービン、３・・・・・・給気
路、４・・・・・・燃料ガス供給用流路、５・・・・・
・燃焼器、８・・・・・・発生器、９・・・・・・放熱
装置、１０・・・・・・凝縮器、１３・・・・・・蒸発
器、１４・・・・・・エジェクター。FIG. 1 is a flow sheet showing an embodiment of the present invention, and FIG. 2 is a flow sheet of a conventional example. la', Ib, lc... Compressor, 2... Gas turbine, 3... Air supply path, 4... Fuel gas supply flow path, 5・・・・・・
・Combustor, 8... Generator, 9... Heat dissipation device, 10... Condenser, 13... Evaporator, 14...・Ejector.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 酸素含有ガスを加圧供給するように直列に接続した複数
のコンプレッサーｌａ、ｌｂ、ｌｃを動力取出用ガスタ
ービン２に連動連結し、前記コンプレッサーｌａ、ｉｂ
、ｌｃ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にガス燃料を供給する流路４を
設け、前記ガスタービン２からの排気熱を熱源として前
記コンプレッサーｌａ、ｌｂ、ｌｃに供給される酸素含
有ガスを冷却する冷凍機を設けた多段圧縮型ガス？−ビ
ン式駆動装置であって、前記冷凍機を構成するに、前記
ガスタービン２からの排気熱により冷媒を気化させる発
生器８、及び、その発生器８からの冷媒蒸気を放熱装置
９により液化させる凝縮器１０を、冷媒が循環されるよ
うに接続すると共に、前記凝縮器１０からの冷媒の蒸発
により前記コンプレッサーのうち上流側のものｌａ、ｌ
ｂから下流側のものｌｂ、ｌｃに供給される酸素含有ガ
スを冷却する蒸発器１３、及び、その蒸発器１３からの
低圧冷媒蒸気を前記発生器８から凝縮器１０に供給され
る高圧冷媒蒸気により吸引させるエジェクター１４を設
けである多段圧縮型ガスタービン式駆動装置。A plurality of compressors la, lb, and lc connected in series so as to supply oxygen-containing gas under pressure are interlocked and connected to the power extraction gas turbine 2, and the compressors la, ib
, a combustor 5 in the air supply path 3 from the lc to the gas turbine 2.
, a flow path 4 for supplying gas fuel to the combustor 5 is provided, and refrigeration is used to cool the oxygen-containing gas supplied to the compressors la, lb, and lc using exhaust heat from the gas turbine 2 as a heat source. Multi-stage compression type gas with a machine? - A bottle-type drive device, which comprises a generator 8 that vaporizes a refrigerant using exhaust heat from the gas turbine 2, and a radiator 9 that liquefies the refrigerant vapor from the generator 8. A condenser 10 is connected so that the refrigerant is circulated, and the evaporation of the refrigerant from the condenser 10 causes the upstream compressors la, l
An evaporator 13 that cools the oxygen-containing gas supplied to downstream parts lb and lc from b, and a high-pressure refrigerant vapor that supplies low-pressure refrigerant vapor from the evaporator 13 to the condenser 10 from the generator 8. A multi-stage compression type gas turbine drive device is provided with an ejector 14 that sucks air.
JP1983100446U 1983-06-29 1983-06-29 Multi-stage compression type gas turbine drive device Pending JPS608432U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1983100446U JPS608432U (en) 1983-06-29 1983-06-29 Multi-stage compression type gas turbine drive device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1983100446U JPS608432U (en) 1983-06-29 1983-06-29 Multi-stage compression type gas turbine drive device

Publications (1)

Publication Number Publication Date
JPS608432U true JPS608432U (en) 1985-01-21

Family

ID=30237616

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1983100446U Pending JPS608432U (en) 1983-06-29 1983-06-29 Multi-stage compression type gas turbine drive device

Country Status (1)

Country Link
JP (1) JPS608432U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021524897A (en) * 2018-05-22 2021-09-16 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ Expanded gas turbine process with expander

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021524897A (en) * 2018-05-22 2021-09-16 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ Expanded gas turbine process with expander
US11492963B2 (en) 2018-05-22 2022-11-08 Siemens Energy Global GmbH & Co. KG Extended gas turbine process having an expander

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