JPS62290358A - Drive stop control system of thyristor rectifier - Google Patents

Drive stop control system of thyristor rectifier

Info

Publication number
JPS62290358A
JPS62290358A JP13210186A JP13210186A JPS62290358A JP S62290358 A JPS62290358 A JP S62290358A JP 13210186 A JP13210186 A JP 13210186A JP 13210186 A JP13210186 A JP 13210186A JP S62290358 A JPS62290358 A JP S62290358A
Authority
JP
Japan
Prior art keywords
signal
gate
zero point
output
supplied
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
JP13210186A
Other languages
Japanese (ja)
Inventor
Eiji Akagawa
赤川 英爾
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP13210186A priority Critical patent/JPS62290358A/en
Publication of JPS62290358A publication Critical patent/JPS62290358A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To prevent breakage of a thyristor, by a method wherein gate firing signal supplied to the thyristor in synchronization with phase zero point of power source voltage disappears at drive stop state. CONSTITUTION:Voltage Xo detected by an instrument transformer is inputted in a synchronous signal making circuit 11, and power source synchronous signal Sv at high level during period of positive voltage of an aerial line is produced, and inputted and supplied to a zero point pulse generator 12 and a three-input AND gate 17. The pulse generator 12 outputs zero point pulse Zp, and supplies reset signal to an integrator 13. Output Is of the integrator 13 is supplied to a comparator 15 and also output Vp of a phase angle command operation circuit 16 is supplied similarly, and the comparison output is outputted to the gate 17. In this case, D flipflop 18 is installed, and its output Df is supplied to the AND gate 17 in place of drive command signal Ds. In this constitution, disappearing timing of the gate firing signal is synchronized with the zero point of the power source voltage, and the gate firing signal of prescribed pulse width is generated.

Description

【発明の詳細な説明】 3、発明の詳細な説明 〔産業上の利用分野〕 本発明は出力電圧可変のサイリスタ整流装置の駆動停止
時の点弧制御方式に関するものである。
Detailed Description of the Invention 3. Detailed Description of the Invention [Industrial Field of Application] The present invention relates to a firing control method when the drive of a thyristor rectifier with variable output voltage is stopped.

C従来技術〕 第3図は電気車輌を駆動する直流電動機の給電回路を示
しており、交流電圧架線31に摺接するパンタグラフ3
2は交流遮断器34を介して降圧変圧器35の1次巻線
に接続され、また架線電圧検出のための計器用変成器(
PT) 33にも接続されている。
C. Prior Art] FIG. 3 shows a power supply circuit for a DC motor that drives an electric vehicle, and shows a pantograph 3 in sliding contact with an AC voltage overhead line 31.
2 is connected to the primary winding of a step-down transformer 35 via an AC circuit breaker 34, and is connected to an instrument transformer (
PT) 33.

降圧変圧器35の2次巻線はサイリスタ37a、37b
及びダイオード38a、38bをブリフジ接続してなる
サイリスタ整流装置36の入力端子に与えられており、
サイリスタ37a 、 37bの点弧位相角i#I御に
より変化する出力電圧が直流電動機39の電機子コイル
39a及び界磁コイル39bの直列回路に与えられてい
る。
The secondary windings of the step-down transformer 35 are thyristors 37a and 37b.
and the input terminal of a thyristor rectifier 36 formed by connecting diodes 38a and 38b in a bridging manner,
An output voltage that changes by controlling the firing phase angle i#I of the thyristors 37a and 37b is applied to a series circuit of an armature coil 39a and a field coil 39b of a DC motor 39.

サイリスタ整流装置36のサイリスタ37a、37bの
ゲートの点弧位相角制御回路は例えば特開昭59−18
5102号公報にて示されており、これを第4図及び第
5図に基づいて説明する。
The firing phase angle control circuit of the gates of the thyristors 37a and 37b of the thyristor rectifier 36 is disclosed in, for example, Japanese Patent Application Laid-open No. 59-18.
This is disclosed in Japanese Patent No. 5102, and will be explained based on FIGS. 4 and 5.

計器用変成器33にて検出された電圧V。(第5図(イ
)〕は同期信号作成回路11へ入力され、ここで電源電
圧、つまり架線31の電圧が正となる期間ハイレベルと
なる電源同期信号Sv  C第5図(ロ)〕が作成され
、この電源同期信号Svは零点パルス発生回路12及び
3人力ANDゲート17へ入力される。
Voltage V detected at instrument transformer 33. (Fig. 5 (a)) is input to the synchronization signal generation circuit 11, where the power supply synchronization signal SvC, which is at a high level during the period when the power supply voltage, that is, the voltage of the overhead wire 31 is positive, is generated. This power synchronization signal Sv is input to the zero point pulse generation circuit 12 and the three-man power AND gate 17.

零点パルス発生回路12は電源同期信号Svの立上り、
立下りに同期する短い時間幅のパルス信号、つまり電源
電圧の零点に同期する零点パルスZp〔第5図(ハ)〕
を出力し、精分器13にリセット信号として与えられる
。14はクロック信号CLKを発振するクロック発振器
であってクロック信号は零点パルス発生回路12及び精
分器13へ与えられる。
The zero point pulse generation circuit 12 detects the rise of the power supply synchronization signal Sv,
A short time width pulse signal that synchronizes with the falling edge, that is, a zero point pulse Zp that synchronizes with the zero point of the power supply voltage [Figure 5 (c)]
is output and given to the separator 13 as a reset signal. A clock oscillator 14 generates a clock signal CLK, and the clock signal is applied to the zero point pulse generation circuit 12 and the separator 13.

精分器13の積分出力Is  (第5図(ニ)実線〕は
比較器15の十入力端子に与えられる。位相角指令演算
回路16は設定信号に応じた電圧信号を出力するもので
あり、この電圧信号、つまり位相角指令信号Vp  C
第5図(ニ)破線〕を比較器15の一入力端子に与える
。従って比較器15はIsがVpより大となった場合に
ハイレベルとなるパルス信号Vq  (第5図(ホ)〕
を出力するが、この出力Vqは3人力ANDゲー)17
に入力される。3人力ANDゲート17の残り1つの入
力は直流電動機39の駆動時にハイレベルとなる駆動指
令信号Ds  [第5ズ(へ)]であり、ANDゲート
17からは第5図(ト)に示すゲート点弧信号Ctが発
せられる。
The integral output Is (FIG. 5 (d) solid line) of the separator 13 is given to the ten input terminal of the comparator 15.The phase angle command calculation circuit 16 outputs a voltage signal according to the setting signal. This voltage signal, that is, the phase angle command signal VpC
5(d) broken line] is applied to one input terminal of the comparator 15. Therefore, the comparator 15 outputs a pulse signal Vq that becomes high level when Is becomes larger than Vp (Fig. 5 (e)).
However, this output Vq is a 3-person AND game) 17
is input. The remaining input of the three-man power AND gate 17 is the drive command signal Ds [5th Z] which becomes high level when the DC motor 39 is driven, and from the AND gate 17, the gate shown in FIG. A firing signal Ct is generated.

クロック信号CLには精分器13に積分対象として与え
られており、また零点パルスzpが積分器13にリセッ
ト信号として与えられるので、積分器13出力は第5図
(ニ)に示す鋸歯状波となり、従って位相角指令信号V
pの高低に応じてパルス幅が変化するゲート点弧信号G
tが得られることになる。
Since the clock signal CL is given to the fine separator 13 as an object to be integrated, and the zero point pulse zp is given to the integrator 13 as a reset signal, the output of the integrator 13 is a sawtooth wave shown in FIG. 5(d). Therefore, the phase angle command signal V
Gate firing signal G whose pulse width changes depending on the height of p
t will be obtained.

なお、第4.5図に示した回路は電源電圧が正である期
間に点弧すべきサイリスタ37aに与えるゲート点弧信
号作成用のものであり、負側のサイリスタ37b用のゲ
ート点弧信号Gtは電源同期信号Svの反転信号を用い
ることにより同様に作成できる。
The circuit shown in Fig. 4.5 is for creating a gate firing signal to be given to the thyristor 37a to be fired during the period when the power supply voltage is positive, and a gate firing signal for the negative side thyristor 37b. Gt can be similarly created by using an inverted signal of the power synchronization signal Sv.

〔発明が解決しようとする問題点3 以上の如き回路においては直流電動機の停止時あるいは
何らかの原因で駆動指令信号Dsが消失する(ローレベ
ルになる)とゲート点弧信号Gtはローレベルとなり、
この消失タイミングによっては最後のゲート点弧パルス
〔第5図(ト)に矢符で示す〕は非常に狭幅となり、こ
のためにサイリスタのゲート点弧信号不足にて所定のゲ
ート電流が供給されず、いわゆる局部的なホ7)スポッ
トを生じ、サイリスタの破壊を惹起するという問題点が
ある。またサイリスタに主回路電流が流れている間にゲ
ート点弧信号が消失することにより同様な不都合も生じ
る。
[Problem to be Solved by the Invention 3] In the circuit as described above, when the DC motor stops or for some reason the drive command signal Ds disappears (becomes low level), the gate firing signal Gt becomes low level,
Depending on the timing of this disappearance, the final gate firing pulse (indicated by the arrow in Figure 5 (G)) becomes very narrow, and because of this, the prescribed gate current is not supplied due to insufficient gate firing signal of the thyristor. First, there is a problem in that so-called local spots occur, causing destruction of the thyristor. A similar problem also occurs when the gate firing signal disappears while the main circuit current is flowing through the thyristor.

本発明は斯かる問題点に鑑みてなされたものであり、駆
動指令信号Dsの消失タイミングの如何に拘わらず、十
分なパルス幅のゲート点弧信号を出力して、サイリスタ
の破壊を防止できる整流装置の提供を目的とする。
The present invention has been made in view of such problems, and provides a rectifier that can output a gate firing signal with a sufficient pulse width and prevent the destruction of the thyristor, regardless of the timing of disappearance of the drive command signal Ds. The purpose is to provide equipment.

〔問題点を解決するための手段〕[Means for solving problems]

本発明に係るサイリスタ整流装置の駆動制御方式はその
駆動停止時に電源電圧の位相零点に同期させてサイリス
タに与えるゲート点弧信号を消失させる。
The drive control method for the thyristor rectifier according to the present invention eliminates the gate firing signal applied to the thyristor in synchronization with the phase zero point of the power supply voltage when the drive is stopped.

〔作用〕[Effect]

本発明においては、装置の駆動停止時にサイリスタに与
えるゲート点弧信号の消失タイミングを電源電圧の零点
に同期させ、所定パルス幅のゲート点弧信号を発生する
In the present invention, the timing at which the gate firing signal applied to the thyristor disappears when the drive of the device is stopped is synchronized with the zero point of the power supply voltage, and a gate firing signal having a predetermined pulse width is generated.

C実路例〕 以下本発明の制御方式をその一実施例を示す図面に基づ
いて詳述する。
C Actual Road Example] The control method of the present invention will be described in detail below based on the drawings showing one embodiment thereof.

第1図は本発明方式を実施する点弧位相角制御回路のブ
ロック図、第2図はそのタイミングチャートである。
FIG. 1 is a block diagram of an ignition phase angle control circuit implementing the method of the present invention, and FIG. 2 is a timing chart thereof.

この回路はDフリップフロップ(エノジトエガータイプ
デークラッチ回路)18を備え、駆動指令信号Dsをそ
のデータ端子りに、また零点パルスZpをそのトリガ端
子Tに与え、その出力端子Qから発せられる出力Df)
tr駆動FII令信号Dsに替えてANDゲート17に
与えるようにした点が第4図に示す従来の回路と異なっ
ている。
This circuit includes a D flip-flop (Enojito Egger type data clutch circuit) 18, applies a drive command signal Ds to its data terminal and a zero point pulse Zp to its trigger terminal T, and outputs an output from its output terminal Q. Df)
This circuit differs from the conventional circuit shown in FIG. 4 in that it is applied to the AND gate 17 instead of the tr drive FII command signal Ds.

叩ち例えば第3図に示す計器用変成器33にて検出され
た電源電圧Vo  (第2図(イ)〕は同期信号作成回
路11へ入力され、ここで電源電圧が正となる期間ハイ
レベルとなる電源同期信号Sν〔第2図(ロ)〕が作成
され、この電源同期信号Svは零点パルス発生回路12
及び3人力ANDゲート17へ入力される。
For example, the power supply voltage Vo detected by the instrument transformer 33 shown in FIG. A power supply synchronization signal Sv [FIG. 2 (b)] is created, and this power supply synchronization signal Sv
and is input to the three-man power AND gate 17.

零点パルス発生回路12は電源同期信号Svの立上り、
立下りに同期する短い時間幅の零点パルスZp  (第
2図(ハ)〕を出力し、積分器13にリセット信号とし
て、またDフリップフロップ18にトリガ信号として与
えられる。14はクロック信号CLにを発振するクロッ
ク発振器であってクロック信号は零点パルス発生回路1
2及び積分器13へ与えられる。積分器13の積分出力
Is  (第2図(ニ)実線〕は比較器15の十入力端
子に与えられる0位相角指令演算回路16は設定信号に
応じた電圧(8号を出力するものであり、この電圧信号
、つまり位相角指令信号Vp  (第2図(ニ)破線〕
を比較器15の一入力端子に与える。従って比較器15
は!SがVpより大となった場合にハイレベルとなるパ
ルス信号Vq  (第2図(ホ)〕を出力するが、この
出力Vqは3人力ANDゲート17に入力される。直流
電動が39の駆動時にハイレベルとなる駆動指令信号D
s  (第2図(へ)〕はDフリップフロップ18のデ
ータ端子りに与えられ、その出力IM  (第2図(ト
)〕が3人力ANDゲート17に入力されている。
The zero point pulse generation circuit 12 detects the rise of the power supply synchronization signal Sv,
A zero-point pulse Zp (FIG. 2 (c)) with a short time width synchronized with the falling edge is output, and is given to the integrator 13 as a reset signal and to the D flip-flop 18 as a trigger signal. A clock oscillator that oscillates a clock signal from a zero-point pulse generation circuit 1.
2 and an integrator 13. The integral output Is (FIG. 2 (d) solid line) of the integrator 13 is given to the ten input terminal of the comparator 15. The zero phase angle command calculation circuit 16 outputs a voltage (No. 8) according to the setting signal. , this voltage signal, that is, the phase angle command signal Vp (Figure 2 (d) broken line)
is applied to one input terminal of the comparator 15. Therefore, comparator 15
teeth! When S becomes larger than Vp, a pulse signal Vq (FIG. 2 (E)) that becomes high level is output, and this output Vq is input to the three-man power AND gate 17.The DC motor drives 39. Drive command signal D that sometimes becomes high level
s (FIG. 2(g)) is applied to the data terminal of the D flip-flop 18, and its output IM (FIG. 2(g)) is input to the three-man power AND gate 17.

ANDゲート17からは第2図(チ)に示すゲート点弧
信号Gtが発せられる。
A gate firing signal Gt shown in FIG. 2 (H) is generated from the AND gate 17.

クロック信号CLKは積分513に積分対象として与え
られており、また零点パルスzpが積分器13にリセッ
ト信号として与えられるので、積分器13出力は第2図
(ニ)に示す鋸歯状波となり、従っ   ′て位相角指
令信号Vpの高低に応じてパルス幅が変化するゲート点
弧信号Gtが得られることになる。
Since the clock signal CLK is given to the integrator 513 as an object to be integrated, and the zero point pulse zp is given to the integrator 13 as a reset signal, the output of the integrator 13 becomes a sawtooth wave as shown in FIG. 2(d). Thus, a gate firing signal Gt whose pulse width changes depending on the level of the phase angle command signal Vp is obtained.

而して駆動指令信号Dsが消失した時点についてみると
Dフリップフロノブのデータ入力はローレベルとなるが
トリガ信号は電源電圧voの零点で与えられるから、そ
のセント状態はトリガ信号が与えられるまで継続され、
従って信号Drは零点パルスzpに同期してローレベル
となる。その結果ゲート点弧信号Gtがその時点でロー
レベルに転じる。従って駆動指令信号消失時においても
ゲート点弧信号Gtのパルス幅が従来のように狭くなる
ことがなく、所定パルス幅のゲート点弧信号Gtを得る
ことができる。
When we look at the point at which the drive command signal Ds disappears, the data input of the D flip-flop knob becomes low level, but since the trigger signal is given at the zero point of the power supply voltage vo, the cent state remains until the trigger signal is given. continued,
Therefore, the signal Dr becomes low level in synchronization with the zero point pulse zp. As a result, the gate firing signal Gt changes to low level at that point. Therefore, even when the drive command signal disappears, the pulse width of the gate firing signal Gt does not become narrower as in the conventional case, and the gate firing signal Gt having a predetermined pulse width can be obtained.

なお、本発明方式は上述の回路に躍ることな〈実施可能
である。
Note that the method of the present invention can be implemented without relying on the circuit described above.

〔効果〕〔effect〕

以上のように本発明においては駆動停止時においてゲー
ト点弧信号を消失させるタイミングを電源電圧の位相零
点に同期させるので、駆動停止指令のタイミングに拘わ
らず、I&後まで十分な時間幅のゲート点弧信号が得ら
れ、従ってサイリスタの波速が防止され、ひいては信頼
性の高いサイリスタ整流装置を得ることができる。
As described above, in the present invention, the timing at which the gate firing signal disappears when the drive is stopped is synchronized with the phase zero point of the power supply voltage. An arc signal is obtained, thus the wave speed of the thyristor is prevented, and thus a reliable thyristor rectifier device can be obtained.

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

第1図は本発明方式の一実施例を示す点弧位相角側御回
路のブロック図、第2図はそのタイミングチャート、第
3図は直流電動機の給電回路図、第4図は従来の点弧位
相角側御回路のブロック図、第5図はそのタイミングチ
ャートである。 11・・・同期信号作成回路 12・・・零点パルス発
生回路 13・・・積分器 15・・・比較器 16・
・・位相角指令演算回路17・・・ANDゲート18・
・・Dフリップフロップ36・・・サイリスタ整流装置
 37a、37b・・・サイリスタ なお、図中、同一符号は同一、又は相当部分を示す。
Fig. 1 is a block diagram of an ignition phase angle side control circuit showing an embodiment of the method of the present invention, Fig. 2 is its timing chart, Fig. 3 is a power supply circuit diagram of a DC motor, and Fig. 4 is a conventional point diagram. FIG. 5 is a block diagram of the arc phase angle side control circuit and its timing chart. 11... Synchronization signal generation circuit 12... Zero point pulse generation circuit 13... Integrator 15... Comparator 16.
・・Phase angle command calculation circuit 17・AND gate 18・
...D flip-flop 36...Thyristor rectifier 37a, 37b...Thyristor In the drawings, the same reference numerals indicate the same or equivalent parts.

Claims (1)

【特許請求の範囲】[Claims] 1、点弧位相角制御により出力電圧を可変としたサイリ
スタ整流装置において、駆動停止時には電源電圧の位相
零点に同期させて、サイリスタに与えるゲート点弧信号
を消失させることを特徴とする駆動停止制御方式。
1. In a thyristor rectifier whose output voltage is variable by firing phase angle control, drive stop control characterized in that when driving is stopped, the gate firing signal applied to the thyristor is synchronized with the phase zero point of the power supply voltage and disappears. method.
JP13210186A 1986-06-06 1986-06-06 Drive stop control system of thyristor rectifier Pending JPS62290358A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13210186A JPS62290358A (en) 1986-06-06 1986-06-06 Drive stop control system of thyristor rectifier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13210186A JPS62290358A (en) 1986-06-06 1986-06-06 Drive stop control system of thyristor rectifier

Publications (1)

Publication Number Publication Date
JPS62290358A true JPS62290358A (en) 1987-12-17

Family

ID=15073484

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13210186A Pending JPS62290358A (en) 1986-06-06 1986-06-06 Drive stop control system of thyristor rectifier

Country Status (1)

Country Link
JP (1) JPS62290358A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104252133A (en) * 2014-07-29 2014-12-31 北京航空航天大学 Longitudinal control law smooth switching method of unmanned aerial vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104252133A (en) * 2014-07-29 2014-12-31 北京航空航天大学 Longitudinal control law smooth switching method of unmanned aerial vehicle
CN104252133B (en) * 2014-07-29 2017-01-25 北京航空航天大学 Longitudinal control law smooth switching method of unmanned aerial vehicle

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