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JPS61171833A - Cooling system for gas turbine and generator - Google Patents

Cooling system for gas turbine and generator

Info

Publication number
JPS61171833A
JPS61171833A JP1077085A JP1077085A JPS61171833A JP S61171833 A JPS61171833 A JP S61171833A JP 1077085 A JP1077085 A JP 1077085A JP 1077085 A JP1077085 A JP 1077085A JP S61171833 A JPS61171833 A JP S61171833A
Authority
JP
Japan
Prior art keywords
cooling
gas turbine
generator
heat exchanger
temperature
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
JP1077085A
Other languages
Japanese (ja)
Inventor
Kazuhiro Kurosawa
一浩 黒澤
Ko Yaginuma
柳沼 效
Akihide Aoki
青木 あきら秀
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.)
Hitachi Ltd
Hitachi Industry and Control Solutions Co Ltd
Original Assignee
Hitachi Engineering Co Ltd
Hitachi 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 Hitachi Engineering Co Ltd, Hitachi Ltd filed Critical Hitachi Engineering Co Ltd
Priority to JP1077085A priority Critical patent/JPS61171833A/en
Publication of JPS61171833A publication Critical patent/JPS61171833A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To permit the black start of a gas turbine by connecting a starting cooler and a cooler in parallel and connecting an emergency cooler on the downstream in series. CONSTITUTION:A starting cooler 1 and a cooler 2 are arranged in parallel, and an emergency cooler 3 is connected in series on the downstream. While, a cooling-water circulation pump 6 driven by a gas turbine through an auxiliary gear 11 and an emergency cooling-water pump 7 controlled by a cooling-water temperature controller 13 are connected in parallel. On starting, the cooling- water circulation pump 6 is driven to cool heat exchangers 8 and 9, and then the starting cooler 1 is started. When the outside air temperature is high, the emergency cooler 3 is started. Thus, the black start of the gas turbine is permitted.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は、ガスタービン及び発電機への冷却水供給装置
に係り、特に密閉冷却を適用するガスタ−ビン発電機に
おいて、起動及び冷却水の安定供給に優れたように改良
したガスタービン及び発電機の冷却水系統に関するもの
である。
DETAILED DESCRIPTION OF THE INVENTION [Field of Application of the Invention] The present invention relates to a cooling water supply system for a gas turbine and a generator, and in particular, in a gas turbine generator to which sealed cooling is applied, it is possible to improve the startup and stability of cooling water. This invention relates to a cooling water system for a gas turbine and generator that has been improved to provide superior water supply.

〔発明の背景〕[Background of the invention]

ガスタービン冷却水循環装置として、例えば特開昭53
−65517号公報に示される様に、冷却水系統内に新
たに熱交換器が追加となった場合ガスタービンの軸駆動
ラジェターファンにより冷却するラジェターに加え、モ
ータ駆動ラジェターファンを備えるラジェターを別置し
て対処していた。しかし、このようにガスタービン単独
の冷却水系統を設けた構造にすると、発電機が密閉式冷
却形である場合はガスタービンの冷却系統と別系統の冷
却系統を設けなければならず、このため外部電源の供給
を受けないで始動すること(以下、ブラックスタートと
言う)が出来ない、また、ガスタービンを屋内に設置し
た場合は該ガスタービンパッケージ内にラジェータを設
置することが極めて困難である(強いて設置しようとす
ると冷却空気取入用のドラフトや排気煙突を設けなけれ
ば屋内温度を過熱させる)。
As a gas turbine cooling water circulation system, for example, JP-A-53
As shown in Publication No. 65517, when a new heat exchanger is added to the cooling water system, in addition to the radiator that is cooled by the shaft-driven radiator fan of the gas turbine, a radiator equipped with a motor-driven radiator fan is installed separately. I was dealing with it. However, if the structure is such that a cooling water system is provided for the gas turbine alone, if the generator is a closed cooling type, a cooling system separate from the gas turbine cooling system must be installed. It is impossible to start without receiving an external power supply (hereinafter referred to as a black start), and if the gas turbine is installed indoors, it is extremely difficult to install a radiator inside the gas turbine package. (If you try to install it forcibly, it will cause the indoor temperature to overheat unless you provide a draft for cooling air intake or an exhaust chimney.)

ガスタービン発電機潤滑油クーラーへ供給される冷却水
は温度制御が行なわれていないため、外気温が低い場合
クーラー人口の冷却水がかなり低温となるので、温度調
節弁に不具合を生じたときガスタービン発電機潤滑油が
過冷却となる。温度調節弁が正常に作動すれば上記の過
冷却は回避されるが、潤滑油の過冷却は重大事故を誘発
するので、温度調節弁のみに頼ることは好ましくなく。
The temperature of the cooling water supplied to the gas turbine generator lubricating oil cooler is not controlled, so if the outside temperature is low, the cooling water in the cooler will be quite low, so if a malfunction occurs in the temperature control valve, the gas Turbine generator lubricating oil becomes supercooled. If the temperature control valve operates normally, the above-mentioned overcooling can be avoided, but since overcooling of the lubricating oil can cause a serious accident, it is not preferable to rely solely on the temperature control valve.

2重、3重の安全措置を講じなければならない。Double and triple safety measures must be taken.

〔発明の目的〕[Purpose of the invention]

本発明の目的は、密閉冷却を適用するガスタービン発電
機において、ブラックスタート(外部電源によらない起
動)を可能とし、冷却水の安定供給に優れ、特に、温度
調節弁のみに頼ることなくタービン発電機潤滑油の過熱
、過冷却を生じる虞れの無いガスタービン及び発電機の
冷却系統を提ヶt a = h i=あう、     
         裏〔発明の概要〕 前記の目的を達成する為に創作した本発明の冷却系統に
ついて、先ず、その基本的原理を説明すると次の如くで
ある。
An object of the present invention is to enable a black start (starting without using an external power source) in a gas turbine generator to which sealed cooling is applied, to provide an excellent stable supply of cooling water, and in particular to provide a gas turbine generator that does not rely solely on a temperature control valve. The cooling system for the gas turbine and generator shall be installed without the risk of overheating or overcooling of the generator lubricating oil.
Back [Summary of the Invention] First, the basic principle of the cooling system of the present invention created to achieve the above object will be explained as follows.

従来の冷却水系統は、ガスタービン発電機の潤滑油冷却
系統と発電機固定子冷却系統と2系列となっており、ガ
スタービン発電機の潤滑油冷却系統は冷却水循環ポンプ
がタービン軸から補機歯車を介して駆動され、さらにラ
ジェータファンもまたタービン軸により駆動され、これ
によって冷却水を冷却していた。また、別置式ラジェー
タを用いる場合はタービン軸駆動のファンに代えて低電
圧起動モータ駆動ファン(発電機が回転を開始するのと
同時に低回転から負荷を取り始め、低電圧電気でモータ
を起動する事、)の設置でブラックスタートに対応して
いた。ガスタービン発電機の潤滑油冷却は上記のように
してブラックスタートを可能にできるが1発電機固定子
冷却系統はこれと別個に冷却水循環ポンプ及びラジェー
タを設けなければならないためブラックスタートが困難
である。
The conventional cooling water system consists of two systems: the gas turbine generator's lubricating oil cooling system and the generator stator cooling system. Driven through gears, the radiator fan was also driven by the turbine shaft, thereby cooling the cooling water. In addition, when using a separate radiator, instead of a turbine shaft-driven fan, a low-voltage startup motor-driven fan (starts to take the load from low rotation at the same time as the generator starts rotating, and starts the motor with low-voltage electricity. ) was installed to support black start. Lubricating oil cooling for gas turbine generators can enable a black start as described above, but a black start is difficult because the generator stator cooling system requires a separate cooling water circulation pump and radiator. .

ここで、本発明者らは次の事情に着目した。Here, the present inventors paid attention to the following circumstances.

発電機固定子の冷却に必要な冷却水温の最高値とガスタ
ービン発電機潤滑油の冷却に必要な冷却水温の最高値に
はひらきがあり、前者は約50℃後者は約60℃となっ
ている。つまり1発電機固定子冷却用熱交換器を通り抜
けた後の冷却水をガスタービン発電機潤滑油冷却用熱交
換器に使用しても十分潤滑油を冷却できる。
There is a difference between the maximum cooling water temperature required to cool the generator stator and the maximum cooling water temperature required to cool the gas turbine generator lubricating oil, with the former being approximately 50°C and the latter being approximately 60°C. There is. In other words, the lubricating oil can be sufficiently cooled even if the cooling water that has passed through the heat exchanger for cooling the stator of one generator is used in the heat exchanger for cooling the lubricating oil of the gas turbine generator.

そこで本発明者らは両者を直列に接続する事により冷却
水循環水量を従来潤滑油の冷却に使用していた場合と比
べほぼ同量とし、従来の潤滑油冷却系統を流用しガスタ
ービン及び発電機の冷却を行ない、前述の問題を解決し
たものである。
Therefore, the inventors of the present invention connected the two systems in series, thereby making the amount of circulating water almost the same as when conventionally used for cooling lubricating oil. This solves the above-mentioned problem.

上記の原理に基づいて前記の目的を達成するため、本発
明のガスタービン及び発電機の冷却系統は、冷却装置に
よって冷却媒体を冷却し、上記の冷却された冷却媒体を
圧送してガスタービン及び発電機に循環せしめる冷却系
統において、複数の冷却装置を並列に配管接続し、上記
複数の冷却装置の下流側に前記と異なる冷却装置を直列
に接続配管し、かつ、前記の冷却媒体を循環せしめる為
の圧送手段はガスタービンによって歯車伝動手段を介し
て定常的に駆動される主ポンプと、外気温が所定値以上
となったとき自動的に運転される非常用補助ポンプとを
備えたものであることを特徴とする。
In order to achieve the above object based on the above principle, the cooling system for a gas turbine and a generator of the present invention cools a cooling medium by a cooling device, and pumps the cooled cooling medium to the gas turbine and the generator. In a cooling system that circulates through a generator, a plurality of cooling devices are connected in parallel via piping, a cooling device different from the above is connected in series downstream of the plurality of cooling devices, and the cooling medium is circulated. The pumping means for this purpose consists of a main pump that is constantly driven by a gas turbine via a gear transmission means, and an emergency auxiliary pump that is automatically operated when the outside temperature exceeds a predetermined value. characterized by something.

〔発明の実施例〕[Embodiments of the invention]

次に1本発明の一実施例を第1図について説明する。 Next, an embodiment of the present invention will be described with reference to FIG.

起動用冷却装置1と冷却装置2とを並列に接続し、その
下流側に非常用冷却装置3を直列に接続する。
The startup cooling device 1 and the cooling device 2 are connected in parallel, and the emergency cooling device 3 is connected in series on the downstream side thereof.

一方、補機歯車11を介してガスタービンによって駆動
される冷却水循環ポンプ6と、冷却水温度制御装置13
によって制御される非常用冷却水ポンプ7とを並列に接
続する。
On the other hand, a cooling water circulation pump 6 driven by a gas turbine via an auxiliary gear 11 and a cooling water temperature control device 13
and an emergency cooling water pump 7 controlled by the system.

前記の非常用冷却装置3と前記のポンプ6.7との間を
連結する冷却水供給配管4の途中に、前記冷却水温度制
御装置13の温度センサ部分を設ける。
A temperature sensor portion of the cooling water temperature control device 13 is provided in the middle of the cooling water supply pipe 4 that connects the emergency cooling device 3 and the pump 6.7.

次に、以上のように構成したガスタービン及び発電機の
冷却系統(第1図)の作用を説明する。
Next, the operation of the gas turbine and generator cooling system (FIG. 1) configured as described above will be explained.

まず、冷却水は起動用冷却装置1.冷却袋w2及び非常
用冷却装置3にて冷却され、冷却水供給配管4.サージ
タンク5を通り冷却水循環装置l!6及び非常用冷却水
循環装置7にて発電機固定子冷却用熱交換器8に送られ
、適度に加温された後にガスタービン発電機潤滑油冷却
用熱交換器9に供給される。
First, the cooling water is supplied to the startup cooling device 1. It is cooled by the cooling bag w2 and the emergency cooling device 3, and the cooling water supply pipe 4. Cooling water circulation system through surge tank 5! 6 and an emergency cooling water circulation system 7 to a heat exchanger 8 for cooling the generator stator, and after being appropriately heated, it is supplied to a heat exchanger 9 for cooling the gas turbine generator lubricating oil.

ガスタービン起動時は、まず、ガスタービン軸駆動の冷
却水循環装置6が、ガスタービン起動と共に補機歯車1
1を介して作動し、発電機固定子冷却用熱交換器8及び
ガスタービン発電機潤滑油冷却用熱交換器9を冷却する
1次に発電機を低回転の状態から励磁し、低電圧の電気
を起動用冷却装置1(低電圧で起動できるモータを使用
している)に供給し同装置を起動し冷却水を冷却する。
At the time of starting the gas turbine, first, the cooling water circulation device 6 driven by the gas turbine shaft rotates the auxiliary gear 1 at the same time as the gas turbine starts.
1 to cool the generator stator cooling heat exchanger 8 and the gas turbine generator lubricating oil cooling heat exchanger 9. Electricity is supplied to the startup cooling device 1 (using a motor that can be started with low voltage) to start the device and cool the cooling water.

#11. =ot″JEJu&−T−lk、、kulF
”−″   管。
#11. =ot″JEJu&-T-lk,,kulF
”−” tube.

ンを駆動しブラックスタートを行なう方法は既に実施さ
れている。
Methods of driving the engine and performing a black start have already been implemented.

更に、ガスタービン発電機が定格となると、冷却水の温
度高を冷却水温度制御装置13が検知し。
Furthermore, when the gas turbine generator reaches its rating, the cooling water temperature control device 13 detects the high temperature of the cooling water.

冷却装置2を起動する。Start the cooling device 2.

外気温が高温となった場合、発電機固定子冷却に必要な
冷却水温度は約50℃程度であり、起動用冷却装置、及
び冷却装置2では適度な温度まで冷却水を冷却する事が
できないため、この下流側に直列に設接した非常用冷却
装置3を冷却水温度制御装置13からの信号により起動
し、冷却性能を向上し冷却水温度を調節する。
When the outside temperature becomes high, the cooling water temperature required to cool the generator stator is approximately 50°C, and the startup cooling system and cooling system 2 cannot cool the cooling water to an appropriate temperature. Therefore, the emergency cooling device 3 connected in series on the downstream side is activated by a signal from the cooling water temperature control device 13 to improve cooling performance and adjust the cooling water temperature.

更に、外気温が上昇した場合、熱交換の入口と出口温度
差が小さくなるため、冷却水量を増加し要求される交換
熱量を満足する必要がある。そこで、非常用冷却水循環
装置7を冷却水温度制御装置13からの信号にて起動す
る事により、冷却水温度を調節する。
Furthermore, when the outside temperature rises, the difference in temperature between the inlet and outlet of heat exchange becomes smaller, so it is necessary to increase the amount of cooling water to satisfy the required amount of exchanged heat. Therefore, by starting the emergency cooling water circulation device 7 with a signal from the cooling water temperature control device 13, the cooling water temperature is adjusted.

更に、発電機の急速な負荷変動にも対応できるように1
発電機出力を計測しこの発電機負荷計測装置10からの
信号を前記冷却水温度制御装置13に送り、冷却水温度
制御装置13からの信号を補正し冷却水温度を制御する
Furthermore, in order to cope with rapid load fluctuations of the generator,
The generator output is measured and a signal from the generator load measuring device 10 is sent to the cooling water temperature control device 13, and the signal from the cooling water temperature control device 13 is corrected to control the cooling water temperature.

又、外気温が低温の場合には、前記冷却水温度制御装置
13により、非常用冷却装置3.非常用冷却水循環ポン
プ7、冷却装置2を運転させたり停止させたりして冷却
水供給温度を制御すると共に、さらに外気温が低下し冷
却水温度が低温となる場合は、発電機固定子冷却用熱交
換lI8人口に設けた温度調節弁14をガスタービン発
電機潤滑油冷却用熱交換器9出口に設けた温度調節計1
5からの信号により作動し、冷却水をバイパス配管工6
に送り、冷却水戻り配管へ戻す事によりガスタービン発
電機潤滑油冷却用熱交換器9の出口温度を、一定に保つ
ように制御する。
Further, when the outside temperature is low, the cooling water temperature control device 13 controls the emergency cooling device 3. In addition to controlling the cooling water supply temperature by operating or stopping the emergency cooling water circulation pump 7 and the cooling device 2, if the outside temperature drops further and the cooling water temperature becomes low, the cooling water supply temperature is A temperature controller 1 having a temperature control valve 14 provided at the heat exchange lI8 port and a temperature control valve 14 provided at the outlet of the heat exchanger 9 for cooling gas turbine generator lubricating oil.
Activated by a signal from 5, the cooling water is bypassed by the plumber 6
The outlet temperature of the gas turbine generator lubricating oil cooling heat exchanger 9 is controlled to be kept constant by sending it to the cooling water and returning it to the cooling water return pipe.

本実施例によれば、ガスタービン発電機潤滑油冷却用熱
交換器9及び発電機固定子冷却用熱交換機8を直列に接
続し冷却水循環量をほぼ従来と同一としたため、冷却水
循環装置として、ガスタービン軸駆動の冷却水循環装置
6を使用可能とし、ガスタービンのブラックスタートが
可能となり、冷却系統を、ガスタービン及び発電機共通
としたためトータル設備費を低減し得た。
According to this embodiment, the gas turbine generator lubricating oil cooling heat exchanger 9 and the generator stator cooling heat exchanger 8 are connected in series, and the amount of circulating water is almost the same as that of the conventional one, so that the cooling water circulation device can be used as a cooling water circulating device. The cooling water circulation device 6 driven by the gas turbine shaft can be used, a black start of the gas turbine is possible, and the cooling system is shared between the gas turbine and the generator, so the total equipment cost can be reduced.

外気温の変動に対し冷却水温度変化装!13からの信号
により冷却装置2.及び非常用冷却装置3の運転制御を
行なうため、第2図に示す様に安定した温度の冷却水供
給が可能であり、さらに外気温が高くなり、熱交換の入
口と出口の温度差が取れなくなった場合でも、非常用冷
却水循環装置7を起動し冷却水量を増加し要求交換熱量
を満足する事ができ、熱交換を円滑に行なえ、運転機器
台数を外気温度に合わせ切換えるため、消費電力の少な
い経済性に優れた運転が可能である。
Cooling water temperature change device for changes in outside temperature! 13, the cooling device 2. and controls the operation of the emergency cooling system 3, it is possible to supply cooling water at a stable temperature as shown in Figure 2, and even when the outside temperature becomes high, the temperature difference between the inlet and outlet of the heat exchanger can be eliminated. Even if the water runs out, the emergency cooling water circulation system 7 can be activated to increase the amount of cooling water to satisfy the required amount of exchanged heat, allowing for smooth heat exchange and switching the number of operating devices according to the outside temperature, reducing power consumption. It is possible to operate with low cost and excellent economic efficiency.

外気温度の変動による冷却水温度の変動に対し、発電機
の負荷変動による冷却水温度の変動の方が急激であるた
め、この負荷変動を発電機負荷計測装置10により計測
し、冷却水温度制御装置13へこの信号を送り、冷却水
温度制御装置13からの信号を補正し冷却水温が変動す
る以前に前記機器の運転を制御するため、発電機負荷急
変による急激な冷却水の温度変化を防止できる。
Since the fluctuation in cooling water temperature due to changes in generator load is more rapid than the fluctuation in cooling water temperature due to fluctuation in outside air temperature, this load fluctuation is measured by the generator load measuring device 10 to control the cooling water temperature. This signal is sent to the device 13, corrects the signal from the cooling water temperature control device 13, and controls the operation of the equipment before the cooling water temperature fluctuates, thereby preventing sudden changes in the cooling water temperature due to sudden changes in the generator load. can.

ガスタービン発電機潤滑油冷却用熱交換器9の上流に発
電機固定子冷却用熱交換器8を設け、さらに、この上流
に設けた温度調節弁14によりガスタービン発電機潤滑
油冷却用熱交換$9の出口冷却水温度を制御する事によ
り、同熱交換器9の入口温度もほぼ一定に保つ事ができ
、外気温が低い場合でも発電機固定子冷却用熱交換器8
にて適度に加温された冷却水がガスタービン発電機潤滑
油冷却用熱交換器9に供給されるため潤滑油の過冷却を
防止できる。
A generator stator cooling heat exchanger 8 is provided upstream of the gas turbine generator lubricating oil cooling heat exchanger 9, and the gas turbine generator lubricating oil cooling heat exchanger is further provided by the temperature control valve 14 provided upstream. By controlling the outlet cooling water temperature of $9, the inlet temperature of the heat exchanger 9 can also be kept almost constant, so even when the outside temperature is low, the generator stator cooling heat exchanger 8
Since the cooling water that has been appropriately heated is supplied to the gas turbine generator lubricating oil cooling heat exchanger 9, overcooling of the lubricating oil can be prevented.

この状態を第3図により説明すると、外気温が非常に低
温となった場合やその他のトラブル等により冷却水温度
が下がったとしても、発電機固定子冷却用熱交換器8人
口の水量を絞り同熱交換器8を通過させるため、冷却水
温度を通常に近づけることができる。なお、ガスタービ
ン及び発電機の潤滑油温度は、ガスタービン発電機潤滑
油冷却用熱交換器9の出口水温を一定に制御しているた
1)”4ffJ−*I;flJ11’hlbsZ°  
      t〔発明の効果〕 本発明によれば、密閉冷却を適用したガスタービン及び
発電機においても、ブラックスタートが可能となり、ま
た、外気温及び負荷変動時においても冷却系統内の温度
変化を最少とする事ができ。
To explain this situation using Figure 3, even if the cooling water temperature drops due to extremely low outside temperatures or other troubles, the amount of water in the generator stator cooling heat exchanger 8 will be reduced. Since the cooling water passes through the heat exchanger 8, the temperature of the cooling water can be brought close to normal. Note that the temperature of the lubricating oil of the gas turbine and generator is controlled to be constant by controlling the outlet water temperature of the heat exchanger 9 for cooling the lubricating oil of the gas turbine generator.
[Effects of the Invention] According to the present invention, a black start is possible even in gas turbines and generators to which sealed cooling is applied, and temperature changes in the cooling system can be minimized even when the outside temperature and load change. I can do that.

さらに、潤滑油冷却用熱交換器に入る冷却水温度をほぼ
一定に保つ事ができるため、ガスタービン及び発電機の
起動及び運転時における信頼性を向上せしめることがで
きるという優れた実用的効果を奏する。
Furthermore, since the temperature of the cooling water entering the lubricating oil cooling heat exchanger can be kept almost constant, it has the excellent practical effect of improving reliability during startup and operation of gas turbines and generators. play.

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

第1図は本発明の一実施例におけるガスタービン及び発
電機冷却水系統図、第2図は外気温度変化に対する冷却
水温度変化のグラフ、第3図は1冷却サイクルの冷却水
温度変化のグラフである。 1・・・起動用冷却装置、2・・・冷却装置、3・・・
非常用冷却装置、4・・・冷却水供給配管、5・・・サ
ージタンク、6・・・冷却水循環ポンプ、7・・・非常
用冷却水循環ポンプ、8・・・発電機固定子冷却用熱交
換器、9・・・ガスタービン発電機潤滑油冷却用熱交換
器、10・・・発電機負荷計測装置、11・・・補機歯
車。 12・・・冷却水戻り配管、13・・・冷却水温度制御
装置、14・・・温度調節弁、15・・・温度調節計、
16・・・バイパス配管、17・・・ガスタービンパッ
ケージ。 18・・・発電機パッケージ。
Fig. 1 is a gas turbine and generator cooling water system diagram in one embodiment of the present invention, Fig. 2 is a graph of cooling water temperature changes with respect to outside air temperature changes, and Fig. 3 is a graph of cooling water temperature changes in one cooling cycle. It is. 1... Start-up cooling device, 2... Cooling device, 3...
Emergency cooling device, 4... Cooling water supply piping, 5... Surge tank, 6... Cooling water circulation pump, 7... Emergency cooling water circulation pump, 8... Generator stator cooling heat Exchanger, 9... Gas turbine generator lubricating oil cooling heat exchanger, 10... Generator load measuring device, 11... Auxiliary gear. 12... Cooling water return pipe, 13... Cooling water temperature control device, 14... Temperature control valve, 15... Temperature controller,
16...Bypass piping, 17...Gas turbine package. 18... Generator package.

Claims (1)

【特許請求の範囲】 1、冷却装置によつて冷却媒体を冷却し、上記の冷却さ
れた冷却媒体を圧送してガスタービン及び発電機に循環
せしめる冷却系統において、複数の冷却装置を並列に配
管接続し、上記複数の冷却装置の下流側に前記と異なる
冷却装置を直列に接続配管し、かつ、前記の冷却媒体を
循環せしめる為の圧送手段はガスタービンによつて歯車
伝動手段を介して定常的に駆動される主ポンプと、外気
温が所定値以上となつたとき自動的に運転される非常用
補助ポンプとを備えたものであることを特徴とする、ガ
スタービン及び発電機の冷却系統。 2、前記の冷却系統は、上流側に発電機固定子冷却用熱
交換器を設け、その直近の下流側にガスタービン発電機
潤滑油冷却用熱交換器を設け、かつ、ガスタービン発電
機潤滑油冷却用熱交換器出口部の冷却媒体の温度を検出
する手段、及び、上記検出手段の信号出力によつて切換
制御される弁手段を設けて、発電機固定子冷却用熱交換
器に流入する冷却媒体の1部をガスタービン発電機潤滑
油冷却用熱交換器の冷却媒体流出口側にバイパスさせて
ガスタービン発電機潤滑油冷却用熱交換器出口の冷却媒
体温度を自動制御するように構成したことを特徴とする
特許請求の範囲第1項に記載のガスタービン及び発電機
の冷却系統。 3、前記の冷却装置と、被冷却機器とを連結する管路に
冷却水温度制御装置の温度検出部を設けるとともに、発
電機負荷計測装置の出力信号を前記冷却媒体温度制御装
置に入力せしめ、該冷却媒体温度制御装置によつて冷却
装置の運転および冷却媒体循環用ポンプの運転を制御す
るように構成したことを特徴とする特許請求の範囲第1
項に記載のガスタービン及び発電機の冷却系統。
[Claims] 1. In a cooling system in which a cooling medium is cooled by a cooling device and the cooled cooling medium is pumped and circulated to a gas turbine and a generator, a plurality of cooling devices are piped in parallel. A cooling device different from the one described above is connected in series on the downstream side of the plurality of cooling devices, and the pressure feeding means for circulating the cooling medium is operated by a gas turbine in a steady state via a gear transmission means. A cooling system for a gas turbine and a generator, characterized in that it is equipped with a main pump that is driven automatically, and an emergency auxiliary pump that is automatically operated when the outside temperature exceeds a predetermined value. . 2. The above-mentioned cooling system includes a heat exchanger for cooling the generator stator on the upstream side, a heat exchanger for cooling the gas turbine generator lubricating oil on the immediate downstream side, and a heat exchanger for cooling the gas turbine generator stator. A means for detecting the temperature of the cooling medium at the outlet of the oil cooling heat exchanger, and a valve means whose switching is controlled by the signal output of the detection means are provided, and the temperature of the cooling medium flowing into the generator stator cooling heat exchanger is provided. The cooling medium temperature at the outlet of the gas turbine generator lubricating oil cooling heat exchanger is automatically controlled by bypassing a part of the cooling medium to the coolant outlet side of the gas turbine generator lubricating oil cooling heat exchanger. A cooling system for a gas turbine and a generator according to claim 1, characterized in that the cooling system is configured as follows. 3. Providing a temperature detection section of a cooling water temperature control device in a conduit connecting the cooling device and the equipment to be cooled, and inputting an output signal of the generator load measuring device to the cooling medium temperature control device; Claim 1, characterized in that the cooling medium temperature control device is configured to control the operation of the cooling device and the operation of the cooling medium circulation pump.
Cooling systems for gas turbines and generators described in Section 1.
JP1077085A 1985-01-25 1985-01-25 Cooling system for gas turbine and generator Pending JPS61171833A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1077085A JPS61171833A (en) 1985-01-25 1985-01-25 Cooling system for gas turbine and generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1077085A JPS61171833A (en) 1985-01-25 1985-01-25 Cooling system for gas turbine and generator

Publications (1)

Publication Number Publication Date
JPS61171833A true JPS61171833A (en) 1986-08-02

Family

ID=11759566

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1077085A Pending JPS61171833A (en) 1985-01-25 1985-01-25 Cooling system for gas turbine and generator

Country Status (1)

Country Link
JP (1) JPS61171833A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005226639A (en) * 2004-01-15 2005-08-25 Hitachi Ltd Gas turbine power generator and silencer used therefor
JP2005315258A (en) * 2004-04-29 2005-11-10 Filterwerk Mann & Hummel Gmbh Flap valve device at flange area of intake system internal-combustion engine
JP2008185031A (en) * 2007-01-29 2008-08-14 General Electric Co <Ge> Plant integrated cooling system
JP2011033328A (en) * 2009-07-07 2011-02-17 Mitsubishi Heavy Ind Ltd Turbo refrigerator control device, turbo refrigerator control method, gas turbine plant, and reconstruction method of existing gas turbine plant

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005226639A (en) * 2004-01-15 2005-08-25 Hitachi Ltd Gas turbine power generator and silencer used therefor
JP2005315258A (en) * 2004-04-29 2005-11-10 Filterwerk Mann & Hummel Gmbh Flap valve device at flange area of intake system internal-combustion engine
JP2008185031A (en) * 2007-01-29 2008-08-14 General Electric Co <Ge> Plant integrated cooling system
JP2011033328A (en) * 2009-07-07 2011-02-17 Mitsubishi Heavy Ind Ltd Turbo refrigerator control device, turbo refrigerator control method, gas turbine plant, and reconstruction method of existing gas turbine plant

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