JPH0711263B2 - Ignition timing control device for internal combustion engine - Google Patents
Ignition timing control device for internal combustion engineInfo
- Publication number
- JPH0711263B2 JPH0711263B2 JP62149131A JP14913187A JPH0711263B2 JP H0711263 B2 JPH0711263 B2 JP H0711263B2 JP 62149131 A JP62149131 A JP 62149131A JP 14913187 A JP14913187 A JP 14913187A JP H0711263 B2 JPH0711263 B2 JP H0711263B2
- Authority
- JP
- Japan
- Prior art keywords
- ignition timing
- ignition
- engine
- acceleration
- operating state
- 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 - Lifetime
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 7
- 230000001133 acceleration Effects 0.000 claims description 44
- 238000012937 correction Methods 0.000 claims description 28
- 238000005259 measurement Methods 0.000 claims description 4
- 238000001514 detection method Methods 0.000 claims description 3
- 230000007423 decrease Effects 0.000 description 12
- 239000000446 fuel Substances 0.000 description 12
- 238000002347 injection Methods 0.000 description 9
- 239000007924 injection Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 230000004043 responsiveness Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 239000013256 coordination polymer Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Landscapes
- Electrical Control Of Ignition Timing (AREA)
Description
【発明の詳細な説明】 〈産業上の利用分野〉 本発明は、内燃機関の点火時期制御装置に関し、特に加
速時のショックを点火時期制御により抑制する技術に関
する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an ignition timing control device for an internal combustion engine, and more particularly to a technique for suppressing shock during acceleration by ignition timing control.
〈従来の技術〉 従来の自動車用内燃機関、特に電子制御燃料噴射装置を
備えた内燃機関にあっては、機関運転状態に応じて燃料
噴射が応答性良く行われるため加速運転時にはスロット
ル弁の開度変化に燃焼圧力(図示平均有効圧)が応答性
良く追従する。<Prior Art> In a conventional internal combustion engine for an automobile, particularly an internal combustion engine equipped with an electronically controlled fuel injection device, fuel injection is performed with high responsiveness according to the engine operating state, so that the throttle valve is opened during acceleration operation. The combustion pressure (the indicated mean effective pressure) follows the temperature change with good responsiveness.
〈発明が解決しようとする問題点〉 ところが、車両は重量が大きく慣性が大きいため、機関
の出力に対して応答性良く追従することができないので
加速を終了して定常状態に移行する際に、車両のゆり返
し(車両前後Gの変動)によるガクガク振動を生じると
共に機関の回転変動を生じ、運転性,乗り心地が悪化す
る。<Problems to be solved by the invention> However, since the vehicle has a large weight and a large inertia, it is not possible to follow the output of the engine with good responsiveness, so when accelerating and shifting to a steady state, Jerky vibrations are generated due to the rolling back of the vehicle (variation in the front-rear direction G of the vehicle), and rotational fluctuations of the engine are generated, which deteriorates drivability and riding comfort.
そこで加速後、機関回転数が下降し始めてから該下降を
抑制すべく点火時期を遅角補正し、その後回転数上昇時
は進角、下降時は遅角補正を行って回転変動を抑制する
ようにしたものもある。Therefore, after acceleration, the ignition timing is retarded to suppress the engine speed from starting to decrease, and then the ignition timing is retarded when the engine speed increases and retarded when the engine speed decreases to suppress the rotational fluctuation. There are also some.
しかしながら、このように、加速終了後から点火時期補
正を開始すると、開始直後、機関運転の定常状態に対応
して設定した基本点火時期は当該運転状態でトルクを可
及的に高めるべく設定された値(いわゆる最適点火時
期)となっているため、この点火時期を進角方向に補正
してもそれ以上トルクを高めることにはならず、回転数
の減少を抑制できないので、回転数の変動を良好に抑制
できるものではなかった。However, when the ignition timing correction is started after the end of acceleration, the basic ignition timing set corresponding to the steady state of the engine operation is set immediately after the start so as to increase the torque as much as possible in the operating state. Since it is a value (so-called optimum ignition timing), even if this ignition timing is corrected in the advance direction, the torque will not be increased any more, and the decrease in rotation speed cannot be suppressed, so fluctuations in rotation speed are suppressed. It could not be suppressed well.
即ち、進角補正により回転数を上昇させるためには、進
角補正前の点火時期が最適点火時期より予め遅角側にあ
って進角により最適点火時期に近づける必要がある。That is, in order to increase the number of revolutions by the advance angle correction, it is necessary that the ignition timing before the advance angle correction is on the retard side in advance from the optimum ignition timing so that the advance timing approaches the optimum ignition timing.
本発明はこのような従来の問題点に着目してなされたも
ので、加速時に予め所定量点火時期を遅角側に補正し、
その後回転数変化に応じた進遅角補正を行うことによ
り、上記問題点を解決した内燃機関の点火時期制御装置
を提供することを目的とする。The present invention has been made by focusing on such a conventional problem, and corrects a predetermined amount of ignition timing to a retard side in advance during acceleration,
It is an object of the present invention to provide an ignition timing control device for an internal combustion engine, which solves the above-mentioned problems by performing advance / retard correction according to a change in the number of revolutions thereafter.
〈問題点を解決するための手段〉 このため本発明は、第1図に示すように機関の運転状態
を検出する機関運転状態検出手段と、 前記運転状態検出手段により検出された機関運転状態に
基づいて基本点火時期を設定する基本点火時期設定手段
と、 前記運転状態検出手段により検出された機関運転状態に
基づいて機関の加速状態を判定する加速判定手段と、 前記加速判定手段により定常状態から加速状態に移行し
たことを判定した時点からの経過時間を計測する計時手
段と、 前記計時手段による計測開始後所定時間は前記基本点火
時期を所定量遅角側に補正する第1の点火時期補正手段
と、 前記計時手段による計測開始後前記所定時間経過後は、
前記第1点火時期補正手段により補正された点火時期を
初期値として、前記運転状態検出手段により検出される
機関回転変動を抑制する方向に当該変動量に応じて点火
時期を補正する第2の点火時期補正手段と、 前記第1の点火時期補正手段及び第2の点火時期補正手
段により補正された点火時期に点火装置に点火信号を出
力する点火信号出力手段と、を備えて構成する。<Means for Solving Problems> Therefore, according to the present invention, as shown in FIG. 1, the engine operating state detecting means for detecting the operating state of the engine and the engine operating state detected by the operating state detecting means are provided. A basic ignition timing setting means for setting a basic ignition timing based on the acceleration determination means for determining the acceleration state of the engine based on the engine operating state detected by the operating state detecting means; and a steady state by the acceleration determining means. A time measuring means for measuring an elapsed time from the time when it is determined that the acceleration state is entered, and a first ignition timing correction for correcting the basic ignition timing to a retard side by a predetermined amount for a predetermined time after the start of measurement by the time measuring means. Means, and after the predetermined time has elapsed after the start of measurement by the time measuring means,
A second ignition in which the ignition timing corrected by the first ignition timing correction means is used as an initial value, and the ignition timing is corrected according to the amount of change in a direction to suppress the engine rotation variation detected by the operating state detection means. And a timing correction means, and an ignition signal output means for outputting an ignition signal to the ignition device at the ignition timing corrected by the first ignition timing correction means and the second ignition timing correction means.
〈作用〉 定常状態から加速状態に移行すると計時手段により計時
される所定時間は基本点火時期が所定量遅角側に補正さ
れる。<Operation> When the steady state shifts to the acceleration state, the basic ignition timing is corrected to the retard side by the predetermined amount for the predetermined time measured by the time measuring means.
前記所定時間経過後に機関回転数が低下に転じてからは
回転数の変動を抑制する方向、つまり、回転数の低下に
対しては点火時期を進角する方向に補正が行われるが、
その際、予め点火時期の初期値が遅角側に補正されてい
るため点火時期を進角補正することによりトルクが高め
られ回転数の低下を抑制することができ、それ以降の回
転変動を良好に抑制できる。After the engine speed has started to decrease after the lapse of the predetermined time, the fluctuation in the rotation speed is suppressed, that is, the correction is performed in the direction in which the ignition timing is advanced with respect to the decrease in the rotation speed.
At that time, since the initial value of the ignition timing is corrected in advance to the retard side, the ignition timing is corrected by advancing the ignition timing to increase the torque and suppress the decrease in the rotation speed, and the subsequent fluctuation in rotation is excellent. Can be suppressed to.
〈実施例〉 以下、本発明の実施例を図に基づいて説明する。<Example> An example of the present invention will be described below with reference to the drawings.
第2図を参照し、機関1には、エアクリーナ2,吸気ダク
ト3,スロットルチャンバ4及び吸気マニホールド5を介
して空気が吸入される。Referring to FIG. 2, air is taken into the engine 1 through the air cleaner 2, the intake duct 3, the throttle chamber 4 and the intake manifold 5.
吸気ダクト3にはエアフローメータ6が設けられてい
て、吸入空気流量を検出する。スロットルチャンバ4に
は図示しないアクセルペダルと連動するスロットル弁7
が設けられていて、吸入空気流量を制御する。スロット
ル弁7にはスロットル弁開度の検出のためポテンショメ
ータ式のスロットルセンサ8が付設されている。吸気マ
ニホールド5には各気筒毎に電磁式燃料噴射弁9が設け
られていて、図示しない燃料ポンプから圧送されプレッ
シャレギュレータにより所定の圧力に制御される燃料を
機関1に噴射供給する。An air flow meter 6 is provided in the intake duct 3 to detect the intake air flow rate. In the throttle chamber 4, there is a throttle valve 7 that works in conjunction with an accelerator pedal (not shown).
Is provided to control the intake air flow rate. The throttle valve 7 is provided with a potentiometer-type throttle sensor 8 for detecting the throttle valve opening. The intake manifold 5 is provided with an electromagnetic fuel injection valve 9 for each cylinder, and injects fuel to the engine 1 which is fed under pressure from a fuel pump (not shown) and is controlled to a predetermined pressure by a pressure regulator.
燃料噴射量の制御は、コントロールユニット20に内蔵さ
れたマイクロコンピュータにおいて、エアフローメータ
6により検出される吸入空気流量Qと後述するディスト
リビュータ13に内蔵されたクランク角センサ10からの信
号に基づいて算出される機関回転数Nとから基本燃料噴
射量Tp=K・Q/N(Kは定数)を演算し、これを適宜補
正して燃料噴射量Ti=Tp・COEF+Ts(COEFは加速補正係
数などを含む各種補正係数、Tsは電圧補正分)を設定
し、これに相応するパルス巾の駆動パルス信号を機関1
の回転に同期して所定のタイミングで燃料噴射弁9に与
えることによって行う。The control of the fuel injection amount is calculated in the microcomputer incorporated in the control unit 20 based on the intake air flow rate Q detected by the air flow meter 6 and the signal from the crank angle sensor 10 incorporated in the distributor 13 described later. The basic fuel injection amount Tp = K · Q / N (K is a constant) is calculated from the engine speed N and the fuel injection amount Ti = Tp · COEF + Ts (COEF includes an acceleration correction coefficient etc.) Various correction factors, Ts is a voltage correction amount), and a drive pulse signal having a pulse width corresponding to this is set in the engine 1.
It is performed by giving the fuel injection valve 9 at a predetermined timing in synchronism with the rotation of.
機関1の各気筒には点火栓11が設けられていて、これら
には点火コイル12にて発生する高電圧がディストリビュ
ータ13を介して順次印加され、これにより火花点火して
混合気を着火燃焼させる。ここで、点火コイル12はそれ
に付設されたパワートランジスタ12aを介して高電圧の
発生時期を制御される。従って、点火時期の制御は、パ
ワートランジスタ12aのオン・オフ時期をコントロール
ユニット20からの点火信号で制御することによって行
う。Each cylinder of the engine 1 is provided with a spark plug 11, to which a high voltage generated in an ignition coil 12 is sequentially applied via a distributor 13, whereby spark ignition is performed to ignite and burn an air-fuel mixture. . Here, the ignition coil 12 has its high voltage generation timing controlled via a power transistor 12a attached thereto. Therefore, the ignition timing is controlled by controlling the on / off timing of the power transistor 12a with the ignition signal from the control unit 20.
この点火時期の制御ため、機関運転状態のパラメータと
して、クランク角センサ10からの信号に基づいて算出さ
れる機関回転数Nと、前記のように演算される基本燃料
噴射量Tpとが用いられる。また、スロットルセンサ7か
らの信号に基づいて検出されるスロットル弁開度TVOが
用いられる。In order to control the ignition timing, the engine speed N calculated based on the signal from the crank angle sensor 10 and the basic fuel injection amount Tp calculated as described above are used as parameters of the engine operating state. Further, the throttle valve opening TVO detected based on the signal from the throttle sensor 7 is used.
ここで、エアフローメータ6,スロットルセンサ8,クラン
ク角センサ10が機関運転状態検出手段に相当し、点火コ
イル12,ディストリビュータ13,点火栓11が点火装置を構
成する。Here, the air flow meter 6, the throttle sensor 8, and the crank angle sensor 10 correspond to the engine operating state detecting means, and the ignition coil 12, the distributor 13, and the spark plug 11 constitute an ignition device.
コントロールユニット20内のマイクロコンピュータのCP
Uにおいては、第3図のフローチャートに従って演算処
理し、点火時期(点火進角)ADVを制御する。CP of microcomputer in control unit 20
In U, arithmetic processing is performed according to the flowchart of FIG. 3 to control the ignition timing (ignition advance) ADV.
ステップ1(図にはS1として記してある。以下同様)で
は現時点の機関回転数Nから前回の機関回転数NoLdを減
算して機関回転数の変動量ΔNを演算する。In step 1 (denoted as S1 in the figure. The same applies to the following), the previous engine speed No L d is subtracted from the current engine speed N to calculate the engine speed fluctuation amount ΔN.
ステップ2では加速判定フラグFの判定を行い、加速判
定プラグFが0の場合(未だ加速判定が行われていない
場合)は、ステップ3へ進む。In step 2, the acceleration determination flag F is determined. If the acceleration determination plug F is 0 (if the acceleration determination has not been performed yet), the process proceeds to step 3.
ステップ3では、現時点のスロットル弁開度TVOから前
回のスロットル弁開度TVOoLdを減算してスロットル弁開
度の変化量ΔTVOを演算する。そして、ステップ4では
スロットル弁開度の変動量ΔTVOと加速判定値CaccCを比
較する。この部分が加速判定手段に相当する。In step 3, the previous throttle valve opening TVOo L d is subtracted from the current throttle valve opening TVO to calculate the change amount ΔTVO of the throttle valve opening. Then, in step 4, the variation amount ΔTVO of the throttle valve opening and the acceleration determination value Cacc C are compared. This part corresponds to the acceleration determination means.
ここで、スロットル弁開度の変動量ΔTVOがCaccC未満の
ときはステップ5へ進んで加速判定フラグFを0に維持
する。そして、次のステップ6ではバックグラウンドジ
ョブとして実行されるルーチンに従って機関回転数Nと
基本燃料噴射量Tpとからマップを参照して定められる点
火進角のマップ値MADV(基本点火時期)を最終的な点火
進角ADVとし、次のステップ7で出力する。Here, when the variation amount ΔTVO of the throttle valve opening is less than Cacc C, the routine proceeds to step 5, and the acceleration determination flag F is maintained at 0. Then, in the next step 6, the map value MADV (basic ignition timing) of the ignition advance angle determined by referring to the map from the engine speed N and the basic fuel injection amount Tp is finally determined according to a routine executed as a background job. Ignition advance angle ADV and output in the next step 7.
ここで、ステップ6の部分が基本点火時期設定手段に相
当し、ステップ7の部分が点火信号出力手段に相当す
る。Here, the part of step 6 corresponds to the basic ignition timing setting means, and the part of step 7 corresponds to the ignition signal output means.
ステップ4での判定において、スロットル弁開度の変動
量ΔTVOが加速判定値Cacc以上で、加速と判定される
と、ステップ8に進んで加速判定フラグFを1にセット
する。In the determination in step 4, if the variation amount ΔTVO of the throttle valve opening is equal to or greater than the acceleration determination value Cacc and it is determined to be accelerated, the process proceeds to step 8 and the acceleration determination flag F is set to 1.
次にステップ9に進んで制御時間のTIMを0にする。そ
して、次のステップ10ではマップを参照して定められる
点火進角のマップ値MADVから所定の遅角量ΔADV0を差し
引いた値を最終的な点火進角ADVとし、次のステップ7
で出力する。尚、制御時間TIMはタイマにより自動的に
計時されるタイマ値であり、したがってこのタイマが計
時手段に相当する。Next, in step 9, TIM of control time is set to 0. Then, in the next step 10, a value obtained by subtracting a predetermined retard angle amount ΔADV 0 from the ignition advance angle map value MADV determined by referring to the map is set as the final ignition advance angle ADV, and the next step 7
To output. The control time TIM is a timer value that is automatically timed by a timer, and thus this timer corresponds to a time measuring means.
加速判定がなされて加速所定フラグFが1にセットされ
た後は、ステップ2の判定においてステップ11以降へ進
んで所定時間B内において、前記遅角量ΔADV0の補正を
維持した後、さらに所定時間(A−B)内において回転
数変動量に応じた進遅角制御を行う。After the acceleration determination is made and the acceleration predetermined flag F is set to 1, the process proceeds to step 11 onward in the determination of step 2, and within the predetermined time B, the correction of the retard amount ΔADV 0 is maintained, and then the predetermined amount is further determined. Within the time (A-B), advance / retard control is performed according to the rotation speed fluctuation amount.
即ち、ステップ11での判定で制御時間TIMが所定時間A
未満の場合はステップ12で制御時間内TIMをAより小の
所定時間Bと比較し、所定時間未満の時は、ステップ10
以降へ進んでマップ進角値MADVから遅角値ΔADV0を差し
引いた値を点火進角とする制御を接続する。尚、この間
ステップ16にてタイマTIMの値をカウントアップする。That is, the control time TIM is determined to be the predetermined time A according to the determination in step 11.
When it is less than the predetermined time, the TIM within the control time is compared with the predetermined time B which is smaller than A in step 12, and when it is less than the predetermined time, step 10
After that, the control for connecting the ignition advance angle with a value obtained by subtracting the retard value ΔADV 0 from the map advance value MADV is connected. During this period, the value of the timer TIM is incremented in step 16.
ここで前記所定時間Bは、加速開始後機関回転数が減少
に移行して車両のゆり返しを生じる直前の状態までの時
間近くに設定されている。これは、車両の前後Gの固有
振動数によって大略決められ、実験的に求められる。但
し、ステップ1において検出される回転数の変動量ΔN
が0近傍となるまでステップ10の制御を継続するように
してもよい。尚、ステップ12によって設定される所定時
間Bの間ステップ10へ進んでマップ進角値MADVを所定量
ΔADV0遅角する機能が第1の点火時期補正手段に相当す
る。Here, the predetermined time B is set close to the time immediately before the state in which the engine speed starts to decrease after acceleration starts to cause the vehicle to swing back. This is roughly determined by the natural frequencies of the front and rear G of the vehicle, and is experimentally obtained. However, the fluctuation amount ΔN of the rotation speed detected in step 1
The control of step 10 may be continued until is near 0. The function of advancing the map advance value MADV by the predetermined amount ΔADV 0 by advancing to step 10 during the predetermined time B set by step 12 corresponds to the first ignition timing correcting means.
ステップ12で制御時間が所定時間B以上(A未満)と判
定されたときは、ステップ13へ進み、制御時間計時用の
タイマTIMをカウントアップする。When it is determined in step 12 that the control time is equal to or longer than the predetermined time B (less than A), the process proceeds to step 13 to count up the timer TIM for measuring the control time.
次いでステップ14では、ステップ1で求めた回転数変動
量ΔN(正,負を含めた値)に応じて進遅角補正量ΔAD
VをROMに記憶したマップから検索する。Next, at step 14, in accordance with the rotational speed fluctuation amount ΔN (value including positive and negative) obtained at step 1, the advance / retard correction amount ΔAD
Search V from the map stored in ROM.
そして、ステップ15では点火進角ADVをマップ進角値MAD
Vから前記所定の遅角量ΔADV0を差し引いた値に前記進
遅角補正量ΔADVを加算した値として設定し、ステップ
7で出力する。このステップ14,15の部分が第2の点火
時期補正手段に相当する。Then, in step 15, the ignition advance angle ADV is set to the map advance value MAD.
The value is set as a value obtained by adding the advance / retard angle correction amount ΔADV to a value obtained by subtracting the predetermined retard angle amount ΔADV 0 from V, and output in step 7. The steps 14 and 15 correspond to the second ignition timing correction means.
また、ステップ11で制御時間TIMが所定時間A以上にな
ったと限定されるとステップ5へ進んで加速判定フラグ
Fが0にリセットされ、ステップ6で検索されたMAP進
角値MADVを点火時期とする制御が行われる。つまり、所
定時間Aの間は一旦加速判定した後の加速判定が禁止さ
れ、その後この禁止を解除して加速判定による前記した
点火時期制御を再開する。When the control time TIM is limited to the predetermined time A or more in step 11, the process proceeds to step 5, the acceleration determination flag F is reset to 0, and the MAP advance value MADV retrieved in step 6 is set as the ignition timing. Control is performed. That is, during the predetermined time A, the acceleration determination after the acceleration determination is once prohibited, and then the prohibition is released and the ignition timing control based on the acceleration determination is restarted.
このようにすれば、第4図に実線で示すように、加速に
より上昇した機関回転数(平均有効圧)が下降し始める
間、予め点火時期を所定量遅角補正し、下降し始めてか
らは遅角補正された点火時期を初期値として回転数の変
化量に応じて回転変動を抑制する方向に進遅角補正する
制御が開始される。したがって、回転数下降直後の進角
補正において点火時期は、トルク優先の最適点火時期に
近づける方向に進角されることになるため、平均有効圧
Piの低下を効果的に抑制でき、もってゆり返し初期の機
関回転数の低下を良好に抑制して引き続く回転変動も十
分に抑制される。図で点線は従来例を示す。尚、加速判
定直後から回転数変化量に応じた点火時期補正を行うこ
とも考えられるが、この場合、遅角補正量が大きくなり
すぎることがあり、満足な加速感が得られない。この
点、本発明の場合、ゆり返しを抑制すべく設定された量
だけ遅角補正するので加速性能に与える影響を小さくで
きる。In this way, as shown by the solid line in FIG. 4, while the engine speed (average effective pressure) increased by acceleration begins to decrease, the ignition timing is previously retarded by a predetermined amount, and after the decrease begins, With the ignition timing corrected for the retard angle as an initial value, the control for advancing / retarding the ignition timing in a direction of suppressing the rotational fluctuation is started according to the amount of change in the rotational speed. Therefore, the ignition timing is advanced in the correction of the advance angle immediately after the rotation speed is lowered, so that the ignition timing is advanced in the direction approaching the optimum ignition timing of the torque priority.
The decrease in Pi can be effectively suppressed, and accordingly, the decrease in the engine speed at the initial stage of the swing back can be effectively suppressed, and the subsequent fluctuation in the rotation speed can be sufficiently suppressed. In the figure, the dotted line shows a conventional example. It is possible to correct the ignition timing in accordance with the rotational speed change amount immediately after the acceleration determination, but in this case, the retard correction amount may become too large, and a satisfactory acceleration feeling cannot be obtained. In this respect, in the case of the present invention, since the retard correction is performed by the amount set to suppress the swing back, the influence on the acceleration performance can be reduced.
尚、この遅角補正量を加速の程度(例えばスロットル弁
開度の変化速度により検出)に応じて設定すれば、加速
の程度によらず加速性能を与える影響を十分小さくでき
ると共に、ゆり返し開始時にゆり返しの程度に応じて最
適点火時期に近づける方向の進角補正制御量(進角制御
により回転減少を抑制できる)を確保でき常に良好な回
転変動抑制効果が得られる。If this retard correction amount is set according to the degree of acceleration (for example, it is detected by the changing speed of the throttle valve opening), the effect on acceleration performance can be sufficiently reduced regardless of the degree of acceleration, and the start of reversing At the same time, it is possible to secure an advance angle correction control amount (which can suppress the rotation decrease by the advance angle control) in the direction of approaching the optimum ignition timing depending on the degree of rebound, and always obtain a good rotation fluctuation suppressing effect.
また、第4図に鎖線で示すように加速検出後所定時間の
間一定の傾きで徐々に遅角量を増大するようにすれば加
速開始点火時期が段差をもって遅角されることがないの
で加速感,加速性能をより良好に確保できる。この場合
でも所定時間後の総遅角量は、一定(又は加速程度に応
じて設定された量)であり、ゆり返しを抑制できる効果
は同様である。Further, as shown by the chain line in FIG. 4, if the retard amount is gradually increased with a constant inclination for a predetermined time after acceleration is detected, the acceleration start ignition timing is not retarded with a step, and therefore the acceleration is accelerated. The feeling and acceleration performance can be better secured. Even in this case, the total retard amount after the predetermined time is constant (or the amount set according to the degree of acceleration), and the effect of suppressing the rebound is the same.
〈発明の効果〉 以上説明したように本発明によれば加速検出後所定時間
点火時期を所定量遅角させたのち回転変動量に応じた進
遅角補正を行うようにしたため、加速性能を確保しつ
つ、ゆり返しを効果的に抑制でき乗り心地を向上でき
る。<Effects of the Invention> As described above, according to the present invention, since the ignition timing is retarded by the predetermined time after the acceleration is detected, the advance / retard correction is performed according to the rotation variation amount, so that the acceleration performance is secured. In addition, it is possible to effectively suppress the swingback and improve the riding comfort.
第1図は本発明の構成を示すブロック図、第2図は本発
明の一実施例の全体構成図、第3図は同上実施例の制御
ルーチンを示すフローチャート、第4図は、同上実施例
における各部状態を示すタイムチャートである。 1……機関、6……エアフローメータ、8……スロット
ルセンサ、10……クランク角センサ、11……点火栓、12
……点火コイル、13……ディストリビュータ、20……コ
ントロールユニットFIG. 1 is a block diagram showing the configuration of the present invention, FIG. 2 is an overall configuration diagram of an embodiment of the present invention, FIG. 3 is a flow chart showing a control routine of the same embodiment, and FIG. 3 is a time chart showing the state of each part in FIG. 1 ... Engine, 6 ... Air flow meter, 8 ... Throttle sensor, 10 ... Crank angle sensor, 11 ... Spark plug, 12
...... Ignition coil, 13 ...... Distributor, 20 ...... Control unit
Claims (1)
出手段と、 前記運転状態検出手段により検出された機関運転状態に
基づいて基本点火時期を設定する基本点火時期設定手段
と、 前記運転状態検出手段により検出された機関運転状態に
基づいて機関の加速状態を判定する加速判定手段と、 前記加速判定手段により定常状態から加速状態に移行し
たことを判定した時点からの経過時間を計測する計時手
段と、 前記計時手段による計測開始後所定時間は前記基本点火
時期を所定量遅角側に補正する第1の点火時期補正手段
と、 前記計時手段による計測開始後前記所定時間経過後は、
前記第1点火時期補正手段により補正された点火時期を
初期値として、前記運転状態検出手段により検出される
機関回転変動を抑制する方向に当該変動量に応じて点火
時期を補正する第2の点火時期補正手段と、 前記第1の点火時期補正手段及び第2の点火時期補正手
段により補正された点火時期に点火装置に点火信号を出
力する点火信号出力手段と、を備えて構成したことを特
徴とする内燃機関の点火時期制御装置。1. An engine operating state detecting means for detecting an operating state of an engine, a basic ignition timing setting means for setting a basic ignition timing based on the engine operating state detected by the operating state detecting means, and the operating state. Acceleration determination means for determining the acceleration state of the engine based on the engine operating state detected by the detection means, and timekeeping for measuring the elapsed time from the time when the acceleration determination means determines that the steady state has changed to the acceleration state. Means, first ignition timing correction means for correcting the basic ignition timing to a retarded side by a predetermined amount for a predetermined time after the start of measurement by the time measuring means, and after the predetermined time has elapsed after the start of measurement by the time measuring means,
A second ignition in which the ignition timing corrected by the first ignition timing correction means is used as an initial value, and the ignition timing is corrected according to the amount of change in a direction to suppress the engine rotation variation detected by the operating state detection means. A timing correction means; and an ignition signal output means for outputting an ignition signal to an ignition device at the ignition timing corrected by the first ignition timing correction means and the second ignition timing correction means. Ignition timing control device for internal combustion engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP62149131A JPH0711263B2 (en) | 1987-06-17 | 1987-06-17 | Ignition timing control device for internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP62149131A JPH0711263B2 (en) | 1987-06-17 | 1987-06-17 | Ignition timing control device for internal combustion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63314370A JPS63314370A (en) | 1988-12-22 |
| JPH0711263B2 true JPH0711263B2 (en) | 1995-02-08 |
Family
ID=15468414
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP62149131A Expired - Lifetime JPH0711263B2 (en) | 1987-06-17 | 1987-06-17 | Ignition timing control device for internal combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0711263B2 (en) |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07117023B2 (en) * | 1986-12-04 | 1995-12-18 | 株式会社日立製作所 | Engine controller |
| JPH076480B2 (en) * | 1987-03-26 | 1995-01-30 | 株式会社ユニシアジェックス | Ignition timing control device for internal combustion engine |
-
1987
- 1987-06-17 JP JP62149131A patent/JPH0711263B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63314370A (en) | 1988-12-22 |
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