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JPS5918211A - Starting control method of steam turbine - Google Patents

Starting control method of steam turbine

Info

Publication number
JPS5918211A
JPS5918211A JP12710582A JP12710582A JPS5918211A JP S5918211 A JPS5918211 A JP S5918211A JP 12710582 A JP12710582 A JP 12710582A JP 12710582 A JP12710582 A JP 12710582A JP S5918211 A JPS5918211 A JP S5918211A
Authority
JP
Japan
Prior art keywords
turbine
starting
startup
thermal stress
schedule
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
JP12710582A
Other languages
Japanese (ja)
Other versions
JPH0442522B2 (en
Inventor
Michio Sakata
坂田 道夫
Yoichiro Kogure
木暮 洋一郎
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.)
Toshiba Corp
Original Assignee
Toshiba Corp
Tokyo Shibaura Electric Co 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 Toshiba Corp, Tokyo Shibaura Electric Co Ltd filed Critical Toshiba Corp
Priority to JP12710582A priority Critical patent/JPS5918211A/en
Publication of JPS5918211A publication Critical patent/JPS5918211A/en
Publication of JPH0442522B2 publication Critical patent/JPH0442522B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D19/00Starting of machines or engines; Regulating, controlling, or safety means in connection therewith

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)

Abstract

PURPOSE:To restrain the thermal stress within the range of specified value and obtain the minimum starting time by a method wherein a starting schedule is calculated, at the starting, according to a generator load when the generator load exceeds the specified value and the turbine rotor thermal stress exceeds the limited value. CONSTITUTION:At the starting of a steam turbine, a starting schedule calculating unit 3 stores a starting control command K from an operator and input signals P1-Pn of the electricity generating process required for the monitor control of the turbine via an input processing device 2 of a turbine starting control device 1. When a generator load exceeds the specified value, and a turbine rotor thermal stress exceeds limited value, also after passage of the specified time, said calculating unit 3 calculates the starting schedule according to the generator load. On the other hand, in case of other than said case, said calculating unit 3 calculates as usual the starting schedule as a function of a main steam temperature, a pressure and a turbine metal temperature, then starts the steam turbine via the starting control unit 4.

Description

【発明の詳細な説明】 〔発明の技術分野〕 本発明は蒸気タービンの起動制御方法に係υ、特にター
ビンの円滑な起動を行なうために最適な起動スケジュー
ルを得るようにした蒸気タービンの起動制御方法に関す
る。
[Detailed Description of the Invention] [Technical Field of the Invention] The present invention relates to a steam turbine startup control method, and particularly to a steam turbine startup control method that obtains an optimal startup schedule for smooth startup of the turbine. Regarding the method.

〔発明の技術的背景〕[Technical background of the invention]

一般に、タービンの起動に際しては、起動中に生ずる寿
命消費量を計画値以内に抑える必要がある為、運転中の
タービンメタル温度の変化を推定し、これによって発生
するロータ熱応力を計画寿命消費に相当する値以内に納
まるように、各起動段階における所要時間(以下、起動
スケジュールと称する)を推奨起動時間としてあらかじ
め決定している。
Generally, when starting a turbine, it is necessary to suppress the lifetime consumption that occurs during startup to within the planned value, so the change in turbine metal temperature during operation is estimated, and the rotor thermal stress that occurs due to this is reduced to the planned lifetime consumption. The time required for each startup stage (hereinafter referred to as a startup schedule) is predetermined as the recommended startup time so that it is within the corresponding value.

通常、比較的高負荷領域では主蒸気温度が一定している
ため、発電機負荷と第1段山口蒸気温度との関係から決
定し、通気時から低負荷領域においては、ボイラおよび
タービンの暖機状態等により主蒸気温度、タービンメタ
ル温度が複雑に変化するため、標準的なボイラおよびタ
ービンの温度特性をもとに想定し、通気時のミスマツチ
温度(第1段山口蒸気温度と第1段ケーソング内面メタ
ル温度との差で定義される温度)と第1段内面メタル温
度との関係から決定している。
Normally, the main steam temperature is constant in a relatively high load area, so it is determined from the relationship between the generator load and the first stage Yamaguchi steam temperature. Because the main steam temperature and turbine metal temperature change in a complicated manner depending on the conditions, etc., we assume that the mismatch temperature during ventilation (1st stage Yamaguchi steam temperature and 1st stage case song temperature) is based on the temperature characteristics of standard boilers and turbines. It is determined from the relationship between the first stage inner metal temperature (temperature defined as the difference from the inner metal temperature) and the first stage inner metal temperature.

〔背最技術の問題点〕[Problems with the latest technology]

ところが、実際の運転に際しては、通気時から低負荷領
域と高負荷領域との区別が極めて不明確であり、特にタ
ービン通気後からの途中起動やプラント事故発生後の再
起動のように通気後に起動制御を開始する場合、どちら
の起動スケジュールを使用するかは非常にあいまいで、
例えば起動プロセスの大きな1ベント(例えば、タービ
ン並列等)によ)区別しているのが実情である。この為
、タイミングによっては無理な起動スケジュールに基づ
いて運転されたり、または逆に必要以上に緩やかな起動
スケジュールに基づいて運転されている。
However, during actual operation, it is extremely unclear to distinguish between low-load areas and high-load areas from the time of ventilation, and especially when starting up after ventilation, such as during a mid-startup after turbine ventilation or restarting after a plant accident. When starting control, it is very ambiguous which startup schedule to use.
For example, the actual situation is that they are differentiated by one large vent in the startup process (for example, turbines in parallel). For this reason, depending on the timing, the system may be operated based on an unreasonable startup schedule, or conversely, it may be operated based on a startup schedule that is more gradual than necessary.

特に近年、原子発電所の増加に伴い、多くの火力発電所
がミドル負荷用としての運転がなされるようになってき
ている為、それによる起動・停止の回数が非常に多くな
り、ロータ熱応力を計画寿命済費に相当する値以内に抑
え、かつプラント起動時間を最短時間とするような起動
スケジュールに晶づくタービンの起動制御が強く望まれ
てきている。
Particularly in recent years, with the increase in the number of nuclear power plants, many thermal power plants are being operated as medium-load power plants, resulting in an extremely large number of startups and shutdowns, resulting in rotor thermal stress. There is a strong desire for turbine start-up control that achieves a start-up schedule that keeps the cost within a value equivalent to the planned lifetime cost and minimizes the plant start-up time.

〔発明の目的〕[Purpose of the invention]

本発明は上記のような事情に鑑みて成されたもので、そ
の目的はタービンの熱応力を計画値以内に抑えて最適な
起動時間とすることができる蒸気タービンの起動制卸指
令を提供することにある。
The present invention has been made in view of the above-mentioned circumstances, and its purpose is to provide a steam turbine startup control command that can suppress the thermal stress of the turbine within a planned value and provide an optimal startup time. There is a particular thing.

〔発明の概要〕[Summary of the invention]

上記目的を達成するために本発明では、タービン通気直
前にボイラからの主蒸気温度・圧力およびタービンのメ
タル温度を関数として各起動段階での所要時間である起
動スケジュールを求め、これに基づいて起動制御を行な
う蒸気タービンの起動制卸方法において、タービン通気
後に起動制卸指令がある場合発電機負荷およびタービン
ロータ熱応力を検出し、発電機負荷が規定値以上でかつ
タービンロータ熱応力が制限値以上と寿って規定時間以
上経過した時は発電機負荷に応じて起動スケジュールを
算出し、それ以外の時はタービン通気直前の主蒸気温度
・圧力およびタービンメタル温度を関数として起動スケ
ジュールを算出して蒸気ターピッを起動するようにした
ことを特徴とする。
In order to achieve the above object, the present invention calculates a startup schedule, which is the time required for each startup stage, as a function of the main steam temperature and pressure from the boiler and the turbine metal temperature just before venting the turbine, and starts the startup based on this. In the start control method for a steam turbine that performs control, if there is a start control command after turbine ventilation, the generator load and turbine rotor thermal stress are detected, and the generator load is greater than a specified value and the turbine rotor thermal stress is a limit value. If the specified time has passed, the startup schedule is calculated according to the generator load. Otherwise, the startup schedule is calculated as a function of the main steam temperature and pressure immediately before turbine ventilation and the turbine metal temperature. The feature is that the steam turbine is activated by

(発明の実施例〕 以下、本発明を図面に示す一実施例について説明する。(Embodiments of the invention) An embodiment of the present invention shown in the drawings will be described below.

第1図は、本発明によるタービン起動制御のシステム構
成例をブロック的に示したものである。第1図において
、1はタービン起動制御装置であシ、タービンの監視制
御に必要な発電プロセスの入力信号(Pl 、P、・・
・。
FIG. 1 is a block diagram showing an example of a system configuration for turbine start-up control according to the present invention. In Fig. 1, reference numeral 1 denotes a turbine start-up control device, which provides input signals (Pl, P, . . . ) for the power generation process necessary for monitoring and controlling the turbine.
・.

Pn)と、運転員からの起動制御指令には入力処理装置
2に読み込まれる。また、起動スケジュール計算部3は
、周期的に発電プロセスの入力信号(p、I p! t
・・・、Pn)と起動制御指令Kを入力処理装置2を介
して続み込み、後述する動作を実行する。さらに、起動
制御部4は起動制御指令Kがあった時(K−1)、起動
スケジュール計算部3で計算された起動スケジュールに
基づいて操作信号Sを出力する。
Pn) and the startup control command from the operator are read into the input processing device 2. In addition, the startup schedule calculation unit 3 periodically calculates the input signal (p, I p! t
. . , Pn) and the activation control command K via the input processing device 2 to execute the operations described below. Further, when there is a startup control command K (K-1), the startup control section 4 outputs an operation signal S based on the startup schedule calculated by the startup schedule calculation section 3.

第2図は、起動スケジュール計算部3の動作をフローチ
ャート図にて示したものである。図において、まずステ
ップ10でタービン通気タイミング成立後の第1回目パ
スかどうかを判断し、YESの時はステップ11で起動
スケジュール計算に必要なパラメータ入力、主蒸気温度
(MST)、主蒸気圧力(MS P )、第1段内面メ
タル温度(TFSI)等を記憶しステップ12へ進む。
FIG. 2 shows the operation of the startup schedule calculation section 3 in a flowchart. In the figure, first, in step 10, it is determined whether this is the first pass after the turbine ventilation timing is established, and if YES, in step 11, the parameters required for calculating the startup schedule, main steam temperature (MST), main steam pressure ( MS P ), first stage inner surface metal temperature (TFSI), etc. are stored, and the process proceeds to step 12.

ステップ12では、起動スケジュール計算タイプを判断
する条件となる、高圧部ロータ熱応力制限値(HPL)
と中圧部ロータ熱応力制限値(IPL)を、第1段内面
メタル温[(TF8I)と再熱蒸気冨内面メタル温度(
TRBI)を関数として計算する。
In step 12, the high pressure rotor thermal stress limit value (HPL) is determined as a condition for determining the startup schedule calculation type.
and intermediate pressure section rotor thermal stress limit value (IPL), first stage inner surface metal temperature [(TF8I) and reheat steam inner surface metal temperature (
TRBI) is calculated as a function.

第3図(a)は、この高圧部ロータ熱応力制限値(HP
L)と第1段内面) 9 ル1M If (TF8I 
)の関係をポすもので、HPL−f a(TF8I)で
表わされ、第3図(blは中圧部ロータ熱応力制限値(
IPL)とセ)熱蒸気室内面メタル温度(TRBI)の
関係を示すもので、IPL−fb(TRB I )で表
わされる。
Figure 3(a) shows this high pressure rotor thermal stress limit value (HP
L) and 1st stage inner surface) 9 Le1M If (TF8I
) is expressed as HPL-fa (TF8I), and in Figure 3 (bl is the intermediate pressure section rotor thermal stress limit value (
It shows the relationship between IPL) and c) thermal steam chamber inner surface metal temperature (TRBI), and is expressed as IPL-fb (TRBI).

一方、上記ステップ10での判断結果がNOの時は、ス
テップ11と12をバイパスしてステップ13へ進む。
On the other hand, if the determination result in step 10 is NO, steps 11 and 12 are bypassed and the process proceeds to step 13.

ステップ13では、運転員からの起動割部指令Kがある
かどうかを判断し、No(K=Q)の時は動作を完rし
次に起動する迄待機する。また、このステップ1つ・の
判断結果がYES(K−1)のときはステップ14へ進
み、発電機負荷(GEN)と高圧部・中圧部ロータ熱応
力を使って起動スゲジュールの計神、タイプを判断し、
計算タイプ1ならばステップ15へ、計算タイプ2なら
ばステップ16へ夫々進む。
In step 13, it is determined whether or not there is a starting dividing section command K from the operator, and if No (K=Q), the operation is completed and the system waits until the next starting. If the judgment result in this step is YES (K-1), proceed to step 14, and use the generator load (GEN) and the thermal stress of the high-pressure and intermediate-pressure rotors to calculate the starting schedule. determine the type,
If the calculation type is 1, the process goes to step 15, and if the calculation type is 2, the process goes to step 16.

ステップ14の判断結果、計算タイプ1が選択されると
ステップ15へ進み、ステップ11で記憶されたタービ
ン通気時の主蒸気温度 。
As a result of the determination in step 14, if calculation type 1 is selected, the process proceeds to step 15, where the main steam temperature during turbine ventilation stored in step 11 is determined.

(MST)、主蒸気圧力(MAT)および第1段内面メ
タル温度(TF8I)を関数として、起動スケジュール
を計算して動作を完了する。
(MST), main steam pressure (MAT), and first stage internal metal temperature (TF8I) to calculate a start-up schedule to complete the operation.

マタ、ステップ14の判断結果、計算タイプ2が選択さ
れるとステップ16へ進み、発電機負荷(GEN)を関
数として起動スゲジュールを計算し動作を完了する。
As a result of the determination in step 14, if calculation type 2 is selected, the process proceeds to step 16, where the startup schedule is calculated using the generator load (GEN) as a function, and the operation is completed.

なお、計算される起動スケジュールの項目としては、タ
ービン昇速率、定速保持時間、定格保持時間、負荷上昇
率、初負荷保持時間等がある。
Note that the items of the startup schedule that are calculated include the turbine speed increase rate, constant speed holding time, rated holding time, load increase rate, initial load holding time, etc.

一方第4図は、上記ステップ14で選択する計算タイプ
1,2の判断を示すロジック・チャート図であシ、第4
図において計算タイプ1が選択されるのは、次の(1)
〜(4)のいづれか1つを満足した時である。
On the other hand, FIG. 4 is a logic chart diagram showing the determination of calculation types 1 and 2 selected in step 14 above.
In the figure, calculation type 1 is selected as follows (1)
This is when any one of (4) to (4) is satisfied.

(11発電機負荷(GEN)が規定値(GL)以下の時
(11 When the generator load (GEN) is below the specified value (GL).

(2)高圧部ロータ熱応力(HPa)が制限値(HL)
 L )以上の時。
(2) High pressure part rotor thermal stress (HPa) limit value (HL)
L) or more.

(3)  中圧部ロータ熱応力(IPa)が制限値(I
PL)以上の時。
(3) The intermediate pressure rotor thermal stress (IPa) is the limit value (I
PL) or more.

(4)発電機負荷(GEN)が規定値(GL)以上、高
圧部ロータ熱応力(HP a )が制限値(HP T、
 )以下、および中圧部ロータ燕応力(IPm)が制限
値(I PL)以下となって規定時間(1)以内の時。
(4) The generator load (GEN) is above the specified value (GL), and the high pressure rotor thermal stress (HP a ) is the limit value (HP T,
) or less, and when the intermediate pressure section rotor swallow stress (IPm) is less than the limit value (I PL) and within the specified time (1).

また、計算タイプ2が選択されるのは次の(5)を満た
した時である。
Further, calculation type 2 is selected when the following (5) is satisfied.

(5)  発電機負荷(GBN)が規定値(GL)以上
、高圧部ロータ熱応力(HPa)が制限値(HPL)以
下、および中圧部ロータ熱応力(IPa)が制限値(I
 PL)以下となって規定時間(11以上の時。
(5) The generator load (GBN) is above the specified value (GL), the high pressure rotor thermal stress (HPa) is below the limit value (HPL), and the intermediate pressure rotor thermal stress (IPa) is below the limit value (I
PL) or less and the specified time (11 or more).

次に、上記(1)〜(5)で述べた規定値(GL)、制
限値(HPL)・(IPL)、および規定時間(t)、
について説明する。まず規定値(GL)は、第1段内面
メタル温度(TFt8I)、再熱蒸気室内面メタル温度
(TRBI)か、定格近くになる負荷帯を設定する。ま
た制限値(HPL)・(IPL)は、ステップ12でタ
ービン通気時の第1段内面メタル温度(TF8I)、ま
たは再熱蒸気室内面メタル温度(TRBI)を関数とし
て計算される。さらに規定時間(1)は、熱応力の安定
する時間であり、主蒸気温度の変化からロータ体積温度
が変化するまでの遅れ時間に対して数倍した値を設定す
る。
Next, the specified value (GL), limit value (HPL)/(IPL), and specified time (t) described in (1) to (5) above,
I will explain about it. First, the specified value (GL) is set to the first stage inner metal temperature (TFt8I), the reheat steam chamber inner metal temperature (TRBI), or a load range close to the rated value. The limit value (HPL) (IPL) is calculated in step 12 as a function of the first stage inner metal temperature (TF8I) during turbine ventilation or the reheat steam chamber inner metal temperature (TRBI). Further, the specified time (1) is a time during which thermal stress is stabilized, and is set to a value several times the delay time from a change in main steam temperature to a change in rotor volume temperature.

尚、上記実施例では、起動スケジュールの計算タイプ1
.2を選択する条件に発電機負荷(GBN)を使用して
いるが、これに代えて主蒸気温度(M8T)、第1段内
面メタル温度(TF8I)tたは再熱蒸気室内面メタル
温度(TRBI)等を使用する事も出来る。
In addition, in the above embodiment, startup schedule calculation type 1
.. The generator load (GBN) is used as the condition for selecting 2, but instead of this, the main steam temperature (M8T), the 1st stage inner metal temperature (TF8I) t, or the reheat steam chamber inner metal temperature ( TRBI) etc. can also be used.

その他、本発明はその要旨を変更しない範囲で、種々に
変形して実施することができるものである。
In addition, the present invention can be modified and implemented in various ways without changing the gist thereof.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明の蒸気タービン起動制御方法
によれば、発電機負荷が規定値以上となシかつタービン
ロータ熱応力が制限値以下となって規定時間経過した時
は発を機負荷に応じて起動スケジュールを計算し、それ
以外の時はタービン通気時の主蒸気温度・圧力および第
1段内面メタル温度を関数として起動スケジュールを計
算し、これに基づいて起動側副を行なうようにしたので
、起動中に発生するタービンのロータ熱応力を計画寿命
消費に相当する値以内に抑え、しかも最もタービンの状
態に適した最短起動時間を得ることができる。また、起
動スケジュールの計算タイプ1,2を区別する条件判定
に使用するロータ熱応力の制限値は、通気時の第1段内
面メタル温度又は再熱蒸気室内面メタル温度を関数とし
て算出しているので、タービンの起動形態に応じた最適
な制限値を得
As explained above, according to the steam turbine startup control method of the present invention, when the generator load is not above the specified value and the turbine rotor thermal stress is below the limit value and a specified period of time has elapsed, the generator is switched to the machine load. At other times, the startup schedule is calculated as a function of the main steam temperature and pressure during turbine ventilation and the first stage inner metal temperature, and startup auxiliaries are performed based on this. Therefore, it is possible to suppress the rotor thermal stress of the turbine generated during startup to within a value corresponding to the planned life consumption, and to obtain the shortest startup time most suitable for the condition of the turbine. In addition, the rotor thermal stress limit value used to determine the conditions for distinguishing startup schedule calculation types 1 and 2 is calculated as a function of the first stage inner metal temperature during ventilation or the reheat steam chamber inner metal temperature. Therefore, the optimal limit value can be obtained depending on the startup mode of the turbine.

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

第1図は本発明のタービン起動制御装置の一実施例を示
す構成図、第2図は第1図における起動スケジュール計
算部の動作を示すフローチャート図、第3図(8)は高
圧部ロータ熱応力制限値と第1段内面メタル温度との関
係を示す図、第3図(h)は中圧部ロータ熱応力制限値
と再熱蒸気室内面メタル温度との関係を示す図、第4図
は起動スケジュールの計算タイプの選択方法を示すロジ
ックチャート図である。 1・・・タービン起動制御装置、2・・・入力処理装置
、3・・・起動スケジュール計算部、4・・・起動制御
部。 出願人代理人 弁理士 鈴 江 武 彦第1図 第2図
Fig. 1 is a configuration diagram showing an embodiment of the turbine start control device of the present invention, Fig. 2 is a flowchart showing the operation of the start schedule calculation section in Fig. 1, and Fig. 3 (8) shows high pressure section rotor heat. Figure 3 (h) is a diagram showing the relationship between the stress limit value and the inner metal temperature of the first stage, and Figure 4 (h) is a diagram showing the relationship between the intermediate pressure section rotor thermal stress limit value and the inner metal temperature of the reheat steam chamber. 2 is a logic chart diagram showing a method for selecting a calculation type of a startup schedule. FIG. DESCRIPTION OF SYMBOLS 1... Turbine start-up control device, 2... Input processing device, 3... Start-up schedule calculation part, 4... Start-up control part. Applicant's representative Patent attorney Takehiko Suzue Figure 1 Figure 2

Claims (1)

【特許請求の範囲】[Claims] (1)  タービン通気直前にボイラからの主蒸気温度
・圧力およびタービンのメタル温度を関数とし7て各起
動段階での所要時間である起動スケジュールを求め、こ
れに基づいて起動制御を行なう蒸気タービンの起動制御
方法において、タービン通気後における起動制卸指令時
、発電機負荷およびタービンロータ熱応力を検出し、発
電機負荷が規定値以上で、かつタービンロータ熱応力が
制限値以上となって規定時間以上経過した時は発電機負
荷に応じて起動スケジュールを算出し、それ以外の時は
タービン通気直前の主蒸気温度・圧力およびタービンメ
タル温度を関数として起動スケジュールを算出して蒸気
タービンを起動するようにしたことを特徴とする蒸気タ
ービンの起動制御方法。 (2、特許請求の範囲第(1)項記載において、タービ
ンロータ熱応力の制限値はタービン通気直前のタービン
のメタル温度を関数として算出するようにしたものであ
る蒸気タービンの起動制御方法。
(1) Immediately before turbine ventilation, a startup schedule, which is the time required for each startup stage, is determined as a function of the main steam temperature and pressure from the boiler and the turbine metal temperature, and the startup control of the steam turbine is performed based on this. In the start-up control method, when a start-up control command is issued after turbine ventilation, the generator load and turbine rotor thermal stress are detected, and the generator load and turbine rotor thermal stress exceed a specified value for a specified period of time. When the above period has elapsed, the startup schedule is calculated according to the generator load, and at other times, the startup schedule is calculated as a function of the main steam temperature and pressure immediately before turbine ventilation, and the turbine metal temperature, and the steam turbine is started. A method for controlling start-up of a steam turbine, characterized in that: (2) A method for starting a steam turbine according to claim (1), wherein the limit value of the turbine rotor thermal stress is calculated as a function of the turbine metal temperature immediately before turbine ventilation.
JP12710582A 1982-07-21 1982-07-21 Starting control method of steam turbine Granted JPS5918211A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12710582A JPS5918211A (en) 1982-07-21 1982-07-21 Starting control method of steam turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12710582A JPS5918211A (en) 1982-07-21 1982-07-21 Starting control method of steam turbine

Publications (2)

Publication Number Publication Date
JPS5918211A true JPS5918211A (en) 1984-01-30
JPH0442522B2 JPH0442522B2 (en) 1992-07-13

Family

ID=14951719

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12710582A Granted JPS5918211A (en) 1982-07-21 1982-07-21 Starting control method of steam turbine

Country Status (1)

Country Link
JP (1) JPS5918211A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6079106A (en) * 1983-10-05 1985-05-04 Hitachi Ltd Starting control method for turbine
JPS62232002A (en) * 1986-04-02 1987-10-12 Hitachi Ltd Method for starting thermal power plant with small loss on schedule
CN103174471A (en) * 2013-04-19 2013-06-26 国家电网公司 Parameter-varying load optimization control method of thermal power generating unit
CN104775856A (en) * 2015-03-03 2015-07-15 国家电网公司 Rapid starting control method and rapid starting control system for steam turbine of combined cycle generating unit
CN106224018A (en) * 2016-07-26 2016-12-14 华电电力科学研究院 A kind of coal unit steam turbine the whole series Start-up and Adjustment method and system
CN106401666A (en) * 2016-07-26 2017-02-15 华电电力科学研究院 Coal-fired unit EH oil and turbine adjusting security system debugging method and system
CN108678814A (en) * 2018-05-14 2018-10-19 哈尔滨汽轮机厂有限责任公司 Steam turbine sequence starts method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5186604A (en) * 1975-01-29 1976-07-29 Hitachi Ltd TAABINSAITANJIKANKIDOSEIGYOHOHO
JPS5267402A (en) * 1975-12-01 1977-06-03 Hitachi Ltd Turbine schedule computer
JPS5534282A (en) * 1979-07-09 1980-03-10 Agency Of Ind Science & Technol Preparation of polymer with high radiation stability

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5186604A (en) * 1975-01-29 1976-07-29 Hitachi Ltd TAABINSAITANJIKANKIDOSEIGYOHOHO
JPS5267402A (en) * 1975-12-01 1977-06-03 Hitachi Ltd Turbine schedule computer
JPS5534282A (en) * 1979-07-09 1980-03-10 Agency Of Ind Science & Technol Preparation of polymer with high radiation stability

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6079106A (en) * 1983-10-05 1985-05-04 Hitachi Ltd Starting control method for turbine
JPH0350084B2 (en) * 1983-10-05 1991-07-31 Hitachi Ltd
JPS62232002A (en) * 1986-04-02 1987-10-12 Hitachi Ltd Method for starting thermal power plant with small loss on schedule
CN103174471A (en) * 2013-04-19 2013-06-26 国家电网公司 Parameter-varying load optimization control method of thermal power generating unit
CN104775856A (en) * 2015-03-03 2015-07-15 国家电网公司 Rapid starting control method and rapid starting control system for steam turbine of combined cycle generating unit
CN106224018A (en) * 2016-07-26 2016-12-14 华电电力科学研究院 A kind of coal unit steam turbine the whole series Start-up and Adjustment method and system
CN106401666A (en) * 2016-07-26 2017-02-15 华电电力科学研究院 Coal-fired unit EH oil and turbine adjusting security system debugging method and system
CN108678814A (en) * 2018-05-14 2018-10-19 哈尔滨汽轮机厂有限责任公司 Steam turbine sequence starts method

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