JPS62258152A - Method for controlling ignition timing of internal combustion engine - Google Patents

Method for controlling ignition timing of internal combustion engine

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Publication number
JPS62258152A
JPS62258152A JP10095886A JP10095886A JPS62258152A JP S62258152 A JPS62258152 A JP S62258152A JP 10095886 A JP10095886 A JP 10095886A JP 10095886 A JP10095886 A JP 10095886A JP S62258152 A JPS62258152 A JP S62258152A
Authority
JP
Japan
Prior art keywords
internal combustion
combustion engine
acceleration
ignition timing
ignition
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.)
Granted
Application number
JP10095886A
Other languages
Japanese (ja)
Other versions
JPH0684749B2 (en
Inventor
Masami Nagano
正美 永野
Takeshi Atago
阿田子 武士
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP61100958A priority Critical patent/JPH0684749B2/en
Publication of JPS62258152A publication Critical patent/JPS62258152A/en
Publication of JPH0684749B2 publication Critical patent/JPH0684749B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Electrical Control Of Ignition Timing (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To eliminate misfire immediately after acceleration, prevent after burning, and improve operatability by delayingly carrying out the lag angle of ignition timing at the time of acceleration of an internal combustion engine by a defined number of misfire after detecting acceleration. CONSTITUTION:A control unit has an MPU 21, etc. and receives various detected signals from various detecting sensors 3, 25, 26, 27, 18, 19, 29 for detecting various operating conditions of an engine via an A/D converter and an input/ output circuit 24. And, after carrying out a certain arithmetic processing, it controls injectors 13, an ignition coil 29, and a fuel pump 10 in accordance with the operated result. In this case, when an ignition timing is gradually advanced after delaying the ignition timing at the time of accelerating an internal combustion engine, the delay of angle is carried out from after a defined number of ignition after the acceleration is detected. Thereby, misfire immediately after acceleration can be eliminated, preventing after burning.

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方法に係り。[Detailed description of the invention] [Industrial application field] The present invention relates to an ignition timing control method for an internal combustion engine.

特に電子式燃料噴射装置において、加速ショックを軽減
するに好適な内燃機関の点火時期制御方法に関する。
In particular, the present invention relates to an ignition timing control method for an internal combustion engine suitable for reducing acceleration shock in an electronic fuel injection system.

〔従来の技術〕[Conventional technology]

従来の電子式燃料噴射装置における内燃機関の点火時期
制御方法では、たとえば特開昭59−162365号に
記載のように加速ショックを軽減するため、加速時に加
速検出直後に点火時期を遅角させたのち除々に点火時期
を進角させる制御方法を採っていた。
In a conventional method for controlling ignition timing of an internal combustion engine using an electronic fuel injection system, the ignition timing is retarded immediately after acceleration is detected during acceleration in order to reduce acceleration shock, as described in JP-A-59-162365, for example. Later, a control method was adopted that gradually advanced the ignition timing.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

しかし上記従来技術は加速時に加速検出直後に点火時期
を遅角させることにより発生する加速直後の失火につい
て配慮されていないため、加速ショックを軽減すべく遅
角量を多くするとアフターバーンが発生する問題点があ
った。
However, the above-mentioned conventional technology does not take into account misfires that occur immediately after acceleration by retarding the ignition timing immediately after acceleration is detected during acceleration, so if the amount of retardation is increased to reduce acceleration shock, afterburn occurs. There was a point.

本発明の目的は加速時に加速ショックを軽減するととも
にアフターバーンを防止する内燃機関の点火時期制御方
法を提供するにある。
An object of the present invention is to provide an ignition timing control method for an internal combustion engine that reduces acceleration shock during acceleration and prevents afterburn.

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

上記目的は、従来技術では加速時の点火時期の遅角を加
速検出直後に行っていたため、加速時に増量した燃料が
吸入されていない気筒が失火してアフターパーンが発生
していたのに着目し、本発明により加速時の点火時期の
遅角を加速検出直後に行うのではなく、加速時の点火時
期の遅角を加速検出後に所定点火回数後から行うように
して。
The above objective was to focus on the fact that in conventional technology, the ignition timing during acceleration was retarded immediately after acceleration was detected, which resulted in misfires in cylinders that had not taken in the increased amount of fuel during acceleration, resulting in afterburn. According to the present invention, the ignition timing during acceleration is not retarded immediately after acceleration is detected, but the ignition timing during acceleration is retarded a predetermined number of times after acceleration is detected.

加速時に増量された燃料が吸入されて爆発する気筒から
遅角を行うことにより達成される。
This is achieved by retarding the cylinder from which the increased amount of fuel is sucked in during acceleration and explodes.

〔作用〕[Effect]

上記手段による内燃機関の点火時期制御方法では、加速
時の点火時期の遅角が加速を検出した後に所定の点火回
数後から行われることによって。
In the ignition timing control method for an internal combustion engine using the above means, the ignition timing is retarded during acceleration a predetermined number of times after acceleration is detected.

加速の瞬間から加速補正により増量された燃料が吸入さ
れて爆発するまでの間は点火時期が遅角されないので、
気筒が失火してアフターバーンを発生させることがない
Since the ignition timing is not retarded from the moment of acceleration until the fuel increased by acceleration correction is inhaled and explodes,
The cylinder will not misfire and cause afterburn.

〔実施例〕〔Example〕

以下に本発明の一実施例を第1図ないし第8図により説
明する。
An embodiment of the present invention will be described below with reference to FIGS. 1 to 8.

まず第2図は本発明による内燃機関の点火時期制御方法
の一実施例を示す電子式燃料噴射装置のシステム構成図
である。第2図において、1はエアクリーナ、2は空気
入口部、3は熱線式空気流量計、4はダクト、5はスロ
ットルボディ、6はコレクタ、7は内燃機関、8は吸気
管である。9は燃料タンク、10は燃料ポンプ、11は
燃料ダンパ、12は燃料フィルタ、13は燃料噴射弁、
14は燃圧レギュレータである。15はコントロールユ
ニット(電子制御回路)、16はデイストリブユータ、
17はイグナイタ、18は02.センサ、19は水温セ
ンサ(温度検出手段)、20は点火プラグである。
First, FIG. 2 is a system configuration diagram of an electronic fuel injection device showing an embodiment of the ignition timing control method for an internal combustion engine according to the present invention. In FIG. 2, 1 is an air cleaner, 2 is an air inlet, 3 is a hot wire air flow meter, 4 is a duct, 5 is a throttle body, 6 is a collector, 7 is an internal combustion engine, and 8 is an intake pipe. 9 is a fuel tank, 10 is a fuel pump, 11 is a fuel damper, 12 is a fuel filter, 13 is a fuel injection valve,
14 is a fuel pressure regulator. 15 is a control unit (electronic control circuit), 16 is a distribution user,
17 is the igniter, 18 is 02. The sensor 19 is a water temperature sensor (temperature detection means), and 20 is a spark plug.

第2図は吸入空気はエアクリーナ1の空気入口部2より
入り、吸入空気量を検出する熱線式空気流量計(空気流
量検出手段)3と、ダクト4と、空気流量を制御する絞
り弁を有するスロットルボディ5を通って、コレクタ6
に入る。これより吸入空気は内燃機関7に連通ずる各吸
気管8に分配され、シリンダ内に吸入される。一方の燃
料は燃料タンク9から燃料ポンプ10で吸引・加圧され
て、燃料ダンパ11と、燃料フィルター2と、噴射弁1
3と、燃料レギュレーター4が配管されている燃料系に
供給される。これより燃料はレギュレータ14により一
定圧力に調圧され、各吸気管8に設けた噴射弁13から
吸気管8内に噴射される。また空気流量計3からは吸入
空気量を検出する信号が出力され、この出力はコントロ
ールユニット15に入力される。デイストリブユータ1
6にはクランク角センサ(回転数検出手段)がパ。
In Fig. 2, intake air enters from an air inlet 2 of an air cleaner 1, which has a hot wire air flow meter (air flow rate detection means) 3 for detecting the amount of intake air, a duct 4, and a throttle valve for controlling the air flow rate. Through the throttle body 5, the collector 6
to go into. From this, the intake air is distributed to each intake pipe 8 communicating with the internal combustion engine 7 and sucked into the cylinder. One fuel is sucked and pressurized from the fuel tank 9 by the fuel pump 10, and is sent to the fuel damper 11, the fuel filter 2, and the injection valve 1.
3 and a fuel regulator 4 are supplied to the fuel system. From this, the pressure of the fuel is regulated to a constant pressure by the regulator 14, and the fuel is injected into the intake pipe 8 from the injection valve 13 provided in each intake pipe 8. Further, the air flow meter 3 outputs a signal for detecting the amount of intake air, and this output is input to the control unit 15. Distributor 1
6 has a crank angle sensor (rotation speed detection means).

−”]内蔵されていて、燃料噴射時期や点火時期の基準
i号および内燃機関回転数を検出する信号が出力され、
コントロールユニット15に入力される。
-”] is built-in, and outputs signals to detect reference number i for fuel injection timing and ignition timing, as well as internal combustion engine rotation speed.
It is input to the control unit 15.

ほかに水温センサー9や02センサ18の検出する信号
などがコントロールユニット15に入力される。
In addition, signals detected by the water temperature sensor 9 and the 02 sensor 18 are input to the control unit 15.

第3図は第2図のコントロールユニット15の制御系の
ブロック構成図である。第2図において。
FIG. 3 is a block diagram of the control system of the control unit 15 shown in FIG. 2. In fig.

コントロールユニット(電子制御回路)15はMPU 
(マイクロプロセッサ)21と、 EPROM 22と
、RAM23と、A/D変換器および入出力回路24を
含む演算装置で構成される。コントロールユニット15
には空気流量計(エアフローセンサ)3と、ディストリ
ブエータ16内のクランク角センサ25と、アイドルス
イッチ26と、スタータスイッチ27と、02センサ1
8と、内燃機関の温度を検出する水温センサ19と、バ
ッテリー電圧28などの出力信号がA/D変換器および
入出力回路24を介して入力される。コントロールユニ
ット15はこれらの所要信号などにより所定演算処理を
行い、その演算結果の出力信号により各噴射弁(インジ
ェクタ)13を所要の噴射パルス幅で作動させて必要量
の燃料を各吸気管8に噴射させると共に、イグナイタ1
7のパワートランジスタに信号を送ってディストリビュ
ータ16のイグニッションコイル29をオン・オフ制御
することにより各点火プラグ20の点火時期を制御する
。ほかに燃料ポンプ10の制御などを行う。
Control unit (electronic control circuit) 15 is MPU
(Microprocessor) 21, EPROM 22, RAM 23, and an arithmetic unit including an A/D converter and an input/output circuit 24. control unit 15
includes an air flow meter (air flow sensor) 3, a crank angle sensor 25 in the distributor 16, an idle switch 26, a starter switch 27, and an 02 sensor 1.
8, a water temperature sensor 19 that detects the temperature of the internal combustion engine, and output signals such as a battery voltage 28 are inputted via an A/D converter and an input/output circuit 24. The control unit 15 performs predetermined calculation processing based on these required signals, and operates each injection valve (injector) 13 with the required injection pulse width based on the output signal of the calculation result to inject the required amount of fuel into each intake pipe 8. At the same time as spraying, igniter 1
The ignition timing of each spark plug 20 is controlled by sending a signal to the power transistor 7 to turn on/off the ignition coil 29 of the distributor 16. It also controls the fuel pump 10, etc.

つぎに第1図は本発明による内燃機関の点火時期制御方
法の一実施例を示す第2図および第3図の点火タイミン
グ図である。第1図において、第2図および第3図の内
燃機関の行程と、燃料噴射タイミングと、空気流量Q1
と1点火タイミングの関係が例示される。第1図のNG
1気筒ないしN(14気筒は一定の空気流量Q&におい
て同期噴射パルス噴射弁13より燃料が噴射される。こ
の状態から加速するためにスロットルボディ5の絞り弁
を開くと、空気流量Q&は図示のように増加する。
Next, FIG. 1 is an ignition timing diagram of FIGS. 2 and 3 showing an embodiment of the ignition timing control method for an internal combustion engine according to the present invention. In FIG. 1, the stroke of the internal combustion engine in FIGS. 2 and 3, the fuel injection timing, and the air flow rate Q1
The relationship between 1 and 1 ignition timing is illustrated. NG in Figure 1
For cylinders 1 to N (14 cylinders, fuel is injected from the synchronous injection pulse injection valve 13 at a constant air flow rate Q&. When the throttle valve of the throttle body 5 is opened to accelerate from this state, the air flow rate Q & increase as follows.

この空気流量の変化量ΔQ&が所定値を越えた時に加速
状態であるこのを検出して、非同期噴射パルスで噴射弁
13より燃料が噴射される。これにより燃料が最初に吸
入されるのは図示のようにNα4気筒であって、この燃
料の混合気が爆発するのは加速検出後の3点火口103
である6本発明による実施例では加速時における点火時
期の遅角は図示のように加速検出後の3点火口103か
ら行い、その後に除々に進角している。したがって薄い
混合気が爆発する加速検出直後の1点火間101および
2点火口102では点火時期が遅角されないので、失火
することがなくアフターパンを発生しない。
When the amount of change ΔQ& in the air flow rate exceeds a predetermined value, this acceleration state is detected, and fuel is injected from the injection valve 13 using an asynchronous injection pulse. As a result, fuel is first sucked into the Nα4 cylinder as shown in the figure, and the fuel mixture explodes at the 3-ignition port 103 after acceleration is detected.
6 In the embodiment according to the present invention, the ignition timing is retarded during acceleration from the three ignition ports 103 after the acceleration is detected, as shown in the figure, and then the ignition timing is gradually advanced. Therefore, the ignition timing is not retarded in the first ignition interval 101 and the second ignition port 102 immediately after acceleration detection in which a lean air-fuel mixture explodes, so misfires do not occur and afterpan does not occur.

第4図は本発明による内燃機関の点火時期制御方法の一
実施例を示す第2図および第3図のコントロールユニッ
ト15の演算処理フローチャートである。第4図におい
て、ステップ111で空気流量Q&またはスロットル開
度0丁りおよび基準点火時期ADVMの信号を読み込み
、ステップ112で加速検出を空気流量変化量ΔQ a
 > X (所定値)またはスロットル開度変化量Δθ
ih>Y(所定値)により行う、ついで加速検出すると
ステップ113で加速検出後の点火回数に対応する遅角
量ΔADVのテーブル検索を行い、点火時期ADV=A
DVM−ΔADVを演算する。この演算結果により内燃
機関15の点火時期を制御する。またステップ114で
基準点火時期ADVMおよび演算結果の点火時期ADV
を所定のアドレスに格納する。第5図は同じくコントロ
ールユニット15の点火時期の遅角量テーブル例の説明
図である。第5図において、点火回数0を加速検出位置
として加速検出後の点火回数1〜nに対応する遅角量Δ
ADVが表示される。本実施例では図示のように加速検
出後に2点火だけ遅らせて3点火目から遅角させ、その
後論々に進角させる。また第6図は同じく他の実施例を
示すコントロールユニット15の演算処理フローチャー
トである。第6図において、加速検出後にステップ11
2aで点火回数ADVCのカウントを行い、点火回数A
DVC=Z (所定回数)で所定の点火位置から点火時
期の遅角を行う、ほかのステップでの動作は第4図と同
様である。
FIG. 4 is an arithmetic processing flowchart of the control unit 15 of FIGS. 2 and 3, showing an embodiment of the ignition timing control method for an internal combustion engine according to the present invention. In FIG. 4, in step 111, signals of air flow rate Q & or throttle opening 0 and reference ignition timing ADVM are read, and in step 112, acceleration detection is performed using air flow rate change amount ΔQ a
> X (predetermined value) or throttle opening change amount Δθ
If ih>Y (predetermined value), then when acceleration is detected, in step 113, a table search is performed for the retard amount ΔADV corresponding to the number of ignitions after acceleration detection, and the ignition timing ADV=A
Calculate DVM-ΔADV. The ignition timing of the internal combustion engine 15 is controlled based on this calculation result. Further, in step 114, the reference ignition timing ADVM and the ignition timing ADV of the calculation result are determined.
is stored at a predetermined address. FIG. 5 is an explanatory diagram of an example of an ignition timing retard amount table of the control unit 15. In FIG. 5, the retard amount Δ corresponds to the number of ignitions 1 to n after acceleration detection, with the number of ignitions being 0 as the acceleration detection position.
ADV will be displayed. In this embodiment, as shown in the figure, after acceleration is detected, the ignition is delayed by two ignitions, the ignition is retarded from the third ignition, and then the ignition is gradually advanced. Further, FIG. 6 is a flowchart of the calculation processing of the control unit 15 showing another embodiment. In FIG. 6, after acceleration detection, step 11
In step 2a, count the number of ignitions ADVC, and calculate the number of ignitions A.
The operation in other steps, in which the ignition timing is retarded from a predetermined ignition position at DVC=Z (a predetermined number of times), is the same as that shown in FIG.

第7図は本発明による内燃機関の点火時期制御方法の一
実施例のテスト結果の説明図である。また第8図は本発
明による前の従来の内燃機関の点火時期制御方法の一例
のテスト結果の説明図である。第8図の従来方法の一例
では空気流量Q&の変化量ΔQaによる加速出直後に点
火時期ADVの遅角を行っていて、加速直後に失火が発
生するため加速後の内燃機関回転数Nの変動がより大き
いのに対して、第7図の本発明による方法の一実施例で
は空気流量Q&の変化量ΔQ&による加速検出後に2点
火遅らせて3点火目から点火時期ADVの遅角を行って
いて二加速直後の失火が発生しないため加速後の内燃機
関回転数Nの変動もより小さくなる。
FIG. 7 is an explanatory diagram of test results of an embodiment of the ignition timing control method for an internal combustion engine according to the present invention. Further, FIG. 8 is an explanatory diagram of test results of an example of the conventional ignition timing control method for an internal combustion engine according to the present invention. In an example of the conventional method shown in Fig. 8, the ignition timing ADV is retarded immediately after acceleration due to the change amount ΔQa in the air flow rate Q&, and misfire occurs immediately after acceleration, so the internal combustion engine rotation speed N changes after acceleration. On the other hand, in one embodiment of the method according to the present invention shown in FIG. 7, after acceleration is detected based on the amount of change ΔQ& in the air flow rate Q&, ignition is delayed by two ignitions, and the ignition timing ADV is retarded from the third ignition. Since a misfire does not occur immediately after second acceleration, fluctuations in the internal combustion engine rotational speed N after acceleration are also smaller.

以上のように本実施例によれば、内燃機関へ燃料を供給
する噴射弁を有し、内燃機関の吸入空気量を検出する空
気流量計またはスロットル開度センサと、内燃機関の回
転数を検出するクランク角センサと、内燃機関の温度を
検出する水温センサなどの信号に基き、噴射弁の噴射パ
ルス幅の演算および点火時期などを決定する電子制御回
路がら口るコントローラユニットなどより構成される電
子式燃料噴射装置において、内燃機関の加速時に点火時
期を遅角させたのち除々に点火時期を進角させる点火時
期制御のさいに、加速を検出したのち所定の点火回数後
から遅角を行うことにより。
As described above, according to this embodiment, the air flow meter or throttle opening sensor has an injection valve that supplies fuel to the internal combustion engine, detects the intake air amount of the internal combustion engine, and detects the rotation speed of the internal combustion engine. An electronic control unit consisting of a controller unit that includes an electronic control circuit that calculates the injection pulse width of the injector and determines the ignition timing based on signals from a crank angle sensor that detects the temperature of the internal combustion engine, and a water temperature sensor that detects the temperature of the internal combustion engine. In a type fuel injection system, during ignition timing control that retards the ignition timing when the internal combustion engine accelerates and then gradually advances the ignition timing, retards the ignition timing after a predetermined number of ignitions after detecting acceleration. By.

加速直後に失火することがないのでアブタバーンを防止
できる。
Since there is no misfire immediately after acceleration, it is possible to prevent an accident.

〔発明の効果〕〔Effect of the invention〕

以上の説明のように本発明によれば、内燃機関の加速時
における点火時期の遅角を加速検出後に所定の失火回数
だけ遅らせてから行うので、加速直後の失火をなくして
アフターバーンを防止し、運転性を向上できる効果があ
る。
As described above, according to the present invention, the ignition timing is retarded when the internal combustion engine accelerates by a predetermined number of misfires after acceleration is detected, thereby eliminating misfires immediately after acceleration and preventing afterburn. , which has the effect of improving drivability.

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

第1図は本発明による内燃機関の点火時期制御方法の一
実施例を示す点火タイミング図、第2図は同じく電子式
燃料噴射装置のシステム図、第3図は第2図の制御系の
ブロック図、第4図は第2図(第3図)の処理フローチ
ャート、第5図は同じく点火時期の遅角量テーブル例図
、第6図は同じく他の処理フローチャート、第7図は同
じくテスト結果図、第8図は従来例のテスト結果図であ
る。 1・・・エアクリーナ、3・・・空気流量計(空気流量
検出手段)、5・・・スロットルボディ、7・・・内燃
機関。 8・・・吸気管、9・・・燃料タンク、10・・・燃料
ポンプ。 13・・・噴射弁、15・・・コントロールユニット(
電子制御回路)、16・・・ディストリビュータ(回転
数検出手段を含む)、19・・・水温センサ(温度検出
手段)、2o・・・点火プラグ。
Fig. 1 is an ignition timing diagram showing an embodiment of the ignition timing control method for an internal combustion engine according to the present invention, Fig. 2 is a system diagram of an electronic fuel injection device, and Fig. 3 is a block diagram of the control system shown in Fig. 2. Figure 4 is the process flowchart of Figure 2 (Figure 3), Figure 5 is an example of the ignition timing retard amount table, Figure 6 is another process flowchart, and Figure 7 is the test result. 8 are test results diagrams of the conventional example. DESCRIPTION OF SYMBOLS 1... Air cleaner, 3... Air flow meter (air flow rate detection means), 5... Throttle body, 7... Internal combustion engine. 8...Intake pipe, 9...Fuel tank, 10...Fuel pump. 13... Injection valve, 15... Control unit (
electronic control circuit), 16... distributor (including rotation speed detection means), 19... water temperature sensor (temperature detection means), 2o... spark plug.

Claims (1)

【特許請求の範囲】[Claims] 1、内燃機関へ燃料を供給する噴射弁と、内燃機関への
吸入空気量を検出する空気流量検出手段と、内燃機関の
回転数を検出する回転数検出手段と、内燃機関の温度を
検出する温解検出手段と、上記各検出手段の検出信号に
基き上記噴射弁の噴射パルス幅および内燃機関の点火時
期を演算して制御する電子制御回路から構成される電子
式燃料噴射装置の加速時に点火時期を遅角させたのち除
々に進角させる内燃機関の点火時期制御方法において、
上記加速時に加速を検出したのち所定の点火回数後から
上記遅角を行うことを特徴とする内燃機関の点火時期制
御方法。
1. An injection valve that supplies fuel to the internal combustion engine, an air flow rate detection device that detects the amount of intake air to the internal combustion engine, a rotation speed detection device that detects the rotation speed of the internal combustion engine, and a temperature detection device that detects the temperature of the internal combustion engine. ignition at the time of acceleration of an electronic fuel injection device consisting of a thermal decomposition detection means and an electronic control circuit that calculates and controls the injection pulse width of the injection valve and the ignition timing of the internal combustion engine based on the detection signals of the respective detection means. In an ignition timing control method for an internal combustion engine in which the timing is retarded and then gradually advanced,
An ignition timing control method for an internal combustion engine, characterized in that the retardation is performed after a predetermined number of ignitions after detecting acceleration during the acceleration.
JP61100958A 1986-05-02 1986-05-02 Ignition timing control method for multi-cylinder internal combustion engine Expired - Fee Related JPH0684749B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61100958A JPH0684749B2 (en) 1986-05-02 1986-05-02 Ignition timing control method for multi-cylinder internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61100958A JPH0684749B2 (en) 1986-05-02 1986-05-02 Ignition timing control method for multi-cylinder internal combustion engine

Publications (2)

Publication Number Publication Date
JPS62258152A true JPS62258152A (en) 1987-11-10
JPH0684749B2 JPH0684749B2 (en) 1994-10-26

Family

ID=14287862

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61100958A Expired - Fee Related JPH0684749B2 (en) 1986-05-02 1986-05-02 Ignition timing control method for multi-cylinder internal combustion engine

Country Status (1)

Country Link
JP (1) JPH0684749B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007092579A (en) * 2005-09-28 2007-04-12 Nissan Motor Co Ltd Ignition timing control device for internal combustion engine
JP2015166558A (en) * 2014-03-03 2015-09-24 トヨタ自動車株式会社 Internal combustion engine controller

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59704A (en) * 1982-06-25 1984-01-05 Kobe Steel Ltd Position control method of robot with high accuracy

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59704A (en) * 1982-06-25 1984-01-05 Kobe Steel Ltd Position control method of robot with high accuracy

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007092579A (en) * 2005-09-28 2007-04-12 Nissan Motor Co Ltd Ignition timing control device for internal combustion engine
JP2015166558A (en) * 2014-03-03 2015-09-24 トヨタ自動車株式会社 Internal combustion engine controller

Also Published As

Publication number Publication date
JPH0684749B2 (en) 1994-10-26

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