JPH0313419B2 - - Google Patents

Info

Publication number
JPH0313419B2
JPH0313419B2 JP57190928A JP19092882A JPH0313419B2 JP H0313419 B2 JPH0313419 B2 JP H0313419B2 JP 57190928 A JP57190928 A JP 57190928A JP 19092882 A JP19092882 A JP 19092882A JP H0313419 B2 JPH0313419 B2 JP H0313419B2
Authority
JP
Japan
Prior art keywords
fuel injection
fuel
timing
engine
injection
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
Application number
JP57190928A
Other languages
Japanese (ja)
Other versions
JPS5982537A (en
Inventor
Koichi Furuta
Akio Kobayashi
Takashi Harada
Shigenori Isomura
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.)
Denso Corp
Original Assignee
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 NipponDenso Co Ltd filed Critical NipponDenso Co Ltd
Priority to JP57190928A priority Critical patent/JPS5982537A/en
Publication of JPS5982537A publication Critical patent/JPS5982537A/en
Publication of JPH0313419B2 publication Critical patent/JPH0313419B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/32Controlling fuel injection of the low pressure type
    • F02D41/34Controlling fuel injection of the low pressure type with means for controlling injection timing or duration
    • F02D41/345Controlling injection timing
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Description

【発明の詳細な説明】 本発明は内燃機関(エンジン)の電子制御式燃
料噴射装置における燃料噴射時期の制御方法に関
するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for controlling fuel injection timing in an electronically controlled fuel injection device for an internal combustion engine.

従来、例えば同期燃料噴射方式多気筒エンジン
は特定の気筒の点火時期に合わせて全気筒同時に
燃料噴射を行うようになされていた。こうした従
来の装置では、第1図タイムチヤートの第1気筒
で示すように、一般的にピストンが下死点を過ぎ
て吸気工程が終了した後でも、混合気の慣性を考
慮し気筒充填効率を上げるために、例えば下死点
から50℃A(クランク角)程過ぎた位置まで吸気
バルブを開放したままにしている。このため吸気
バルブの閉鎖直前あるいは直後に燃料の噴射が行
われると吸気バルブの閉鎖タイミングが僅かにズ
レたり、エンジン回転数の変化等によつて次の圧
縮行程によつて混合気が吸気バルブを通じて吸気
系に吹返されて燃料の気筒分配が悪化すると言う
問題があつた。
Conventionally, for example, in a synchronous fuel injection multi-cylinder engine, fuel is injected into all cylinders simultaneously in accordance with the ignition timing of a specific cylinder. In such conventional devices, as shown in the first cylinder of the time chart in Figure 1, even after the piston has passed the bottom dead center and the intake stroke has ended, the cylinder filling efficiency is generally adjusted in consideration of the inertia of the air-fuel mixture. In order to increase the engine speed, the intake valve is kept open until it is, for example, about 50 degrees Celsius (crank angle) past bottom dead center. Therefore, if fuel is injected just before or after the intake valve is closed, the timing of the intake valve's closing may be slightly off, or due to changes in engine speed, the air-fuel mixture may pass through the intake valve during the next compression stroke. There was a problem that fuel was blown back into the intake system, worsening the distribution of fuel into the cylinders.

そこで、こうした燃料の吹返しを防止するため
に、燃料噴射時期を正確に制御する必要がある。
こうした場合の従来の対策としては、例えば特開
昭57−2431号公報記載の様に、精度よくクランク
角を検出し、これに基づいて燃料噴射時期を決定
するという方法が採用されていた。このため、高
価なクランク角センサを必要としたり、高速処理
能力が要求されるという問題があつた。
Therefore, in order to prevent such fuel blowback, it is necessary to accurately control the fuel injection timing.
As a conventional countermeasure in such a case, a method has been adopted in which the crank angle is accurately detected and the fuel injection timing is determined based on this, as described in, for example, Japanese Patent Laid-Open No. 57-2431. Therefore, there are problems in that an expensive crank angle sensor is required and high-speed processing capability is required.

本発明は上記点に鑑みなされたもので混合気の
吹返しによる燃料の気筒分配の悪化を防止し、ま
た、排気ガス中の有害HC及びCO成分の排出量を
抑制すると共に、燃料効率の向上等を実現する燃
料噴射時期の制御方法を提供することを目的とし
ている。
The present invention has been developed in view of the above points, and prevents the deterioration of fuel distribution into cylinders due to air-fuel mixture blowback, suppresses the amount of harmful HC and CO components in exhaust gas, and improves fuel efficiency. The purpose of the present invention is to provide a fuel injection timing control method that achieves the following.

また、この様な目的を達成する上で、高価なク
ランク角センサや高速処理能力を必要としない簡
便な方法の提供をも目的としている。
Another object of the present invention is to provide a simple method that does not require an expensive crank angle sensor or high-speed processing capability to achieve this purpose.

かかる目的は、エンジンの負荷に基づいて燃料
の基本噴射時間を求めた後、該基本噴射時間をエ
ンジンの運転状態に応じて補正して最終噴射時間
を決定し、多気筒エンジンの各気筒毎に備えた燃
料噴射弁から全気筒一斉に燃料を噴射する全気筒
同時噴射方式の内燃機関の燃料噴射装置における
燃料噴射時期の制御方法において、燃料噴射開始
時期を、気筒の吸気バルブ閉鎖時期の直前または
直後に燃料の噴射期間が重複しないように考慮し
て、点火時期からの最適な遅延時間にて表し、該
遅延時間をエンジンの運転状態に対応させたマツ
プデータとしてメモリ内に予め格納し、点火時期
を検知した後、前記マツプデータに基づく遅延時
間の経過を待つてから全気筒一斉に燃料の噴射を
開始することを特徴とする燃料噴射時期の制御方
法によつて達成される。
This purpose is to determine the basic injection time of fuel based on the engine load, then correct the basic injection time according to the engine operating condition to determine the final injection time, and then calculate the final injection time for each cylinder of a multi-cylinder engine. In a method for controlling fuel injection timing in a fuel injection system for an internal combustion engine with an all-cylinder simultaneous injection method in which fuel is injected simultaneously from all cylinders from fuel injection valves equipped with the fuel injection valve, the fuel injection start timing is set to immediately before the intake valve closing timing of the cylinder or Taking into account that the fuel injection period does not overlap immediately after, it is expressed as an optimal delay time from the ignition timing, and the delay time is stored in advance in memory as map data that corresponds to the engine operating state, and the ignition timing is This is achieved by a fuel injection timing control method characterized in that, after detecting , the fuel injection timing is started in all cylinders simultaneously after waiting for the elapse of a delay time based on the map data.

以下、図面に基づいて本発明の実施例について
説明する。
Embodiments of the present invention will be described below based on the drawings.

第2図は本発明方法が適用された毎回転全気筒
同時同期噴射方式の燃料噴射装置の電子制御回路
のブロツク図で、マイクロコンピユータ1にはデ
イストリビユータ2からの点火信号F、エアフロ
メータ3からの吸入空気量信号Qが入力されると
共に、水温センサ等の各種センサ4からA/D変
換器5を介して補正信号Cが入力され、更に、前
記点火信号Fよりエンジン回転数Nを算出すると
共に吸入空気量信号Qで表わされる吸入空気量を
エンジン回転数で除したエンジン負荷を示す値に
基づいて基本噴射時間Tpを演算するアナログ演
算回路6から、該基本噴射時間Tpを表わす信号
と、エンジン回転数Nを表わす信号が入力されて
いる。そして、マイクロコンピユータ1は入力さ
れた前記基本噴射時間Tpに対して各種センサ4
からの補正信号に応じて補正を加えて最終噴射時
間Tiとして内蔵のメモリに記憶するようになさ
れている。
FIG. 2 is a block diagram of an electronic control circuit of a fuel injection system for simultaneous synchronous injection of all cylinders at every revolution to which the method of the present invention is applied. An intake air amount signal Q is inputted from the engine, and a correction signal C is inputted from various sensors 4 such as a water temperature sensor via an A/D converter 5. Furthermore, the engine rotation speed N is calculated from the ignition signal F. At the same time, a signal representing the basic injection time Tp is generated from an analog calculation circuit 6 that calculates the basic injection time Tp based on a value indicating the engine load obtained by dividing the intake air amount represented by the intake air amount signal Q by the engine rotation speed. , a signal representing the engine rotational speed N is input. Then, the microcomputer 1 uses various sensors 4 for the input basic injection time Tp.
The final injection time Ti is stored in the built-in memory after being corrected in accordance with the correction signal from the final injection time Ti.

前記マイクロコンピユータ1の出力側には図示
せぬプリツセツトダウンカウンタ、タイヤ等が備
えられ、タイマの出力はトランジスタ等のドライ
ブ回路7を介してインジエクタ8に接続され、該
インジエクタ8はマイクロコンピユータ1が出力
する最終噴射時間Tiだけ駆動開弁されて燃料噴
射が行われる。
The output side of the microcomputer 1 is equipped with a preset down counter, tires, etc. (not shown), and the output of the timer is connected to an injector 8 via a drive circuit 7 such as a transistor. The valve is driven open for the final injection time Ti to be output, and fuel injection is performed.

また、マイクロコンピユータ1内の不揮発性の
メモリには第3図に示すように、点火時期から噴
射開始時期までの最適な遅延時間tのデータが、
例えば吸入空気量Q1、エンジン回転数N1なるエ
ンジンの運転状態に対応して遅延時間t1がマツプ
データとして格納され、また第4図のフローチヤ
ートに示す如き制御プログラムが格納されてい
る。
In addition, as shown in FIG. 3, the non-volatile memory in the microcomputer 1 stores data on the optimal delay time t from the ignition timing to the injection start timing.
For example, a delay time t 1 is stored as map data corresponding to the operating state of the engine, such as intake air amount Q 1 and engine speed N 1 , and a control program as shown in the flowchart of FIG. 4 is also stored.

即ち、点火時期は、エンジン負荷を表がす値
Q、N等によつてBTDC0゜〜30℃Aの範囲で常に
変化することから、前記遅延時間tは点火時期補
正時間分を予め考慮し、噴射開始時期の遅延によ
つていずれかの気筒の吸気行程下死点から例えば
60℃A以内で、つまり吸気バルブ閉鎖の前後の位
置で燃料の噴射が行われる事のないような値とさ
れている。
That is, since the ignition timing always changes within the range of 0° to 30°C BTDC depending on the values Q, N, etc. representing the engine load, the delay time t takes into account the ignition timing correction time in advance, For example, due to the delay in the injection start timing, from the bottom dead center of the intake stroke of any cylinder.
This value is set to within 60℃, which means that fuel injection will not occur before or after the intake valve is closed.

尚、遅延時間tは吸入空気量Qの代わりにエン
ジンの運転状態を表わす吸気管圧力Pを用いたマ
ツプデータとしても良く、そして、点火時期が冷
却水温で変化するような構成の場合は、エンジン
回転数N、吸入空気量Qまたは吸気管圧力Pと水
温センサからの信号との三次元マツプデータとす
ることもできる。
Note that the delay time t may be map data using the intake pipe pressure P, which represents the engine operating state, instead of the intake air amount Q, and in the case of a configuration in which the ignition timing changes depending on the cooling water temperature, the engine rotation It may also be three-dimensional map data of the number N, intake air amount Q or intake pipe pressure P, and a signal from a water temperature sensor.

この様に構成された燃料噴射装置は第4図フロ
ーチヤートに沿つて以下の様に作動する。
The fuel injection device constructed in this manner operates as follows according to the flowchart in FIG.

まず、図示せぬスタータスイツチがオンされる
とマイクロコンピユータ1の所定のイニシアル処
理が行われた後に点火信号等の所定のタイミング
で本ルーチンの処理が始まり、ステツプ20に示す
如く各センサ等から点火信号F、吸入空気量Q、
エンジン回転数N、水温等の補正用データが入力
され、次ステツプに移行する。
First, when a starter switch (not shown) is turned on, the microcomputer 1 performs a predetermined initial process, and then the process of this routine starts at a predetermined timing such as an ignition signal, and as shown in step 20, ignition is started from each sensor, etc. Signal F, intake air amount Q,
Correction data such as engine speed N and water temperature are input, and the process moves to the next step.

次ステツプ30では前ステツプで入力されてエン
ジン回転数N、吸入空気量Qより第3図マツプデ
ータ上の遅延時間tが検索される。
In the next step 30, the delay time t on the map data in FIG. 3 is retrieved from the engine speed N and intake air amount Q input in the previous step.

次のステツプ40ではアナログ演算器6にて演算
された基本噴射時間Tpが読込まれ、次ステツプ
50に進む。
In the next step 40, the basic injection time Tp calculated by the analog calculator 6 is read, and the next step is started.
Go to 50.

ステツプ50では、水温等の補正用データに基づ
いて前記基本噴射時間Tpを補正し最終噴射時間
Tiを求める。
In step 50, the basic injection time Tp is corrected based on correction data such as water temperature, and the final injection time is determined.
Find Ti.

そして、次のステツプ60にて前述ステツプ30で
検索された遅延時間tに対応するデジタル値がプ
リセツトダウンカウンタにセツトされ、次ステツ
プ70に移行する。
Then, in the next step 60, the digital value corresponding to the delay time t retrieved in the step 30 is set in the preset down counter, and the process proceeds to the next step 70.

次ステツプ70では、前記ステツプ50で演算され
た最終噴射時間Tiがタイマにセツトされ、本ル
ーチンの処理を終える。
In the next step 70, the final injection time Ti calculated in the step 50 is set in a timer, and the processing of this routine ends.

この様に処理されることによつてカウンタにセ
ツトされた遅延時間tに対応するデジタル値がマ
イクロコンピユータ1の基準クロツク信号等によ
りダウンカウントされ、カウンタ内容が「0」と
なつた時に、タイマにセツトされた最終噴射時間
Tiだけインジエクタ8が駆動、開弁されて、燃
料が噴射される。
Through this processing, the digital value corresponding to the delay time t set in the counter is counted down by the reference clock signal of the microcomputer 1, etc., and when the counter content reaches "0", the timer is Final injection time set
The injector 8 is driven and opened only by Ti, and fuel is injected.

上述の動作を第2図及び第5図のタイムチヤー
トに沿つて更に説明すると、従来、第1図に示す
如く第3気筒の吸気工程の終了する下死点付近で
噴射されていた燃料は、本実施例においては吸入
空気量がQ1、エンジン回転数がN1の場合第5図
タイムチヤートで示す如く、遅延時間がt1とさ
れ、第1〜第3気筒の吸気バルブが閉鎖されてい
るタイミングであつて、第4気筒の吸気工程の中
程で噴射されることになり、混合気の吹返しによ
る燃料の気筒分配の悪化が抑制されることとな
る。
To further explain the above-mentioned operation along the time charts of FIGS. 2 and 5, the fuel that was conventionally injected near the bottom dead center at the end of the intake stroke of the third cylinder as shown in FIG. In this embodiment, when the intake air amount is Q 1 and the engine speed is N 1 , the delay time is set to t 1 and the intake valves of the first to third cylinders are closed, as shown in the time chart of Fig. 5. The fuel is injected in the middle of the intake stroke of the fourth cylinder, and deterioration in the cylinder distribution of fuel due to blowback of the air-fuel mixture is suppressed.

以上詳述したように、本発明方法は点火時期か
ら噴射開始時期までの最適な遅延時間をマイクロ
コンピユータのメモリ内に予め格納されたマツプ
形式データに基づいて燃料噴射開始時期を決定す
る燃料噴射時期の制御方法であり、これによつて
エンジンの運転状態の変化に応じて常に予め設定
した最適な時期に燃料噴射ができることから、吸
気バルブの閉鎖直前、直後に燃料噴射をすること
がなくなり、従つて燃料の気筒分配の悪化を防止
できる効果がある。
As described in detail above, the method of the present invention determines the fuel injection start timing based on the map format data pre-stored in the memory of the microcomputer to determine the optimal delay time from the ignition timing to the injection start timing. This is a control method that allows fuel injection to always be performed at the optimal timing set in advance according to changes in engine operating conditions, eliminating the need to inject fuel just before or after the intake valve closes. This has the effect of preventing deterioration of fuel distribution into cylinders.

また、マイクロコンピユータに入力する信号は
エンジン回転数と吸入空気量だけで良く、他の例
えばクランクアングルセンサ等の特別なセンサを
用いることなく目的を達成できる効果がある。
Furthermore, the only signals input to the microcomputer are the engine speed and intake air amount, which has the effect of achieving the objective without using any other special sensors, such as a crank angle sensor.

更に、噴射時期の制御が可能となることで燃焼
変動によるエミツシヨン悪化を防止できる効果が
ある。
Furthermore, since the injection timing can be controlled, deterioration in emissions due to combustion fluctuations can be prevented.

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

第1図は従来の燃料噴射時期制御方法による動
作を説明するタイムチヤート、第2図は本発明方
法が適用された実施例の電子制御回路のブロツク
図、第3図はマツプデータの模式図、第4図は制
御プログラムを示すフローチヤート、第5図は本
実施例の動作を説明するタイムチヤートを表わし
ている。 1……マイクロコンピユータ、2……デイスト
リビユータ、3……エアフロメータ、4……各種
センサ、6……アナログ演算回路、8……インジ
エクタ。
FIG. 1 is a time chart explaining the operation according to the conventional fuel injection timing control method, FIG. 2 is a block diagram of an electronic control circuit of an embodiment to which the method of the present invention is applied, and FIG. 3 is a schematic diagram of map data. FIG. 4 is a flowchart showing the control program, and FIG. 5 is a time chart explaining the operation of this embodiment. 1... Microcomputer, 2... Distributor, 3... Air flow meter, 4... Various sensors, 6... Analog calculation circuit, 8... Injector.

Claims (1)

【特許請求の範囲】 1 エンジンの負荷に基づいて燃料の基本噴射時
間を求めた後、該基本噴射時間をエンジンの運転
状態に応じて補正して最終噴射時間を決定し、多
気筒エンジンの各気筒毎に備えた燃料噴射弁から
全気筒一斉に燃料を噴射する全気筒同時噴射方式
の内燃機関の燃料噴射装置における燃料噴射時期
の制御方法において、 燃料噴射開始時期を、気筒の吸気バルブ閉鎖時
期の直前または直後に燃料の噴射期間が重複しな
いように考慮して、点火時期からの最適な遅延時
間にて表し、 該遅延時間をエンジンの運転状態に対応させた
マツプデータとしてメモリ内に予め格納し、 点火時期を検知した後、前記マツプデータに基
づく遅延時間の経過を待つてから全気筒一斉に燃
料の噴射を開始することを特徴とする燃料噴射時
期の制御方法。
[Scope of Claims] 1. After determining the basic injection time of fuel based on the engine load, the final injection time is determined by correcting the basic injection time according to the operating condition of the engine. In a method for controlling fuel injection timing in a fuel injection system for an internal combustion engine with an all-cylinder simultaneous injection method in which fuel is injected simultaneously from a fuel injection valve provided in each cylinder to all cylinders, the fuel injection start timing is set to the intake valve closing timing of each cylinder. The fuel injection period is expressed as an optimal delay time from the ignition timing, taking into account that the fuel injection period does not overlap immediately before or after the engine, and the delay time is stored in advance in the memory as map data that corresponds to the engine operating state. . A method for controlling fuel injection timing, characterized in that after detecting the ignition timing, fuel injection is started in all cylinders at once after waiting for a delay time based on the map data to elapse.
JP57190928A 1982-10-30 1982-10-30 Control of fuel injection timing Granted JPS5982537A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57190928A JPS5982537A (en) 1982-10-30 1982-10-30 Control of fuel injection timing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57190928A JPS5982537A (en) 1982-10-30 1982-10-30 Control of fuel injection timing

Publications (2)

Publication Number Publication Date
JPS5982537A JPS5982537A (en) 1984-05-12
JPH0313419B2 true JPH0313419B2 (en) 1991-02-22

Family

ID=16266015

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57190928A Granted JPS5982537A (en) 1982-10-30 1982-10-30 Control of fuel injection timing

Country Status (1)

Country Link
JP (1) JPS5982537A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014220953A1 (en) * 2014-10-16 2016-04-21 Robert Bosch Gmbh Electrode for a combination of supercapacitor and battery and process for their preparation
DE102014224856A1 (en) * 2014-12-04 2016-06-09 Robert Bosch Gmbh Electrode with active material mixture and process for its preparation

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5519933A (en) * 1978-07-26 1980-02-13 Hitachi Ltd Fuel injection system in gasoline engine
JPS5650228A (en) * 1979-09-28 1981-05-07 Isuzu Motors Ltd Electronic controlling device for fuel injection timing
JPS572431A (en) * 1980-06-06 1982-01-07 Nissan Motor Co Ltd Electronically controlled fuel injection device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5519933A (en) * 1978-07-26 1980-02-13 Hitachi Ltd Fuel injection system in gasoline engine
JPS5650228A (en) * 1979-09-28 1981-05-07 Isuzu Motors Ltd Electronic controlling device for fuel injection timing
JPS572431A (en) * 1980-06-06 1982-01-07 Nissan Motor Co Ltd Electronically controlled fuel injection device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014220953A1 (en) * 2014-10-16 2016-04-21 Robert Bosch Gmbh Electrode for a combination of supercapacitor and battery and process for their preparation
DE102014224856A1 (en) * 2014-12-04 2016-06-09 Robert Bosch Gmbh Electrode with active material mixture and process for its preparation

Also Published As

Publication number Publication date
JPS5982537A (en) 1984-05-12

Similar Documents

Publication Publication Date Title
US4479186A (en) Method and apparatus for controlling an internal combustion engine
US4257377A (en) Engine control system
US4442812A (en) Method and apparatus for controlling internal combustion engines
US4242728A (en) Input/output electronic for microprocessor-based engine control system
JP2577210B2 (en) Electronically controlled fuel injection device for internal combustion engine
JPS6347893B2 (en)
JPS6214704B2 (en)
JPH0517390B2 (en)
JPS6256342B2 (en)
JPH0723582Y2 (en) Ignition timing control device for internal combustion engine
US4706196A (en) Apparatus and method for injecting fuel into engine according to group injection system
JPS6138139A (en) Fuel injection control device in internal-combustion engine
JPH0515908B2 (en)
JPH0313419B2 (en)
US5093793A (en) Method of transferring signals within electronic control system for internal combustion engines
JPS59120779A (en) Ignition timing control circuit of internal-combustion engine
JP3295150B2 (en) Basic fuel injection method
JPH0246777B2 (en)
JPS5968530A (en) Control method of internal-combustion engine
JP3078008B2 (en) Engine fuel control device
JPS6165037A (en) Air-fuel ratio control system for internal-combustion engine
JPS63173826A (en) Fuel injection method for internal combustion engine
JPH0629587B2 (en) Fuel supply control device for internal combustion engine
JPH0792007B2 (en) Electronically controlled fuel injection type internal combustion engine interrupt injection control device
JP2590942B2 (en) Fuel injection amount control method for internal combustion engine