JPH0792006B2 - Electronically controlled fuel injection device for internal combustion engine - Google Patents

Electronically controlled fuel injection device for internal combustion engine

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Publication number
JPH0792006B2
JPH0792006B2 JP23809586A JP23809586A JPH0792006B2 JP H0792006 B2 JPH0792006 B2 JP H0792006B2 JP 23809586 A JP23809586 A JP 23809586A JP 23809586 A JP23809586 A JP 23809586A JP H0792006 B2 JPH0792006 B2 JP H0792006B2
Authority
JP
Japan
Prior art keywords
air flow
flow rate
intake air
fuel injection
throttle valve
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
JP23809586A
Other languages
Japanese (ja)
Other versions
JPS6394045A (en
Inventor
正信 大崎
隆生 野口
Original Assignee
株式会社ユニシアジェックス
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Publication date
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Priority to JP23809586A priority Critical patent/JPH0792006B2/en
Publication of JPS6394045A publication Critical patent/JPS6394045A/en
Publication of JPH0792006B2 publication Critical patent/JPH0792006B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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電子制御燃料噴射装置に関し、特に
加速運転時の改善に関する。
Description: TECHNICAL FIELD The present invention relates to an electronically controlled fuel injection device for an internal combustion engine, and more particularly to improvement during acceleration operation.

〈従来の技術〉 内燃機関の電子制御燃料噴射装置の従来例として以下の
ようなものがある(実願昭60−066558号参照)。
<Prior Art> The following is a conventional example of an electronically controlled fuel injection device for an internal combustion engine (see Japanese Utility Model Application No. 60-066558).

すなわち、エアフローメータにより検出された吸入空気
流量Qと機関回転速度Nとから基本噴射量Tp=K×Q/N
(Kは定数)を演算すると共に、主として水温に応じた
各種補正係数COEFと空燃比フィードバック補正係数αと
バッテリ電圧による補正係数Tsとを演算した後、定常運
転時における燃料噴射量Ti=Tp×COEF×α+Tsを演算す
る。
That is, the basic injection amount Tp = K × Q / N from the intake air flow rate Q detected by the air flow meter and the engine rotation speed N.
(K is a constant) and at the same time, after calculating various correction coefficients COEF mainly according to the water temperature, the air-fuel ratio feedback correction coefficient α and the correction coefficient Ts based on the battery voltage, the fuel injection amount Ti = Tp × during steady operation Calculate COEF x α + Ts.

そして、例えばシングルポイントインジェクションシス
テム(以下SPI方式)では、機関の1/2回転毎に点火信号
等に同期して燃料噴射弁に対し前記燃料噴射量Tiに対応
するパルス巾の噴射パルス信号を出力し機関に燃料を供
給する。
Then, for example, in a single point injection system (hereinafter referred to as SPI method), an injection pulse signal having a pulse width corresponding to the fuel injection amount Ti is output to the fuel injection valve in synchronization with an ignition signal or the like every 1/2 revolution of the engine. Supply fuel to the engine.

さらに加速運転時には吸気絞弁開度の変化率等から加速
時増量噴射量を算出し該増量噴射量を前記燃料噴射量Ti
に加算することにより、燃料の加速時増量を図り機関出
力を増大させる。
Further, during acceleration operation, the increased injection amount during acceleration is calculated from the rate of change of the intake throttle opening, and the increased injection amount is calculated as the fuel injection amount Ti.
To increase the fuel output during acceleration and increase the engine output.

加速時増量は通常の噴射パルス信号の間に加速時の噴射
パルスを割り込ませて行う割込み噴射によっても行われ
る。
The acceleration increase is also performed by interrupt injection performed by interrupting the injection pulse during acceleration during the normal injection pulse signal.

〈発明が解決しようとする問題点〉 しかしながら、このような従来の電子制御燃料噴射装置
においては、機関吸気通路に介装されたエアフローメー
タにより検出された吸入空気流量に基づいて燃料噴射量
を演算するため、特に加速運転時に不具合があった。
<Problems to be Solved by the Invention> However, in such a conventional electronically controlled fuel injection device, the fuel injection amount is calculated based on the intake air flow rate detected by the air flow meter interposed in the engine intake passage. Therefore, there was a problem especially during acceleration operation.

すなわち、スロットル弁が開弁動作している期間(第4
図中t1)では、応答遅れによりエアフローメータにより
検出された吸入空気流量(第4図中実線示,以下エアフ
ロ吸入空気流量と呼ぶ)は機関に供給される真の吸入空
気流量(第4図中破線示)よりも低くなる。
That is, the period during which the throttle valve is operating (4th
At t 1 ) in the figure, the intake air flow rate detected by the air flow meter due to the response delay (shown by the solid line in FIG. 4, hereinafter referred to as the airflow intake air flow rate) is the true intake air flow rate supplied to the engine (see FIG. 4). It is lower than the middle dashed line).

また、スロットル弁の開弁動作が終了した直後には、オ
ーバシュートによりエアフロ吸入空気流量が真の吸入空
気流量を大巾に超え、その後アンダシュートによりエア
フロ吸入空気流量が真の吸入空気流量よりも大巾に低下
する。そして、その後エアフロ吸入空気流量は真の吸入
空気流量に近づくようになる。かかる現象は吸気通路に
板状のフラップを設けて吸入空気流量を検出するフラッ
プ式エアフローメータではフラップの慣性力により顕著
になっていた。
Immediately after the opening operation of the throttle valve is finished, the airflow intake air flow rate greatly exceeds the true intake air flow rate due to the overshoot, and the airflow intake air flow rate is later than the true intake air flow rate due to the undershoot. It drops significantly. Then, thereafter, the airflow intake air flow rate comes close to the true intake air flow rate. In a flap type air flow meter in which a plate-like flap is provided in the intake passage to detect the intake air flow rate, such a phenomenon has become remarkable due to the inertial force of the flap.

これにより、空燃比が適正値になるようにエアフロ吸入
空気流量に基づいて演算された燃料噴射量から燃料を機
関に供給すると、その燃料噴射量が真の吸入空気流量に
対応しなくなり実際の空燃比が適正値から大きくずれ
る。このため、エアフロ吸入空気流量が真の吸入空気流
量を超えるオーバシュート期間(第4図中t2)では実際
の空燃比がリッチ化しまたスロットル弁の開弁動作中に
期間(第4図中t1)とエアフロ吸入空気流量が真の吸入
空気流量より低下するアンダシュート期間(第4図中
t3)とでは実際の空燃比がリーン化しヘージテーション
の発生を招くという不具合がある。
As a result, when fuel is supplied to the engine from the fuel injection amount calculated based on the air flow intake air flow rate so that the air-fuel ratio becomes an appropriate value, the fuel injection amount does not correspond to the true intake air flow rate The fuel ratio deviates greatly from the proper value. Therefore, the actual air-fuel ratio becomes rich during the overshoot period (t 2 in FIG. 4) in which the air flow intake air flow rate exceeds the true intake air flow rate, and the period during the opening operation of the throttle valve (t in FIG. 4) is increased. 1 ) and the underflow period during which the airflow intake air flow rate falls below the true intake air flow rate (in Fig. 4
With t 3 ), there is a problem that the actual air-fuel ratio becomes lean and hazing occurs.

本発明は、このような実状に鑑みてなされたもので、実
際の空燃比の最適に制御できる電子制御燃料噴射装置を
提供することを目的とする。
The present invention has been made in view of such a situation, and an object thereof is to provide an electronically controlled fuel injection device capable of optimally controlling an actual air-fuel ratio.

〈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Aの吸入
空気流量を直接検出する吸入空気流量検出手段Bと、ス
ロットル弁の開度を検出するスロットル弁開度検出手段
Cと、機関回転速度を検出する回転速度検出手段Dと、
検出されたスロットル弁開度と機関回転速度とに基づい
て吸入空気流量を設定する吸入空気流量設定手段Eと、
前記検出されたスロットル弁の開度に基づいて開弁速度
を演算する開弁速度検算手段Fと、該演算された開弁速
度に基づいてスロットル弁の加速動作終了時を判定する
加速動作終了時判定手段Gと、加速動作終了時を判定さ
れたときから設定時間の間、前記設定された吸入空気流
量を選択する一方、前記設定時間経過後は吸入空気流量
検出手段Bにより検出された吸入空気流量を選択する選
択手段Hと、選択された吸入空気流量に基づいて燃料噴
射量を演算する燃料噴射量演算手段Iと、演算された燃
料噴射量に対応する噴射パルス信号を燃料噴射弁Jに出
力する駆動パルス出力手段Kと、を備えるようにした。
<Means for Solving Problems> Therefore, according to the present invention, as shown in FIG. 1, the intake air flow rate detecting means B for directly detecting the intake air flow rate of the engine A and the opening degree of the throttle valve are detected. Throttle valve opening detection means C, rotation speed detection means D for detecting engine rotation speed,
Intake air flow rate setting means E for setting an intake air flow rate based on the detected throttle valve opening degree and engine rotation speed,
A valve opening speed calculation means F for calculating the valve opening speed on the basis of the detected opening degree of the throttle valve, and an acceleration operation ending time for judging the ending time of the acceleration operation of the throttle valve based on the calculated valve opening speed. The determination unit G selects the set intake air flow rate for a set time from when the end of the acceleration operation is determined, while the intake air detected by the intake air flow rate detection unit B after the set time elapses. A selection means H for selecting a flow rate, a fuel injection amount calculation means I for calculating a fuel injection amount based on the selected intake air flow rate, and an injection pulse signal corresponding to the calculated fuel injection amount to a fuel injection valve J. The driving pulse output means K for outputting is provided.

〈作用〉 このようにして、加速動作終了時から設定時間の間は真
の吸入空気流量に対応するスロットル弁の開度に基づく
吸入空気流量によって燃料噴射量を設定し、もって実際
の空燃比を最適にするようにした。
<Operation> In this way, during the set time from the end of the acceleration operation, the fuel injection amount is set by the intake air flow rate based on the opening degree of the throttle valve corresponding to the true intake air flow rate, and thus the actual air-fuel ratio is set. I tried to optimize it.

〈実施例〉 以下に、本発明の一実施例を第2図及び第3図に基づい
て説明する。
<Embodiment> An embodiment of the present invention will be described below with reference to FIGS. 2 and 3.

図において例えばマイクロコンピュータからなる制御装
置1には、回転速度検出手段としての回転速度センサ2
により検出される回転速度N信号、吸入空気流量検出手
段としてのエアフローメータ3により検出されたエアフ
ロ吸入空気流量QA信号,スロットル弁開度検出手段とし
てのスロットル弁開度センサ4により検出されたスロッ
トル弁開度α信号,水温センサ5により検出された冷却
水温度Tw信号と、が入力されている。
In the figure, a control device 1 including, for example, a microcomputer includes a rotation speed sensor 2 as a rotation speed detection unit
Rotational speed N signal detected by, the air flow intake air flow rate Q A signal detected by the air flow meter 3 as the intake air flow rate detecting means, throttle detected by the throttle valve opening sensor 4 as the throttle valve opening detecting means The valve opening α signal and the cooling water temperature Tw signal detected by the water temperature sensor 5 are input.

制御装置1は第3図に示すフローチャートに従って作動
し、燃料噴射弁6に駆動回路7を介して駆動パルス信号
を出力する。
The control device 1 operates according to the flowchart shown in FIG. 3, and outputs a drive pulse signal to the fuel injection valve 6 via the drive circuit 7.

ここでは、制御装置1が吸入空気流量演算手段と開弁速
度検出手段と加速動作終了時判定手段と比較手段とを構
成する。また、制御装置1と駆動回路6とにより駆動パ
ルス出力手段を構成する。
Here, the control device 1 constitutes intake air flow rate calculation means, valve opening speed detection means, acceleration operation end time determination means, and comparison means. Further, the control device 1 and the drive circuit 6 constitute a drive pulse output means.

次に作用を第3図のフローチャートに従って説明する。Next, the operation will be described with reference to the flowchart of FIG.

S1では、検出された回転速度N,エアフロ吸入空気流量
QA,スロットル弁開度α等の各種信号を読込む。
In S1, the detected rotational speed N and air flow intake air flow rate
Read various signals such as Q A and throttle valve opening α.

S2では、検出されたスロットル弁開度からスロットル弁
の開弁速度Δαを演算する。
In S2, the valve opening speed Δα of the throttle valve is calculated from the detected throttle valve opening.

S3では検出されたスロットル弁開弁α及び機関回転速度
Nとに基づきROMに記憶された吸入空気流量の3次元マ
ップテーブルから当該運転領域に対応する吸入空気流量
Qα(以下、検索吸入空気流量Qαと呼ぶ)を検索す
る。
In S3, based on the detected throttle valve opening α and the engine speed N, the intake air flow rate Qα (hereinafter, the search intake air flow rate Qα) corresponding to the operating region is calculated from the intake air flow rate three-dimensional map table stored in the ROM. Search).

S4では、演算された開弁速度Δαからスロットル弁の開
弁動作中か否かを判定し、YESのとき(Δα>0)には
加速動作中と判定しS5に進みNOのとき(Δα=0)には
S7に進む。
In S4, it is determined from the calculated valve opening speed Δα whether or not the throttle valve opening operation is in progress. If YES (Δα> 0), it is determined that acceleration operation is in progress, and the process proceeds to S5 and NO (Δα = 0)
Go to S7.

S5ではスロットル弁の開弁動作中であることをフラッグ
=1としてRAMに記憶し、S6に進む。また、フラッグ=
0はスロットル弁の開弁速度Δα=0の状態を示す。
At S5, the fact that the throttle valve is being opened is stored in the RAM as flag = 1, and the process proceeds to S6. Also, the flag =
0 indicates a state where the throttle valve opening speed Δα = 0.

S6では、エアフローメータ3により直接検出されたエア
フロ吸入空気流量QAと前記検索吸入空気流量Qαとを比
較し、QA≧Qαのときには後述のS16に進みQA<Qαの
ときには後述するS15に進む。
In S6, to step S15 to compare directly detected airflow intake air flow rate Q A and the search intake air flow rate Qa by the air flow meter 3, when the Q A ≧ Qa to be described later when Q A <Qa proceeds to S16 described later move on.

S7では、RAMに記憶されているフラッグを判定し、フラ
ッグ=1のときにはスロットル弁の加速動作が終了した
と判定しS8に進みフラッグ=0のときには継続して定常
運転状態と判定しS9に進む。
In S7, the flag stored in the RAM is determined. When the flag = 1, it is determined that the acceleration operation of the throttle valve has ended, and the process proceeds to S8. When the flag = 0, it is continuously determined to be the steady operation state, and the process proceeds to S9. .

S8では第1タイマをリセットして新たにカウントを開始
させた後S9に進む。
In S8, the first timer is reset to newly start counting, and then the process proceeds to S9.

S9では、フラッグ=0をRAMに記憶させた後S10に進む。In S9, the flag = 0 is stored in the RAM, and then the process proceeds to S10.

S10では第1タイマのカウント時間TM1と制御ディレー設
定時間Acc1とを比較し、TM1≧Acc1のときにはS16に進み
TM1<Acc1のときにはS11に進む。ここで、前記ディレー
設定時間Acc1は第4図に示すようにスロットル弁の開弁
動作終了時からエアフロ吸入空気流量QAと検索吸入空気
流量Qαとが略同様になるときまでの時間より大き目に
設定されている。
In S10, the count time T M1 of the first timer is compared with the control delay setting time Acc 1, and when T M1 ≧ Acc 1 , the process proceeds to S16.
When T M1 <Acc 1 , proceed to S11. Here, the delay setting time Acc 1 is larger than the time from the end of the opening operation of the throttle valve to the time when the air flow intake air flow rate Q A and the search intake air flow rate Q α become substantially the same as shown in FIG. Is set to.

S11では、エアフロ吸入空気流量QAが検索吸入空気流量
Qα未満になったか否かを判定し、YESのときにはS12に
進みNOのときにはS13に進む。
In S11, it is determined whether or not the air flow intake air flow rate Q A has become less than the search intake air flow rate Qα. If YES, the process proceeds to S12, and if NO, the process proceeds to S13.

S12では第2タイマのカウント値をリセットし初期値に
戻した後S13では第2タイマのカウント値TM2に+1を加
算しS14に進む。
In S12, the count value of the second timer is reset and returned to the initial value, and in S13, +1 is added to the count value T M2 of the second timer and the process proceeds to S14.

S14では、第2タイマのカウント時間TM2と制御時間Acc2
とを比較し、TM2≧Acc2のときにはS16に進みTM2<Acc2
のときにはS15に進む。ここで、前記制御時間Acc2はエ
アフロ吸入空気流量QAが検索吸入空気流量Qαを下回っ
たときからそれらが同様な値になるまでの時間より大き
目に設定されている。
In S14, the count time T M2 of the second timer and the control time Acc 2
And T M2 ≧ Acc 2 , proceed to S16 and T M2 <Acc 2
If so, proceed to S15. Here, the control time Acc 2 is set to be larger than the time from when the air flow intake air flow rate Q A becomes less than the search intake air flow rate Q α until they become similar values.

S15では、検索吸入空気流量Qαと回転速度Nとに基づ
いて基本噴射量Tp(=K.Qα/N,Kは定数)を演算する。
In S15, the basic injection amount Tp (= K.Qα / N, K is a constant) is calculated based on the retrieved intake air flow rate Qα and the rotation speed N.

S16では、エアフロ吸入空気流量QAと回転速度Nとに基
づいて基本噴射量Tp(=K.QA/N)を演算する。
In S16, the basic injection amount Tp (= KQ A / N) is calculated based on the air flow intake air flow rate Q A and the rotation speed N.

S17では最終的な燃料噴射量Tiを従来例と同様に演算す
る。
In S17, the final fuel injection amount Ti is calculated as in the conventional example.

S18では、S17で演算されたTiに相当するパルス幅をもつ
噴射パルス信号を駆動回路6を介して燃料噴射弁7に出
力する。
In S18, an injection pulse signal having a pulse width corresponding to Ti calculated in S17 is output to the fuel injection valve 7 via the drive circuit 6.

このようにすると、加速動作終了時から制御ディレー設
定時間Acc1が経過するまで或いは制御Acc2が経過するま
では検索吸入空気流量Qαに基づいて燃料噴射量Tiが演
算される。これによりエアフロ吸入空気流量QAが機関に
実際に吸入される真の吸入空気流量と異なる期間(第4
図中t2,t3)では真の吸入空気流量に対応する検索吸入
空気流量Qαによって燃料噴射が行われるので、実際の
空燃比を適正値にできるため、ヘージテーションの発生
を防止できる。
In this way, the fuel injection amount Ti is calculated based on the search intake air flow rate Qα from the end of the acceleration operation until the control delay setting time Acc 1 or the control Acc 2 elapses. As a result, the period when the air flow intake air flow rate Q A is different from the true intake air flow rate actually sucked into the engine (4th
At t 2 , t 3 ) in the figure, the fuel injection is performed at the search intake air flow rate Qα corresponding to the true intake air flow rate, so that the actual air-fuel ratio can be set to an appropriate value, so that generation of hazing can be prevented.

また、スロットル弁の開弁動作期間(第4図中t1)で
は、エアフロ吸入空気流量QAと検索吸入空気流量Qαの
大なる方の値に基づいて燃料噴射量を演算するようにし
たので、燃料噴射量を増大でき加速性能の向上を図れ
る。
Further, during the opening operation period of the throttle valve (t 1 in FIG. 4), the fuel injection amount is calculated based on the larger value of the air flow intake air flow rate Q A and the search intake air flow rate Q α. The fuel injection amount can be increased and the acceleration performance can be improved.

〈発明の効果〉 本発明は、以上説明したようにスロットル弁の加速動作
終了時から設定時間の間はスロットル弁の開弁に基づい
て設定された吸入空気流量によって燃料噴射量を演算す
るようにしたので、機関の実際の空燃比を最適にでき、
もってヘージテーションの発生を防止できる。
<Effects of the Invention> As described above, according to the present invention, the fuel injection amount is calculated from the intake air flow rate set based on the opening of the throttle valve from the end of the acceleration operation of the throttle valve to the set time. As a result, the actual air-fuel ratio of the engine can be optimized,
Therefore, the generation of hazing can be prevented.

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

第1図は本発明のクレーム対応図、第2図は本発明の一
実施例を示す構成図、第3図は同上のフローチャート、
第4図は従来の欠点及び実施例の作用を説明するための
図である。 1……制御装置、2……回転速度センサ、3……エアフ
ローメータ、4……スロットル弁開度センサ、6……駆
動回路、7……燃料噴射弁
FIG. 1 is a diagram corresponding to the claims of the present invention, FIG. 2 is a configuration diagram showing an embodiment of the present invention, FIG.
FIG. 4 is a diagram for explaining the conventional drawbacks and the operation of the embodiment. 1 ... Control device, 2 ... Rotation speed sensor, 3 ... Air flow meter, 4 ... Throttle valve opening sensor, 6 ... Drive circuit, 7 ... Fuel injection valve

フロントページの続き (56)参考文献 特開 昭60−62638(JP,A) 特開 昭59−170433(JP,A) 特開 昭59−176428(JP,A) 特開 昭62−258143(JP,A) 実開 昭62−184145(JP,U) 実開 昭62−183044(JP,U)Continuation of front page (56) Reference JP-A-60-62638 (JP, A) JP-A-59-170433 (JP, A) JP-A-59-176428 (JP, A) JP-A-62-258143 (JP , A) Actual development 62-184145 (JP, U) Actual development 62-183044 (JP, U)

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】機関の吸入空気流量を直接検出する吸入空
気流量検出手段と、スロットル弁の開度を検出するスロ
ットル弁開度検出手段と、機関回転速度を検出する回転
速度検出手段と、検出されたスロットル弁開度と機関回
転速度とに基づいて吸入空気流量を設定する吸入空気流
量設定手段と、前記検出されたスロットル弁の開度に基
づいて開弁速度を演算する開弁速度演算手段と、該演算
された開弁速度に基づいてスロットル弁の加速動作終了
時を判定する加速動作終了時判定手段と、加速動作終了
時と判定されたときから設定時間の間、前記設定された
吸入空気流量を選択する一方、前記設定時間経過後は吸
入空気流量検出手段により検出された吸入空気流量を選
択する選択手段と、選択された吸入空気流量に基づいて
燃料噴射量を演算する燃料噴射量演算手段と、演算され
た燃料噴射量に対応する噴射パルス信号を燃料噴射弁に
出力する駆動パルス出力手段と、を備えたことを特徴と
する内燃機関の電子制御燃料噴射装置。
1. An intake air flow rate detecting means for directly detecting an intake air flow rate of an engine, a throttle valve opening degree detecting means for detecting an opening degree of a throttle valve, a rotational speed detecting means for detecting an engine rotational speed, and a detecting means. Intake air flow rate setting means for setting the intake air flow rate based on the detected throttle valve opening and engine speed, and valve opening speed calculation means for calculating the valve opening speed based on the detected opening of the throttle valve. And an acceleration operation end time determination means for determining the end time of the acceleration operation of the throttle valve based on the calculated valve opening speed, and the set suction for a set time from the time when the acceleration operation end time is determined. While selecting the air flow rate, after the set time has elapsed, the selection means for selecting the intake air flow rate detected by the intake air flow rate detection means, and the fuel injection amount is calculated based on the selected intake air flow rate. That the fuel injection amount calculating means, calculated driving pulse output means for the injection pulse signal corresponding to the fuel injection amount is output to the fuel injection valves, electronically controlled fuel injection system for an internal combustion engine, characterized in that it comprises a.
JP23809586A 1986-10-08 1986-10-08 Electronically controlled fuel injection device for internal combustion engine Expired - Lifetime JPH0792006B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23809586A JPH0792006B2 (en) 1986-10-08 1986-10-08 Electronically controlled fuel injection device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23809586A JPH0792006B2 (en) 1986-10-08 1986-10-08 Electronically controlled fuel injection device for internal combustion engine

Publications (2)

Publication Number Publication Date
JPS6394045A JPS6394045A (en) 1988-04-25
JPH0792006B2 true JPH0792006B2 (en) 1995-10-09

Family

ID=17025091

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23809586A Expired - Lifetime JPH0792006B2 (en) 1986-10-08 1986-10-08 Electronically controlled fuel injection device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH0792006B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100232462B1 (en) * 1997-04-29 1999-12-01 류정열 Engine hedge detection device and control method thereof

Also Published As

Publication number Publication date
JPS6394045A (en) 1988-04-25

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