JP2000018050A - Outlet steam monitoring system for steam cooling type gas turbine - Google Patents
Outlet steam monitoring system for steam cooling type gas turbineInfo
- Publication number
- JP2000018050A JP2000018050A JP19032798A JP19032798A JP2000018050A JP 2000018050 A JP2000018050 A JP 2000018050A JP 19032798 A JP19032798 A JP 19032798A JP 19032798 A JP19032798 A JP 19032798A JP 2000018050 A JP2000018050 A JP 2000018050A
- Authority
- JP
- Japan
- Prior art keywords
- steam
- temperature
- outlet
- cooling
- 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.)
- Granted
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 51
- 238000012544 monitoring process Methods 0.000 title claims abstract description 14
- 239000000446 fuel Substances 0.000 claims description 20
- 238000001514 detection method Methods 0.000 claims description 9
- 238000011084 recovery Methods 0.000 abstract description 22
- 230000005856 abnormality Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 5
- 230000002159 abnormal effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
- F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
- F01K23/10—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle
- F01K23/101—Regulating means specially adapted therefor
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は蒸気冷却式ガスター
ビンの出口蒸気監視システムに関し、冷却用蒸気の出口
温度を監視することにより燃焼器や翼の異常の発生を早
期に検知できるようにしたものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an outlet steam monitoring system for a steam-cooled gas turbine, which monitors an outlet temperature of cooling steam so that an abnormality in a combustor or a blade can be detected at an early stage. It is.
【0002】[0002]
【従来の技術】近年の発電プラントの高温、高効率化に
伴ってコンバインドプラントが多く建設されるに従い、
ガスタービンの有力な冷却方式として空気冷却方式に代
わり、蒸気冷却方式が検討されており、実プラントに採
用されるようになってきている。2. Description of the Related Art In recent years, as many combined plants have been constructed with the high temperature and high efficiency of power plants,
As an effective cooling method for gas turbines, a steam cooling method is being studied instead of an air cooling method, and it has been adopted in actual plants.
【0003】図3は蒸気冷却方式を採用したガスタービ
ンの燃焼器を示し、本出願人により開発された先行技術
の一例で、(a)は構成図、(b)はその冷却壁面の一
部を示す斜視図、(c)は(b)におけるA−A断面図
である。これら図(a)において、20は燃焼器本体、
21はパイロットノズルであり、パイロット燃料40が
供給される。22はメインノズルであり、パイロットノ
ズル21の周囲に複数本配置されてメイン燃料41が供
給され燃焼に供される。23はメイン燃料供給管、24
はパイロット燃料供給管であり、それぞれ燃料41,4
0が供給される。[0003] Fig. 3 shows a combustor of a gas turbine employing a steam cooling system, which is an example of a prior art developed by the present applicant, wherein (a) is a configuration diagram, and (b) is a part of a cooling wall surface thereof. And (c) is a cross-sectional view taken along the line AA in (b). In these figures (a), 20 is a combustor body,
Reference numeral 21 denotes a pilot nozzle to which pilot fuel 40 is supplied. Reference numeral 22 denotes a main nozzle, and a plurality of main nozzles are arranged around the pilot nozzle 21 to supply a main fuel 41 to be used for combustion. 23 is a main fuel supply pipe, 24
Is a pilot fuel supply pipe, and fuels 41 and 4 respectively.
0 is supplied.
【0004】25は冷却蒸気供給管で冷却用蒸気31が
導かれ、26,27は冷却蒸気回収管であり、後述する
ように本体20の壁面内部を通り、冷却した後の蒸気3
0,32が回収され、取り出される。Numeral 25 denotes a cooling steam supply pipe through which cooling steam 31 is guided, and reference numerals 26 and 27 denote cooling steam recovery pipes.
0,32 is collected and removed.
【0005】図3(b)は本体20の壁の一部を示す斜
視図であり、壁20a内部には多数の蒸気通路50が穿
設されており、本体20の周囲に設けられる構成であ
る。図(c)に示すように各蒸気通路50は供給穴50
aと回収穴50bとに連通しており、冷却用蒸気が供給
され、内部を流れて壁20aを冷却し、回収されるもの
である。FIG. 3 (b) is a perspective view showing a part of the wall of the main body 20, in which a number of steam passages 50 are formed inside the wall 20a and provided around the main body 20. . As shown in FIG. 4C, each steam passage 50 is provided with a supply hole 50.
a and the recovery hole 50b, cooling steam is supplied, flows through the inside, cools the wall 20a, and is recovered.
【0006】蒸気冷却方式のガスタービンの燃焼器の蒸
気冷却は上記のような構成で、冷却蒸気供給管25から
冷却用蒸気31が導かれ、本体20の壁20a内に設け
られた多数の蒸気通路50内を流れ、本体20の周囲を
冷却した後、冷却蒸気回収管26と27から回収され
る。[0006] The steam cooling of the combustor of the gas turbine of the steam cooling system is configured as described above, and the cooling steam 31 is guided from the cooling steam supply pipe 25, and a large number of steams provided in the wall 20 a of the main body 20 are provided. After flowing in the passage 50 and cooling the periphery of the main body 20, it is recovered from the cooling steam recovery pipes 26 and 27.
【0007】図4は蒸気冷却方式を採用したガスタービ
ンの静翼であり、これも本出願人が開発した一例を示
す。図において60は2段目の静翼を示し、70は隣接
する動翼である。61は外側シュラウド、62は内側シ
ュラウド、63はシールチューブで静翼60の内部を貫
通し、内側のキャビティにシール用空気を導いている。
64は翼環に設けられたマニホールドであり、65はマ
ニホールド64に接続する蒸気供給用の接続管であり、
冷却用蒸気80が導かれる。66もマニホールドであ
り、67は蒸気回収用接続管で、マニホールド66に接
続し、静翼60内を通り、翼を冷却した後の回収蒸気8
1を導き回収するものである。FIG. 4 shows a stationary blade of a gas turbine employing a steam cooling system, which is also an example developed by the present applicant. In the figure, reference numeral 60 denotes a second stage stationary blade, and reference numeral 70 denotes an adjacent moving blade. 61 is an outer shroud, 62 is an inner shroud, and 63 is a seal tube which penetrates through the inside of the stationary blade 60 and guides sealing air to an inner cavity.
64 is a manifold provided on the blade ring, 65 is a connection pipe for steam supply connected to the manifold 64,
Cooling steam 80 is led. 66 is also a manifold, and 67 is a connecting pipe for steam recovery, which is connected to the manifold 66, passes through the inside of the stationary blade 60, and cools the recovered steam 8 after cooling the blade.
1 is to be collected.
【0008】このような構成において、冷却用の蒸気8
0はマニホールド64から蒸気供給用接続管65に導入
され、静翼60内に流入し、静翼60内に連通して設け
られた図示省略の蒸気通路を通り、翼を冷却しながら蒸
気回収用接続管67に流出し、マニホールド66から回
収経路に導かれて蒸気タービンの蒸気系統に戻され、有
効活用される。In such a configuration, the cooling steam 8
Numeral 0 is introduced from the manifold 64 to the connecting pipe 65 for steam supply, flows into the stationary blade 60, passes through a steam passage (not shown) provided in communication with the stationary blade 60, and collects steam while cooling the blade. It flows out to the connection pipe 67, is guided from the manifold 66 to the recovery path, returns to the steam system of the steam turbine, and is effectively used.
【0009】又、図示省略したが、動翼にも蒸気冷却方
式が採用されており、この場合には、冷却用蒸気はロー
タエンドからロータ内部に設けられた軸方向の供給蒸気
通路を通り、ロータディスクに設けられた通路から動翼
内部に導かれ、動翼内に同様に連通する蒸気通路を流れ
て動翼を冷却し、再びロータディスクからロータ内の回
収蒸気通路を通り、ロータエンドから回収される。Although not shown, a steam cooling system is also used for the moving blades. In this case, the cooling steam passes from the rotor end through an axial supply steam passage provided inside the rotor. It is guided from the passage provided in the rotor disk to the inside of the rotor blade, flows through the steam passage communicating similarly in the rotor blade, cools the rotor blade, passes again from the rotor disk through the recovery steam passage in the rotor, and from the rotor end. Collected.
【0010】[0010]
【発明が解決しようとする課題】前述のように近年のガ
スタービンにおいては、空気冷却方式に代わり、蒸気冷
却方式が採用され始めているが、燃焼器は高温で燃焼
し、又、冷却用蒸気供給系も複雑であり、冷却用蒸気温
度を監視することがむずかしい環境にある。現状では蒸
気冷却方式における蒸気供給、蒸気回収系の構造面での
技術は相当研究され、開発されているが、蒸気温度は監
視技術は確立されていないのが現状である。冷却蒸気温
度の状態を正確に監視できれば、冷却する対象部、即
ち、燃焼器、静翼、動翼の健全性も確認できるので、こ
のような蒸気温度の監視技術の確立が強く望まれてい
る。As described above, in recent gas turbines, a steam cooling system has begun to be used instead of an air cooling system. However, a combustor burns at a high temperature, and a cooling steam supply system is provided. The system is also complex and it is difficult to monitor the cooling steam temperature. At present, the technology for the structure of the steam supply and steam recovery system in the steam cooling system has been studied and developed considerably, but the technology for monitoring the steam temperature has not yet been established. If the state of the cooling steam temperature can be accurately monitored, the soundness of the target portion to be cooled, that is, the combustor, the stationary blade, and the moving blade can also be confirmed. Therefore, establishment of such a steam temperature monitoring technique is strongly desired. .
【0011】そこで本発明は蒸気冷却方式のガスタービ
ンにおいて、燃焼器や翼の蒸気冷却対象部の冷却蒸気の
出口温度を計測し、その温度変化により、対象部のクラ
ックの発生、蒸気系統の詰まり、等の異常を早期に検出
し、ガスタービンの安全運転を行うことのできる出口蒸
気温度監視システムを提供することを課題としてなされ
たものである。Therefore, the present invention measures the temperature of the outlet of the cooling steam of a steam-cooled portion of a combustor or blades in a steam-cooled gas turbine, and the temperature change causes cracks in the target portion and blockage of the steam system. It is an object of the present invention to provide an outlet steam temperature monitoring system capable of detecting an abnormality such as an abnormality at an early stage and performing a safe operation of the gas turbine.
【0012】[0012]
【課題を解決するための手段】本発明は前述の課題を解
決するために次の手段を提供する。The present invention provides the following means for solving the above-mentioned problems.
【0013】燃焼器や翼等の冷却対象部に冷却用蒸気を
供給し、冷却後の蒸気を回収する蒸気冷却式ガスタービ
ンにおいて、前記冷却後の蒸気の出口温度を検出する温
度検出器と、同温度検出器の検出信号を入力し、あらか
じめ設定された設定温度と比較し、同検出した温度が前
記設定値を超えると警報信号、燃料流量調節弁の開度を
所定開度に絞る信号又は遮断弁を閉じる信号を出力する
制御装置とを具備してなることを特徴とする蒸気冷却式
ガスタービンの出口蒸気監視システム。In a steam-cooled gas turbine for supplying cooling steam to a portion to be cooled, such as a combustor or a blade, and recovering the cooled steam, a temperature detector for detecting an outlet temperature of the cooled steam; The detection signal of the temperature detector is input, compared with a preset set temperature, and when the detected temperature exceeds the set value, an alarm signal, a signal for narrowing the opening of the fuel flow control valve to a predetermined opening or A control device for outputting a signal for closing a shut-off valve; and an outlet steam monitoring system for a steam-cooled gas turbine.
【0014】本発明の出口蒸気監視システムは、温度検
出器が冷却対象部を冷却した後の出口蒸気温度を検出
し、この検出信号は制御装置に入力される。制御装置は
あらかじめ正常な状態での出口蒸気温度、危険な状態で
の温度、燃料を遮断すべき上限の温度等を設定してお
き、検出した温度と比較し、設定された温度を超えると
警報信号、流量調節弁の開度を絞る信号、遮断弁を閉じ
る信号をそれぞれの上昇温度レベルに応じて出力する。
これにより冷却対象部の異常を早期に検知すると共に、
制御装置の上記信号により危険な状態を回避することが
できる。The outlet steam monitoring system of the present invention detects the outlet steam temperature after the temperature detector has cooled the cooling target portion, and this detection signal is input to the control device. The controller sets the outlet steam temperature under normal conditions, the temperature under dangerous conditions, the upper limit temperature at which fuel should be shut off, etc., compares it with the detected temperature, and issues an alarm if the temperature exceeds the set temperature A signal, a signal for reducing the opening of the flow control valve, and a signal for closing the shutoff valve are output according to the respective temperature rise levels.
This allows early detection of abnormalities in the cooling target,
Dangerous situations can be avoided by means of the signals of the control device.
【0015】[0015]
【発明の実施の形態】以下、本発明の実施の形態につい
て図面に基づいて具体的に説明する。図1は本発明の実
施の一形態に係る蒸気冷却方式ガスタービンの出口蒸気
温度監視システムの構成図であり、燃焼器の蒸気温度を
監視する例である。Embodiments of the present invention will be specifically described below with reference to the drawings. FIG. 1 is a configuration diagram of an outlet steam temperature monitoring system of a steam-cooled gas turbine according to an embodiment of the present invention, and is an example of monitoring a steam temperature of a combustor.
【0016】図1において、1は蒸気供給マニホール
ド、2は流量調節弁であり、供給される蒸気の流量が制
御される。3は供給ラインであり、各複数の燃焼器本体
20の冷却蒸気供給管25へ蒸気供給マニホールドから
冷却用蒸気を供給する。4は回収ライン、5蒸気回収マ
ニホールドであり、回収ライン4で各燃焼器本体20の
冷却蒸気回収管26,27から回収した蒸気をマニホー
ルド5へ回収している。In FIG. 1, reference numeral 1 denotes a steam supply manifold, and reference numeral 2 denotes a flow control valve, which controls the flow rate of the supplied steam. Reference numeral 3 denotes a supply line, which supplies cooling steam from a steam supply manifold to the cooling steam supply pipes 25 of the plurality of combustor bodies 20. Reference numeral 4 denotes a recovery line and a five-vapor recovery manifold. The recovery line 4 recovers the steam recovered from the cooling steam recovery pipes 26 and 27 of each combustor body 20 to the manifold 5.
【0017】6は温度検出器であり、各燃焼器本体20
への供給ライン3を流れる入口蒸気の温度を検出し、入
口温度検出ライン7を介して制御装置10へそれらの信
号を入力している。8も温度検出器であり、各回収ライ
ン4を流れる冷却蒸気回収管26,27から回収後の蒸
気温度を検出し、出口温度検出ライン9を介してそれら
の信号は制御装置10へ入力している。Reference numeral 6 denotes a temperature detector, and each combustor body 20
The temperature of the inlet steam flowing through the supply line 3 to the supply line is detected, and those signals are input to the control device 10 through the inlet temperature detection line 7. Numeral 8 denotes a temperature detector, which detects the temperature of the recovered steam from the cooling steam recovery pipes 26 and 27 flowing through each recovery line 4, and inputs those signals to the control device 10 through the outlet temperature detection line 9. I have.
【0018】10は前述の制御装置であり、11は表示
装置で制御装置10で演算した結果を表示するもの、1
2は警報装置であり、制御装置10で演算した結果、異
常と判定された時にアラーム等で知らせるものである。
13は制御信号ラインであり、ライン13aは燃料系統
14の流量調節弁15の開度を制御する信号を、ライン
13bは遮断弁16の開閉を制御する信号を、それぞれ
伝送する。Reference numeral 10 denotes the control device described above, and reference numeral 11 denotes a display device for displaying a result calculated by the control device 10;
Reference numeral 2 denotes an alarm device, which notifies an alarm or the like when it is determined as abnormal as a result of calculation by the control device 10.
Reference numeral 13 denotes a control signal line. A line 13a transmits a signal for controlling the opening of the flow control valve 15 of the fuel system 14, and a line 13b transmits a signal for controlling the opening and closing of the shutoff valve 16.
【0019】上記の構成において、制御装置10には温
度検出器6から各燃焼器の入口蒸気温度が検出され、更
に温度検出器8から各燃焼器の冷却蒸気回収管26,2
7から回収される出口蒸気温度が検出され、それぞれ入
力される。In the above configuration, the controller 10 detects the inlet steam temperature of each combustor from the temperature detector 6, and further detects the cooling steam recovery pipes 26, 2 of each combustor from the temperature detector 8.
The outlet steam temperature recovered from 7 is detected and input.
【0020】供給される蒸気温度は、計画供給温度程
度、回収される蒸気の温度は正常作動時で計画出口温度
程度であり、制御装置10はまず、入口蒸気温度が計画
供給温度前後で正常であるか否かを確認し、蒸気出口温
度を監視する。蒸気出口温度は正常時は計画出口温度程
度であり、燃焼器本体20の蒸気通路が詰まったり、あ
るいはクラック等が生じ、異常な状態となると温度が上
昇し、危険温度以上となると危険な状態となるので、こ
の状態を表示装置11に表示すると共に、警報装置12
に信号を送り、警報を発するように制御する。The temperature of the supplied steam is about the planned supply temperature, the temperature of the recovered steam is about the planned outlet temperature during normal operation, and the controller 10 first determines that the inlet steam temperature is normal around the planned supply temperature. Check if there is, and monitor the steam outlet temperature. The steam outlet temperature is about the planned outlet temperature during normal times, and the steam passage of the combustor body 20 becomes clogged or cracks occur. If the temperature is abnormal, the temperature rises. Therefore, this state is displayed on the display device 11 and the alarm device 12
Control to generate a warning.
【0021】更に、温度が上昇する状態が継続すると、
制御装置10は制御信号ライン13bに制御信号を出
し、流量調節弁15の開度を絞り、燃料系統の燃料を低
減して負荷量を制御し、更に温度が上昇し、上限温度、
例えば遮断温度以上となると、制御信号ライン13aに
制御信号を出力し、遮断弁16を閉じるように制御し、
ガスタービンをトリップさせる。Further, if the temperature rise continues,
The control device 10 outputs a control signal to the control signal line 13b, reduces the opening of the flow control valve 15, controls the load by reducing the fuel in the fuel system, further increases the temperature, increases the upper limit temperature,
For example, when the temperature becomes equal to or higher than the shut-off temperature, a control signal is output to the control signal line 13a to control the shut-off valve 16 to be closed,
Trip the gas turbine.
【0022】図2は上記に説明した状態を示す図であ
り、(a)は出口蒸気温度の推移、(b)は温度に応じ
た制御信号を示し、(a)において、正常時には(x)
で示すように計画出口温度前後の状態であり、(Y1 )
で示すように出口温度が時刻t 1 において上昇し、危険
温度を超えると制御装置10は燃焼器本体20が危険な
状態と判断し、(b)に示すように警報信号S1 を出力
し、危険温度を超えるt 1 〜t2 の間信号を継続して出
力し、警報装置11を作動させる。FIG. 2 is a diagram showing the state described above.
(A) shows the transition of the outlet steam temperature, and (b) shows the change according to the temperature.
(A) in normal operation, (x)
As shown by, the state is around the planned outlet temperature, and (Y1)
As shown in FIG. 1Rising in danger
If the temperature is exceeded, the control device 10 causes the combustor body 20 to be dangerous.
The state is determined, and as shown in FIG.1Output
And the temperature exceeds the dangerous temperature 1~ TTwoSignal is continuously output during
To activate the alarm device 11.
【0023】又、このt1 〜t2 の間で一定の時間継続
してt1 ’まで温度上昇が続くと、制御装置は(b)図
に示すように負荷量低下信号S3 を出力し、燃料系統1
4の流量調節弁15の開度を絞るように制御する。更
に、温度が上昇し、(Y2 )で示すように時刻t3 にお
いて遮断温度を超えると、(b)図のように遮断信号S
2 を出力し、燃料系統14の遮断弁16を遮断し、ガス
タービンをトリップさせる。Also, this t1~ TTwoConstant time between
Then t1If the temperature rise continues to ', the control device
As shown in FIG.ThreeAnd the fuel system 1
The control is performed so that the opening of the flow control valve 15 of No. 4 is reduced. Change
Then, the temperature rises and (YTwo), The time tThreeIn
When the temperature exceeds the shut-off temperature, the shut-off signal S as shown in FIG.
TwoAnd shut off the shutoff valve 16 of the fuel system 14 to
Trip the turbine.
【0024】なお図1の構成図においては複数の燃焼器
本体20で燃料系統14を共通にして流量調節弁15、
遮断弁16を共通に制御する例で省略して図示している
が、もちろん、各燃焼器本体20それぞれの燃料系統の
各流量調節弁、遮断弁をそれぞれ独立に制御することが
必要であり、各燃焼器の故障や異常をそれぞれ検出し、
異常を検出した燃焼器のみの燃料流量を制御し、遮断弁
を閉じるようにするものである。In the configuration diagram of FIG. 1, the flow control valve 15, the fuel system 14 is shared by a plurality of
Although the illustration is omitted in an example in which the shutoff valve 16 is commonly controlled, it is needless to say that it is necessary to control each flow control valve and the shutoff valve of the fuel system of each combustor body 20 independently. Detects failures and abnormalities of each combustor,
The fuel flow rate of only the combustor that has detected the abnormality is controlled to close the shutoff valve.
【0025】又、上記の実施の形態においては、燃焼器
の蒸気冷却の例で説明したが、本発明はこれに限定する
ものではなく、冷却対象部が燃焼器のみならず、静翼、
動翼の場合にも同様に温度監視ができ、同じ作用、効果
を奏することはもちろんである。Further, in the above embodiment, the example of steam cooling of the combustor has been described. However, the present invention is not limited to this.
In the case of the moving blade, the temperature can be monitored in the same manner, and the same operation and effect can be obtained.
【0026】以上説明の実施の形態によれば、燃焼器本
体20の冷却蒸気回収管26,27から回収ライン4で
回収される出口蒸気の温度を温度検出器8で検出し、制
御装置10に入力し、制御装置10で温度上昇を監視
し、出口蒸気の温度があらかじめ設定した温度を超える
と、警報装置12を作動させて警報を発し、又、流量調
節弁15を制御して燃料流量を制御したり、遮断弁16
を閉じて燃料を遮断するようにしたので、燃焼器の異常
の検出が出口蒸気温度の変化により早期に検知でき、ガ
スタービンの安全運転がなされる。According to the embodiment described above, the temperature of the outlet steam recovered from the cooling steam recovery pipes 26 and 27 of the combustor body 20 in the recovery line 4 is detected by the temperature detector 8 and When the temperature of the outlet steam exceeds a preset temperature, the alarm is activated by issuing an alarm, and the flow control valve 15 is controlled to control the fuel flow rate. Control or shut-off valve 16
Is closed to shut off the fuel, so that the abnormality of the combustor can be detected early by the change of the outlet steam temperature, and the safe operation of the gas turbine is performed.
【0027】[0027]
【発明の効果】本発明の蒸気冷却式ガスタービンの出口
蒸気監視システムは、燃焼器や翼等の冷却対象部に冷却
用蒸気を供給し、冷却後の蒸気を回収する蒸気冷却式ガ
スタービンにおいて、前記冷却後の蒸気の出口温度を検
出する温度検出器と、同温度検出器の検出信号を入力
し、あらかじめ設定された設定温度と比較し、同検出し
た温度が前記設定値を超えると警報信号、燃料流量調節
弁の開度を所定開度に絞る信号又は遮断弁を閉じる信号
を出力する制御装置とを具備してなることを特徴として
いる。このような構成により、冷却後の蒸気出口温度の
変化により、冷却対象部の異常が早期に検知されると共
に、制御装置からの制御信号が出力され、危険を回避す
ることができる。The outlet steam monitoring system for a steam-cooled gas turbine according to the present invention provides a steam-cooled gas turbine that supplies cooling steam to a portion to be cooled such as a combustor or a blade and collects the cooled steam. A temperature detector for detecting the outlet temperature of the steam after cooling, and a detection signal of the temperature detector is input, compared with a preset set temperature, and an alarm is issued when the detected temperature exceeds the set value. And a control device for outputting a signal, a signal for narrowing the opening of the fuel flow control valve to a predetermined opening, or a signal for closing the shutoff valve. With such a configuration, an abnormality in the cooling target portion is detected early due to a change in the steam outlet temperature after cooling, and a control signal is output from the control device, so that danger can be avoided.
【図1】本発明の実施の一形態に係る蒸気冷却式ガスタ
ービンの出口蒸気監視システムの構成図である。FIG. 1 is a configuration diagram of an outlet steam monitoring system of a steam-cooled gas turbine according to an embodiment of the present invention.
【図2】本発明の実施の一形態に係る蒸気冷却式ガスタ
ービンの出口蒸気監視システムの温度状態と制御信号の
関係を示し、(a)は温度状態、(b)は制御信号をそ
れぞれ示す。FIG. 2 shows a relationship between a temperature state and a control signal of an outlet steam monitoring system of a steam-cooled gas turbine according to an embodiment of the present invention, where (a) shows a temperature state and (b) shows a control signal, respectively. .
【図3】先行技術に係る蒸気冷却方式のガスタービン燃
焼器を示し、(a)がその概略側面図、(b)は本体壁
の一部の斜視図、(c)は(b)におけるA−A断面図
をそれぞれ示す。3A and 3B show a steam-cooled gas turbine combustor according to the prior art, wherein FIG. 3A is a schematic side view, FIG. 3B is a perspective view of a part of a main body wall, and FIG. 3C is A in FIG. -A sectional drawing is shown, respectively.
【図4】先行技術に係る蒸気冷却方式のガスタービン静
翼の断面図である。FIG. 4 is a sectional view of a steam-cooled gas turbine vane according to the prior art.
1 蒸気供給マニホールド 3 供給ライン 4 回収ライン 5 蒸気回収マニホールド 6,8 温度検出器 7 入口温度検出ライン 9 出口温度検出ライン 10 制御装置 11 表示装置 12 警報装置 13 制御信号ライン 14 燃料系統 15 流量調節弁 16 遮断弁 20 燃焼器本体 25 冷却蒸気供給管 26,27 冷却蒸気回収管 DESCRIPTION OF SYMBOLS 1 Steam supply manifold 3 Supply line 4 Recovery line 5 Steam recovery manifold 6,8 Temperature detector 7 Inlet temperature detection line 9 Outlet temperature detection line 10 Control device 11 Display device 12 Alarm device 13 Control signal line 14 Fuel system 15 Flow control valve 16 Shut-off valve 20 Combustor body 25 Cooling steam supply pipe 26, 27 Cooling steam recovery pipe
Claims (1)
を供給し、冷却後の蒸気を回収する蒸気冷却式ガスター
ビンにおいて、前記冷却後の蒸気の出口温度を検出する
温度検出器と、同温度検出器の検出信号を入力し、あら
かじめ設定された設定温度と比較し、同検出した温度が
前記設定値を超えると警報信号、燃料流量調節弁の開度
を所定開度に絞る信号又は遮断弁を閉じる信号を出力す
る制御装置とを具備してなることを特徴とする蒸気冷却
式ガスタービンの出口蒸気監視システム。1. A steam-cooled gas turbine for supplying cooling steam to a portion to be cooled such as a combustor or a blade and recovering the cooled steam, a temperature detector for detecting an outlet temperature of the cooled steam. And a detection signal of the same temperature detector, and compares it with a preset set temperature. If the detected temperature exceeds the set value, an alarm signal and the opening of the fuel flow control valve are reduced to a predetermined opening. A controller for outputting a signal or a signal for closing a shut-off valve, the outlet steam monitoring system for a steam-cooled gas turbine.
Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19032798A JP3735203B2 (en) | 1998-07-06 | 1998-07-06 | Steam monitoring system for steam cooled gas turbine |
| DE69931413T DE69931413T2 (en) | 1998-01-29 | 1999-01-22 | Cooled system in a combined cycle power plant |
| EP06100284A EP1752618A3 (en) | 1998-01-29 | 1999-01-22 | Steam cooled system in combined cycle power plant |
| EP01126611A EP1182330B1 (en) | 1998-01-29 | 1999-01-22 | Outlet steam monitoring system in steam cooled type gas turbine |
| DE69930557T DE69930557T2 (en) | 1998-01-29 | 1999-01-22 | Outlet flow monitoring system in a steam cooled gas turbine |
| EP99101211A EP0933505B1 (en) | 1998-01-29 | 1999-01-22 | Steam cooled system in combined cycle power plant |
| US09/237,845 US6324829B1 (en) | 1998-01-29 | 1999-01-27 | Steam cooled system in combined cycle power plant |
| CA002260415A CA2260415C (en) | 1998-01-29 | 1999-01-27 | Steam cooled system in combined cycle power plant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19032798A JP3735203B2 (en) | 1998-07-06 | 1998-07-06 | Steam monitoring system for steam cooled gas turbine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2000018050A true JP2000018050A (en) | 2000-01-18 |
| JP3735203B2 JP3735203B2 (en) | 2006-01-18 |
Family
ID=16256348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19032798A Expired - Lifetime JP3735203B2 (en) | 1998-01-29 | 1998-07-06 | Steam monitoring system for steam cooled gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3735203B2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6782691B2 (en) | 2001-04-17 | 2004-08-31 | Mitsubishi Heavy Industries, Ltd. | Gas turbine plant with high detection sensitivity of extraordinary state |
| US7788895B2 (en) | 2005-07-08 | 2010-09-07 | Mitsubishi Heavy Industries, Ltd. | Flashback-detecting equipment, flashback-detecting method and gas turbine |
-
1998
- 1998-07-06 JP JP19032798A patent/JP3735203B2/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6782691B2 (en) | 2001-04-17 | 2004-08-31 | Mitsubishi Heavy Industries, Ltd. | Gas turbine plant with high detection sensitivity of extraordinary state |
| US6868663B2 (en) | 2001-04-17 | 2005-03-22 | Mitsubishi Heavy Industries, Ltd. | Gas turbine plant with high detection sensitivity of extraordinary state |
| EP1251258A3 (en) * | 2001-04-17 | 2007-02-28 | Mitsubishi Heavy Industries, Ltd. | Gas turbine plant with detector of extraordinary state |
| US7788895B2 (en) | 2005-07-08 | 2010-09-07 | Mitsubishi Heavy Industries, Ltd. | Flashback-detecting equipment, flashback-detecting method and gas turbine |
| DE102006031551B4 (en) * | 2005-07-08 | 2014-09-04 | Mitsubishi Heavy Industries, Ltd. | Flashback detection device, flashback detection method and gas turbine |
Also Published As
| Publication number | Publication date |
|---|---|
| JP3735203B2 (en) | 2006-01-18 |
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