JPH0666155A - Outside combustion type gas turbine combined power plant - Google Patents
Outside combustion type gas turbine combined power plantInfo
- Publication number
- JPH0666155A JPH0666155A JP24269592A JP24269592A JPH0666155A JP H0666155 A JPH0666155 A JP H0666155A JP 24269592 A JP24269592 A JP 24269592A JP 24269592 A JP24269592 A JP 24269592A JP H0666155 A JPH0666155 A JP H0666155A
- Authority
- JP
- Japan
- Prior art keywords
- shut
- valve
- air compressor
- check valve
- air
- 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.)
- Withdrawn
Links
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
- Control Of Turbines (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は外部燃焼型ガスタービン
複合発電プラントに関し、外部に加圧流動床ボイラなど
の外部燃焼炉を有する複合発電設備に適用することがで
きる。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an external combustion type gas turbine combined cycle power generation plant, and can be applied to a combined cycle power generation facility having an external combustion furnace such as a pressurized fluidized bed boiler outside.
【0002】[0002]
【従来の技術】図3は加圧流動床燃焼器(PFBC)と
呼ばれる外部燃焼型ガスタービン複合発電プラントの1
つの系統図である。図中、符号1は軸流空気圧縮機、2
は外部燃焼炉とする加圧流動床ボイラなどの加圧燃焼ボ
イラ、3はろ過器、4はガスエキスパンダ、5は発電
機、6は蒸気タービン、7は発電機、8は復水器、9は
復水ポンプ、10は補助燃焼器、V1ないしV3は遮断
弁、V4は蒸気止め弁、V5は蒸気加減弁、V6及びV
7は遮断弁である。2. Description of the Related Art FIG. 3 shows an external combustion type gas turbine combined cycle power plant called a pressurized fluidized bed combustor (PFBC).
It is one system diagram. In the figure, reference numeral 1 is an axial air compressor, 2
Is a pressurized combustion boiler such as a pressurized fluidized bed boiler which is an external combustion furnace, 3 is a filter, 4 is a gas expander, 5 is a generator, 6 is a steam turbine, 7 is a generator, 8 is a condenser, 9 is a condensate pump, 10 is an auxiliary combustor, V1 to V3 are cutoff valves, V4 is a steam stop valve, V5 is a steam control valve, V6 and V
Reference numeral 7 is a shutoff valve.
【0003】軸流空気圧縮機1で圧縮された空気は加圧
燃焼ボイラ2で石炭を燃焼させて高温となり、蒸気発生
に供されたのち、その排ガスはろ過器3を経て、ガスエ
キスパンダ4に流入する。ガスエキスパンダ4は空気圧
縮機1と共に発電機5を駆動する。The air compressed by the axial air compressor 1 burns coal in a pressurized combustion boiler 2 to a high temperature and is used for steam generation. The exhaust gas passes through a filter 3 and a gas expander 4 Flow into. The gas expander 4 drives the generator 5 together with the air compressor 1.
【0004】加圧燃焼ボイラ2で発生した蒸気は蒸気止
め弁V4、蒸気加減弁V5を経て、蒸気タービン6に流
入して、発電機7を駆動する。その後復水器8で復水
し、復水ポンプ9及び図に示されていない給水加熱器、
脱気器、給水ポンプ等を経て、加圧燃焼ボイラ2に流入
する。The steam generated in the pressurized combustion boiler 2 flows into the steam turbine 6 through the steam stop valve V4 and the steam control valve V5, and drives the generator 7. After that, the water is condensed by the condenser 8, and the condensate pump 9 and the feed water heater not shown in the figure,
It flows into the pressurized combustion boiler 2 via a deaerator, a water supply pump and the like.
【0005】プラント起動時は遮断弁V1,V2を閉
め、遮断弁V3を開いて、圧縮空気を補助燃焼器10に
導き、ガス又は液体燃料を燃焼させて、ガスエキスパン
ダ4を駆動する。なおタービン室とボイラとの距離は通
常10〜100m程度となっている。When the plant is started, the shut-off valves V1 and V2 are closed, the shut-off valve V3 is opened, the compressed air is guided to the auxiliary combustor 10, the gas or liquid fuel is burned, and the gas expander 4 is driven. The distance between the turbine chamber and the boiler is usually about 10 to 100 m.
【0006】図3の弁状態は運転時を示すが、プラント
がトリップしたときには、図4に示すように遮断弁V
1,V2を閉じ、遮断弁V6,V7が開いて、空気圧縮
機1の吐出空気はガスエキスパンダ4へ、そして加圧燃
焼ボイラ2及び配管内の燃焼ガス及び圧縮空気は排気側
へそれぞれバイパスされる。これはトリップ時ガスエキ
スパンダ軸の過速を防止するためである。The valve state in FIG. 3 shows the operation, but when the plant trips, the shut-off valve V as shown in FIG.
1, V2 are closed, shutoff valves V6, V7 are opened, the discharge air of the air compressor 1 is bypassed to the gas expander 4, and the combustion gas and compressed air in the pressurized combustion boiler 2 and the piping are bypassed to the exhaust side. To be done. This is to prevent the gas expander shaft from overspeeding during a trip.
【0007】[0007]
【発明が解決しようとする課題】加圧燃焼ボイラは通常
のガスタービン燃焼器に比べて、その容量が極めて大き
い。また、ボイラは通常タービン室から10〜100m
程度離れて設置され、圧縮空気の配管容量も極めて大き
い。このため、プラントトリップ時に遮断弁V1の閉動
作が早いと、空気圧縮機吐出空気圧が上昇して、空気圧
縮機はサージングに突入することがある。一方、軸流空
気圧縮機は発電機が結合されているために定速であり、
かつ遠心式に比べて風量変化範囲が小さい。加えてその
吐出圧が高いため、上記の場合に吐出圧の変動が非常に
大きくなってサージングが発生し、プラント操業を不能
にする場合があった。The pressurized combustion boiler has an extremely large capacity as compared with an ordinary gas turbine combustor. The boiler is usually 10 to 100 m from the turbine room.
Installed at some distance, the compressed air piping capacity is extremely large. Therefore, if the shutoff valve V1 closes quickly during a plant trip, the air compressor discharge air pressure rises and the air compressor may rush into surging. On the other hand, the axial air compressor has a constant speed because the generator is connected,
Moreover, the change range of the air volume is smaller than that of the centrifugal type. In addition, since the discharge pressure is high, in the above case, the fluctuation of the discharge pressure becomes so large that surging occurs, which may make the plant operation impossible.
【0008】本発明は上記事情にかんがみてなされたも
ので、プラントトリップ時における空気圧縮機のサージ
ング突入防止が可能な外部燃焼型ガスタービン複合発電
プラントを提供することを目的とする。The present invention has been made in view of the above circumstances, and an object thereof is to provide an external combustion type gas turbine combined cycle power plant capable of preventing surging of the air compressor during a plant trip.
【0009】[0009]
【課題を解決するための手段】上記目的に対し、本発明
によれば、空気圧縮機出口と外部に設けられた加圧燃焼
ボイラなどの外部燃焼炉とを連通させる高圧空気配管に
設置されている遮断弁を、遮断用ロック機構を有する逆
止弁に置換したことを特徴とする外部燃焼型ガスタービ
ン複合発電プラントが提供される。To solve the above problems, according to the present invention, it is installed in a high-pressure air pipe for communicating an air compressor outlet with an external combustion furnace such as a pressurized combustion boiler provided outside. There is provided an external combustion type gas turbine combined cycle power plant characterized in that the shut-off valve is replaced with a check valve having a shut-off lock mechanism.
【0010】[0010]
【作用】プラントトリップ時には、逆止弁を介して外部
燃焼炉へ通じているため空気圧縮機吐出空気が閉塞され
ず、吐出空気圧の上昇やそれに伴うサージングが発生し
ない。また、運転中は、加圧燃焼ボイラから空気圧縮機
への逆流が逆止弁によって遮断される。逆止弁のロック
機構は、プラント起動時にガスタービン軸系のみを単独
で運転するとき、逆止弁を閉じるために使用される。When the plant is tripped, the air discharged to the air compressor is not blocked because it communicates with the external combustion furnace through the check valve, and the discharge air pressure does not rise and surging does not occur. Further, during operation, the check valve shuts off the reverse flow from the pressurized combustion boiler to the air compressor. The check valve locking mechanism is used to close the check valve when only the gas turbine shaft system is operated alone at plant startup.
【0011】[0011]
【実施例】図1は本発明の一実施例を示す外部燃焼型ガ
スタービン複合発電プラントの系統図であり、図中、図
3に示したものと同一の部分については同一の符号を付
して、その詳細な説明は省略する。FIG. 1 is a system diagram of an external combustion type gas turbine combined cycle power plant showing one embodiment of the present invention. In the figure, the same parts as those shown in FIG. Therefore, detailed description thereof will be omitted.
【0012】図1によれば、軸流空気圧縮機1の出口と
加圧燃焼ボイラ2とを連通させる高圧空気配管11に
は、遮断弁V1に代わって、逆止弁V8が設置されてい
る。これにより、プラントがトリップして遮断弁V2及
びV7が閉じ、遮断弁V6が開いた場合、空気圧縮機1
の吐出空気は逆止弁V8を通って加圧燃焼ボイラ2へ通
じる大容量の高圧空気配管11へ流入することができ、
吐出空気圧力の上昇及びこれに伴うサージングの発生は
防止されることになる。According to FIG. 1, a check valve V8 is installed in place of the shutoff valve V1 in the high-pressure air pipe 11 which connects the outlet of the axial air compressor 1 and the pressurized combustion boiler 2 to each other. . As a result, when the plant trips, the shutoff valves V2 and V7 are closed, and the shutoff valve V6 is opened, the air compressor 1
Discharge air can flow into the large-capacity high-pressure air pipe 11 leading to the pressurized combustion boiler 2 through the check valve V8,
The rise in discharge air pressure and the resulting surging will be prevented.
【0013】図2は逆止弁V8の一実施例を示したもの
で、図中、21は弁本体、22は弁体であり、ロック棒
23及びロック棒操作ギア24によって遮断用ロック機
構を構成している。FIG. 2 shows an embodiment of the check valve V8. In the figure, 21 is a valve body, 22 is a valve body, and a lock rod 23 and a lock rod operating gear 24 form a shut-off lock mechanism. I am configuring.
【0014】図2に示す遮断用ロック機構を有する逆止
弁によれば、通常の運転中はロック機構は解除されてい
て通常の逆止弁のように作用し、加圧燃焼ボイラ2から
空気圧縮機1への逆流がある場合にはこれを遮断する。
一方、プラント起動時のように、ガスタービン軸系のみ
を単独運転する場合には、図2の一点鎖線で示したよう
にロック棒23を挿入し、弁体22を弁閉位置に固定す
る。According to the check valve having the shut-off lock mechanism shown in FIG. 2, the lock mechanism is released during normal operation and acts like a normal check valve, so that the pressurized combustion boiler 2 is operated by air. If there is a reverse flow to the compressor 1, this is shut off.
On the other hand, when the gas turbine shaft system alone is operated as in the case of starting the plant, the lock rod 23 is inserted as shown by the alternate long and short dash line in FIG. 2 to fix the valve body 22 to the valve closed position.
【0015】[0015]
【発明の効果】本発明によれば、プラントトリップ時、
遮断弁切替不調によって、従来発生していた空気圧縮機
のサージングがほぼ完全に防止される。従って、外部燃
焼型ガスタービン複合発電プラントの信頼性を向上させ
ることができる。According to the present invention, during a plant trip,
Due to the malfunction of the shutoff valve switching, the surging of the air compressor, which has conventionally occurred, is almost completely prevented. Therefore, the reliability of the external combustion type gas turbine combined cycle power plant can be improved.
【図1】本発明による外部燃焼型ガスタービン複合発電
プラントの一実施例を示す系統図である。FIG. 1 is a system diagram showing an embodiment of an external combustion gas turbine combined cycle power plant according to the present invention.
【図2】本発明による外部燃焼型ガスタービン複合発電
プラントの要部の一実施例を示す断面図である。FIG. 2 is a cross-sectional view showing an example of a main part of an external combustion gas turbine combined cycle power plant according to the present invention.
【図3】従来の外部燃焼型ガスタービン複合発電プラン
トの一実施例を示す通常運転時の系統図である。FIG. 3 is a system diagram during normal operation showing an embodiment of a conventional external combustion gas turbine combined cycle power plant.
【図4】図3の外部燃焼型ガスタービン複合発電プラン
トのタービントリップ時を示した系統図である。FIG. 4 is a system diagram showing a turbine trip of the external combustion gas turbine combined cycle power generation plant of FIG.
1 軸流空気圧縮機 2 加圧燃焼ボイラ 11 高圧空気配管 V8 逆止弁 23 ロック棒 24 ロック操作ギア 1 Axial Flow Air Compressor 2 Pressurized Combustion Boiler 11 High Pressure Air Piping V8 Check Valve 23 Lock Rod 24 Lock Operation Gear
Claims (1)
焼ボイラなどの外部燃焼炉とを連通させる高圧空気配管
に設置されている遮断弁を、遮断用ロック機構を有する
逆止弁に置換したことを特徴とする外部燃焼型ガスター
ビン複合発電プラント。1. A shut-off valve installed in a high-pressure air pipe that connects an outlet of an air compressor and an external combustion furnace such as a pressurized combustion boiler provided outside to a check valve having a shut-off lock mechanism. An external combustion type gas turbine combined cycle power plant characterized by being replaced.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP24269592A JPH0666155A (en) | 1992-08-19 | 1992-08-19 | Outside combustion type gas turbine combined power plant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP24269592A JPH0666155A (en) | 1992-08-19 | 1992-08-19 | Outside combustion type gas turbine combined power plant |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0666155A true JPH0666155A (en) | 1994-03-08 |
Family
ID=17092870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP24269592A Withdrawn JPH0666155A (en) | 1992-08-19 | 1992-08-19 | Outside combustion type gas turbine combined power plant |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0666155A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1186761A2 (en) * | 2000-09-11 | 2002-03-13 | General Electric Company | Energy recovery from compressor discharge bleed air in gas turbine plants |
-
1992
- 1992-08-19 JP JP24269592A patent/JPH0666155A/en not_active Withdrawn
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1186761A2 (en) * | 2000-09-11 | 2002-03-13 | General Electric Company | Energy recovery from compressor discharge bleed air in gas turbine plants |
US6442941B1 (en) * | 2000-09-11 | 2002-09-03 | General Electric Company | Compressor discharge bleed air circuit in gas turbine plants and related method |
US6543234B2 (en) | 2000-09-11 | 2003-04-08 | General Electric Company | Compressor discharge bleed air circuit in gas turbine plants and related method |
EP1186761A3 (en) * | 2000-09-11 | 2003-11-05 | General Electric Company | Energy recovery from compressor discharge bleed air in gas turbine plants |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 19991102 |