JPS5922457B2 - Synchronous machine step-out prediction method - Google Patents
Synchronous machine step-out prediction methodInfo
- Publication number
- JPS5922457B2 JPS5922457B2 JP54023410A JP2341079A JPS5922457B2 JP S5922457 B2 JPS5922457 B2 JP S5922457B2 JP 54023410 A JP54023410 A JP 54023410A JP 2341079 A JP2341079 A JP 2341079A JP S5922457 B2 JPS5922457 B2 JP S5922457B2
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- Japan
- Prior art keywords
- synchronous machine
- magnetic flux
- synchronous
- torque
- flux
- 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.)
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- Supply And Distribution Of Alternating Current (AREA)
- Control Of Eletrric Generators (AREA)
Description
【発明の詳細な説明】
この発明は、同期機が脱調する恐れのある危険状態にあ
ることを検知して脱調を予測する同期機の脱調子測方式
に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an out-of-step measurement method for a synchronous machine that detects that the synchronous machine is in a dangerous state where there is a risk of out-of-step and predicts out-of-step.
電力系統に接続された同期機が脱調(同期はずれ)状態
になつた場合は、その系統全体が乱調状態に陥る危険が
ある。If a synchronous machine connected to an electric power system goes out of synchronization (out of synchronization), there is a risk that the entire system will fall into disorder.
そこで、同期機が脱調する恐れのある危険状態になつた
場合には、脱調状態に至らしめないよう界磁制御するか
、またはその同期機を系統から分離する等の処置を施す
必要がある。従来における同期機脱調検出方式として、
電力継電器とインピーダンス継電器との組合せによる方
式が使用されている。Therefore, if the synchronous machine is in a dangerous state where it may lose synchronization, it is necessary to take measures such as performing field control to prevent the synchronization machine from going out of synchronization or separating the synchronous machine from the system. As a conventional synchronous machine step-out detection method,
A combination of power relay and impedance relay is used.
これは、第1図に示すように、横軸に抵抗成分Rをとり
、縦軸にリアクタンス成分Xをとつた場合、電力継電器
W4はR軸上の所定の設定点aを通過する縦軸に平行な
直線を限界として図における・・ツチングを施した領域
において動作し、電力継電器W2はR軸上の所定の設定
点−aを通過する縦軸に平行な直線を限界としてハッチ
シダを施した領域において動作し、そしてインピーダン
ス継電器Zは所定のインピーダンスz(■ 4!/ に
2+ x2、たゞしには抵抗を表わし、Xはリアクタン
スを表わす)を半径とする円内の領域において動作する
よう構成されている。従つて、同期機が脱調状態に移行
して継電器設置点から見た等価インピーダンスが正常運
転時の位置Z。点から曲線lで示す軌跡を描いて移動し
た場合、電力継電器W1、W2およびインピーダンス継
電器Zのそれぞれの関連動作により脱調検出シーケンス
回路(図示せず)が動作して脱調状態が検出される。し
かしながら、この従来の方式は同期機の脱調後における
脱調を検出する方式であり、脱調する恐れのある危険状
態における脱調子測の機能は有していない〇また、従来
に訃ける脱調子測機能を有する方式としては、安定限界
制御用継電器による脱調子測方式が使用されている。This means that, as shown in Figure 1, if the horizontal axis is the resistance component R and the vertical axis is the reactance component The power relay W2 operates in the hatched area in the figure with parallel straight lines as the limit, and the power relay W2 operates in the hatched area with the limit being a straight line parallel to the vertical axis passing through a predetermined set point -a on the R axis. and the impedance relay Z is configured to operate in a region within a circle whose radius is a predetermined impedance z (■ 4!/ 2 + x2, where only resistance is represented and X is reactance). has been done. Therefore, when the synchronous machine enters an out-of-step state, the equivalent impedance seen from the relay installation point is at position Z during normal operation. When moving from a point along a trajectory shown by curve l, a step-out detection sequence circuit (not shown) operates due to the related operations of power relays W1, W2 and impedance relay Z, and a step-out state is detected. . However, this conventional method detects synchronization after the synchronous machine has lost synchronization, and does not have the function of measuring synchronization in a dangerous situation where there is a risk of synchronization. As a method having a condition measurement function, a de-conditioning measurement method using a stability limit control relay is used.
これは、例えば、同期発電機について説明すれば、第2
図に示すように、横軸に有効電力Pをとり、縦軸に無効
電力Qをとり、同期発電機の出力限界曲線をLとし、定
態安定限界曲線をmとした場合、曲線gを限界としてハ
ツチングを施した領域において動作する安定限界制御用
継電器Gを設け、同期発電機出力のベクトル座標W(=
P+JQ)が正常運転時の曳点から曲線sで示す軌跡を
描いて安定限界曲線gを越え、脱調領域方向に移行した
際、安定限界制御用継電器Gの動作により同期発電機の
励磁を強めて出力ベクトル座標Wを正常な位置に戻し、
脱調状態に移行することを防止するよう構成されている
Oしかしながら、この安定限界制御用継電器による脱調
子測方式訃よび前述の電力継電器とインピーダンス継電
器との組合せによる脱調検出方式は、いずれも同期機の
外部的電気諸量(端子電圧、出力電流、インピーダンス
、出力、無効電力、相差角など)を検出用入力としてお
り同期機内部に訃ける物理的な量の異常状態に基づいて
ないため、検出結果が同期機の実際の状態に即している
か否かは疑わしい難点がある〇そこで、発明者等は種々
検討並びに試験を重ねた結果、同期機の空隙磁束より導
かれるトルクが、第3図に示すように、脱調移行直前に
おいて気激に減少することを知見し、空隙磁束より導か
れるトルクの関数値を検知して同期機の脱調を予測し得
ることを突き止めた。For example, if we explain a synchronous generator, this means that the second
As shown in the figure, if the horizontal axis is active power P, the vertical axis is reactive power Q, the output limit curve of the synchronous generator is L, and the steady state stability limit curve is m, then curve g is the limit. A stability limit control relay G that operates in the hatched area is provided, and the vector coordinate W of the synchronous generator output (=
When P+JQ) traces the trajectory shown by curve s from the towing point during normal operation and crosses stability limit curve g and moves toward the out-of-step region, the excitation of the synchronous generator is strengthened by the operation of stability limit control relay G. to return the output vector coordinate W to the normal position,
However, both the out-of-step measurement method using this stability limit control relay and the out-of-step detection method using a combination of a power relay and an impedance relay described above are Since the external electrical quantities of the synchronous machine (terminal voltage, output current, impedance, output, reactive power, phase difference angle, etc.) are used as the detection input, it is not based on abnormal states of physical quantities that may occur inside the synchronous machine. , there is a drawback in that it is doubtful whether the detection results correspond to the actual state of the synchronous machine.Therefore, the inventors conducted various studies and tests, and found that the torque derived from the air gap magnetic flux of the synchronous machine is As shown in Figure 3, we found that the torque decreases dramatically just before transition to out-of-step, and found that it is possible to predict out-of-step in a synchronous machine by detecting the function value of the torque derived from the air gap magnetic flux.
従つて、本発明の一般的な目的は、同期機が脱調する恐
れのある危険状態にあることを適確に予測することがで
きる同期機の脱調子測方式を提供するにある。SUMMARY OF THE INVENTION Accordingly, a general object of the present invention is to provide a method for measuring out-of-step of a synchronous machine that can accurately predict that the synchronous machine is in a dangerous state in which there is a possibility of out-of-step.
この目的を達成するため、本発明においては同期機の空
隙磁束から導かれるトルクが異常低下したことを判別す
ることにより脱調を予測することを特徴とする。In order to achieve this object, the present invention is characterized in that step-out is predicted by determining that the torque derived from the air gap magnetic flux of the synchronous machine has abnormally decreased.
前記の同期機の脱調子測方式において、空隙磁束より導
かれるトルクが所定の基準レベル以下に減少したことを
検知して脱調を予測することができる。In the method for measuring out-of-step of a synchronous machine, it is possible to predict out-of-step by detecting that the torque guided by the air gap magnetic flux has decreased below a predetermined reference level.
次に、本発明に係る同期機の脱調子測方式につき添付図
面を参照しながら以下詳細に説明する。Next, the synchronous machine detuning measurement method according to the present invention will be described in detail below with reference to the accompanying drawings.
第4図は同期発電機の制御回路を示すもので参照符号1
0は同期発電機を示し、同期発電機10の電機子端子は
インピーダンス12を介して電力系統14に接続する。
また、同期発電機10の電機子端子は電圧偏差検出器1
6の入力端子に電圧変成器18を介して接続し、電圧偏
差検出器16には基準電圧電源V8を接続し、電圧偏差
検出器16の出力端子は加算演算器20の入力端子aに
接続する。また、加算演算器20の入力端子bには、振
動抑制用安定器等の励磁システム補助装置22を接続し
、加算演算器20の出力端子は自動電圧調整器24の入
力端子に接続し、自動電圧調整器24の出力側は励磁装
置26を介して同期発電機10の界磁巻線10aに接続
する。同期発電機10の励磁回路には、励磁電流検出器
28を接続し、同期発電機10の内部には空隙磁束検出
器30}よび界磁位置検出器32を装着する。Figure 4 shows the control circuit of the synchronous generator, reference numeral 1.
0 indicates a synchronous generator, and the armature terminal of the synchronous generator 10 is connected to the power grid 14 via an impedance 12.
Further, the armature terminal of the synchronous generator 10 is connected to the voltage deviation detector 1.
6 via a voltage transformer 18, a reference voltage power supply V8 is connected to the voltage deviation detector 16, and the output terminal of the voltage deviation detector 16 is connected to the input terminal a of the addition calculator 20. . In addition, an excitation system auxiliary device 22 such as a vibration suppression stabilizer is connected to the input terminal b of the addition calculator 20, and the output terminal of the addition calculator 20 is connected to the input terminal of the automatic voltage regulator 24. The output side of the voltage regulator 24 is connected via an excitation device 26 to the field winding 10a of the synchronous generator 10. An excitation current detector 28 is connected to the excitation circuit of the synchronous generator 10, and an air gap magnetic flux detector 30} and a field position detector 32 are installed inside the synchronous generator 10.
励磁電流検出器28の出力端子は、界磁々束算定器34
と電機子反作用磁束分析器36とトルク分析器38と信
号レベル比較器40と増幅器42とからなる脱調子測装
置44の入力端子aを介して界磁々束算定器34の入力
端子に接続する。The output terminal of the exciting current detector 28 is connected to the field flux calculator 34.
is connected to the input terminal of the field flux calculator 34 through the input terminal a of the detuning measuring device 44, which includes an armature reaction flux analyzer 36, a torque analyzer 38, a signal level comparator 40, and an amplifier 42. .
界磁々束算定器34の出力端子は電機子反作用磁束分析
器36の入力端子a1に接続し、空隙磁束検出器30卦
よび界磁位置検出器32のそれぞれの出力端子は、脱調
子測装置44の入力端子bおよびcを介して電機子反作
用磁束分析器36の入力端子B,}よびC1に接続する
。また、界磁々束算定器34}よび電機子反作用磁束分
析器36のそれぞれの出力端子はトルク分析器38の入
力端子P1}よびP2に接続し、トルク分析器38の出
力端子は信号レベル比較器40および増幅器42を介し
て脱調子測装置44の出力端子dから加算演算器20の
入力端子cに接続する。The output terminal of the field flux calculator 34 is connected to the input terminal a1 of the armature reaction flux analyzer 36, and the output terminals of the air gap flux detector 30 and the field position detector 32 are connected to the detuning measuring device. 44 to input terminals B, } and C1 of the armature reaction flux analyzer 36. Further, the output terminals of the field flux calculator 34} and the armature reaction flux analyzer 36 are connected to the input terminals P1} and P2 of the torque analyzer 38, and the output terminal of the torque analyzer 38 is used for signal level comparison. The output terminal d of the detuning measuring device 44 is connected to the input terminal c of the adder 20 via the amplifier 40 and the amplifier 42.
次に、このように構成した回路の動作と共に本発明方式
について説明する。Next, the system of the present invention will be explained along with the operation of the circuit configured as described above.
同期発電機10により起生された発電機端子電圧は電圧
変成器18を介し電圧偏差検出器16に供給されて所定
の基準電圧V8と比較され、その偏差が加算演算器20
の入力端子aに供給されると共に、励磁システム補助装
置22の出力が加算演算器20の入力端子bに供給され
て加算され、加算演算器20の出力力咄動電圧調整器2
4の入力端子に供給される。自動電圧調整器24は入力
に対応した出力を励磁装置26に供給し、同期発電機1
0の端子電圧が所定の基準電圧V8に対応した値になる
ような励磁電流を同期発電機10の界磁巻線10aに供
給し、同期発電機10は所定の大きさの電圧を起生して
電力系統14と同期して運転されている。この場合、界
磁々束算定器34においては、励磁電流検出器28から
供給された電磁電流1fに基づいて各瞬時の界磁々束φ
fが算定され、この算定された出力が電機子反作用磁束
分析器36の入力端子a1に供給される。また、空隙磁
束検出器30により検出?れた空隙磁束φ が電機子反
g作用磁束分析器36の入力端子B,に供給され、界磁
位置検出器32により検出された各瞬時の界磁々極の位
置が電機子反作用磁束分析器36の入力端子C1に供給
される。The generator terminal voltage generated by the synchronous generator 10 is supplied to the voltage deviation detector 16 via the voltage transformer 18 and compared with a predetermined reference voltage V8.
At the same time, the output of the excitation system auxiliary device 22 is supplied to the input terminal b of the addition calculator 20 and added thereto, and the output power of the addition calculator 20 is applied to the perturbation voltage regulator 2.
4 input terminals. The automatic voltage regulator 24 supplies an output corresponding to the input to the excitation device 26, and the synchronous generator 1
An excitation current such that the terminal voltage of 0 becomes a value corresponding to a predetermined reference voltage V8 is supplied to the field winding 10a of the synchronous generator 10, and the synchronous generator 10 generates a voltage of a predetermined magnitude. It is operated in synchronization with the power grid 14. In this case, the field flux calculator 34 calculates each instantaneous field flux φ based on the electromagnetic current 1f supplied from the exciting current detector 28.
f is determined and the determined output is supplied to the input terminal a1 of the armature reaction flux analyzer 36. Also detected by the air gap magnetic flux detector 30? The air gap magnetic flux φ is supplied to the input terminal B of the armature reaction flux analyzer 36, and the position of the field magnetic pole at each instant detected by the field position detector 32 is input to the armature reaction flux analyzer 36. 36 input terminal C1.
一般に、空隙磁束φ8および界磁々束φfと電機子反作
用磁束φa′との間には下記の関係φa′=φ,−φf
・・・・・・(1)がある。Generally, the following relationship φa'=φ, -φf exists between the air gap magnetic flux φ8, the field magnetic flux φf, and the armature reaction magnetic flux φa'.
...There is (1).
電機子反作用磁束分析器36においては、入力端子C,
に供給された各瞬時の界磁々極の位置に基づいて上記(
1)式に示す演算が行われ、界磁磁束φfとの位相差α
を考慮した電機子反作用磁束φ3が検出される。界磁々
束算定器34により算定づれた界磁々束φfおよび電機
子状作用磁束分析器により検出された電機子反作用磁束
φ,は、それぞれトルク分析器38の入力端子Plおよ
びP2に供給される。一般に、同期機に卦いて空隙磁束
により起生されるトルクTは、次式により表わすことが
できる。In the armature reaction flux analyzer 36, input terminals C,
Based on the position of the field poles at each instant supplied to
1) The calculation shown in the formula is performed, and the phase difference α with the field magnetic flux φf is
The armature reaction magnetic flux φ3 is detected. The field flux φf calculated by the field flux calculator 34 and the armature reaction magnetic flux φ detected by the armature action flux analyzer are supplied to input terminals Pl and P2 of the torque analyzer 38, respectively. Ru. Generally, the torque T generated by the air gap magnetic flux in a synchronous machine can be expressed by the following equation.
′9τノゞ
但し、x・・・空隙部円周上の座標原点からの円周距離
α・・・界磁々束φfと電機子反作用磁束φ3との位相
差
トルク分析器38においては、例えば1ポールピツチ分
のトルクが演算され、入力端子P2およびP1に供給さ
れた1ポールピツチ分の界磁々束φfと1ポールピツチ
分の電機子反作用磁束φ3とから上記(2)式に従つて
トルクTが検出され、この検出された出力信号が信号レ
ベル比較器40に供給される。'9τ No However, x... Circumferential distance from the coordinate origin on the circumference of the gap α... Phase difference between field magnetic flux φf and armature reaction magnetic flux φ3 In the torque analyzer 38, for example, The torque for one pole pitch is calculated, and the torque T is calculated from the field flux φf for one pole pitch and the armature reaction magnetic flux φ3 for one pole pitch supplied to the input terminals P2 and P1 according to the above equation (2). The detected output signal is supplied to a signal level comparator 40.
信号レベル比較器40は入力信号が所定の基準レベルR
(第3図参照)より大きい場合は出力が零になるよう構
成づれている。従つて、同期発電機10が正常状態、す
なわち脱調に移行するような危険状態でない場合には、
信号レベル比較器40は出力が零の状態に維持され、増
幅器42から加算演算器20の人力端子cに入力が供給
されないため、同期発電機10は励磁電流の補正動作が
行われずに運転されている。いま、何等かの原因により
同期発電機10が脱調する恐れのある危険状態となり、
信号レベル比較器40に供給されたトルク検出信号が第
3図に示す基準レベルR以下に減少した場合には、信号
レベル比較器40の出力端子に起生された危険状態にあ
ることを示す出力信号が増幅器42により増幅されて脱
調子測装置44の出力端子から加算演算器20の入力端
子cに供給される。The signal level comparator 40 detects that the input signal is at a predetermined reference level R.
(See Fig. 3) The configuration is such that the output becomes zero when the value is larger than that. Therefore, when the synchronous generator 10 is in a normal state, that is, when it is not in a dangerous state where it will go out of synchronization,
Since the output of the signal level comparator 40 is maintained at zero and no input is supplied from the amplifier 42 to the human power terminal c of the addition calculator 20, the synchronous generator 10 is operated without correcting the excitation current. There is. Now, due to some reason, the synchronous generator 10 is in a dangerous state where it may lose synchronization.
When the torque detection signal supplied to the signal level comparator 40 decreases below the reference level R shown in FIG. The signal is amplified by the amplifier 42 and supplied from the output terminal of the detuning measuring device 44 to the input terminal c of the addition calculator 20.
従つて、加算演算器20の出力は増加し、自動電圧調整
器24は励磁装置26を介して界磁巻線10aの励磁を
強め、同期発電機10の脱調状態への移行が防止される
。上述の実施例に卦いては、空隙磁束より導かれるトル
クTの大きさを検知したが、一般に空隙磁束より導かれ
るトルクTの関数値を検知して脱調を予測することがで
き、例えば、空隙磁束より導かれるトルクTの減少率(
−DT/Dt)が所定の基準レベル以上に増加したこと
を検知して土述の実施例と同様に脱調を予測することが
できる。Therefore, the output of the adder 20 increases, the automatic voltage regulator 24 strengthens the excitation of the field winding 10a via the excitation device 26, and the synchronous generator 10 is prevented from going out of synchronization. . In the above-described embodiments, the magnitude of the torque T derived from the air gap magnetic flux was detected, but in general, step-out can be predicted by detecting the function value of the torque T derived from the air gap magnetic flux. For example, Decrease rate of torque T derived from air gap magnetic flux (
-DT/Dt) increases above a predetermined reference level, it is possible to predict out-of-step as in the embodiment described above.
上述の実施例は、同期発電機を対象としたが同期電動機
、同期調相機など同期機全般に対しても同様に本発明方
式を適用することができる。本発明方式によれば、空隙
磁束より導かれるトルクの関数値を検知して同期機の脱
調を適確に予測することができ、同期機制御機能の向上
に資する効果が極めて大きい。さらに、本発明方式は脱
調以外の同期機の状態変化の検知に応用することができ
る。Although the above-described embodiments are directed to synchronous generators, the method of the present invention can be similarly applied to synchronous machines in general, such as synchronous motors and synchronous phase modifiers. According to the method of the present invention, it is possible to accurately predict the out-of-step of a synchronous machine by detecting the function value of the torque derived from the air gap magnetic flux, and the effect of contributing to the improvement of the synchronous machine control function is extremely large. Furthermore, the method of the present invention can be applied to detecting changes in the state of a synchronous machine other than step-out.
以上、本発明の好適な実施例について説明したが、本発
明の精神を逸脱しない範囲内に卦いて種種の設計変更を
なし得ることは勿論である。Although the preferred embodiments of the present invention have been described above, it goes without saying that various design changes can be made without departing from the spirit of the present invention.
第1図は従来における同期機の脱調検出方式の作用を示
す説明図、第2図は従来における同期機の脱調子測方式
の作用を示す説明図、第3図は同期機の脱調前後におけ
る空隙磁束より導かれるトルクの変化を示す波形図、第
4図は本発明に係る同期機の脱調子測方式による同期発
電機制御回路の構成を示すプロツク結線図である。
10・・・・・・同期発電機、10a・・・・・・界磁
巻線、12・・・・・・インピーダンス、14・・・・
・・電力系統、16・・・・・・電圧偏差検出器、18
・・・・・・電圧変成器、20・・・・・・加算演算器
、22・・・・・・励磁システム補助装置、24・・・
・・迫動電圧調整器、26・・・・・・励磁装置、28
・・・・・・励磁電流検出器、30・・・・・・空隙磁
束検出器、32・・・・・・界磁位置検出器、34・・
・・・・界磁磁束算定器、36・・・・・・電機子反作
用磁束分析器、38・・・・・・トルク分析器、40・
・・・・・信号レベル比較器、42・・・・・・増幅器
、44・・・・・・脱調子測装置。Fig. 1 is an explanatory diagram showing the operation of a conventional out-of-step detection method for a synchronous machine, Fig. 2 is an explanatory diagram showing the operation of a conventional out-of-step measurement method for a synchronous machine, and Fig. 3 is an explanatory diagram showing the operation of a conventional out-of-step detection method for a synchronous machine. FIG. 4 is a block diagram showing the configuration of a synchronous generator control circuit using a detuning measurement method for a synchronous machine according to the present invention. 10...Synchronous generator, 10a...Field winding, 12...Impedance, 14...
...Power system, 16... Voltage deviation detector, 18
... Voltage transformer, 20 ... Addition calculator, 22 ... Excitation system auxiliary device, 24 ...
... Urging voltage regulator, 26... Excitation device, 28
...Exciting current detector, 30...Air gap magnetic flux detector, 32...Field position detector, 34...
... Field magnetic flux calculator, 36 ... Armature reaction magnetic flux analyzer, 38 ... Torque analyzer, 40.
... Signal level comparator, 42 ... Amplifier, 44 ... De-tuning measuring device.
Claims (1)
たことを判別することにより脱調を予測することを特徴
とする同期機の脱調予測方式。 2 前記異常低下は空隙磁束から導かれるトルクが所定
の基準レベル以下に減少したことをもつて判別すること
を特徴とする特許請求の範囲第1項記載の同期機の脱調
予測方式。 3 前記異常低下は空隙磁束から導かれるトルクの減少
率が所定の基準レベル以上に増加したことをもつて判別
することを特徴とする特許請求の範囲第1項記載の同期
機の脱調予測方式。[Scope of Claims] 1. A step-out prediction method for a synchronous machine, characterized in that step-out is predicted by determining that the torque derived from the air-gap magnetic flux of the synchronous machine has decreased abnormally. 2. The step-out prediction method for a synchronous machine according to claim 1, wherein the abnormal decrease is determined based on the fact that the torque derived from the air gap magnetic flux has decreased below a predetermined reference level. 3. The step-out prediction method for a synchronous machine according to claim 1, wherein the abnormal decrease is determined based on an increase in the rate of decrease in the torque derived from the air gap magnetic flux to a predetermined reference level or higher. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP54023410A JPS5922457B2 (en) | 1979-03-02 | 1979-03-02 | Synchronous machine step-out prediction method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP54023410A JPS5922457B2 (en) | 1979-03-02 | 1979-03-02 | Synchronous machine step-out prediction method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS55117441A JPS55117441A (en) | 1980-09-09 |
| JPS5922457B2 true JPS5922457B2 (en) | 1984-05-26 |
Family
ID=12109720
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP54023410A Expired JPS5922457B2 (en) | 1979-03-02 | 1979-03-02 | Synchronous machine step-out prediction method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5922457B2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS61121475U (en) * | 1985-01-18 | 1986-07-31 | ||
| JPS63187170U (en) * | 1987-05-18 | 1988-11-30 |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0681557B2 (en) * | 1982-04-19 | 1994-10-12 | 株式会社日立製作所 | Synchronous machine excitation controller |
-
1979
- 1979-03-02 JP JP54023410A patent/JPS5922457B2/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS61121475U (en) * | 1985-01-18 | 1986-07-31 | ||
| JPS63187170U (en) * | 1987-05-18 | 1988-11-30 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS55117441A (en) | 1980-09-09 |
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