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JPS5886441U - Intake precooling gas turbine - Google Patents

Intake precooling gas turbine

Info

Publication number
JPS5886441U
JPS5886441U JP18103581U JP18103581U JPS5886441U JP S5886441 U JPS5886441 U JP S5886441U JP 18103581 U JP18103581 U JP 18103581U JP 18103581 U JP18103581 U JP 18103581U JP S5886441 U JPS5886441 U JP S5886441U
Authority
JP
Japan
Prior art keywords
heat medium
intermediate heat
gas turbine
intake air
heat exchanger
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
JP18103581U
Other languages
Japanese (ja)
Other versions
JPS6137794Y2 (en
Inventor
角谷 修二
畔蒜 鏡一郎
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 JP18103581U priority Critical patent/JPS5886441U/en
Publication of JPS5886441U publication Critical patent/JPS5886441U/en
Application granted granted Critical
Publication of JPS6137794Y2 publication Critical patent/JPS6137794Y2/ja
Granted legal-status Critical Current

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  • Engine Equipment That Uses Special Cycles (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図はガスタービンに於ける吸気温度と出力の関係を
示す特性図、第2図は本考案に係る吸気予冷ガスタービ
ンの一実施例を示す系統図、第3図は本考案の作用を説
明するために示した大気温度と直触式吸気予冷熱交換器
の出口吸気温度との関係を示した特性図、第4図は本考
案の効果を説明するために示した大気温度とガスタービ
ン出力との関係を示した特性図である。 1・・・・・・ガスタービン、2・・・・・・負荷、4
・・・・・・直触式吸気予冷熱交換器、5・・・・・・
中間熱媒体熱交換器、6.7・・・・・・ポンプ、8.
9・・・・・・管路、11.i2゜13.15・・・・
・・弁、11・・・・・・ブライン再生器。 第1図 第3図
Fig. 1 is a characteristic diagram showing the relationship between intake air temperature and output in a gas turbine, Fig. 2 is a system diagram showing an embodiment of the intake air precooling gas turbine according to the present invention, and Fig. 3 is a diagram showing the operation of the present invention. A characteristic diagram showing the relationship between the atmospheric temperature and the outlet air temperature of the direct-contact intake air precooling heat exchanger is shown for the purpose of explanation. FIG. 3 is a characteristic diagram showing the relationship with output. 1...Gas turbine, 2...Load, 4
・・・・・・Direct contact type intake air precooling heat exchanger, 5・・・・・・
Intermediate heat medium heat exchanger, 6.7... Pump, 8.
9...Pipe line, 11. i2゜13.15...
...Valve, 11...Brine regenerator. Figure 1 Figure 3

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ガスタービンと、このガスタービンの吸気ヲ予め冷却す
るための吸気を中間熱媒体に直接接触させて所定温度に
冷却する直触式吸気予冷熱交換器と、この熱交換器にて
加熱された前記中間熱媒体を冷却する中間熱媒体熱交換
器と、この中間熱媒体熱交換器と前記直触式吸気子冷熱
交換器との間に前記中間熱媒体を循環させる循環系と、
この循環系に大気条件に応じて異種の中間熱媒体を導入
するかもしくは中間熱媒体の濃度を調整するようにした
中間熱媒体加換調整回路とを具備することを特徴とする
吸気予冷ガスタービン。
A gas turbine, a direct contact type intake air precooling heat exchanger for precooling the intake air of the gas turbine, which cools the intake air to a predetermined temperature by bringing the intake air into direct contact with an intermediate heat medium, and the intake air heated by the heat exchanger. an intermediate heat medium heat exchanger that cools the intermediate heat medium; a circulation system that circulates the intermediate heat medium between the intermediate heat medium heat exchanger and the direct contact type inlet cold heat exchanger;
An intake precooling gas turbine characterized in that the circulation system is equipped with an intermediate heat medium exchange and adjustment circuit that introduces different types of intermediate heat medium or adjusts the concentration of the intermediate heat medium depending on atmospheric conditions. .
JP18103581U 1981-12-07 1981-12-07 Intake precooling gas turbine Granted JPS5886441U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18103581U JPS5886441U (en) 1981-12-07 1981-12-07 Intake precooling gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18103581U JPS5886441U (en) 1981-12-07 1981-12-07 Intake precooling gas turbine

Publications (2)

Publication Number Publication Date
JPS5886441U true JPS5886441U (en) 1983-06-11
JPS6137794Y2 JPS6137794Y2 (en) 1986-11-01

Family

ID=29978159

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18103581U Granted JPS5886441U (en) 1981-12-07 1981-12-07 Intake precooling gas turbine

Country Status (1)

Country Link
JP (1) JPS5886441U (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2382847A (en) 2001-12-06 2003-06-11 Alstom Gas turbine wet compression
GB2382848A (en) 2001-12-06 2003-06-11 Alstom Gas turbine wet compression
DE10256193A1 (en) 2002-12-02 2004-06-09 Alstom Technology Ltd Method for controlling the liquid injection into an inflow channel of an engine or machine

Also Published As

Publication number Publication date
JPS6137794Y2 (en) 1986-11-01

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