JPS5939949A - Automatic controlling method for engine of diesel generator in parallel operation - Google Patents

Automatic controlling method for engine of diesel generator in parallel operation

Info

Publication number
JPS5939949A
JPS5939949A JP14878982A JP14878982A JPS5939949A JP S5939949 A JPS5939949 A JP S5939949A JP 14878982 A JP14878982 A JP 14878982A JP 14878982 A JP14878982 A JP 14878982A JP S5939949 A JPS5939949 A JP S5939949A
Authority
JP
Japan
Prior art keywords
engine
contact
started
relay
battery
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
JP14878982A
Other languages
Japanese (ja)
Inventor
Nobuhiko Koike
小池 順彦
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.)
Nippon Sharyo Ltd
Original Assignee
Nippon Sharyo 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 Nippon Sharyo Ltd filed Critical Nippon Sharyo Ltd
Priority to JP14878982A priority Critical patent/JPS5939949A/en
Publication of JPS5939949A publication Critical patent/JPS5939949A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N33/00Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
    • G01N33/48Biological material, e.g. blood, urine; Haemocytometers
    • G01N33/50Chemical analysis of biological material, e.g. blood, urine; Testing involving biospecific ligand binding methods; Immunological testing
    • G01N33/58Chemical analysis of biological material, e.g. blood, urine; Testing involving biospecific ligand binding methods; Immunological testing involving labelled substances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D25/00Controlling two or more co-operating engines

Abstract

PURPOSE:To enable interruption of the running of arbitrary one of Diesel generators by operating a running cut-off switch which cuts off an engine start command circuit, an engine start detecting circuit, and an engine stop command circuit at a time. CONSTITUTION:An engine automatic controller 1' consists of a controlling power supply change-over part A', an engine start command part B', an engine start detecting part C' (not shown), an engine stop part D' (not shown), and a running cut-off switch 43EG. The running cut-off switch 43EG is an interrupting circuit for interrupting the running of arbitrary one of four generators EG1 to EG4. Thus, the running of an arbitrary generator may be interrupted by one engine controller.

Description

【発明の詳細な説明】 本発明は複数台を並列運転するディーゼル発電機のエン
ジン自動制御方法に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an automatic engine control method for diesel generators in which a plurality of diesel generators are operated in parallel.

従来のディーゼル発電機のエンジン始動指令を第1図に
示すディーゼル発電機のエンジン制御装置により説明す
ると、テイーゼル発を機EGはディーゼルエンジン(以
下エンジンという)I)Bを駆動源として発電機Gが駆
動される。
To explain the engine start command of a conventional diesel generator using the diesel generator engine control device shown in Fig. 1, when the tasel is emitted, the generator G uses the diesel engine (hereinafter referred to as engine) I)B as the drive source. Driven.

このエンジンD Hの始動・停止はエンジン自動制御装
置1によって制御される。エンジン自動制曽 軸装@1は制御電源部へと、起動停止開閉3EG、起動
継電器61回接点6a、始動継電器88MX、同接点8
8MXa、起動成功継電器接点14b、、14b2から
なるエンジン始動指令部Bと、起動成功継電器14−2
.同接点14a、からなるエンジン始動検知部Cと、停
止継電器5X、同接点5X a +停止補助継電器5Z
、同接点sZa、接点6bからなるエンジン停止部りを
備えており、エンジンDBの起動は、起動停止開閉器3
 EGの投入にニジ起動継電器6が励磁し接点6bがO
FF、接点6aがONL、始動継電器88MXが励磁さ
れて接点88MXaがONし、マグネットリレーM−R
が励磁されてスタータモータSMが起動する。
Starting and stopping of this engine DH is controlled by an automatic engine control device 1. The engine automatic control shaft @1 is connected to the control power supply section, starting/stopping opening/closing 3EG, starting relay 61 times contact 6a, starting relay 88MX, same contact 8
8MXa, an engine start command section B consisting of successful start relay contacts 14b, 14b2, and a successful start relay 14-2.
.. An engine start detection section C consisting of the same contact 14a, a stop relay 5X, the same contact 5X a + a stop auxiliary relay 5Z
, a contact sZa, and a contact 6b.The engine DB is started by a start stop switch 3.
When the EG is turned on, the starting relay 6 is energized and the contact 6b is OFF.
FF, contact 6a is ONL, starting relay 88MX is excited, contact 88MXa is ON, magnetic relay M-R
is excited and starter motor SM starts.

エンジンDEが自爆すると、エンジン側の始動成功継電
器14−1の励磁によって接点14a1がONされ、継
電器14−2が励磁され、接点14a、がON、接点1
4 b、e 14 b、カOFFサレル(7)でエンジ
ン始動指令はOFFとなシ、エンジンDEは正常運転に
入る。
When the engine DE self-destructs, the contact 14a1 is turned ON by the excitation of the successful start relay 14-1 on the engine side, the relay 14-2 is energized, the contact 14a is turned ON, and the contact 1
4 b, e 14 b, The engine start command is turned OFF with the power OFF signal (7), and the engine DE enters normal operation.

エンジンDBを停止する場合は開閉器3EGをOFFす
ることによって継電器6が消磁され、接点6aがOFF
、接点6bがONされて停止継電器5Xが励磁され、接
点5Xaが0.Nシ停止リレー S ’l’ P −R
が励磁し、停止ソレノイドS ’1” P −8Oを一
定時間励磁して燃料をカットしてエンジンDEを停止さ
せる。
When stopping the engine DB, the relay 6 is demagnetized by turning off the switch 3EG, and the contact 6a is turned off.
, the contact 6b is turned on, the stop relay 5X is energized, and the contact 5Xa is set to 0. N stop relay S 'l' P -R
is energized, and the stop solenoid S'1''P-8O is energized for a certain period of time to cut the fuel and stop the engine DE.

停止補助継電器5Zは停止ソレノイドS ’I’ P 
−8Oと同様に励磁されておシ、接点sZaはONされ
て継電器5Xは励磁されているが、エンジン回転数が低
下するとともに継電器14−1が消磁し接点14 a、
75fOF Fされ、継電器14−2が消磁して、接点
14b+ 114 btがONL、接点14a2がOF
Fされる。一定時間経過後継電器5Zは消磁して、接点
5Zaが0FFL、継電器5Xが消磁して接点5Xaが
OF’ Fシ、エンジン制御装置1は第1図の如く初期
状態となる。
Stop auxiliary relay 5Z is stop solenoid S 'I' P
-8O is energized, contact sZa is turned on and relay 5X is energized, but as the engine speed decreases, relay 14-1 is demagnetized and contact 14a,
75fOF, relay 14-2 is demagnetized, contact 14b + 114 bt is ONL, and contact 14a2 is OFF.
F is given. After a certain period of time has elapsed, the succeeding electric appliance 5Z is demagnetized and the contact 5Za is set to 0FFL, the relay 5X is demagnetized and the contact 5Xa is set to OFF', and the engine control device 1 is in the initial state as shown in FIG.

なお、C−DはバッチIJ B Tのチャージングダイ
ナモを示す。
Note that CD indicates a charging dynamo of batch IJBT.

第2図及び第3図は、エンジン始動開始後の経過時間と
エンジン回転数N及びバッチ’) ’Ill圧■の関係
を示す説明図であシ、第2図(a)はエンジンが始動成
功して回転数N。が時間の経過とともに上昇する状態を
示し、@3図(a)はエンジンが自爆しない場合の回転
数NI N、 I N、を表わす。第2図(b)はエン
ジン始動時xDエンジン自爆点0を経て、バッテリ電圧
Voが回復する状態を示し、第3図(b)はエンジン始
動時より一定時間経過してバッテリ電圧V、 、 V、
 、 V、が回復した状態を表わしており、■はバッテ
リが無負荷時のバッテリ電圧、VAはエンジン制御装置
の最低操作電圧であって、第2図(b)に示す如くエン
ジン自爆後であっても、一定時間はバッテリ電圧■。は
最低操作電圧■よシも低く、第3図(b)はバッテリ電
圧V、 、 V、 、 V、いずれも最低操作電圧VA
、Cυ低く、従ってエンジン制御電源には不適当である
Figures 2 and 3 are explanatory diagrams showing the relationship between the elapsed time after starting the engine, the engine speed N, and the batch'Ill pressure. and the number of revolutions N. Fig. 3 (a) shows the rotational speed NI N, IN when the engine does not self-destruct. Fig. 2(b) shows a state in which the battery voltage Vo recovers after passing through xD engine self-destruction point 0 at the time of engine starting, and Fig. 3(b) shows a state in which the battery voltage Vo recovers after a certain period of time has elapsed from the time of engine starting. ,
, V, represent the recovered state, ■ is the battery voltage when the battery is under no load, VA is the minimum operating voltage of the engine control device, and as shown in Figure 2 (b), after the engine self-destruction. However, for a certain period of time, the battery voltage ■. is the minimum operating voltage.
, Cυ are low and therefore unsuitable for engine control power supply.

一般にエンジン自動制御装置の制御電源は第1Dのバッ
テリBTより安定化電源装置2を介して電源を供給する
か、あるいは他の独立したバッテリB T、 (第1図
鎖線部)を設けてエンジン制御電源を供給している。
Generally, the control power source for the automatic engine control device is supplied from the first battery BT via the stabilizing power supply device 2, or by providing another independent battery BT (shown with chain lines in Figure 1) to control the engine. Supplying power.

電機BDに設けられており、その操作も繁雑である0 本発明は上記に鑑みなされたものであって、その目的と
するところは、従来の如くエンジン制御装置の制御電源
として安定化電源装置、あるいは独立した制御電源用の
バッテリを要せず、かつ複数台のエンジン制御装置を設
けることなく、任意ン自動制御方法を提供するものであ
る。
The present invention has been made in view of the above, and its purpose is to provide a stabilized power supply device as a control power source for an engine control device as in the past. Alternatively, an arbitrary automatic control method is provided without requiring an independent control power source battery and without providing a plurality of engine control devices.

法において先発始動するエンジンの制御電源は後発始動
するエンジンのバッテリから供給し、先発始動のエンジ
ンが始動完了すると、後発始動するエンジンのバッテリ
からの電源供給をカットし、先発始動エンジンのバッテ
リ電圧が回復する一定時間経過したのち、後発始動エン
ジンの制御電源を先発始動エンジンのバッテリに切替え
て供給することにあり、第2の発明は第1の発明におい
て、エンジン始動前に、始動指令回路、:始Bur検知
回路。
According to the law, control power for the engine started earlier is supplied from the battery of the engine started later, and when the engine started earlier finishes starting, the power supply from the battery of the engine started later is cut off, and the battery voltage of the engine started earlier is reduced. After a certain period of recovery time has elapsed, the control power source for the late-starting engine is switched to and supplied to the battery of the first-starting engine, and the second invention is based on the first invention, and includes, before starting the engine, a start command circuit: First Bur detection circuit.

電機の運転を休止できるようにしたことにある。The reason is that it is possible to stop the operation of electrical equipment.

以下本発明の一実施例を第4図乃至第6図によって詳細
に説明する。
An embodiment of the present invention will be described in detail below with reference to FIGS. 4 to 6.

第4図(a)と第4図(l:0は左右に連続しているも
ので、不発り]方法に係るエンジン自動制御装置の電気
回路を示す図であって、図中第1図と同符号のものは同
一のものを表わす。
FIG. 4(a) and FIG. 4 are diagrams showing the electric circuit of the automatic engine control device according to the method (l:0 is continuous on the left and right, no firing), and FIG. Items with the same reference numerals represent the same item.

エンジン自動制御装置1は制御電源切替部A′、工より
構成される。
The automatic engine control device 1 is composed of a control power supply switching section A' and a control power supply switching section A'.

4台の発電機EGG、 BG、、 BG8. EG、は
、それぞれバッテリB T、、 B T、、 B T3
. B T、を設けてあり、バッテリB T、は配線B
、。l Bll l Elo * E、、で制御電源切
替部A/ K接続され、バッテリ13 TsiJ配線B
、3゜B141 ”’181 B14で制御電源切替部
A′に接続しである。
4 generators EGG, BG,, BG8. EG, are the batteries BT, BT, BT3, respectively.
.. BT is provided, and the battery BT is connected to the wiring B.
,. l Bll l Elo * E,, control power supply switching unit A/K is connected, battery 13 TsiJ wiring B
, 3°B141'''181 Connected to the control power supply switching section A' at B14.

制御電源切替部A/には始動停止開閉器3 E G、停
止継電器接点sXk>1(以下接点という)、起動継電
器6.タイマBT、タイマ接点s Ta、補助継電器8
X、同接点8 X a、 l 8 X a、T 8 X
 b、 I瞬時励磁式機械保持型継電器8−12. 8
−34 (以下継電器という)、接点8−12a、、 
8−12blI8−34a118−34b、l起動成功
継電器接点14 12a+、14 12k)1,14 
34k)1+ 14−34 b、 (以下接点という)
、冷機運転用タイマ接点5Tb (以下接点という)を
配#1lll乃至1エンジン始動指令部B′は閉塞解除
スイッチ3−86 R,接点5 X b2.起動継電器
接点6a(以下接点という)、接点14t)1+ 14
bt、14k)3+ 14 ba v 14 12 b
2 + 14 ’ 34 bs *接点8−12a2+
8 12a3+ 8 12a4+ 8 34a2* 8
−34a8,8−34aB渋滞検出継電器48.接点4
B?L?渋滞補助継電器48X、接点48 X ia+
48Xb、 始動継電器88MX、始動継電器接点8 
sMXa、8 sMXa!、88MXa8,88MXa
4(以下接点という)を配線B+t + E12@ 2
0 乃至43で接続しである。
The control power switching unit A/ includes a start/stop switch 3 EG, a stop relay contact sXk>1 (hereinafter referred to as a contact), and a start relay 6. Timer BT, timer contact s Ta, auxiliary relay 8
X, same contact 8 X a, l 8 X a, T 8 X
b, I instantaneous excitation type mechanically held relay 8-12. 8
-34 (hereinafter referred to as relay), contact 8-12a,...
8-12blI8-34a118-34b, l startup success relay contact 14 12a+, 14 12k) 1,14
34k) 1+ 14-34 b, (hereinafter referred to as contact)
, cold engine operation timer contact 5Tb (hereinafter referred to as contact) is arranged for #1lll to 1 engine start command section B', block release switch 3-86R, contact 5X b2. Starting relay contact 6a (hereinafter referred to as contact), contact 14t) 1+ 14
bt, 14k) 3+ 14 ba v 14 12 b
2 + 14' 34 bs *Contact 8-12a2+
8 12a3+ 8 12a4+ 8 34a2* 8
-34a8, 8-34aB traffic jam detection relay 48. Contact 4
B? L? Traffic jam auxiliary relay 48X, contact 48X ia+
48Xb, starting relay 88MX, starting relay contact 8
sMXa, 8 sMXa! ,88MXa8,88MXa
4 (hereinafter referred to as contact) is wired B+t + E12@2
0 to 43 are connected.

エンジン始動検知部C′には起動成功継電器14−12
s14 34(以下継電器という)p接点14a++ 
14a2+ 14a3+ 14a4を配線Bn + B
、、 。
The engine start detection section C' has a start success relay 14-12.
s14 34 (hereinafter referred to as relay) p contact 14a++
14a2+ 14a3+ 14a4 wiring Bn + B
,, .

44乃至47で接続しである。44 to 47 are connected.

エンジン停止部D′は冷機運転用タイマ5TIタイマ接
点5Ta、停止継電器5X、接点5 X J +5 X
 aり 5 X asl 5 X 1a4 +接点6b
、接点14−12at+ 14−34a+停止補助継電
器接点5Z11 341 35.381 39.421
 43で接続し、エンジン始動検知部C′に接点861
8@ + 87 r Sgtを配線B12* 44y 
 44t  45+ ’B12t46+  46+47
で接続し、エンジン停止部D′に接点81+18101
Sll l st!を配線52,53,55,56,5
8゜59.61.62で接続しである。
Engine stop part D' includes cold engine operation timer 5TI timer contact 5Ta, stop relay 5X, contact 5
ari 5 X asl 5 X 1a4 + contact 6b
, contact 14-12at+ 14-34a+stop auxiliary relay contact 5Z11 341 35.381 39.421
43, and contact 861 to the engine start detection section C'.
8@ + 87 r Wire Sgt B12* 44y
44t 45+ 'B12t46+ 46+47
Connect with 81+18101 to engine stop part D'.
Sll l st! Wiring 52, 53, 55, 56, 5
It is connected at 8°59.61.62.

したがってその操作方法についで説明すると、4台の発
電機B GI、EG2 、E Gs * F’丸は先発
の発電機EG、、EG2と後発の発電機HG31 El
への2組に分けられておシ、各々のバッテリスイッチB
S、。
Therefore, to explain how to operate it, there are four generators B GI, EG2, EGs * Circle F' is the first generator EG, EG2 and the second generator HG31 El.
Divided into two sets, each battery switch B
S.

B S、、 B S、、 B S、をONにしておく。Turn BS, , BS, , BS, ON.

まず継電器8−34のり“ローツなグコイル8−34C
Cが励磁され、制御電源切替部A′の接点8−34a、
+エンジン始動指令部B′の接点8−34a2.8−3
4a3 + 8 34 a4がONし、制御電源切替部
A’1lll17)接点8−34b、がOFFとなり、
配線B14と配線Bltが、配線E14と配線E8.が
それぞれ接続されてエンジン制御装置1′!の電源はバ
ッチIJ B T、から供給される。
First of all, relay 8-34 glue "Rotz na gcoil 8-34C"
C is excited, and the contact 8-34a of the control power switching section A',
+ Contact point 8-34a2.8-3 of engine start command section B'
4a3 + 8 34 a4 turns on, control power switching unit A'1ll17) contact 8-34b turns off,
Wiring B14 and wiring Blt are connected to wiring E14 and wiring E8. are connected to the engine control device 1'! Power is supplied from the batch IJBT.

次に開閉器3EGをONにすると、起動継電器6が励磁
し、エンジン停止部D′の接点6bがOFFし、エンジ
ン始動検知部B′の接点6aはONされるので、断続継
電器66を介して始動継電器88MXが一定時間励磁さ
れ、接点88MXa、、88 MXa、t 88 MX
 a3+  88 MX a4カONスル力、発電機E
G、EGtの接点8−12a、、 8−12a、1がO
FFのため発電機B G、 、 B G2にのみ始動指
令が発せられる。
Next, when the switch 3EG is turned ON, the starting relay 6 is excited, the contact 6b of the engine stop section D' is turned OFF, and the contact 6a of the engine start detection section B' is turned ON. The starting relay 88MX is energized for a certain period of time, and the contacts 88MXa, , 88 MXa, t 88 MX
a3+ 88 MX a4 power, generator E
G, EGt contacts 8-12a, 8-12a, 1 are O
Since the generators are FF, a start command is issued only to generators BG, BG2.

発電機EG、、EG2の起動が成功すると接点14al
+ 、1 a−atがONL、接点14 b、、 、+
 4 btt:tOFFし、エンジン始動検知部C′の
III電器14−12が励磁され、制御電源切替部A′
の接点14−12 b、がOFF、接点14−12 a
、がON、エンジン始動指令部B′の接点14−12 
b、がOI” F、エンジン停止部D′の接点14−1
2 a、カON L4、バッテリBTI工りタイマ8T
、補助継電器8Xが励磁され、接点8XaI、8Xa2
がONされる。接点8 X a、は電源切替を安定して
行うまために継電器8Xの自己保持用として設けである
When the generators EG, EG2 are successfully started, the contact 14al
+ , 1 a-at is ONL, contact 14 b, , , +
4 btt: tOFF, the III electric appliance 14-12 of the engine start detection section C' is excited, and the control power supply switching section A' is turned off.
Contact 14-12 b is OFF, contact 14-12 a
, is ON, contact 14-12 of engine start command section B'
b, is OI'' F, contact 14-1 of engine stop part D'
2 a, power ON L4, battery BTI timer 8T
, auxiliary relay 8X is energized, contacts 8XaI, 8Xa2
is turned on. The contact 8Xa is provided for self-holding of the relay 8X in order to stably switch the power supply.

接点8 X a、がONされると、継電器8−34のリ
セットコイル8−34RCが励磁し、接点8−34b皿
がON、接点8−’34a、乃至8−34 a4がOF
 ];’ L、配置 Fl14(!l−配線13+t 
l 配置E、、’ト配mE、、カOF Fされて、エン
ジン始動指令部B/、同始動検知部C′・同停止部D′
への電源はカットされる。次にバッチIJ B T、の
バッテリ電圧が回復する一定時間(約5秒間)をタイマ
8Tがカウントしたのち、接点8TaがONし、継電器
8−12のクロージングコイル8−12CCが励磁し、
接点8−12a1乃至8−12 a、がONし、配線B
0.ト配線]、:l、、 、配線E11と配線B(2が
ギれぞれ接続されて、制御電源はバッテリB T、がら
バッチIJ HT、に切替えが完了する0 発電機EOs、EG、の始動指令は前述の発電機EG、
 、 E G2と同様であり、エンジン始動指令部B′
のエンジン始動の渋滞については説明を省略する。
When contact 8Xa is turned on, reset coil 8-34RC of relay 8-34 is excited, contact 8-34b is turned on, and contacts 8-'34a to 8-34a4 are turned off.
];' L, arrangement Fl14 (!l-wiring 13+t
l Arrangement E, , 'T' mE,, is turned OFF, and the engine start command part B/, the engine start detection part C', and the engine stop part D'
power is cut off. Next, after the timer 8T counts a certain period of time (approximately 5 seconds) for the battery voltage of the batch IJB T to recover, the contact 8Ta turns ON, and the closing coil 8-12CC of the relay 8-12 is energized.
Contacts 8-12a1 to 8-12a are turned on, and wiring B
0. Wiring E11 and Wiring B (2) are connected, and the control power source is switched from battery B T to batch IJ HT.0 Generators EOs and EG The starting command is from the aforementioned generator EG,
, E Same as G2, engine start command section B'
An explanation of the congestion caused by starting the engine will be omitted.

発電機BG、、EG4の起動が成功すると接点14a3
 + 14 a4がON、継電器14−34が励磁され
て、接点14−34aをON、接点14bx+14b4
* 14−34 b++ 14 ’ 34b2+ l 
4 34b3がOFFされ、断続継電器66への通電が
OFFされ、以後エンジン始動指令が断となる一万、タ
イマ8T、補助継電器8Xが消磁して接点8 X b。
When the generators BG, EG4 are successfully started, the contact 14a3
+14 a4 is ON, relay 14-34 is energized, contact 14-34a is ON, contact 14bx+14b4
* 14-34 b++ 14' 34b2+ l
4 34b3 is turned off, the power supply to the intermittent relay 66 is turned off, and the engine start command is thereafter cut off.10,000, the timer 8T and the auxiliary relay 8X are demagnetized, and the contact 8Xb is turned off.

をONL、接点8 T a +  8 X J +  
8 X ?L2がOFFとなる。
ONL, contact 8 T a + 8 X J +
8X? L2 turns OFF.

次にエンジン停止の操作について説明する。Next, the operation for stopping the engine will be explained.

開閉器aEGをOF l’にすると継電器6が消磁され
、接点6aがOF1喝゛し、接点−6bがONする。
When the switch aEG is set to OF1', the relay 6 is demagnetized, the contact 6a is activated OF1, and the contact -6b is turned on.

接点14−12at、14 34aはONさレテイるの
で冷機運転用タイマ5Tが励磁されて、一定時間(約6
0秒間)冷機運転したのち、、al’R&がα′RRン
、接点sTaがONL、、停止継電器5Xが励磁され接
点5 X b、をOF)’、接点5X a、乃至s X
 a4をONして発電機E G、乃至E G4の停止ソ
レノイドを一定時間励磁[7て燃料をカットする。
Since the contacts 14-12at and 14-34a are turned on, the cold machine operation timer 5T is energized for a certain period of time (approximately 6
After cold operation (for 0 seconds), al'R& is α'RR, contact sTa is ONL, stop relay 5X is energized and contact 5X b is turned off)', contact 5X a to sX
Turn on a4 to energize the stop solenoids of generators EG and EG4 for a certain period of time [7 to cut the fuel.

エンジンが低速になるにしたがって接点14 a。As the engine speed decreases, contact 14a.

乃”A 14 a、カOF F−2れ、継電器14−1
2.14−34が消磁され、接点14−12 b、シ至
1412by、14b、乃至14b4114 34bl
乃至14−34 b3がON、9点14−12a、、1
4−12a2.14−34aがOF F l、、冷機運
転用タイマ5Tは消磁して、接点5TbはON、接点5
TaViOFFされるが、停止ソレノイドはエンジンが
完全に停止されるまで(約30秒間)励磁されており、
その後消磁されると、接点5 Z a、乃至5Za4が
OFFされ、継電器5Xが消磁し°[接点5Xa、乃至
5 X a、がOFF、接点5 X b、が0N−jる
ので、継電器8−12のリセットコイル8−12R,C
が励磁され、接点8−12 a、乃至8−12 a。
乃"A 14 a, KA OF F-2, relay 14-1
2.14-34 is demagnetized, contacts 14-12b, 1412by, 14b, 14b4114 34bl
~14-34 b3 is ON, 9 points 14-12a, 1
4-12a2.14-34a is OFF F l, cold operation timer 5T is demagnetized, contact 5Tb is ON, contact 5
TaVi is turned off, but the stop solenoid is energized until the engine is completely stopped (about 30 seconds).
After that, when demagnetized, the contacts 5Za to 5Za4 are turned OFF, and the relay 5X is demagnetized. 12 reset coils 8-12R,C
is energized, and contacts 8-12a to 8-12a.

がOFF l、、接点8−12 b、がONとなり、継
電器8−34のクロージングコイルに8−34CCが励
磁され、接点8−34 b、を01” )’ L、、接
点8−34 &、乃至8−34a、1ONlcして、エ
ンジン自動制御装置1′の制御電源は、エンジンが完全
に停止したのちにバッテリB T、からバッチ!jBT
、に切替えられる。
is OFF, contact 8-12b is turned ON, 8-34CC is excited in the closing coil of relay 8-34, and contact 8-34b is turned 01")' L,, contact 8-34 &, 8-34a to 8-34a, 1 ONlc, and the control power source for the automatic engine control device 1' is switched from the battery BT to the batch!jBT after the engine has completely stopped.
, can be switched to .

運転カットアウトスイッチ43EGは4台の発電機EG
、、 EG、、 EG、、 EG4のうち任意の1台の
運転を休止させるための休止回路であって、接点S、、
S?乃至SI2のモードは第5図に示す通りであって、
4台の発電機EG、、 EG2. EG、、 EG4に
全て運転する場合には第4図の如(、接点Sl乃至S4
゜SQ乃至SrtはON、接点Sl乃至S、はOF F
となっている。
Operation cutout switch 43EG is for four generators EG
,, EG,, EG,, A stop circuit for stopping the operation of any one of the EG4, the contact S,...
S? The modes of SI2 to SI2 are as shown in FIG.
4 generators EG,, EG2. When operating all EG, EG4, as shown in Figure 4 (contacts Sl to S4
゜SQ to Srt are ON, contacts Sl to S are OFF F
It becomes.

例えば発電機E Q、の運転を休止させる場合には運転
カットアウトスイッチ43EGの1号機を指定すれば接
点S、、S、がOFFされ、接点S、がONされる。こ
の状態でいま起動停止開閉器3 E C3をONすると
、エンジン始動指令部B′の接点、S、がOI” F−
Jれているので、発電機EQ、への始動指令は発せられ
ない。
For example, when stopping the operation of generator EQ, specifying the No. 1 operation cutout switch 43EG turns contacts S, , S, OFF and contacts S, ON. In this state, if the start/stop switch 3EC3 is turned ON, the contact point S of the engine start command section B' becomes OI"F-
Since the engine is closed, no starting command is issued to the generator EQ.

発電機Eへが始動成功すれば、発電機E G、からの始
動成功指令がなくても、接点S、はONとなっているの
で、継電器14−12は励磁されて前述の如く制御電源
の切替が可能であυ、エンジン停止の場合には接点s 
X a、がONされても接点S、が0、FFされている
ので、発電機E G、には停止指令がカットされる。
If the generator E is successfully started, the relay 14-12 is energized and the control power supply is turned on as described above, since the contact S is ON even if there is no successful start command from the generator EG. It is possible to switch υ, and in case of engine stop, contact s
Even if Xa is turned on, contact S is 0 and FF, so a stop command is cut off to generator EG.

本発明は発′RL装置を常用電源として運転する場合、
非常用電源として運転する場合、いずれの場合でも可能
であり、並列運転台数1.エンジン始動順序、運転休止
台数等は本実施例に限定されるものではない。
When the present invention operates the generator RL device as a regular power source,
When operating as an emergency power source, it is possible in either case, and the number of units operated in parallel is 1. The engine starting order, the number of out-of-operation vehicles, etc. are not limited to this embodiment.

以上の説明から明らかなように本方法を実施すると従来
のようにエンジン制御装置の制御電源に安定化電源装置
や他の独立したバッテリを設けることすく、シかも1台
のエンジン制御装置で複数台の発電機のエンジン制御が
可能であって、かつ任意の発電機の運転休止も可能であ
り運転操作が容易である等の利点がある。
As is clear from the above explanation, when this method is implemented, it is not necessary to provide a stabilized power supply device or other independent battery as the control power source of the engine control device as in the past, and it is possible to use multiple batteries with one engine control device. It is possible to control the engines of several generators, and it is also possible to stop the operation of any generator, which has advantages such as easy operation and operation.

制御装置の説明図、第2図及び第3図はエンジン回転数
とバッテリ電圧の関係を示す説明図、第4図(a)、(
b)は連続するものであって、本発明に係るエンジン自
動制御装置の電気回路図、第5図は運転カットアウトス
イッチのモード図であるOA′は制御電源切替部、B′
はエンジン始動指令部、C′はエンジン始動検知部、D
′はエンジン停止部、1′はエンジン自動制御装置、3
BGは起動停止開閉器、3−86Rは閉塞解除スイッチ
、5Tは冷機運転用タイマ、5Ta、s’rbは冷機運
転用タイ−q接点、5Xは停止継電器、5 X a、乃
至5 X a4+5Xb、、5Xb、は停止継電器接点
、5zは停止補助継電器、5 Z a、乃至5 Z a
4は停止補助継電器接点、6は起動継電器、6a、6b
は起動継電器接点、8Tはタイマ、8Taはタイマ接点
、8Xは補助継電器、8 X a、 l 8 X a2
 + 8 X b+は補助継電器接点、8−12.8−
34は瞬時励磁式機械保持型継電器、8−12 a、乃
至8−12a4,8−12b、58−34a、乃至8−
34a4+8−34b、は同上接点、14−12.14
−34は起動成功継1?斥十ヒ34a、14費刊胎片 接点、 48は渋滞検出継電器、48a、け同上接点、48Xは
渋滞補助継電器、4sXa+  4”sxbは同上接点
、66は断続継電器、88MXは始動継電器、SI乃至
S12は運転カットアウトスイッチ接点である。
An explanatory diagram of the control device, Figures 2 and 3 are explanatory diagrams showing the relationship between engine speed and battery voltage, and Figures 4 (a) and (
b) is a continuous electrical circuit diagram of the automatic engine control device according to the present invention; FIG. 5 is a mode diagram of the operation cut-out switch; OA' is a control power switching unit;
is the engine start command section, C' is the engine start detection section, D
' is the engine stop part, 1' is the engine automatic control device, 3
BG is a start/stop switch, 3-86R is a block release switch, 5T is a timer for cold machine operation, 5Ta, s'rb are tie-q contacts for cold machine operation, 5X is a stop relay, 5 X a, to 5 X a4+5Xb, , 5Xb is a stop relay contact, 5z is a stop auxiliary relay, 5 Z a to 5 Z a
4 is a stop auxiliary relay contact, 6 is a starting relay, 6a, 6b
is the starting relay contact, 8T is the timer, 8Ta is the timer contact, 8X is the auxiliary relay, 8 X a, l 8 X a2
+ 8 X b+ is auxiliary relay contact, 8-12.8-
34 is an instantaneous excitation type mechanically held relay, 8-12 a to 8-12a4, 8-12b, 58-34a to 8-
34a4+8-34b, same contact as above, 14-12.14
-34 is the first successful start? 34a, 14 contacts, 48 is a traffic jam detection relay, 48a is a contact as above, 48X is a traffic jam auxiliary relay, 4sXa+4"sxb is a contact as above, 66 is an intermittent relay, 88MX is a starting relay, SI to S12 is an operation cutout switch contact.

豪2図 一吋間 舟3図 −吟閤Australia 2 map An hour Boat 3 −Ginja

Claims (1)

【特許請求の範囲】 1、複数台のディーゼル発電機を並列運転制御する方法
において、先発始動するエンジンの制御電源に後発始動
するエンジンのバッテリから供給し、先発始動のエンジ
ンが始動完了すると、後発始動するエンジンのバッテリ
からの電源供給をカットし、先発始動エンジンのバッテ
リ電圧が回復する一定時間経過したのち、後発始動エン
ジンの制御電源を先発始動エンジンのバッテリに切替え
て供給することを特徴とする並列運転ディーゼル発電機
のエンジン自動制御方法。 2、 複数台のディーゼル発電機を並列運転制御する方
法において、エンジン始動前に、始動指令回路、始動検
知回路、エンジン停止指令回路を一斉にカットする運転
カットアウトスイッチを操作して、任意のディーゼル発
電機の運転を休【卜し、先発始動するエンジンの制御電
源を後発始動するエンジンのバッテリから供給し、先発
始動のエンジンが始動完了すると、後発始動するエンジ
ンのバッテリからの電源供給をカットし、先発始動エン
ジンのバッチIJ を圧が回復する一定時間経過したの
ち、後発始動エンジンの制御電源を先発始動エンジンの
バッテリに切替えて供給することを特徴とする並列運転
ディーゼル発電機のエンジン自動制御方法。
[Claims] 1. In a method for controlling parallel operation of a plurality of diesel generators, the control power of the engine to be started first is supplied from the battery of the engine to be started later, and when the earlier started engine has finished starting, The power supply from the battery of the engine to be started is cut off, and after a certain period of time has elapsed for the battery voltage of the earlier started engine to recover, the control power for the later started engine is switched and supplied to the battery of the earlier started engine. Automatic engine control method for parallel operating diesel generators. 2. In the method of controlling multiple diesel generators in parallel operation, before starting the engine, operate the operation cut-out switch that cuts off the start command circuit, start detection circuit, and engine stop command circuit all at once, The generator is stopped, the control power for the engine to be started earlier is supplied from the battery of the engine to be started later, and when the engine started earlier has finished starting, the power supply from the battery to the engine to be started later is cut off. , an automatic engine control method for a parallel-operated diesel generator, characterized in that after a certain period of time has elapsed for pressure to recover in the batch IJ of the earlier-started engine, the control power source for the later-started engine is switched to the battery of the earlier-started engine and supplied. .
JP14878982A 1982-08-27 1982-08-27 Automatic controlling method for engine of diesel generator in parallel operation Pending JPS5939949A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14878982A JPS5939949A (en) 1982-08-27 1982-08-27 Automatic controlling method for engine of diesel generator in parallel operation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14878982A JPS5939949A (en) 1982-08-27 1982-08-27 Automatic controlling method for engine of diesel generator in parallel operation

Publications (1)

Publication Number Publication Date
JPS5939949A true JPS5939949A (en) 1984-03-05

Family

ID=15460719

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14878982A Pending JPS5939949A (en) 1982-08-27 1982-08-27 Automatic controlling method for engine of diesel generator in parallel operation

Country Status (1)

Country Link
JP (1) JPS5939949A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997026453A1 (en) * 1996-01-19 1997-07-24 Komatsu Ltd. Automatic load distributing apparatus for generator and method of controlling same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997026453A1 (en) * 1996-01-19 1997-07-24 Komatsu Ltd. Automatic load distributing apparatus for generator and method of controlling same
US6066897A (en) * 1996-01-19 2000-05-23 Komatsu Ltd. Automatic load distributing apparatus for generator and method of controlling same

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