JPH02238103A - Turbine controller - Google Patents

Turbine controller

Info

Publication number
JPH02238103A
JPH02238103A JP5773089A JP5773089A JPH02238103A JP H02238103 A JPH02238103 A JP H02238103A JP 5773089 A JP5773089 A JP 5773089A JP 5773089 A JP5773089 A JP 5773089A JP H02238103 A JPH02238103 A JP H02238103A
Authority
JP
Japan
Prior art keywords
turbine
valve
speed
control
steam
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
JP5773089A
Other languages
Japanese (ja)
Inventor
Takumi Kawai
河合 巧
Tadahiko Iijima
忠彦 飯島
Sadao Yanagida
柳田 貞雄
Shintaro Tsuji
真太郎 辻
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 Ibaraki
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 Ibaraki, Hitachi Ltd filed Critical Hitachi Engineering Co Ltd Ibaraki
Priority to JP5773089A priority Critical patent/JPH02238103A/en
Publication of JPH02238103A publication Critical patent/JPH02238103A/en
Pending legal-status Critical Current

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  • Control Of Turbines (AREA)

Abstract

PURPOSE:To improve the controllability by once closing a reducing valve and an intercepting valve in the turbine speed run back control mode and setting the opening degree of the reducing valve to a memorized run back opening degree on the reopening and carrying out the turbine speed control with the intercepting valve. CONSTITUTION:When the turbine speed is increased, the difference between the aimed accelerating speed 105 and the aimed speed 101 is PI-calculated by a calculator 106, and the output is inputted into an integrator 109, and a control signal 130 is obtained. A reducing valve 3 is opened by the output which is obtained by adding the bias 112 on the start of opening of the reducing valve onto the control signal 130 by an adder 113, and the turbine speed increase is started. In run back, a switch 103 is turned OFF, and a switch 104 is turned ON, and the aimed speed is switched to the aimed run-back speed 102, and the difference from the turbine speed 128 is PI-calculated in the calculation part 106. A switch 121 is turned ON by the output of a comparator 115, and an intercepting valve control signal 150 as the output of a subtraction calculator 114 is added onto the reducing valve control signal by an adder 117, and the reducing valve 3 is perfectly closed.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、タービンバイパス系統を有する蒸気タービン
に係わり、特に該蒸気タービンの速度制御に関するもの
である。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a steam turbine having a turbine bypass system, and particularly to speed control of the steam turbine.

〔従来の技術〕[Conventional technology]

従来装置はタービン起動時加減弁を開し、一定開度とし
その後インターセプト弁を開し定格速度まで昇速する方
式となっていた。
Conventional equipment opens the regulator valve when starting the turbine, maintains a constant opening, and then opens the intercept valve to increase the speed to the rated speed.

タービン起動時加減弁を一定開度とするのは高圧タービ
ンの暖機に必要な手段である。
Setting the regulating valve to a constant opening degree when starting the turbine is a necessary means for warming up the high-pressure turbine.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

上記従来技術では、タービン速度のランバック制御の点
について配慮がされておらず、タービン速度のランバッ
ク制御時、インターセプトバイパス弁は閉動作するが、
加減弁が閉動作せず、夕一ビン速度がランバックしない
という問題点があった. 本発明の目的は、タービン速度ランバック時、すみやか
にタービン速度をランバックさせ、制御性を向上させる
ことにある。
In the above conventional technology, no consideration is given to the runback control of the turbine speed, and the intercept bypass valve closes during the runback control of the turbine speed.
There was a problem that the control valve did not close and the Yuichi bin speed did not run back. An object of the present invention is to promptly run back the turbine speed at the time of turbine speed runback and improve controllability.

〔課題を解決するための手段〕[Means to solve the problem]

上記目的は、タービン速度ランバック時インターセプト
バイパス弁と、加減弁を同時に全開とし、タービン速度
をランバックさせ、タービン速度が、目標ランバック速
度に達した時点でタービン速度の安定性と高圧タービン
の暖機のため、インターセプトバイパス弁と、加減弁を
再度開動作させるものである。
The above purpose is to fully open the intercept bypass valve and the control valve at the same time at the time of turbine speed runback, runback the turbine speed, and improve the stability of the turbine speed and the high pressure turbine when the turbine speed reaches the target runback speed. To warm up, the intercept bypass valve and control valve are opened again.

〔作用〕[Effect]

中圧タービンの起動方法は、高圧タービンの暖機のため
加減弁を一定開度し、インターセプト弁バスパス弁開し
中圧タービンに蒸気を流入させることによりタービンを
起動するものである。夕一ビン速度を最も早く下降させ
るためには、タービンに流入する蒸気を遮断することで
ある.従って、タービン速度ランバック時はタービン危
険速度範囲をすみやかに通過させるために、高圧タービ
ン、及び中圧タービンへ流入する蒸気量を制御する加減
弁、インターセプトバイパス弁を全閉させるものである
A method for starting an intermediate pressure turbine is to start the turbine by opening a control valve to a certain degree to warm up the high pressure turbine, and opening an intercept valve and bus pass valve to allow steam to flow into the intermediate pressure turbine. The fastest way to reduce the speed of the turbine is to cut off the steam flowing into the turbine. Therefore, during turbine speed runback, the regulator valve and intercept bypass valve that control the amount of steam flowing into the high-pressure turbine and intermediate-pressure turbine are fully closed in order to quickly pass through the critical turbine speed range.

〔実施例〕〔Example〕

第2図にタービンバイパス系統を有するタービン系統図
を示す。タービンバイパスとは、ボイラの加熱器で発生
した蒸気を蒸気タービンを通さずに、ボイラの再熱器,
復水器と循環させて、ボイラの起動時間の短縮,所内単
独運転の継続等を目的とするものである。第2図につい
て、タービンバイパス系統運転中の蒸気の流れを説明す
る。
FIG. 2 shows a turbine system diagram having a turbine bypass system. Turbine bypass refers to steam generated in the boiler heater being passed through the boiler reheater, without passing through the steam turbine.
The purpose of this system is to circulate the water with the condenser to shorten the boiler startup time and continue independent operation within the plant. Referring to FIG. 2, the flow of steam during operation of the turbine bypass system will be explained.

ボイラ1の加熱器18から発生した蒸気は,主蒸気系統
21からタービンバイパス系統23に流入し,タービン
バイパス系統の高圧バイパス弁(HPBV)14を通る
ことにより高圧タービン4をバイパスしてボイラ1の再
熱器6へ流入する。
Steam generated from the heater 18 of the boiler 1 flows from the main steam system 21 into the turbine bypass system 23, passes through the high pressure bypass valve (HPBV) 14 of the turbine bypass system, bypasses the high pressure turbine 4, and is supplied to the boiler 1. It flows into the reheater 6.

再熱器6を経て再熱された蒸気は、低圧バイパス弁15
を通って蒸気系統24より復水器12へ流入する. 従って中圧タービン10,低圧タービン11もバイパス
されることになる。以上の様にボイラ1で発生した蒸気
は、主蒸気系統21,タービンバイパス系統23,再熱
系統22,蒸気系統24を経て復水器12へ流入し蒸気
タービンをバイパスする。
The steam reheated through the reheater 6 is passed through the low pressure bypass valve 15.
It flows into the condenser 12 from the steam system 24 through the steam line 24. Therefore, the intermediate pressure turbine 10 and the low pressure turbine 11 are also bypassed. As described above, the steam generated in the boiler 1 flows into the condenser 12 through the main steam system 21, the turbine bypass system 23, the reheat system 22, and the steam system 24, and bypasses the steam turbine.

逆止弁5は、タービンバイパス系統23から、高圧ター
ビン4への蒸気の逆流を防止するためのものである.ボ
イラ1の加熱器18から高圧タービン4に至る主蒸気系
統21には、主蒸気止め弁(MSV)2、及び蒸気流量
を制御する加減弁(CV)3が設けられ、ボイラ1の再
熱器6から中圧タービン10に至る再熱系統22には再
熱蒸気止め弁(RSV)7と蒸気流量を制御するインタ
ーセプトバイパス弁(工cV)8及びインターセプトバ
イパス弁(ICBV)9が設けられている。そして、復
水器12の復水はポンプ装置19を備えた復水系統25
によってボイラ1の加熱器18に送給されるようになっ
ている。また発電機13は、蒸気タービンの負荷を取っ
ている.タービンバイパス系統を有する蒸気タービンを
起動する場合には、まず蒸気タービンをリセットし主蒸
気止め弁2と再熱蒸気止め弁7を全開しておき、高圧タ
ービンの暖機のため加減弁3を一定開度とし、インター
セプト弁バイパス弁9を徐々に開き蒸気タービンに蒸気
を流入させタービンを昇速させる。
The check valve 5 is for preventing backflow of steam from the turbine bypass system 23 to the high pressure turbine 4. The main steam system 21 from the heater 18 of the boiler 1 to the high-pressure turbine 4 is provided with a main steam stop valve (MSV) 2 and a control valve (CV) 3 that controls the steam flow rate. The reheat system 22 extending from the steam turbine 6 to the intermediate pressure turbine 10 is provided with a reheat steam stop valve (RSV) 7, an intercept bypass valve (engineering cV) 8, and an intercept bypass valve (ICBV) 9 that control the steam flow rate. . The condensate of the condenser 12 is supplied to a condensate system 25 equipped with a pump device 19.
The water is supplied to the heater 18 of the boiler 1 by the following. In addition, the generator 13 takes the load from the steam turbine. When starting a steam turbine with a turbine bypass system, first reset the steam turbine, fully open the main steam stop valve 2 and the reheat steam stop valve 7, and keep the control valve 3 at a constant level to warm up the high-pressure turbine. The intercept valve bypass valve 9 is gradually opened to allow steam to flow into the steam turbine and speed up the turbine.

併入後インターセプトバイパス弁9、及びインターセプ
ト弁8が開きインターセプト弁8が全開後、加減弁3が
関し、更に多くの蒸気流量をタービンに流入する.蒸気
タービンへの蒸気の流入量が増大するにつれ、高圧バイ
パス弁14,低圧バイパス弁15は閉まり、最終的には
全閉し通常の運転状態となる。
After the merging, the intercept bypass valve 9 and the intercept valve 8 are opened, and after the intercept valve 8 is fully opened, the control valve 3 is engaged, allowing even more steam to flow into the turbine. As the amount of steam flowing into the steam turbine increases, the high-pressure bypass valve 14 and the low-pressure bypass valve 15 close, and finally, they are fully closed and enter a normal operating state.

この蒸気タービンの速度制御の従来例を第3図により説
明する.タービン昇速時、目標加速度105と目標速度
101を設定することにより、演算部106でその偏差
をPI演算しその出力を積分器109に入力する。
A conventional example of speed control for this steam turbine will be explained with reference to FIG. When the turbine speed is increased, by setting the target acceleration 105 and target speed 101, the calculating section 106 calculates the PI of the deviation and inputs the output to the integrator 109.

積分器出力の制御信号130は保持回路110を通して
加算器13に入力される。加算器113ではさらに加減
弁開き始めバイアス112が入力される。
The control signal 130 output from the integrator is input to the adder 13 through the holding circuit 110. The adder 113 further receives a regulating valve opening start bias 112 as input.

この加算器113の出力で加減弁が開し、夕一ビンが昇
速始まる。インターセプト弁と加算弁の関係は第4図に
示す特性、すなわち制御信号130に対し先にインター
セプト弁が開しインターセプト弁全開後、加減弁が開す
る様に関数発生器118,119で決めている。
The output of this adder 113 opens the control valve, and the speed-up of the Yuichi bin begins. The relationship between the intercept valve and the addition valve is determined by the function generators 118 and 119 so that the intercept valve opens first in response to the control signal 130, and after the intercept valve is fully opened, the control valve opens. .

この加減弁3開度はタービン速度が50Orpm以上を
検出する比較器111が動作すると、その時のタービン
速度に相当する加減弁開度を記憶する保持回路110及
び切替SW120がONし加減弁は一定開度を保持する
When the comparator 111 that detects the turbine speed of 50 Orpm or more operates, the holding circuit 110 and the switching SW 120 that store the opening of the regulating valve corresponding to the turbine speed at that time are turned on, and the regulating valve 3 is kept open at a constant level. Maintain degree.

この後さらにタービン速度が上昇するにつれ積分器10
9の出力である制御信号130が大きくなり加算器11
4の出力は0から増加しインターセプトバイパス弁9が
開き、定格速度まで上昇する。
After this, as the turbine speed further increases, the integrator 10
The control signal 130 which is the output of adder 11 becomes large.
The output of No. 4 increases from 0, the intercept bypass valve 9 opens, and the output speed increases to the rated speed.

この時加減弁3は、併入するまで一定開度を保持する。At this time, the adjustment valve 3 maintains a constant opening degree until the joint is entered.

?ービン昇速過程で、タービンの振動が発生するとター
ビン速度を、ランバックさせる必要があるが、インター
セプトバイパス弁9のみ全開にしても加減弁3はウオー
ミングのために開しているためタービン速度がランバッ
ク目標速度まで下降する時間が長くタービン本体にとっ
て好ましくない。
? - When vibration occurs in the turbine during the speed-up process, it is necessary to run back the turbine speed, but even if only the intercept bypass valve 9 is fully opened, the regulator valve 3 is open for warming, so the turbine speed will not run back. It takes a long time to descend to the target back speed, which is unfavorable for the turbine body.

本発明は、高圧タービンのウオーミング機能をそこなう
ことなく、上記問題点を解決することにある。第1図は
本発明の制御内容を示す制御系統図である。
The present invention aims to solve the above-mentioned problems without impairing the warming function of the high-pressure turbine. FIG. 1 is a control system diagram showing the control contents of the present invention.

タービン速度は、目標速度101を目標として上昇して
いくが、例えば、第5図の時刻toのタービン速度30
00rpmでタービン振動大となると、目標速度をSW
103をOFF.SW104をONL,ランバック目標
速度102 (1000rpm)に切替る.この操作に
より、■ランバック目標速度102とタービン速度12
8との偏差(マイナス)を演算部106でPI演算し、
その出力を積分器109に入力する。
The turbine speed increases with the target speed 101 as the target, but for example, the turbine speed 30 at time to in FIG.
If the turbine vibration becomes large at 00 rpm, change the target speed to SW.
Turn off 103. Switch SW104 to ONL, runback target speed 102 (1000 rpm). With this operation, ■ Runback target speed 102 and turbine speed 12
The deviation (minus) from 8 is calculated by the calculation unit 106, and
The output is input to an integrator 109.

今時刻Toにおける制御信号130(EL)加減弁制御
信号140 (CVEL)インターセプト弁制御信号1
50(IVE!L)の値は第4図に示す様に、下記とな
っているとする。
Control signal 130 (EL) Adjustment valve control signal 140 (CVEL) Intercept valve control signal 1 at current time To
Assume that the value of 50 (IVE!L) is as follows, as shown in FIG.

CVIEL=CV開き始め位置+タービン速度500r
pm相当位置=10+5=15 EL=10 IVE;,=タービン速度3000rpm相当位置=5
(EL一タービン速度500rpJ当位置)制御信号1
30は上記した様にtoで10であるが、速度ランバッ
ク時(to=tt)演算部106でマイナスとなってい
るので、制御信号130は減少しプラス領域からマイナ
ス領域となる.従って減算器114の出力(IVEL)
はマイナスとなり比較器115が動作しSWI 21を
ONし、減算器114の出力であるインターセプト弁制
御信号150 (IVεし)を加減弁制御信号に加える
ことより加減弁制御信号140は15より減少し加減弁
開き始め点10以下となり加減弁3は20%開度から0
%開度(全開)となる。
CVIEL = CV opening start position + turbine speed 500r
pm equivalent position = 10 + 5 = 15 EL = 10 IVE;, = turbine speed 3000 rpm equivalent position = 5
(EL-Turbine speed 500rpJ current position) Control signal 1
30 is 10 in to as described above, but since it is negative in the calculation unit 106 during speed runback (to=tt), the control signal 130 decreases and changes from a positive region to a negative region. Therefore, the output of subtractor 114 (IVEL)
becomes negative, the comparator 115 operates, turns on the SWI 21, and adds the intercept valve control signal 150 (IVε), which is the output of the subtractor 114, to the regulator valve control signal, so that the regulator valve control signal 140 decreases from 15. The opening point of the adjustment valve becomes 10 or less, and the adjustment valve 3 goes from 20% opening to 0.
% opening (fully open).

これによりタービン速度はすみやかに降下しランバック
速度で整定することになる。
This causes the turbine speed to drop quickly and settle at the runback speed.

また、加減弁閉する手段として上記以外に速度ランバッ
ク時に (1)開き始めバイアスをOにする。
In addition, as a means for closing the adjustment valve, in addition to the above, (1) the opening bias is set to O during speed runback.

(2)切替SW120を○FFL制御信号130の信号
を加算器113に入力する。
(2) Input the switch SW 120 to the FFL control signal 130 to the adder 113.

が考えられる。is possible.

〔発明の効果〕〔Effect of the invention〕

速度ランバック時、積分器109出力は、マイナスの大
きな値になりランバック後の再起動時の制御性を考慮し
て例えば−10程度の下限リミツタを設けることにより
、再起動時積分積器109出力はすみやかにプラス領域
となりかつ、この時SWI 21がOFFになるため起
動時の500rpm相当位置まですみやかに関するため
再起動時の速度制御性の向上が計れる。
At the time of speed runback, the output of the integrator 109 becomes a large negative value. Considering the controllability at restart after the runback, a lower limiter of about -10, for example, is provided, so that the output of the integrator 109 at the time of restart is reduced. The output quickly reaches the positive range, and since the SWI 21 is turned off at this time, it quickly reaches the position equivalent to 500 rpm at startup, which improves speed controllability at restart.

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

第1図は本発明の実施例を示す図、第2図はシステム系
統図、第3図は従来技術の制御系統図、第4図は本発明
の動作を示す図、第5図は本発明の動作を示す図である
。 1・・・ボイラ、4・・・高圧タービン、10・・・中
圧タービン、11・・・低圧タービン、13・・・発電
機、101・・・目標速度設定、102・・・ランバッ
ク目標速度設定、103,104,120,121−・
−SW、105・・・目標加速度設定、106・・演算
部、109・・・積分器、110・・・保持回路、11
1,115・・・比較器、112・・・加減弁開き始め
バイアス、113,114,117・・・加算器、11
8,119・・・関数M2図
Fig. 1 is a diagram showing an embodiment of the present invention, Fig. 2 is a system diagram, Fig. 3 is a control system diagram of the prior art, Fig. 4 is a diagram showing the operation of the present invention, and Fig. 5 is a diagram of the present invention. FIG. DESCRIPTION OF SYMBOLS 1... Boiler, 4... High pressure turbine, 10... Intermediate pressure turbine, 11... Low pressure turbine, 13... Generator, 101... Target speed setting, 102... Runback target Speed setting, 103, 104, 120, 121-・
-SW, 105... Target acceleration setting, 106... Arithmetic unit, 109... Integrator, 110... Holding circuit, 11
1,115...Comparator, 112...Adjustment valve opening start bias, 113,114,117...Adder, 11
8,119...Function M2 diagram

Claims (1)

【特許請求の範囲】 1、ボイラからの蒸気が加減弁を経て高圧タービンに流
入し、さらに再熱器、タンターセプト弁を経て、中圧タ
ービンに流入する発電設備で、高圧タービン、中低圧タ
ービンをバイパスするバイパス弁を具備し、タービン起
動時はインターセプト弁により、タービン速度を制御す
ると同時に高圧タービンの暖機のため加減弁を開する手
段を有する制御装置において、加減弁開度記憶手段を設
け、振動発生時のタービン速度ランバック制御モードに
於て、タービン暖機制御中の、加減弁並びにインターセ
プト弁を同時に閉し、再開時、加減弁開度を、記憶せる
ランバック時開度にし、タービン速度制御をインターセ
プト弁で行うことを特徴としたタービン制御装置。 2、請求項1記載のタービン制御装置に於いて、速度制
御PI演算出力に下限リミッタを設けたことを特徴とし
たタービン制御装置。
[Claims] 1. A power generation facility in which steam from a boiler flows into a high-pressure turbine through a control valve, and further flows into an intermediate-pressure turbine through a reheater and a tantercept valve. In a control device that is equipped with a bypass valve for bypassing, and has means for controlling the turbine speed using an intercept valve when starting the turbine and at the same time opening the regulating valve to warm up the high-pressure turbine, a regulating valve opening degree storage means is provided, In the turbine speed runback control mode when vibration occurs, the regulator valve and intercept valve are closed simultaneously during turbine warm-up control, and when restarting, the regulator valve opening is set to the memorized runback opening, and the turbine is A turbine control device characterized by speed control using an intercept valve. 2. The turbine control device according to claim 1, further comprising a lower limiter provided for the speed control PI calculation output.
JP5773089A 1989-03-13 1989-03-13 Turbine controller Pending JPH02238103A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5773089A JPH02238103A (en) 1989-03-13 1989-03-13 Turbine controller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5773089A JPH02238103A (en) 1989-03-13 1989-03-13 Turbine controller

Publications (1)

Publication Number Publication Date
JPH02238103A true JPH02238103A (en) 1990-09-20

Family

ID=13064038

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5773089A Pending JPH02238103A (en) 1989-03-13 1989-03-13 Turbine controller

Country Status (1)

Country Link
JP (1) JPH02238103A (en)

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