JPS6038522B2 - Turbine control device - Google Patents

Turbine control device

Info

Publication number
JPS6038522B2
JPS6038522B2 JP55183985A JP18398580A JPS6038522B2 JP S6038522 B2 JPS6038522 B2 JP S6038522B2 JP 55183985 A JP55183985 A JP 55183985A JP 18398580 A JP18398580 A JP 18398580A JP S6038522 B2 JPS6038522 B2 JP S6038522B2
Authority
JP
Japan
Prior art keywords
speed
signal
valve opening
turbine
control section
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.)
Expired
Application number
JP55183985A
Other languages
Japanese (ja)
Other versions
JPS57108401A (en
Inventor
芳直 佐野
洋一 戸根
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
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 Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Priority to JP55183985A priority Critical patent/JPS6038522B2/en
Publication of JPS57108401A publication Critical patent/JPS57108401A/en
Publication of JPS6038522B2 publication Critical patent/JPS6038522B2/en
Expired legal-status Critical Current

Links

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin

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  • Control Of Turbines (AREA)

Description

【発明の詳細な説明】 本発明はタービンの制御装置に係り、特にその信頼性を
考慮したタービン制御装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a turbine control device, and particularly to a turbine control device that takes its reliability into consideration.

一般に、タービン制御装置は、第1のブロック1で示す
ように、速度制御部2と弁開度制御部3とから構成され
、入力する速度指令信号aに基づき、タービン4に流入
する蒸気流量を調整することにより、タービン4の速度
を指令値通りに制御するように構成されている。即ち、
入力速度指令信号aは、速度制御部2の比較器21でタ
ービン4の速度検出器5から帰還される美速度信号bと
比較され、その偏差信号は、補償器22で補償演算され
、弁関度指令信号cに変換される。
Generally, a turbine control device is composed of a speed control section 2 and a valve opening control section 3, as shown in a first block 1, and controls the flow rate of steam flowing into the turbine 4 based on an input speed command signal a. By adjusting, the speed of the turbine 4 is controlled according to the command value. That is,
The input speed command signal a is compared with the speed signal b fed back from the speed detector 5 of the turbine 4 by the comparator 21 of the speed control section 2, and the deviation signal is subjected to compensatory calculation by the compensator 22, and then the valve is converted into a degree command signal c.

この弁開度指令信号cは、弁開度制御部の比較器31で
タービン4に流入する蒸気流量を調節する弁6に設けら
れた弁開度検出器7から帰還される実速度信号dと比較
される。その偏差信号は補償器32を介して関度調節信
号dに変換される。この開度調節信号dにより弁駁動部
8を介して弁6の関度が調節され、タービン4への流入
蒸気量が調整される。これにより、タービン4は流入蒸
気量と実負荷とに応じて加速または減速され、最終的に
双方がバランスした状態で定常運転が行われる。ところ
で、タービン4には図示せぬ発電機が接続され、その発
生電力を電力系統に出力しているため、タービン制御装
置1自体の故障あるいは速度検出器5の故障により、タ
ービン4の制御が正常に行われなくなると、電力系統に
周波数変動等の悪影響を及ぼし、最悪の場合は系統運用
にも支障を来たすことになる。
This valve opening command signal c is combined with an actual speed signal d fed back from a valve opening detector 7 provided in a valve 6 that controls the flow rate of steam flowing into the turbine 4 by a comparator 31 of a valve opening controller. be compared. The deviation signal is converted into a relationship adjustment signal d via a compensator 32. This opening adjustment signal d adjusts the valve 6 via the valve reversal unit 8, and the amount of steam flowing into the turbine 4 is adjusted. As a result, the turbine 4 is accelerated or decelerated depending on the amount of incoming steam and the actual load, and finally steady operation is performed with both of them being balanced. By the way, since a generator (not shown) is connected to the turbine 4 and outputs the generated power to the power grid, the control of the turbine 4 may not be normal due to a failure of the turbine control device 1 itself or a failure of the speed detector 5. If this is not done properly, it will have a negative impact on the power system, such as frequency fluctuations, and in the worst case, it will also disrupt system operation.

このため、従釆は、タービン4に蒸気流量を供給する蒸
気経路に複数個の弁6、弁開度検出器7、弁駁動部8を
設ける一方、速度検出器5を2個設け、タービン制御装
置第2図に示すように構成し、タービン制御装置の信頼
性の向上を計っていた。
For this reason, the follower is provided with a plurality of valves 6, a valve opening degree detector 7, and a valve reversal part 8 in the steam path that supplies the steam flow rate to the turbine 4, and two speed detectors 5 are provided, and the turbine The control device was constructed as shown in Figure 2 in order to improve the reliability of the turbine control device.

即ち、2個の速度検出器5からそれぞれ個別に帰還され
る実速度信号q,Qは対応する2系統の速度制御部2で
、それぞれれ速度指令信号aと比較され、偏差補償演算
が行われて、弁開度指令信号c,,c2に変換される。
That is, the actual speed signals q and Q fed back individually from the two speed detectors 5 are compared with the speed command signal a in the corresponding two systems of speed control sections 2, and a deviation compensation calculation is performed. are converted into valve opening command signals c, , c2.

これらの弁開度指令信号c,,c2は、低値選択回路9
により、そのうち代数的低値の信号cが選択され、複数
個の弁関度制御部3に出力される。この弁関度指令信号
cは各弁開度制御部3でそれぞれ個別に帰還される実開
度信号d.,Q,d3・・・と比較され、偏差補償演算
が行われて、それぞれの弁開度調節信号だ,,e2,e
2・・・変換され、それぞれ対応する弁駆動部8に出力
され、タービン4の制御が行われる。上記従来構成によ
れば、速度検出器5と速度制御部2が2系統存在するた
め、これら2系統のうちいずれか一方に異常が生じ、こ
れら2系統のうちいずれか一方に異常が生じ、その結果
、弁開度指令信号c,,c2のいずれか一方が異常高と
なっても、低値選択回路9により、正常な信号が選択さ
れ、弁開度指令信号cとして各弁開度制御部3に出力さ
れる。
These valve opening command signals c, , c2 are sent to the low value selection circuit 9
Accordingly, the signal c having an algebraically low value is selected and outputted to the plurality of valve function control units 3. This valve function command signal c is an actual opening degree signal d. which is fed back individually by each valve opening degree control section 3. , Q, d3..., deviation compensation calculation is performed, and the respective valve opening adjustment signals, , e2, e
2... are converted and output to the corresponding valve drive units 8, and the turbine 4 is controlled. According to the above conventional configuration, since there are two systems of the speed detector 5 and the speed control section 2, an abnormality occurs in one of these two systems; As a result, even if one of the valve opening command signals c, c2 becomes abnormally high, a normal signal is selected by the low value selection circuit 9 and is sent to each valve opening control unit as the valve opening command signal c. 3 is output.

従って、弁開度指令信号に,,c2のいずれか一方が異
常高となるような速度検出器5または速度制御部2の故
障に対しては、正常な運転の継続が行われ、タービン制
御装置の信頼性の向上が見られる。しかしながら、上記
従来のタービン制御装置においては、‘1}、弁開度指
令c,,c2の一方が異常低に落ちるような故障が生じ
た場合、低値選択回路9で故障系統の信号が選択され、
この結果、他方の系統が正常な弁関度指令信号を出力し
ているにもかかわらず、弁6が閉鎖方向に制御され、タ
ービンが運転停止する。
Therefore, in the event of a failure in the speed detector 5 or the speed control unit 2 in which either the valve opening command signal or c2 becomes abnormally high, normal operation continues, and the turbine control device An improvement in reliability can be seen. However, in the conventional turbine control device described above, when a failure occurs in which one of the valve opening commands c, c2 falls to an abnormally low value, the low value selection circuit 9 selects the signal of the failure system. is,
As a result, the valve 6 is controlled in the closing direction, and the turbine is stopped, even though the other system is outputting a normal valve function command signal.

‘2)、速度検出器5または速度制御部2を点検するた
めに、2系統のうち一方の機能を停止させると、弁関度
指令信号c.,c2の一方が異常低となり、運転停止に
つながる。{3’、低値選択回路9には冗長性がないた
め、もしこれが故障すると、全ての弁6の制御が不能と
なる等の不具合があった。本発明は、上記不具合を除き
、タービンの速度検出器あるいは制御装置内部系統の単
一故障により、高/低いずれの異常信号が生じても、タ
ービンの正常運転を可能とする信頼性の高いタービン制
御装置を提供することを目的とする。
'2) When the function of one of the two systems is stopped in order to inspect the speed detector 5 or the speed control unit 2, the valve function command signal c. , c2 becomes abnormally low, leading to a shutdown of the operation. {3') Since the low value selection circuit 9 does not have redundancy, if this circuit were to fail, there would be problems such as control of all valves 6 becoming impossible. The present invention provides a highly reliable turbine that allows normal operation of the turbine even if either a high or low abnormal signal occurs due to a single failure in the turbine speed detector or control device internal system, except for the above-mentioned problems. The purpose is to provide a control device.

この目的を達成するため、本発明は、タービンの速度検
出器および速度制御部をそれぞれ3個ずつ設け、各速度
検出器から出力される各実速度信号のうち、中間値を各
速度制御部に入力し、更に各速度制御部から出力される
信号のうち、中間値を弁関度指令信号として、弁関度制
御部に入力するようにしたことを特徴とする。
In order to achieve this object, the present invention provides three speed detectors and three speed control units for the turbine, and sends an intermediate value of each actual speed signal output from each speed detector to each speed control unit. The present invention is characterized in that an intermediate value of the signals input and further output from each speed control section is input to the valve speed control section as a valve speed command signal.

以下、本発明を第3図を参照して説明する。The present invention will be explained below with reference to FIG.

第3図は、本発明の一実施例に係るタービン制御装置の
姿部構成図で、図中、第1図および第2図と同一符号は
同一又は相当部分を示し、第2図の従来構成と異なる点
は、速度検出器5、速度制御部2をそれぞれ3個ずつ設
けると共に、各速度制御部2および弁関度制御部3の手
前には、それぞれ中間値選択回路10および1 1を設
置し、3個の速度検出器5から出力される各実速度信号
q,b2,b3を中間値選択回路101こ入力する一方
、3個の速度制御部2から出力される各弁開度信号に,
,c2,c3を各中間値選択回路1 1に入力すること
により、タービン制御装置の信頼性を高めた点にある。
この中間値選択回路10および1 1は入力する3つの
信号のうち、代数的中闇値をもつ信号を選択し出力する
ように構成されている。
FIG. 3 is a schematic diagram of a turbine control device according to an embodiment of the present invention, in which the same reference numerals as in FIGS. 1 and 2 indicate the same or corresponding parts, and the conventional configuration The difference is that three speed detectors 5 and three speed control sections 2 are provided, and intermediate value selection circuits 10 and 11 are provided in front of each speed control section 2 and valve control degree control section 3, respectively. The actual speed signals q, b2, b3 output from the three speed detectors 5 are input to the intermediate value selection circuit 101, while the valve opening signals output from the three speed controllers 2 are inputted to the intermediate value selection circuit 101. ,
, c2, and c3 are input to each intermediate value selection circuit 11, thereby increasing the reliability of the turbine control device.
The intermediate value selection circuits 10 and 11 are configured to select and output a signal having an algebraic intermediate value from among the three input signals.

本実施例のタービン制御装置はこのように構成されて、
3個の速度検出器5から出力される実速度信号広,Q,
b3は、それぞれ各中間値選択回路101こ入力される
The turbine control device of this embodiment is configured as described above,
Actual speed signals output from three speed detectors 5, Q,
b3 is input to each intermediate value selection circuit 101, respectively.

すると、各中間値選択回路10からは、そのうちの代数
的中間値を示す信号、即ち、bm=mean(q,Q,
b3) …0〕なる実速度信号bmが出力
される。
Then, each intermediate value selection circuit 10 outputs a signal indicating the algebraic intermediate value, that is, bm=mean(q, Q,
b3) ...0] is output.

その実速度信号bmは、速度制御部2で前述したように
、速度指令信号aと比較され、その偏差補償演算が行わ
れ、3個の速度制御部2からは、それぞれ弁開度指令信
号c,,c2,c3が出力される。同様にして、これら
の弁関度指令信号c,,c2,c3も複数個の弁開度制
御部3の手前に設けられた各中間値選択回路1 1に入
力され、各中間値直選択回路11からは、cm=mea
n(c,,c2,c3) …‘21なる弁
関度信号cmが出力される。
As described above, the actual speed signal bm is compared with the speed command signal a in the speed control section 2, and the deviation compensation calculation is performed, and the three speed control sections 2 output the valve opening command signal c, , c2, c3 are output. Similarly, these valve function command signals c, c2, c3 are also input to each intermediate value selection circuit 11 provided before the plurality of valve opening degree control sections 3, and each intermediate value direct selection circuit From 11, cm=mea
A valve function degree signal cm of n(c,,c2,c3)...'21 is output.

更に、この弁開度信号cmと実弁関度信号d,,も,d
3・・・とに基づき、各弁開度制御部3からは各弁開度
調節信号el’e2’e3…が出力される。これらの弁
関度調節信号e,,e2,e3・・・により、タービン
蒸気流入経路に並列に設けられた弁6の開度が調節され
る結果、速度検出器5、速度制御部2に単一故障が生じ
ても、常に、タービンの回転速度は指令値通りに制御さ
れる。
Furthermore, this valve opening degree signal cm and the actual valve relationship signal d,, are also
3..., each valve opening degree control section 3 outputs each valve opening degree adjustment signal el'e2'e3.... These valve function adjustment signals e,, e2, e3... adjust the opening degree of the valve 6 provided in parallel to the turbine steam inflow path. Even if a single failure occurs, the rotational speed of the turbine is always controlled according to the command value.

即ち、今、各速度検出器5から出力される実速度信号q
,Q,b3が次のような値であるとする。
That is, the actual speed signal q now output from each speed detector 5
, Q, b3 have the following values.

b,=Q+8, …【3
}Q=Q …{4}Q
=Q−B2 …{51(但し
、8,,82は共に0に近い正の値とする)すると、前
記‘1ー式により、中間値選択回路10からは、実速度
信号bm=Q=Qが出力される。
b,=Q+8, …[3
}Q=Q ...{4}Q
=Q-B2...{51 (however, 8, , 82 are both positive values close to 0) Then, according to the above formula '1-, the intermediate value selection circuit 10 outputs the actual speed signal bm=Q=Q is output.

このとき、実速度信号らが異常となり、b2>Q+6.
に変化すれば、bm=b,=Q+8,となり、実速度信
号Qに代って広が選択され出力される。一方、実速度信
号b{ニーが広くQ−82に変化すれば、bm=広=Q
+82となり、美速度信号広が選択され出力されれる。
このことから、実速度信号らの異常高、異常低いずれの
変化に対しても、中間値選択回路10から出力される美
速度信号bmは、高々8(8=B,or82)にとどま
り、速度検出器の故障の波及が防止されることが判る。
At this time, the actual speed signals become abnormal, and b2>Q+6.
If it changes to , then bm=b,=Q+8, and instead of the actual speed signal Q, it is selected and output. On the other hand, if the actual speed signal b{knee changes to wide Q-82, bm=wide=Q
+82, and the beautiful speed signal is selected and output.
Therefore, regardless of whether the actual speed signal is abnormally high or abnormally low, the beautiful speed signal bm output from the intermediate value selection circuit 10 remains at most 8 (8=B, or 82), and the speed It can be seen that the spread of detector failure is prevented.

勿論、これは美速度信号Qの異常だけでなく、実速度信
号b,あるいはb3の異常に対しても同様なことが言え
る。同様にして、各速度制御部2から出力される弁関度
指令信号c.,c2,c3は、中間値選択回路1 1に
より選択され出力される結果、弁開度指令信号C,,C
2,C3のうち1つの信号が異常高または異常低になっ
たとしても、それぞれの弁開度制御部3には、正常な弁
開度指令信号cmが入力される。
Of course, the same applies not only to abnormalities in the beautiful speed signal Q but also to abnormalities in the actual speed signal b or b3. Similarly, each speed control section 2 outputs a valve function command signal c. , c2, c3 are selected and output by the intermediate value selection circuit 11, resulting in valve opening command signals C,, C
Even if one of the signals C2 and C3 becomes abnormally high or abnormally low, a normal valve opening command signal cm is input to each valve opening control section 3.

このように、速度検出器5の単一故障に帰因する実速度
信号q,Q,b3のうちの1つの信号の異常は他の実速
度信号で補償され、また、速度制御部2の単一故障に帰
因する弁閥度指令信号c,,c2,c3のうち1つの信
号の異常は他の弁開度指令信号で補償される結果「速度
検出器の単一故障は下流の速度制御部に波及することな
く、また、速度制御部の単一故障は下流の弁関度制御部
に波及することなく、運転員の継続が可能となる。また
、本実施例では、3個存在する速度検出器5あるいは速
度制御部2の1つを点検のため制御ループから切り離し
ても、上述した理由により、タービンの運転に何ら支障
を及ぼさない。更に、本実施例では、中間値選択回路1
0を各速度制御部2に付属して設けているため、そのう
ち1個が故障しても上述同様運転に支障を及ぼさない。
In this way, an abnormality in one of the actual speed signals q, Q, b3 due to a single failure in the speed detector 5 is compensated for by the other actual speed signal, and the single fault in the speed controller 2 An abnormality in one of the valve opening command signals c, c2, c3 caused by a single failure is compensated for by the other valve opening command signal. In addition, a single failure in the speed control section will not affect the downstream valve control section, allowing operators to continue operating.In addition, in this embodiment, there are three Even if the speed detector 5 or one of the speed controllers 2 is disconnected from the control loop for inspection, there will be no problem in the operation of the turbine for the reasons mentioned above.Furthermore, in this embodiment, the intermediate value selection circuit 1
0 attached to each speed control section 2, even if one of them breaks down, the operation will not be affected as described above.

尚、上記実施例における3つの実速度信号b,,Q,b
3および3つの弁開度指令信号c,,c2,c3をモニ
タリングすることにより、速度検出器5および速度制御
部2の故障を診断することが可能となり、タービン制御
装置の信頼性を高めることができる。
In addition, the three actual speed signals b, , Q, b in the above embodiment
By monitoring the valve opening command signals c, , c2, and c3, it is possible to diagnose a failure in the speed detector 5 and the speed control unit 2, thereby increasing the reliability of the turbine control device. can.

また、中間値選択回路11あるいは弁開度制御部3の故
障による弁6の調節不能が生じても、上位ループよりの
負荷指令で補償することにより、応急的なタービンの運
転継続が可能となる。更にまた、上記実施例では、中間
値選択回路10,11を各速度B制御部3にそれぞれ付
属して設け、冗長度を大きくし、信頼性を高めるように
したが、この中間値選択回路10,1は、それ自体の信
頼性が他の回路に比べて非常に大きければ、減らすこと
も可能である。
Furthermore, even if the valve 6 cannot be adjusted due to a failure in the intermediate value selection circuit 11 or the valve opening control unit 3, it is possible to continue operating the turbine in an emergency by compensating with the load command from the upper loop. . Furthermore, in the above embodiment, the intermediate value selection circuits 10 and 11 are provided attached to each speed B control section 3 to increase redundancy and improve reliability. , 1 can be reduced if the reliability of the circuit itself is very high compared to other circuits.

以上のように、本発明によれば、速度検出器、速度制御
部をそれぞれ3個ずつ設け、前段より出力される3つの
信号のうちの中間値信号を次段に供給するようにしたの
で、速度検出器あるいは速度制御部の単一故障による高
低いずれの異常信号に対しても正常運転可能、オンライ
ン状態で保守点検可能および故障の影響を極小化したき
わめて信頼性の高いタービン制御装慣が得られる。
As described above, according to the present invention, three speed detectors and three speed control units are provided, and the intermediate value signal of the three signals output from the previous stage is supplied to the next stage. An extremely reliable turbine control system that allows normal operation even when high or low abnormal signals are caused by a single failure in the speed detector or speed control unit, allows online maintenance and inspection, and minimizes the effects of failures. It will be done.

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

第1図は一般的なタービン制御装置のブロック構成図、
第2図は従来のタービン制御装置の要部構成図、第3図
は本発明の一実施例を示すタービン制御装置のブロック
構成図である。 1・・・タービン制御装置、2・・・速度制御部、3・
・・弁関度制御部、4・・・タービン、5・・・速度検
出器、6・・・弁、7・・・弁開度検出器、8・・・弁
駆動部、9・・・低値選択回路、10,11・・・中間
値選択回路、21,31・・・比較器、22,23・・
・補償器。 第1図第2図 第3図
Figure 1 is a block diagram of a general turbine control device.
FIG. 2 is a block diagram of a main part of a conventional turbine control device, and FIG. 3 is a block diagram of a turbine control device showing an embodiment of the present invention. DESCRIPTION OF SYMBOLS 1... Turbine control device, 2... Speed control part, 3...
...Valve function control section, 4...Turbine, 5...Speed detector, 6...Valve, 7...Valve opening degree detector, 8...Valve drive unit, 9... Low value selection circuit, 10, 11... Intermediate value selection circuit, 21, 31... Comparator, 22, 23...
・Compensator. Figure 1 Figure 2 Figure 3

Claims (1)

【特許請求の範囲】[Claims] 1 タービンの回転速度を検出して実速度信号を出力す
る速度検出器と、速度指令信号と上記実速度信号を入力
してタービン蒸気流量を調整する弁の弁開度指令信号を
出力し、タービンの速度を制御する速度制御部と、上記
弁開度指令信号と上記弁の実開度信号を入力として弁開
度調整信号を出力し、弁開度を制御する弁開度制御部と
から成るタービン制御装置において、上記速度検出器と
、上記速度制御部とをそれぞれ3個ずつ設けると共に、
上記速度制御部および上記弁開度制御部の手前にそれぞ
れ中間値選択回路を設け、上記3個の速度検出器から出
力される3つの実速度信号の中間値の信号を上記速度制
御部に供給すると共に、上記3個の速度制御部から出力
される3つの弁開度指令信号の中間値の信号を上記弁開
度制御部に供給することを特徴とするタービン制御装置
1 A speed detector that detects the rotational speed of the turbine and outputs an actual speed signal; and a speed detector that inputs the speed command signal and the actual speed signal to output a valve opening command signal for adjusting the turbine steam flow rate; and a valve opening control section that receives the valve opening command signal and the actual valve opening signal as input, outputs a valve opening adjustment signal, and controls the valve opening. In the turbine control device, three speed detectors and three speed control units are provided, and
An intermediate value selection circuit is provided before the speed control section and the valve opening control section, and a signal of an intermediate value of the three actual speed signals output from the three speed detectors is supplied to the speed control section. At the same time, the turbine control device is characterized in that a signal having an intermediate value of the three valve opening command signals outputted from the three speed control sections is supplied to the valve opening control section.
JP55183985A 1980-12-26 1980-12-26 Turbine control device Expired JPS6038522B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55183985A JPS6038522B2 (en) 1980-12-26 1980-12-26 Turbine control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55183985A JPS6038522B2 (en) 1980-12-26 1980-12-26 Turbine control device

Publications (2)

Publication Number Publication Date
JPS57108401A JPS57108401A (en) 1982-07-06
JPS6038522B2 true JPS6038522B2 (en) 1985-09-02

Family

ID=16145292

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55183985A Expired JPS6038522B2 (en) 1980-12-26 1980-12-26 Turbine control device

Country Status (1)

Country Link
JP (1) JPS6038522B2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60259709A (en) * 1984-06-05 1985-12-21 Mitsubishi Electric Corp Control unit for steam turbine
US5192493A (en) * 1989-08-30 1993-03-09 Westinghouse Electric Corp. Median signal selector for feedwater control systems
KR100326523B1 (en) * 1999-08-27 2002-03-02 윤영석 Device and method for sensing overspeed prime mover
KR101134139B1 (en) 2009-08-05 2012-04-09 한국전력공사 Method and driver monitoring system for continuing operation of turbine generator on loss of speed pick unit
JP6013168B2 (en) * 2012-12-12 2016-10-25 株式会社東芝 Turbine overspeed prevention system and method

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS552562Y2 (en) * 1974-08-19 1980-01-23
JPS56101202A (en) * 1980-01-16 1981-08-13 Mitsubishi Atom Power Ind Inc Multiplex control method of process

Also Published As

Publication number Publication date
JPS57108401A (en) 1982-07-06

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