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JPS6347906B2 - - Google Patents
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JPS6347906B2 - - Google Patents

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Publication number
JPS6347906B2
JPS6347906B2 JP22392683A JP22392683A JPS6347906B2 JP S6347906 B2 JPS6347906 B2 JP S6347906B2 JP 22392683 A JP22392683 A JP 22392683A JP 22392683 A JP22392683 A JP 22392683A JP S6347906 B2 JPS6347906 B2 JP S6347906B2
Authority
JP
Japan
Prior art keywords
transistor
circuit
capacitor
constant
angle signal
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
JP22392683A
Other languages
Japanese (ja)
Other versions
JPS60116866A (en
Inventor
Hideki Ninomya
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.)
Fuji Electric Co Ltd
Denso Corp
Original Assignee
Fuji Electric Co Ltd
Fuji Electric Corporate Research and Development Ltd
NipponDenso 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 Fuji Electric Co Ltd, Fuji Electric Corporate Research and Development Ltd, NipponDenso Co Ltd filed Critical Fuji Electric Co Ltd
Priority to JP22392683A priority Critical patent/JPS60116866A/en
Publication of JPS60116866A publication Critical patent/JPS60116866A/en
Publication of JPS6347906B2 publication Critical patent/JPS6347906B2/ja
Granted legal-status Critical Current

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  • Ignition Installations For Internal Combustion Engines (AREA)
  • Electrical Control Of Ignition Timing (AREA)

Description

【発明の詳細な説明】 〔発明の属する技術分野〕 本発明は、火花点火式内燃機関の点火時期制御
装置に関し、特に電子回路で点火時期を決定する
方式の内、少なくとも1個のコンデンサの充放電
で点火時期を制御する電子式点火時期制御装置の
改良に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Technical field to which the invention pertains] The present invention relates to an ignition timing control device for a spark-ignited internal combustion engine, and in particular to a method of determining ignition timing using an electronic circuit. This invention relates to an improvement of an electronic ignition timing control device that controls ignition timing by electric discharge.

〔従来技術とその問題点〕[Prior art and its problems]

電子回路で点火時期を決定する一般的な回路構
成を第1図に示す。この回路は、機関回転数に同
期して回転するロータ1、そのロータの回転に応
じて出力信号を出す電磁ピツクアツプコイル2、
このピツクアツプコイルの出力信号を波形整形す
る入力回路3、進角時間を演算する進角演算回路
4、点火コイルの一次電流通電時間を制御する閉
角制御回路5、進角及び閉角演算結果を合成・増
幅する増幅回路6、点火コイル一次電流を制御す
るパワートランジスタ7および点火コイル8等で
構成されている。
FIG. 1 shows a general circuit configuration for determining ignition timing using an electronic circuit. This circuit consists of a rotor 1 that rotates in synchronization with the engine speed, an electromagnetic pickup coil 2 that outputs an output signal according to the rotation of the rotor,
An input circuit 3 that shapes the waveform of the output signal of this pickup coil, a lead angle calculation circuit 4 that calculates the lead angle time, a closing angle control circuit 5 that controls the primary current conduction time of the ignition coil, and a lead angle and closing angle calculation result. It is comprised of an amplifier circuit 6 for combining and amplifying, a power transistor 7 for controlling the ignition coil primary current, an ignition coil 8, and the like.

第2図に1個のコンデンサの充放電で点火時期
を制御する従来の電子式点火時期制御装置の進角
原理図を示す。第2図において、Aはピツクアツ
プコイルの出力波形、Bは入力回路の出力波形、
Cは進角演算用コンデンサの充放電電圧波形、D
は進角演算用コンデンサを充放電する定電流波形
でIP1、IP2が定電流放電波形IQが定電流充電波形、
Eは進角信号出力波形である。又、B波形のθ1
θ2は、機関回転数とは無関係にロータの形状、ピ
ツクアツプコイル、入力回路によつて決定される
一定角度信号である。第3図に、進角度特性の一
例を示す。
FIG. 2 shows a diagram of the advance principle of a conventional electronic ignition timing control device that controls ignition timing by charging and discharging a single capacitor. In Figure 2, A is the output waveform of the pickup coil, B is the output waveform of the input circuit,
C is the charging/discharging voltage waveform of the lead angle calculation capacitor, D
is the constant current waveform that charges and discharges the lead angle calculation capacitor, I P1 is the constant current discharge waveform , I Q is the constant current charging waveform,
E is the advance angle signal output waveform. Also, θ 1 of the B waveform,
θ 2 is a constant angle signal determined by the rotor shape, pickup coil, and input circuit, regardless of engine speed. FIG. 3 shows an example of advance angle characteristics.

さて、第2図において、一定角度θ2の期間、進
角演算用コンデンサに、IP1、IP2と値の異なつた
定電流で充電する。次に一定角度θ1の期間に、定
電流IQで放電し、放電終了時点、すなわち、前記
定電流充電による充電電荷量がゼロになつた時点
を点火位置とする。E波形taが進角時間となる。
この結果、第3図に示すように機関回転数N1
N2の期間の進角度はt1+tx2期間の充電電流
(IP1、IP2)で決定され、又、N2−N3の期間は、
t1(実際には後述するtx1)期間の充電電流(IP1
で決定される。
Now, in FIG. 2, during a period of a constant angle θ 2 , the advance angle calculation capacitor is charged with constant currents having different values I P1 and I P2 . Next, during a period of a constant angle θ 1 , the battery is discharged with a constant current IQ , and the ignition position is set at the time when the discharge ends, that is, when the amount of charge due to the constant current charging becomes zero. The E waveform t a becomes the advance time.
As a result, as shown in Fig. 3, the engine speed N 1
The advance angle for the period N 2 is determined by the charging current (I P1 , I P2 ) for the period t 1 + tx 2 , and for the period N 2 - N 3 ,
Charging current (I P1 ) during t 1 (actually tx 1 described later)
determined by

この様に動作する進角演算方式では、機関回転
数N2−N3期間の理論進角度は、第3図ロの様な
一定値θaとなる。
In the advance angle calculation method that operates in this manner, the theoretical advance angle during the period of engine rotational speed N 2 -N 3 becomes a constant value θ a as shown in FIG. 3B.

第3図において、機関回転数がNX1の時の進角
度を求める。
In Figure 3, find the advance angle when the engine speed is N X1 .

θ1+θ2=360゜ ……(1) t〓1+t〓2=60/Nx1 ……(2) Nx1の時のt1をtx1とすると、充電電荷量と放
電電荷量は同じであるから、 IP1tx1=IQtx3 ……(3) 進角時間taは、 ta=t〓1−tx3=t〓1−tx1・IP1/IQ ……(4) (4)式を進角度に変換すると、進角度θaは、 θa=6Nx1・t〓1(1+IP1/IQ)−360゜ ・IP1/IQ ……(5) 6Nx1・t〓1は機関回転数Nxの時のt〓1を角度に
変換した値θ1で、(5)式は θa=θ1(1+IP1/IQ)−360゜・IP1/IQ ……(6) となる。
θ 1 + θ 2 = 360゜ ...(1) t〓 1 +t〓 2 = 60/Nx 1 ...(2) If t 1 at Nx 1 is tx 1 , the amount of charged charge and the amount of discharged charge are the same Therefore, I P1 tx 1 = I Q tx 3 ...(3) The advance time ta is ta=t〓 1 −tx 3 =t〓 1 −tx 1・I P1 /I Q ...(4) Converting equation (4) to an advance angle, the advance angle θa is: θa=6Nx 1・t〓 1 (1+I P1 /I Q )−360° ・I P1 /I Q ……(5) 6Nx 1・t〓 1 is the value θ 1 obtained by converting t〓 1 into an angle at engine speed Nx, and formula (5) is θa = θ 1 (1 + I P1 /I Q ) - 360°・I P1 /I Q ...( 6) becomes.

(6)式において、θ1は機関回転数には無関係な一
定角度信号であり、又、IP1、IQとも定電流で一定
値である。この為、θaは機関回転数とは無関係
に一定値となる。
In equation (6), θ 1 is a constant angle signal that is unrelated to the engine speed, and both I P1 and I Q are constant currents and have constant values. Therefore, θa is a constant value regardless of the engine speed.

なお、同様にNx2の時のθbを求めると、 θb=θ1−6Nx2(t1・IP1/IQ+tx2) ……(7) となり、t1、θ1、IP1、IQは一定値なので、tx2によ
つて変化する進角度となる。
Similarly, when θb is calculated for Nx 2 , θb=θ 1 −6Nx 2 (t 1・I P1 /I Q +tx 2 ) ...(7), and t 1 , θ 1 , I P1 , I Since Q is a constant value, it becomes an advance angle that changes depending on tx 2 .

さて、以上の様に、機関回転数N2−N3期間の
進角度は、理論上一定値θaとなるが、実際に点
火位置を測定すると第3図ハの様な特性になつて
いる。これは、電子式点火時期制御装置の回路構
成が第1図の様になつている為、入力回路からパ
ワートランジスタ間の電気的遅れが原因であると
考えられる。
Now, as described above, the advance angle during the period of engine speed N2 - N3 is theoretically a constant value θa, but when the ignition position is actually measured, it has the characteristics as shown in FIG. 3C. This is thought to be caused by an electrical delay between the input circuit and the power transistor, since the circuit configuration of the electronic ignition timing control device is as shown in FIG.

進角特性がハの様になると、機関回転の高速領
域において機関の出力低下、排気ガスの汚染等が
考えられ好ましくない。
If the advance angle characteristic becomes as shown in (c), it is undesirable because it may cause a decrease in engine output in the high-speed region of engine rotation, contamination of exhaust gas, etc.

〔発明の目的〕[Purpose of the invention]

本発明の目的は、第3図ハの様な進角特性を是
正し、機関の種類に応じて、第3図ロ,イの様な
進角特性を得ることにある。
An object of the present invention is to correct the advance angle characteristics shown in FIG. 3C and to obtain advance angle characteristics shown in FIGS. 3B and 3D depending on the type of engine.

〔発明の要点〕[Key points of the invention]

本発明はコンデンサの充電電荷量と放電電荷量
が等しくなることをもつて点火タイミングを演算
する回路を設け、前記放電電荷量がゼロになるよ
りある一定時間だけ早く点火信号を出すようにす
ることを特徴とする。
The present invention provides a circuit that calculates the ignition timing based on the fact that the amount of charged charge and the amount of discharged charge of the capacitor become equal, and outputs the ignition signal a certain period of time earlier than the amount of discharged charge becomes zero. It is characterized by

〔発明の実施例〕[Embodiments of the invention]

以下図面を用いて本発明の一実施例を説明す
る。
An embodiment of the present invention will be described below with reference to the drawings.

第4図に本発明の一実施例を示す。第4図にお
いて、充放電用コンデンサ9の端子○ニはトランジ
スタ10、定電流源11に接続され、もう片方の
端子○ホは、トランジスタ12、定電流源13に接
続され、定電流源11,13にはそれぞれスイツ
チS1,S2及びトランジスタ12がそれぞれのタイ
ミングでON、OFFすることにより、コンデンサ
9を定電流で充放電するようになつている。
FIG. 4 shows an embodiment of the present invention. In FIG. 4, terminal ○D of the charging/discharging capacitor 9 is connected to a transistor 10 and a constant current source 11, and the other terminal ○H is connected to a transistor 12 and a constant current source 13, and the constant current source 11, 13, switches S 1 and S 2 and a transistor 12 are turned on and off at respective timings to charge and discharge the capacitor 9 with a constant current.

トランジスタ10には電源Vccから抵抗14が
接続され、抵抗14とトランジスタ10の接点へ
にはもう一つの抵抗15を通してトランジスタ1
6が接続され、トランジスタ16がON、OFFす
ることにより、接点への電位が抵抗14と抵抗1
5の比だけ変動するようになつている。
A resistor 14 is connected to the transistor 10 from the power supply Vcc, and another resistor 15 is connected to the contact point between the resistor 14 and the transistor 10 to connect the transistor 1 to the transistor 10.
6 is connected, and the transistor 16 turns on and off, so that the potential to the contact point changes between the resistor 14 and the resistor 1.
It is designed to fluctuate by a ratio of 5.

またトランジスタ10のコレクタには放電終了
検知回路17が接続され、トランジスタ10のコ
レクタ電流の有無を検知するようになつている。
Further, a discharge end detection circuit 17 is connected to the collector of the transistor 10, and is configured to detect the presence or absence of a collector current of the transistor 10.

放電終了検知回路17の出力はフリツプフロツ
プ回路18に入力され、フリツプフロツプ回路1
8の出力は論理回路19に入力され、論理回路1
9は進角進号を出力する。
The output of the discharge end detection circuit 17 is input to the flip-flop circuit 18,
The output of 8 is input to logic circuit 19, and logic circuit 1
9 outputs the advance angle advance sign.

一方、フリツプフロツプ回路18の出力はトラ
ンジスタ16にも接続され、トランジスタを
ON、OFFさせる。
On the other hand, the output of the flip-flop circuit 18 is also connected to the transistor 16, and the transistor
Turn it on and off.

放電終了検知回路17の出力はNOR回路20
にも入力され、またNOR回路20のもう片方の
端子にはフリツプフロツプ回路18の出力が遅延
回路21を通して入力される。
The output of the discharge end detection circuit 17 is the NOR circuit 20
Also, the output of the flip-flop circuit 18 is inputted to the other terminal of the NOR circuit 20 through a delay circuit 21.

NOR回路20の出力は論理回路22に入力さ
れ、論理回路22の出力はスイツチS1,S2及びト
ランジスタ12をそれぞれのタイミングに応じて
ON、OFFさせる。
The output of the NOR circuit 20 is input to the logic circuit 22, and the output of the logic circuit 22 controls the switches S 1 and S 2 and the transistor 12 according to their respective timings.
Turn it on and off.

フリツプフロツプ回路18にはリセツト入力ト
が用意され、リセツト信号によつてリセツトされ
る。
The flip-flop circuit 18 is provided with a reset input and is reset by a reset signal.

また定電流源13はタイマー23の信号によ
り、定電流量を変化させるようになつている。
Further, the constant current source 13 is adapted to change the amount of constant current according to a signal from a timer 23.

以下、第4図の一実施例の動作を、第5図の動
作波形図を基に説明する。なお、第5図は、第3
図のN2−N3期間の動作波形図である。
The operation of the embodiment shown in FIG. 4 will be explained below based on the operation waveform diagram shown in FIG. 5. Furthermore, Figure 5 shows the third
FIG. 3 is an operation waveform diagram during the N 2 -N 3 period in the figure.

機関の回転に同期して発生する一定角度信号で
ある第5図Fに示す信号を基準タイミング信号と
し、θ2の期間コンデンサ9を充電経路IPで充電す
る。
The signal shown in FIG. 5F, which is a constant angle signal generated in synchronization with the rotation of the engine, is used as a reference timing signal, and the capacitor 9 is charged on the charging path IP for a period of θ 2 .

充電経路IP:電源Vcc→抵抗14→トランジスタ
10→コンデンサ9→定電流源13→スイツチ
S2→アース この時トランジスタ16はON、トランジスタ
12はOFF、スイツチS2はON、スイツチS1
OFFになつている。またコンデンサ9と定電流
源13の接点ホの波形は、第5図Hの様になる。
Charging path I P : Power supply Vcc → Resistor 14 → Transistor 10 → Capacitor 9 → Constant current source 13 → Switch
S 2 → Ground At this time, transistor 16 is ON, transistor 12 is OFF, switch S 2 is ON, and switch S 1 is
It's turned off. Further, the waveform at the contact point E between the capacitor 9 and the constant current source 13 is as shown in FIG. 5H.

次にθ1の期間になると、リセツト信号第5図G
がフリツプフロツプ回路のリセツト入力トに入力
され、このためフリツプフロツプはリセツトさ
れ、トランジスタ16をOFFさせる。一方論理
回路22はスイツチS1とトランジスタ12を
ON、スイツチS2をOFFさせ、コンデンサ9を放
電状態とする。
Next, in the period θ 1 , the reset signal (Fig. 5G) is activated.
is input to the reset input of the flip-flop circuit, thereby resetting the flip-flop and turning off transistor 16. On the other hand, the logic circuit 22 connects the switch S1 and the transistor 12.
ON, switch S2 is turned OFF, and the capacitor 9 is discharged.

放電経路IQ:電源Vcc→トランジスタ12→コン
デンサ9→定電流11→スイツチS1→アース この時コンデンサ9と定電流源11の接点○ニの
波形は第5図Jの様になる。J波形で示す様に接
点○ニの電位はリセツト信号と同時に押し上げられ
この為、トランジスタ10は自動的にOFF状態
になる。
Discharge path I Q : Power supply Vcc → Transistor 12 → Capacitor 9 → Constant current 11 → Switch S 1 → Earth At this time, the waveform at contact point ○2 between capacitor 9 and constant current source 11 is as shown in Figure 5 J. As shown by the J waveform, the potential of the contact ○2 is raised simultaneously with the reset signal, so that the transistor 10 is automatically turned off.

さて、放電が進み、接点○ニの電位が電源電圧
Vccよりも約VBEだけ小さくなつた時、トランジ
スタ10には微少のベース電流が流れ、このため
コレクタ電流Icが流れ、このIcを放電終了検知回
路17が検知し、フリツプフロツプ回路18を動
作させる。フリツプフロツプ回路18の出力はま
ず論理回路19を動作させて進角信号第5図Kを
出させると共に、トランジスタ16をONさせ
る。トランジスタ16がONになると、トランジ
スタ10のエミツタ側接続点○ヘの電位が抵抗14
と抵抗15の比だけ低くなり、トランジスタ10
は再びOFF状態になる。トランジスタ10が
OFFになるとコレクタ電流Icは流れなくなる。し
かし、トランジスタ16はフリツプフロツプ出力
により、ON状態を維持する。
Now, the discharge progresses and the potential of contact ○2 becomes the power supply voltage.
When the voltage becomes smaller than VCC by about VBE , a small base current flows through the transistor 10, and therefore a collector current Ic flows.The discharge end detection circuit 17 detects this Ic and operates the flip-flop circuit 18. The output of the flip-flop circuit 18 first operates the logic circuit 19 to output the advance angle signal K in FIG. 5, and turns on the transistor 16. When the transistor 16 turns on, the potential at the emitter side connection point ○ of the transistor 10 changes to the resistor 14.
becomes lower by the ratio of resistor 15 and transistor 10
becomes OFF again. The transistor 10
When turned OFF, collector current Ic stops flowing. However, transistor 16 maintains the ON state due to the flip-flop output.

なお、前記の様にトランジスタ10のコレクタ
電流Icが流れた時、放電終了検知回路が動作し
て、フリツプフロツプ回路18を動作させると同
時に、放電終了検知回路の出力はNOR回路20
にも入力される。ところが、フリツプフロツプ回
路の出力が遅延回路21で遅延されている間に、
前記の様にトランジスタ10がOFFになつてし
まうため、NOR回路20はこの段階では動作し
ない。
Note that when the collector current Ic of the transistor 10 flows as described above, the discharge end detection circuit operates and operates the flip-flop circuit 18, and at the same time, the output of the discharge end detection circuit is output to the NOR circuit 20.
is also entered. However, while the output of the flip-flop circuit is delayed by the delay circuit 21,
Since the transistor 10 is turned off as described above, the NOR circuit 20 does not operate at this stage.

コンデンサ9は引き続き放電され、接点○ニの電
位が接点○ヘの電位よりもVBEだけ低くなつた時、
すなわち第5図Jの波形でtbだけ時間が経過する
と、トランジスタ10には再びベース電流が流
れ、コレクタ電流Icが流れ、このIc電流を放電終
了検知回路17が再び検知し、NOR回路20に
入力する。この時NOR回路20のもう片方の入
力にはすでにフリツプフロツプ回路の出力が到達
しており、NOR回路は直ちに動作して論理回路
22を動作させ、論理回路22はトランジスタ1
2をOFFさせる。こうして放電状態が終了する。
但しスイツチS1とS2についてはθ1の期間中はスイ
ツチS1がON、S2がOFFの状態を維持する。この
ため、トランジスタ10のベース電流は定電流源
11スイツチS1を通して流れ続ける。
Capacitor 9 continues to be discharged, and when the potential of contact ○2 becomes lower than the potential of contact ○ by V BE ,
In other words, when time tb has elapsed with the waveform shown in FIG. do. At this time, the output of the flip-flop circuit has already reached the other input of the NOR circuit 20, and the NOR circuit immediately operates to operate the logic circuit 22, which in turn operates the transistor 1.
Turn 2 off. In this way, the discharge state ends.
However, regarding the switches S1 and S2 , during the period θ1 , the switch S1 remains ON and the switch S2 remains OFF. Therefore, the base current of the transistor 10 continues to flow through the constant current source 11 switch S1 .

なお、第5図に示すように、進角信号Kの発生
時点からコンデンサ9の放電終了時点までの時間
tbは、トランジスタ16がOFFのときにトラン
ジスタ10が導通する接点○ニの電圧(電源電圧
Vccよりトランジスタ10のベース・エミツタ間
電圧VBEだけ低い電圧)とトランジスタ16が
ONのときにトランジスタ10が導通する接点○ニ
の電圧(電源電圧Vccを抵抗14と15により分
圧した電圧よりVBEだけ低い電圧)の差の電圧Va
によつて決定され、Vaが一定だとtbも一定にな
り、Vaは抵抗14と15の比によつて決定され
る。
Furthermore, as shown in FIG.
tb is the voltage at contact ○2 (power supply voltage) at which transistor 10 conducts when transistor 16 is OFF.
Vcc is lower than the base-emitter voltage of transistor 10 ( VBE ) and transistor 16 is
The voltage Va that is the difference between the voltage of the contact ○2 at which the transistor 10 conducts when it is ON (a voltage lower by V BE than the voltage obtained by dividing the power supply voltage Vcc by the resistors 14 and 15)
If Va is constant, tb is also constant, and Va is determined by the ratio of resistors 14 and 15.

さて、次にθ2の期間になると、論理回路19が
動作してスイツチS1をOFF、スイツチS2をONさ
せて再び充電状態になり、前記の動作が繰り返さ
れる。
Now, in the next period θ 2 , the logic circuit 19 operates to turn off the switch S 1 and turn on the switch S 2 to enter the charging state again, and the above-described operation is repeated.

なお、タイマー23はある設定された時間によ
つて定電流源13の定電流量を変化させることが
できる。第2図Cのt1の期間が第3図N2−N3
間、t1+t2の期間がN1−N2期間である。
Note that the timer 23 can change the constant current amount of the constant current source 13 according to a certain set time. The period t 1 in FIG. 2C is the period N 2 -N 3 in FIG. 3, and the period t 1 +t 2 is the period N 1 -N 2 in FIG.

以上の様にコンデンサ9が完全に放電仕切る時
間よりもtbだけ早く進角信号を出すようにする
と、第3図イの様な進角信号が得られる。
As described above, if the advance angle signal is outputted tb earlier than the time when the capacitor 9 is completely discharged, the advance angle signal as shown in FIG. 3A can be obtained.

第5図において、進角時間tcは tc=t〓1−tx3+tb ……(8) (8)式を進角度に変換すると(但し、機関回転数
はNx1)進角度θcは となる。
In Fig. 5, the advance angle time tc is tc=t〓 1 −tx 3 +tb ……(8) When formula (8) is converted to the advance angle (however, the engine speed is Nx 1 ), the advance angle θc is becomes.

(9)式において、θ1は機関回転数には無関係な一
定角度信号、IP0、IQ0は、定電流で一定値である。
又、tbはVaとIQ0を一定にすると、機関回転数と
は無関係に一定値になる。このため、Yの項は、
機関回転数とは無関係な一定角度、Xの項は、機
関回転数に応じて変動することになる。このた
め、進角度θcは、機関回転数によつて変化し、第
3図イの様な進角特性が得られる。又、イの右上
り角度αはtbを変化させることにより、自由に変
更が可能である。
In equation (9), θ 1 is a constant angle signal that is unrelated to the engine speed, and I P0 and I Q0 are constant currents and constant values.
Furthermore, if Va and I Q0 are kept constant, tb becomes a constant value regardless of the engine speed. Therefore, the term Y is
The term X, which is a constant angle unrelated to the engine speed, will vary depending on the engine speed. Therefore, the advance angle θc changes depending on the engine speed, and the advance angle characteristic shown in FIG. 3A is obtained. Further, the upward right angle α of A can be freely changed by changing tb.

この様に理論進角度特性をイの様にし、又その
右上がり角度αを自由に変更できる様にしたた
め、機関の種類、内部電気回路の遅れ等を考慮し
て、最適の進角特性に設定可能となつた。
In this way, the theoretical advance angle characteristic is set as shown in A, and the rising angle α can be changed freely, so the optimum advance angle characteristic is set by taking into account the type of engine, internal electrical circuit delay, etc. It became possible.

〔発明の効果〕〔Effect of the invention〕

以上説明したように、本発明によれば、実質
上、1個のコンデンサ9の充電電荷量と放電電荷
量が等しくなることをもつて、点火タイミングを
演算する回路を備え、前記点火タイミングを放電
電荷量がゼロになるより、ある設定された一定時
間tbだけ早く点火信号を出すようにしたので、機
関の高速回転領域、すなわち第3図N2−N3の領
域の進角特性がハの様に右下がりとなることな
く、機関の出力低下、排ガスの汚染等が防止でき
る。
As explained above, according to the present invention, a circuit is provided which calculates the ignition timing based on the fact that the amount of charged charge and the amount of discharged charge of one capacitor 9 become equal, and the ignition timing is set to be equal to the amount of discharged charge. Since the ignition signal is issued a certain fixed time tb earlier than the amount of electric charge becomes zero, the advance angle characteristic in the high speed rotation region of the engine, that is, the region N 2 - N 3 in Figure 3, is This prevents the engine from sloping downward and prevents engine output from decreasing and exhaust gas from being contaminated.

また本発明の特に有利な実施態様によれば、前
記一定時間tbを設定するのに抵抗14,15の分
割比を用い、又、前記コンデンサ9の充電電荷量
と放電電荷量が最終的に同じになる様にするため
に遅延回路21を用いたので、コンデンサ9によ
る進角演算特性を損うことなく機関の種類に応じ
て、自由に進角特性が設定できる効果がある。
According to a particularly advantageous embodiment of the present invention, a dividing ratio of resistors 14 and 15 is used to set the predetermined time tb, and the amount of charged charge and the amount of discharged charge of the capacitor 9 are ultimately the same. Since the delay circuit 21 is used in order to achieve this, there is an effect that the advance angle characteristic can be freely set according to the type of engine without impairing the advance angle calculation characteristic by the capacitor 9.

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

第1図は電子回路で点火時期を決定する一般的
な電子進角点火装置の回路構成図、第2図は従来
の進角原理動作波形図、第3図は進角特性例の特
性図、第4図は本発明の一実施例の回路図、第5
図は第4図の実施例の動作を説明するための動作
波形図である。 1……ロータ、2……電磁ピツクアツプコイ
ル、3……入力回路、4……進角演算回路、5…
…閉角制御回路、6……増幅回路、7……パワー
トランジスタ、8……点火コイル、9……コンデ
ンサ、10,12,16,24……トランジス
タ、11,13……定電流源、14,15……抵
抗、17……放電終了検知回路、18……フリツ
プフロツプ回路、19,22……論理回路、20
……NOR回路、21……遅延回路、23……タ
イマー回路。
Figure 1 is a circuit configuration diagram of a general electronic advance ignition device that determines ignition timing using an electronic circuit, Figure 2 is a waveform diagram of the conventional advance principle operation, and Figure 3 is a characteristic diagram of an example of advance angle characteristics. FIG. 4 is a circuit diagram of an embodiment of the present invention, and FIG.
The figure is an operational waveform diagram for explaining the operation of the embodiment of FIG. 4. DESCRIPTION OF SYMBOLS 1... Rotor, 2... Electromagnetic pick-up coil, 3... Input circuit, 4... Advance angle calculation circuit, 5...
... Closed angle control circuit, 6 ... Amplification circuit, 7 ... Power transistor, 8 ... Ignition coil, 9 ... Capacitor, 10, 12, 16, 24 ... Transistor, 11, 13 ... Constant current source, 14 , 15...Resistor, 17...Discharge end detection circuit, 18...Flip-flop circuit, 19, 22...Logic circuit, 20
...NOR circuit, 21 ... delay circuit, 23 ... timer circuit.

Claims (1)

【特許請求の範囲】[Claims] 1 機関の回転に同期して各周期の前半の一定角
度の間第1値となり、後半は第2値となる一定角
度信号を発生する一定角度信号発生手段と、充放
電用コンデンサ9と、該コンデンサの一端と基準
電位点との間に接続された第1の定電流源13
と、前記コンデンサの他端と基準電位点との間に
接続された第2の定電流源11と、前記コンデン
サの一端と電源電位点との間に接続された第1の
トランジスタ12と、前記コンデンサの他端にベ
ースが接続され、エミツタが第1の抵抗14を介
して電源電位点と接続された第2のトランジスタ
10と、該第2のトランジスタのエミツタと第1
の抵抗との接続点と基準電位点との間に第2の抵
抗15を介して接続された第3のトランジスタ1
6と、該第3のトランジスタのコレクタ電流の有
無を検知する放電終了検知回路17と、前記一定
角度信号の第2値の開始時点でリセツトされると
共に、前記放電終了検知回路の電流有り検知によ
りセツトされ、セツト出力により前記第3のトラ
ンジスタを導通させるフリツプフロツプ回路18
と、該フリツプフロツプ回路のセツト出力を所定
時間遅延する遅延回路21と、該遅延回路の出力
と前記フリツプフロツプ回路のセツト出力とが共
に発生したことを検出して出力するゲート回路2
0と、前記一定角度信号の第1値および第2値に
よりそれぞれ前記第1の定電流源および第2の定
電流源を動作させると共に、一定角度信号の第2
値の開始から前記ゲート回路の出力発生まで前記
第1のトランジスタを導通させる充放電制御手段
22と、前記フリツプフロツプ回路のセツト出力
に応答して進角信号を発生する進角信号発生手段
19とを備えることを特徴とする内燃機関用電子
式進角点火装置。
1. A constant angle signal generating means that generates a constant angle signal that takes a first value during a constant angle in the first half of each cycle and takes a second value in the second half in synchronization with the rotation of the engine; a charging/discharging capacitor 9; A first constant current source 13 connected between one end of the capacitor and a reference potential point
a second constant current source 11 connected between the other end of the capacitor and a reference potential point; a first transistor 12 connected between one end of the capacitor and a power supply potential point; A second transistor 10 whose base is connected to the other end of the capacitor and whose emitter is connected to the power supply potential point via the first resistor 14;
a third transistor 1 connected via a second resistor 15 between the connection point with the resistor and the reference potential point;
6, a discharge end detection circuit 17 that detects the presence or absence of the collector current of the third transistor, and is reset at the start of the second value of the constant angle signal, and is reset by the discharge end detection circuit detecting the presence of current. flip-flop circuit 18 which is set and makes the third transistor conductive by the set output.
, a delay circuit 21 that delays the set output of the flip-flop circuit for a predetermined period of time, and a gate circuit 2 that detects and outputs the occurrence of both the output of the delay circuit and the set output of the flip-flop circuit.
0, the first constant current source and the second constant current source are operated by the first value and the second value of the constant angle signal, respectively, and the second value of the constant angle signal is operated.
charge/discharge control means 22 that conducts the first transistor from the start of the value until generation of the output of the gate circuit; and lead angle signal generation means 19 that generates the lead angle signal in response to the set output of the flip-flop circuit. An electronic advance ignition device for an internal combustion engine, comprising: an electronic advance ignition device for an internal combustion engine.
JP22392683A 1983-11-28 1983-11-28 Electronic ignition timing controlling apparatus for internal-combustion engine Granted JPS60116866A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP22392683A JPS60116866A (en) 1983-11-28 1983-11-28 Electronic ignition timing controlling apparatus for internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP22392683A JPS60116866A (en) 1983-11-28 1983-11-28 Electronic ignition timing controlling apparatus for internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS60116866A JPS60116866A (en) 1985-06-24
JPS6347906B2 true JPS6347906B2 (en) 1988-09-26

Family

ID=16805871

Family Applications (1)

Application Number Title Priority Date Filing Date
JP22392683A Granted JPS60116866A (en) 1983-11-28 1983-11-28 Electronic ignition timing controlling apparatus for internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS60116866A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6371577A (en) * 1986-09-12 1988-03-31 Kokusan Denki Co Ltd Signal generating circuit for igniter of internal combustion engine
JPS63131868A (en) * 1986-11-21 1988-06-03 Kokusan Denki Co Ltd Ignitor for internal combustion engine

Also Published As

Publication number Publication date
JPS60116866A (en) 1985-06-24

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