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JPS635596B2 - - Google Patents
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JPS635596B2 - - Google Patents

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Publication number
JPS635596B2
JPS635596B2 JP58159930A JP15993083A JPS635596B2 JP S635596 B2 JPS635596 B2 JP S635596B2 JP 58159930 A JP58159930 A JP 58159930A JP 15993083 A JP15993083 A JP 15993083A JP S635596 B2 JPS635596 B2 JP S635596B2
Authority
JP
Japan
Prior art keywords
capacitor
circuit
voltage
ignition
triangular wave
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
JP58159930A
Other languages
Japanese (ja)
Other versions
JPS6053668A (en
Inventor
Eiji Kondo
Seiji Niizeki
Kunio Matsuzaki
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.)
Shindengen Electric Manufacturing Co Ltd
Original Assignee
Shindengen Electric Manufacturing 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 Shindengen Electric Manufacturing Co Ltd filed Critical Shindengen Electric Manufacturing Co Ltd
Priority to JP58159930A priority Critical patent/JPS6053668A/en
Publication of JPS6053668A publication Critical patent/JPS6053668A/en
Publication of JPS635596B2 publication Critical patent/JPS635596B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P5/00Advancing or retarding ignition; Control therefor
    • F02P5/04Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
    • F02P5/145Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using electrical means
    • F02P5/155Analogue data processing
    • F02P5/1553Analogue data processing by determination of elapsed angle with reference to a particular point on the motor axle, dependent on specific conditions
    • F02P5/1556Analogue data processing by determination of elapsed angle with reference to a particular point on the motor axle, dependent on specific conditions using a stepped control, dependent on speed
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Signal Processing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Ignition Timing (AREA)

Description

【発明の詳細な説明】 本発明はコンデンサ充放電式点火装置に関する
もので、特にエンジンの出力特性に適合する如く
点火時期(角度)をエンジン回転数が所要設定数
以下ではほぼ一定の進角角度の点火特性を得、又
該設定数を越えた回転数の時は上記角度より進角
したほぼ一定の点火角度特性を得ることの可能な
安価経済的な点火装置を提供するものである。以
下図面を用いて、本発明を詳細に説明する。第1
図、第2図、第3図及び第4図は夫々本発明の一
実施例回路図、その各部動作波形図、動作説明図
及び点火特性図で、図においてEXTはエンジン
により回転する磁石式発電機等の発電コイル、D
6は整流用ダイオード、Cは前記発電コイル
EXTの発生電圧により前記ダイオードD6を介
して充電される点火電源用コンデンサ、SCRは
後述するトリガ信号で導通するサイリスタで、こ
れにより前記コンデンサCの充電々荷を点火コイ
ルgcに放電せしめ、その2次巻線n2を介し
て点火栓SPに火花を発生する。以上で主回路
を構成する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a capacitor charging/discharging type ignition device, and in particular, the ignition timing (angle) is adjusted to a nearly constant advance angle when the engine speed is below a predetermined number so as to match the output characteristics of the engine. To provide an inexpensive and economical ignition device capable of obtaining an ignition characteristic of 1, and a substantially constant ignition angle characteristic advanced from the above angle when the rotation speed exceeds the set value. The present invention will be explained in detail below using the drawings. 1st
2, 3, and 4 are a circuit diagram of an embodiment of the present invention, an operation waveform diagram of each part, an operation explanatory diagram, and an ignition characteristic diagram, respectively. In the figure, EXT is a magnet type power generator rotated by the engine. generator coils for machines, etc., D
6 is a rectifier diode, and C is the generator coil.
The ignition power supply capacitor SCR, which is charged via the diode D6 by the voltage generated by EXT, is a thyristor that becomes conductive in response to a trigger signal, which will be described later.This discharges the charge of the capacitor C to the ignition coil gc, A spark is generated at the spark plug SP via the next winding n2. The main circuit is configured above.

次にPCはエンジン回転サイクル毎に予め設定
された最大及び最少点火角度の第1、第2タイミ
ングパルス(以下第1TP、第2TP)を発生する点
火信号発生コイル(以下パルサコイル)、は前
記第2TPと同期して所定の傾斜角で立上り次サイ
クル時の第2TPと同期して立下る三角波を発生す
る三角波発生回路、は第1TPと同期して所定の
傾斜角で立上り後該尖頭値を一定値に制限し、第
2TPと同期して立下る台形波を発生する台形波発
生回路、は前記三角波(電圧)及び台形波を比
較し、台形波の尖頭値が三角波の尖頭値を越した
時出力する比較器、は前記比較器の出力によ
りサイリスタSCRのゲートをトリガするゲート
回路である。以下回路乃至について詳述す
る。
Next, the PC is an ignition signal generating coil (hereinafter referred to as a pulsar coil) that generates first and second timing pulses (hereinafter referred to as 1st TP, 2nd TP) with preset maximum and minimum ignition angles for each engine rotation cycle, and the 2nd TP The triangular wave generation circuit generates a triangular wave that rises at a predetermined slope angle in synchronization with the 1st TP and falls in synchronization with the 2nd TP in the next cycle. value, and
The trapezoidal wave generation circuit that generates a falling trapezoidal wave in synchronization with 2TP is a comparator that compares the triangular wave (voltage) and the trapezoidal wave and outputs when the peak value of the trapezoidal wave exceeds the peak value of the triangular wave. , is a gate circuit that triggers the gate of the thyristor SCR by the output of the comparator. The circuit will be explained in detail below.

先ずDZはパルサコイルPCの信号電圧(第
1TP)を制限(クランプ)する定電圧素子、D
3,C3はパルサコイルPCの両端間に接続され
たダイオード及びコンデンサで、該コンデンサC
3は上記第1TPにより前記クランプ電圧まで充電
される。C4は前記コンデンサC3の充電々圧を
電源として抵抗R4との時定数で充電されて所定
の傾斜角で立上る。
First, DZ is the pulser coil PC signal voltage (first
Constant voltage element that limits (clamps) 1TP), D
3, C3 is a diode and a capacitor connected between both ends of the pulsar coil PC, and the capacitor C
3 is charged to the clamp voltage by the first TP. C4 is charged with the time constant of resistor R4 using the charging voltage of capacitor C3 as a power source, and rises at a predetermined inclination angle.

Q5は前記コンデンサC4の両端間に抵抗R1
0R12を介して接続されるトランジスタで該ト
ランジスタQ5は信号電圧(第2TP)により導通
して該コンデンサC4の放電回路を形成し、これ
によりコンデンサC4は前記第2TPと同期して立
下る。なお、C5,R11は第1TP、第2TPのノ
イズ吸収用コンデンサ及び抵抗、D5,D7は整
流用ダイオードで、以上で回路を形成する。次
にC1は第1TPによりダイオードD4を介して充
電されるコンデンサ、C2は抵抗R3を介してコ
ンデンサC1に接続されたコンデンサで該コンデ
ンサC1を電源として抵抗R3との時定数で充電
されて所定の傾斜角で立上る。ZD2は前記コン
デンサC2の両端に接続された定電圧ダイオード
でこれにより該コンデンサの電圧(尖頭値)を一
定値に制限する。以上で回路を形成する。Q2
は比較回路を形成するトランジスタで、エミツ
タを前記回路の台形波出力端(点)に、ベー
スを前記回路の三角波出力端(点)に夫々接
続され、又コレクタを比較出力端として抵抗R5
を介してゲート回路に接続される。次にQ3,
Q4は増巾用トランジスタで、該トランジスタQ
3は前記比較回路の出力により導通し、これに
より該トランジスタQ4を導通せしめる。そして
該トランジスタQ4の導通によりサイリスタ
SCRは主にコンデンサC1よりトリガ電流を供
給されて導通する。
Q5 is a resistor R1 across the capacitor C4.
The transistor Q5, which is a transistor connected through 0R12, is turned on by the signal voltage (second TP) to form a discharge circuit for the capacitor C4, so that the capacitor C4 falls in synchronization with the second TP. Note that C5 and R11 are noise absorbing capacitors and resistors of the first TP and second TP, D5 and D7 are rectifying diodes, and the above form a circuit. Next, C1 is a capacitor charged by the first TP via a diode D4, and C2 is a capacitor connected to the capacitor C1 via a resistor R3. Using the capacitor C1 as a power source, the capacitor is charged with a time constant with a resistor R3 to a predetermined level. Stands up at an angle of inclination. ZD2 is a constant voltage diode connected across the capacitor C2, which limits the voltage (peak value) of the capacitor to a constant value. With the above steps, a circuit is formed. Q2
is a transistor forming a comparison circuit, whose emitter is connected to the trapezoidal wave output terminal (point) of the circuit, and whose base is connected to the triangular wave output terminal (point) of the circuit, and whose collector is connected to the comparison output terminal and resistor R5.
connected to the gate circuit via. Next, Q3,
Q4 is a transistor for amplification, and the transistor Q
3 is made conductive by the output of the comparison circuit, thereby making the transistor Q4 conductive. Then, due to the conduction of the transistor Q4, the thyristor
The SCR is mainly supplied with a trigger current from the capacitor C1 and becomes conductive.

次に、本発明装置の回路動作について第2図、
第3図を参照して説明する。
Next, FIG. 2 shows the circuit operation of the device of the present invention.
This will be explained with reference to FIG.

先ず第4図において横軸はエンジン回転数N、
縦軸は点火角度(Θ)を示す。N0〜N1の間を設
定数以下の回転数、N1以上を設定数以上の回転
数とする。発電コイルEXTの極性が第1図に示
す如く上側がの時コンデンサCはダイオードD
6を介して図示の極性に充電される。そして前記
コイルEXTの極性が前記と反対の時は該コンデ
ンサCはダイオードD6に阻止されて充電され
ず、又前半サイクル時の充電々荷は放電回路が形
成されず、図示の充電状態を維持する。一方パル
サコイルPCの信号(第1TP、第2TP)は該発電
コイルEXTの上側がの時に後述するゲート回
路を介してサイリスタSCRのゲートに給電さ
れ、該SCRをオンせしめるため、この間該コン
デンサCの充電々荷はサイリスタSCRを介して
点火コイルgcに放電され、所要点火時期(角
度)において点火栓SPに火花を生じせしめる。
第2図Aは信号電圧波形では図示しないエンジ
ンの上止点から最大(角度)進角した位置におけ
る正の信触電圧(第1TP)、は最少進角した位
置における負の信号電圧(第2TP)を示し、該第
1TP及び第2TPの信号はエンジン(フライホイ
ル)が1回転に夫々1度発生する。なお、′及
び′は次サイクル時の第1TP及び第2TPを示す。
そこで第2図Aの第1TPが発生すると該信号電
圧はダイオードD5を介して整流され、又定電圧
素子DZ1により定電圧化されて回路及びに
印加される。即ち先ずコンデンサC3はダイオー
ドD3を通して該定電圧VZまで充電される。(第
2図B) 次に回路のコンデンサC4は前記コンデンサ
C3を電源として抵抗R4との時定数で充電され
て所定傾斜角で立上り又第2TPの到来によりトラ
ンジスタQ5を介し放電回路が形成されるため、
該第2TPと同期して立下る三角波を形成する。
(第2図E)又、回路のコンデンサC1は該第
1TPと同期してダイオードD4を通して該定電圧
まで充電され、後述するサイリスタSCRのトリ
ガにより放電回路が形成される。(第2図C)一
方コンデンサC2は該コンデンサC1を電源とし
て(即ち第1TPと同期して)抵抗R3との時定数
で充電されるため所要傾斜角で立上り、その尖頭
値が定電圧ダイオードDZ2の電圧VZ2に達する
とこの電圧に制限され後述する比較回路のトラ
ンジスタQ2の導通により放電回路が形成されて
立下る台形波を形成する。(第2図D)次に比較
回路及びゲート回路の動作を第3図を参照し
て説明する。第3図において三角波0及び台
形波はエンジン回転数N1の時の夫々コ
ンデンサC4及びC2の電圧波形を拡大して示し
たものであり、又ΘMは最大進角角度(第1TP)、
Θmは最少進角角度(第2TP)θ0は設定進角角度
を示す。比較回路のトランジスタQ2はベース
が第1図に示す点に、又エミツタが点に夫々
接続され、点の電位が点の電位より高位の時
順バイアスされて導通する。そこでエンジンの設
定回転数(N1)を例えば4000rpmとした時、第
2TPと次サイクル時の第2TP′の間の周期を
T2又次サイクル時の第1TP′と第2TP′の周
期をT1とし、該周期T2における三角波(コン
デンサC4)の出力電圧を第3図e0とし又その
尖頭値がとなる如く抵抗R4との時定数を設
定すると該三角波はエンジン回転数が上記設定数
(N1)以下の時(低速時)は第2TPの到来が遅
れ、該コンデンサC4のトランジスタQ5を介す
放電時期が遅れこの間該コンデンサC4は充電さ
れるためその出力電圧は第3図e2,e1の如く
高位にある。一方、設定回転時周期T1における
台形波(コンデンサC2)の電圧は該期間T1の
所要時期で定電圧ダイオードの電圧VZ2に達し
(第3図)この電圧を保持する如く、該電圧VZ
2及び抵抗R3との時定数が設定されると該三角
波0と台形波の交点付近でトラン
ジスタQ2は導通し、ゲート回路Vのトランジス
タQ3及びQ4をオンにする。このためコンデン
サC1→トランジスタQ4→サイリスタSCRの
経路に該コンデンサの放電によるトリガ電流が流
れサイリスタSCRを導通せしめる。即ち台形波
は予めパルサコイルPCにより設定され
た最大及び最少進角角度の第1TP(ΘM)及び第
2TP(Θm)間で形成されているため上記交点
即ち角度(Θ0)でコンデンサCは放電して火花
を生じせしめる。(第4図イ)次に回転数が設定
数(N1)に達しない場合は前述の如く三角波の
出力e1,e2は該周期T1において台形波より
高位である。このため該三角波(コンデンサC
4)の出力電圧e1e2は第2TPの到来によりト
ランジスタQ5が導通し、放電回路が形成され、
その電位低下する時点で台形波より低位となる。
即ち第1図点電位が点電位より低下しトラン
ジスタQ2は導通する。つまり最少進角の第2TP
と同期して点火信号が発生するため、第4図ロに
示す角度Θmで点火する特性を得ることができ
る。一方回転数が設定数(N1)以上の時は第3
図に示す如く周期T2はT2′に又T1はT1′に
夫々変化する。なお、周期T1における台形波は
周期T1′では該周期終端で設定電圧VZ2に達す
るため三角波′′′としとらえることができ
る。このため両者の関係は周期T1における見掛
上の三角波と比較で説明できる。即ち両者
の変化の比即ち(T1/T2)及び(T1′/T
2′)は一定である。従つて三角波0′′と三
角波′′′の交点′は第1TP及び第2TP間で
上記交点と同一比の位置にある。つまり回転数
の変化に係わらず進角角度は同一となる。(第4
図イ)このように本発明によれば台形波電圧即ち
定電圧ダイオードDZ2の電圧設定により、三角
波電圧が該設定電圧VZ2より常に高い時には
(低速回転時)は第2TPの到来と同期した最少進
角角度(Θm)の一定進角特性を得て、又該設定
電圧に達する設定回転数以上になると前記角度よ
り進角した一定角度の進角特性所謂2段(階段
状)進角特性を得ることができる。なお、このス
テツプ巾つまり最少進角(Θm)からの進角巾は
該設定電圧を第3図中VZ2′,Vz2″の如く低下
せしめることにより第4図ハの如く大きく最大進
角位置(ΘM)に近接せしめることが可能であ
る。以上の説明から明らかなように本発明によれ
ばエンジン回転数が設定数以下の時は一定の最少
進角点火特性を得、又設定数以上の時はこれより
進角した一定の進角点火特性が構成簡単、安価に
得られるので実用上の効果は極めて大きい。
First, in Fig. 4, the horizontal axis is the engine rotation speed N,
The vertical axis shows the ignition angle (Θ). The number of revolutions between N0 and N1 is below the set number, and the number of revolutions above N1 is above the set number. When the polarity of the generator coil EXT is on the upper side as shown in Figure 1, the capacitor C becomes the diode D.
6 to the polarity shown. When the polarity of the coil EXT is opposite to that described above, the capacitor C is blocked by the diode D6 and is not charged, and a discharge circuit is not formed for the charge during the first half cycle, and the charging state shown in the figure is maintained. . On the other hand, the signals of the pulsar coil PC (1st TP, 2nd TP) are supplied to the gate of the thyristor SCR via the gate circuit described later when the upper side of the generating coil EXT is on, and in order to turn on the SCR, the capacitor C is charged during this time. The charge is discharged to the ignition coil GC via the thyristor SCR, causing a spark to be generated at the ignition plug SP at a predetermined ignition timing (angle).
Figure 2A shows the signal voltage waveform, which shows the positive signal voltage (1st TP) at the maximum (angle) advanced position from the engine's top end point (not shown), and the negative signal voltage (2nd TP) at the minimum advanced position. ), and the corresponding number
The 1TP and 2nd TP signals are generated once per revolution of the engine (flywheel). Note that ' and ' indicate the first TP and second TP in the next cycle.
Therefore, when the first TP in FIG. 2A occurs, the signal voltage is rectified via the diode D5, and is made into a constant voltage by the constant voltage element DZ1 and applied to the circuit. That is, first, capacitor C3 is charged to the constant voltage VZ through diode D3. (Fig. 2B) Next, the capacitor C4 of the circuit is charged with the time constant of the resistor R4 using the capacitor C3 as a power source, and rises at a predetermined slope angle, and when the second TP arrives, a discharge circuit is formed via the transistor Q5. For,
A triangular wave falling in synchronization with the second TP is formed.
(Fig. 2 E) Also, the capacitor C1 of the circuit is
It is charged to the constant voltage through the diode D4 in synchronization with 1TP, and a discharge circuit is formed by the trigger of the thyristor SCR, which will be described later. (Fig. 2C) On the other hand, capacitor C2 is charged with the time constant of resistor R3 using capacitor C1 as a power source (that is, in synchronization with the first TP), so it rises at the required slope angle, and its peak value is the voltage regulator diode. When the voltage of DZ2 reaches VZ2, it is limited to this voltage, and a discharge circuit is formed by conduction of a transistor Q2 of a comparison circuit, which will be described later, to form a falling trapezoidal wave. (FIG. 2D) Next, the operation of the comparator circuit and the gate circuit will be explained with reference to FIG. 3. In Fig. 3, the triangular wave 0 and the trapezoidal wave are enlarged views of the voltage waveforms of capacitors C4 and C2, respectively, when the engine speed is N1, and ΘM is the maximum advance angle (1st TP),
Θm is the minimum advance angle (second TP) and θ0 is the set advance angle. The transistor Q2 of the comparator circuit has its base connected to the point shown in FIG. 1, and its emitter connected to the point shown in FIG. 1, and is made conductive by being biased over time so that the potential at the point is higher than the potential at the point. Therefore, when the set engine speed (N1) is set to 4000 rpm, for example,
The period between 2TP and 2TP' in the next cycle is T2, and the period between 1TP' and 2TP' in the next cycle is T1, and the output voltage of the triangular wave (capacitor C4) in this period T2 is shown in Figure 3 as e0. Then, if the time constant with the resistor R4 is set so that its peak value becomes The discharge timing through the transistor Q5 is delayed, and during this time the capacitor C4 is charged, so its output voltage is at a high level as shown in e2 and e1 in FIG. On the other hand, the voltage of the trapezoidal wave (capacitor C2) in the set rotation period T1 reaches the voltage VZ2 of the voltage regulator diode at the required time of the period T1 (Fig. 3).
When the time constant between the triangular wave 0 and the trapezoidal wave is set, the transistor Q2 becomes conductive near the intersection of the triangular wave 0 and the trapezoidal wave, turning on the transistors Q3 and Q4 of the gate circuit V. Therefore, a trigger current due to the discharge of the capacitor flows through the path of the capacitor C1→transistor Q4→thyristor SCR and makes the thyristor SCR conductive. In other words, the trapezoidal wave is generated by the 1st TP (ΘM) and the 1st TP (ΘM) of the maximum and minimum advance angles set in advance by the pulser coil PC.
Since it is formed between 2TP (Θm), the capacitor C discharges at the above-mentioned intersection point, that is, the angle (Θ0), and generates a spark. (FIG. 4A) Next, when the number of revolutions does not reach the set number (N1), the triangular wave outputs e1 and e2 are higher than the trapezoidal wave in the period T1, as described above. Therefore, the triangular wave (capacitor C
The output voltage e1e2 of 4) becomes conductive due to the arrival of the second TP, and a discharge circuit is formed.
At the point when the potential drops, it becomes lower than the trapezoidal wave.
That is, the potential at the point in FIG. 1 becomes lower than the potential at the point, and the transistor Q2 becomes conductive. In other words, the 2nd TP with the minimum advance angle
Since the ignition signal is generated in synchronization with the ignition signal, it is possible to obtain the characteristic of ignition at the angle Θm shown in FIG. 4B. On the other hand, when the rotation speed is higher than the set number (N1), the third
As shown in the figure, the period T2 changes to T2' and T1 changes to T1'. Note that the trapezoidal wave in the period T1 reaches the set voltage VZ2 at the end of the period in the period T1', so it can be regarded as a triangular wave ''''. Therefore, the relationship between the two can be explained by comparing the apparent triangular wave at period T1. That is, the ratio of both changes, ie (T1/T2) and (T1'/T
2′) is constant. Therefore, the intersection point between the triangular wave 0'' and the triangular wave ``'' is located at the same ratio as the above-mentioned intersection point between the first TP and the second TP. In other words, the advance angle remains the same regardless of the change in rotational speed. (4th
Figure A) According to the present invention, when the triangular wave voltage is always higher than the set voltage VZ2 (during low speed rotation), the trapezoidal wave voltage, that is, the voltage setting of the constant voltage diode DZ2, according to the present invention, the minimum advance is synchronized with the arrival of the second TP. Obtains a constant advance characteristic of the angular angle (Θm), and obtains a so-called two-stage (step-like) advance characteristic of a constant angle advanced from the above angle when the rotation speed reaches the set voltage or higher. be able to. This step width, that is, the advance angle width from the minimum advance angle (Θm) can be increased to the maximum advance angle position (ΘM) as shown in FIG. ).As is clear from the above explanation, according to the present invention, when the engine speed is below the set number, a certain minimum advance ignition characteristic is obtained, and when the engine speed is above the set number, a certain minimum advance ignition characteristic is obtained. Since a constant advance ignition characteristic that is more advanced than this can be obtained with a simple construction and at low cost, the practical effect is extremely large.

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

第1図、第2図は本発明の一実施例回路図及び
その各部動作波形図、第3図は本発明の動作説明
図、第4図は本発明の特性図である。図において
は主回路、は三角波発生回路、は台形波発
生回路、は比較回路、はゲート回路、C,C
1,C2,C3及びC4はコンデンサ、SCRは
サイリスタ、D1,D2,D3,D4,D5,D
6及びD7はダイオード、gtはイグニツシヨン
コイル、DZ1,DZ2は定電圧素子、Q2,Q
3,Q4及びQ5はトランジスタ、R3,R4は
抵抗、PCはパルス発生コイル(回路)である。
1 and 2 are circuit diagrams of an embodiment of the present invention and operation waveform diagrams of each part thereof, FIG. 3 is an explanatory diagram of the operation of the present invention, and FIG. 4 is a characteristic diagram of the present invention. In the figure, the main circuit, is a triangular wave generation circuit, is a trapezoidal wave generation circuit, is a comparison circuit, is a gate circuit, C, C
1, C2, C3 and C4 are capacitors, SCR is a thyristor, D1, D2, D3, D4, D5, D
6 and D7 are diodes, gt is an ignition coil, DZ1, DZ2 are constant voltage elements, Q2, Q
3, Q4 and Q5 are transistors, R3 and R4 are resistors, and PC is a pulse generating coil (circuit).

Claims (1)

【特許請求の範囲】 1 (イ) 発電コイルの電圧によりコンデンサを充
電し、該コンデンサの充電々荷をトリガ信号に
より導通するサイリスタを介して点火コイルに
放電せしめるようにした主回路、 (ロ) エンジン回転サイクル毎に予め設定された最
大及び最少点火角度の第1及び第2タイミング
パルスを発生するパルス発生回路、 (ハ) 前記第2タイミングパルスと同期して所定の
傾斜角で立上り、次サイクル時の第2タイミン
グパルスと同期して立下る三角波を発生する三
角波発生回路、 (ニ) 前記第1タイミングパルスと同期して所定の
傾斜角で立上りの後、尖頭値を一定に制限さ
れ、且つ第2タイミングパルスと同期して立下
る台形波を発生する台形波発生回路、 (ホ) 前記三角波及び台形波を比較し、前記台形波
の尖頭値が三角波の尖頭値を越えた時に出力す
る比較回路と (ヘ) 前記比較回路の出力により前記サイリスタを
トリガするゲート回路、 以上(イ)乃至(ヘ)を備えたコンデンサ充放電式点火装
置。
[Scope of Claims] 1. (a) A main circuit that charges a capacitor with the voltage of the generator coil and discharges the charge of the capacitor to the ignition coil via a thyristor that conducts in response to a trigger signal; (b) a pulse generation circuit that generates first and second timing pulses with preset maximum and minimum ignition angles for each engine rotation cycle; (d) a triangular wave generating circuit that generates a triangular wave that falls in synchronization with a second timing pulse at a time; and a trapezoidal wave generation circuit that generates a trapezoidal wave that falls in synchronization with the second timing pulse; A capacitor charging/discharging type ignition device comprising: a comparison circuit that outputs an output; and (f) a gate circuit that triggers the thyristor based on the output of the comparison circuit.
JP58159930A 1983-08-31 1983-08-31 Condenser charge and discharge type ignitor Granted JPS6053668A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58159930A JPS6053668A (en) 1983-08-31 1983-08-31 Condenser charge and discharge type ignitor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58159930A JPS6053668A (en) 1983-08-31 1983-08-31 Condenser charge and discharge type ignitor

Publications (2)

Publication Number Publication Date
JPS6053668A JPS6053668A (en) 1985-03-27
JPS635596B2 true JPS635596B2 (en) 1988-02-04

Family

ID=15704254

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58159930A Granted JPS6053668A (en) 1983-08-31 1983-08-31 Condenser charge and discharge type ignitor

Country Status (1)

Country Link
JP (1) JPS6053668A (en)

Also Published As

Publication number Publication date
JPS6053668A (en) 1985-03-27

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