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JPH076436B2 - Fuel injection control device for internal combustion engine - Google Patents
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JPH076436B2 - Fuel injection control device for internal combustion engine - Google Patents

Fuel injection control device for internal combustion engine

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Publication number
JPH076436B2
JPH076436B2 JP60070340A JP7034085A JPH076436B2 JP H076436 B2 JPH076436 B2 JP H076436B2 JP 60070340 A JP60070340 A JP 60070340A JP 7034085 A JP7034085 A JP 7034085A JP H076436 B2 JPH076436 B2 JP H076436B2
Authority
JP
Japan
Prior art keywords
injection
fuel
fuel injection
cylinder
simultaneous
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
JP60070340A
Other languages
Japanese (ja)
Other versions
JPS61229956A (en
Inventor
昭二 古橋
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP60070340A priority Critical patent/JPH076436B2/en
Publication of JPS61229956A publication Critical patent/JPS61229956A/en
Publication of JPH076436B2 publication Critical patent/JPH076436B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Description

【発明の詳細な説明】 (産業上の利用分野) この発明は、各気筒毎に燃料噴射弁を備えた内燃機関の
燃料噴射制御装置に関する。
Description: TECHNICAL FIELD The present invention relates to a fuel injection control device for an internal combustion engine having a fuel injection valve for each cylinder.

(従来の技術) 従来のこの種の装置としては、例えば特開昭56−54929
号公報にも記載されているように、機関の吸気マニホー
ルドの各ブランチに取付けた燃料噴射弁をそれぞれ対応
する気筒の吸気行程直前に開弁して、機関要求量に応じ
た燃料を噴射するようにした装置が知られている。
(Prior Art) As a conventional device of this type, for example, JP-A-56-54929 is known.
As described in the publication, the fuel injection valve attached to each branch of the intake manifold of the engine is opened immediately before the intake stroke of the corresponding cylinder to inject fuel according to the engine demand. Known devices are

しかし、このような装置では各燃料噴射弁を機関の回転
に同期した一つパルス信号によって開閉しているため、
機関が比較的低速低負荷で燃料噴射量が少ない即ち燃料
噴射機関が比較的短い条件下では、良好な燃料供給を得
られるものの、高速高負荷域のように燃料噴射機関が長
くなり燃料噴射弁の開弁時期が重なってしまうと、その
開閉を的確に制御することは難しい。
However, in such a device, since each fuel injection valve is opened and closed by one pulse signal synchronized with the rotation of the engine,
Under a condition where the engine is at a relatively low speed and a low load and the fuel injection amount is small, that is, when the fuel injection engine is relatively short, a good fuel supply can be obtained, but the fuel injection engine becomes longer as in the high speed and high load region and the fuel injection valve If the valve opening times of are overlapped, it is difficult to control the opening and closing of them accurately.

そこで、燃料噴射機関がある程度長くなる運転条件で
は、機関が1回転する毎に全燃料噴射弁を同時に開弁し
て、燃料をいっせいに噴射することが考えられている。
Therefore, under operating conditions in which the fuel injection engine is lengthened to some extent, it is considered that all fuel injection valves are simultaneously opened every injection of the engine to inject fuel all at once.

この場合、各燃料噴射弁からは機関1回転毎に要求量の
半分の燃料を噴射する。
In this case, each fuel injection valve injects half the required amount of fuel for each revolution of the engine.

(発明が解決しようとする問題点) ところが、このようにすると、気筒毎に順次燃料を噴射
する順次噴射から同時噴射に切換る際に次のような問題
点を生じる。
(Problems to be Solved by the Invention) However, this causes the following problems when switching from sequential injection in which fuel is sequentially injected to each cylinder to simultaneous injection.

第8図は4気筒エンジンにおける噴射タイミングを示し
たもので、順次噴射では各気筒#1〜#4の点火順序に
したがって燃料噴射弁からそれぞれ吸気行程直前に燃料
が噴射されるが、この状態から同時噴射に入り各気筒#
1〜#4同時に燃料が噴射されると、例えば順次噴射の
最後に燃料が噴射された気筒#1では噴射が連続して行
なわれるため、燃料が過剰となってしまう。
FIG. 8 shows the injection timing in a 4-cylinder engine. In sequential injection, fuel is injected from the fuel injection valve immediately before the intake stroke in accordance with the ignition order of each cylinder # 1 to # 4. Simultaneous injection enters each cylinder #
When fuel is injected simultaneously in 1 to # 4, for example, in the cylinder # 1 in which the fuel is injected at the end of the sequential injection, the injection is continuously performed, so the fuel becomes excessive.

また、同時噴射ではクランク角360゜毎に要求燃料量の
半分を噴射するため、同時噴射の直後に吸気行程がくる
気筒#3では燃料が半分しか供給されないことになり、
このため切換過渡時に正常な燃料が損なわれるのであ
る。
Further, in the simultaneous injection, half of the required fuel amount is injected at every crank angle of 360 °, so that only half the fuel is supplied to cylinder # 3 where the intake stroke comes immediately after the simultaneous injection,
As a result, normal fuel is lost during the switching transition.

(問題点を解決するための手段) この発明は、第1図に示すように、各気筒毎に燃料噴射
弁A〜Dを備えると共に、機関の回転角を検出する手段
Eと、機関の運転条件を検出する手段Fと、これらの検
出信号に基づき前記燃料噴射弁から各気筒の点火順序に
したがって順次燃料を噴射させる順次噴射駆動回路G
と、この順次噴射に代わり所定の運転条件下で燃料噴射
弁から所定回転数毎に回転同期で各気筒同時に燃料を噴
射させる同時噴射駆動回路Hとを備えた内燃機関の燃料
噴射制御装置において、燃料噴射期間を判定する手段I
と、該燃料噴射期間が所定値よりも短い場合には直ちに
順次噴射を、所定値よりも長い場合には直ちに同時噴射
をそれぞれ前記対応する駆動回路に指令する手段Jと、
順次噴射から同時噴射に切換える際、同時噴射の直前に
噴射を行なう燃料噴射弁の噴射量を所定量減量する噴射
量減量回路Kと、同時噴射の直後に吸気行程がくる気筒
の燃料噴射弁の噴射量を1回限り所定量増量する噴射量
増量回路Lとを設ける。
(Means for Solving Problems) This invention, as shown in FIG. 1, includes fuel injection valves A to D for each cylinder, a means E for detecting a rotation angle of the engine, and an operation of the engine. Means F for detecting conditions, and a sequential injection drive circuit G for sequentially injecting fuel from the fuel injection valve in accordance with the ignition order of each cylinder based on these detection signals.
And a simultaneous injection drive circuit H that simultaneously injects fuel from each of the fuel injection valves at a predetermined rotational speed under a predetermined operating condition in stead of the sequential injection, and at the same time, in a fuel injection control device for an internal combustion engine, Means I for determining the fuel injection period
And means J for instructing the corresponding drive circuits to perform sequential injection immediately when the fuel injection period is shorter than a predetermined value, and to perform simultaneous injection immediately when the fuel injection period is longer than a predetermined value.
When switching from sequential injection to simultaneous injection, an injection amount reduction circuit K that reduces the injection amount of the fuel injection valve that performs injection immediately before simultaneous injection and a fuel injection valve for the cylinder that has an intake stroke immediately after simultaneous injection are provided. An injection amount increasing circuit L for increasing the injection amount only once is provided.

なお、燃料噴射期間は燃料噴射量を意味しており、通常
は機関回転速度や吸入空気量等の運転条件信号に基づい
て演算される燃料噴射パルス幅によって代表される。
The fuel injection period means the fuel injection amount, and is typically represented by the fuel injection pulse width calculated based on the operating condition signals such as the engine speed and the intake air amount.

(作用) したがって、順次噴射から同時噴射に切換る際に、順次
噴射の最後に燃料が噴射される気筒で燃料が過剰となっ
たり、同時噴射の直後に吸気行程がくる気筒で燃料が不
足したりすることはなく、常に適正量の燃料を供給する
ことができ、切換過渡時でも安定した燃焼が維持され
る。
(Operation) Therefore, when switching from the sequential injection to the simultaneous injection, the fuel is excessive in the cylinder where the fuel is injected at the end of the sequential injection, or the fuel is insufficient in the cylinder in which the intake stroke comes immediately after the simultaneous injection. Therefore, a proper amount of fuel can always be supplied, and stable combustion can be maintained even during a transitional transition.

(実施例) 第2図は本発明を4気筒エンジンに適用した実施例を示
す制御ブロック図で、1は機関の吸入空気量を検出する
エアフローメータ、2は機関の回転角を検出するクラン
ク角センサ、3は制御回路、A〜Dは吸気マニホールド
の各ブランチに設置された燃料噴射弁である。
(Embodiment) FIG. 2 is a control block diagram showing an embodiment in which the present invention is applied to a four-cylinder engine. 1 is an air flow meter for detecting the intake air amount of the engine, and 2 is a crank angle for detecting the rotation angle of the engine. Sensors, 3 are control circuits, and A to D are fuel injection valves installed in each branch of the intake manifold.

クランク角センサ2から出力される720゜信号(気筒判
別信号)、180゜信号(基準角度信号)、2゜信号(単
位角度信号)は、エアフローメータ1からの吸気量信号
とともに制御回路3のCPU(演算回路)4に送られる。
The 720 ° signal (cylinder discrimination signal), 180 ° signal (reference angle signal) and 2 ° signal (unit angle signal) output from the crank angle sensor 2 are the CPU of the control circuit 3 together with the intake air amount signal from the air flow meter 1. (Arithmetic circuit) 4 is sent.

CPU4はこれらの信号とROM(メモリ)5に記憶されたプ
ログラムをもとに、順次噴射の運転条件か同時噴射の運
転条件かを判別すると共に、機関に要求される燃料噴射
量と燃料噴射時期を演算し、各制御信号を出力する。
Based on these signals and the program stored in the ROM (memory) 5, the CPU 4 determines whether the operating conditions are sequential injection or simultaneous injection, and determines the fuel injection amount and fuel injection timing required for the engine. Is calculated and each control signal is output.

6は2進−10進変換器で、CPU4からクランク角180゜毎
に入力されるシーケンシャル信号D0、D1を変換して、出
力側から第3図に示すように順次ハイレベル[1]とロ
ーレベル[0]に切換る信号を発生する。
A binary-decimal converter 6 converts the sequential signals D 0 and D 1 input from the CPU 4 at every crank angle of 180 °, and sequentially outputs high level [1] from the output side as shown in FIG. And a signal for switching to low level [0] is generated.

論理和回路(OR回路)7は2進−10進変換器6からの信
号に応じて順々にゲートを開き、またCPU4から同時噴射
信号D2が入力されるとすべてのゲートを開く。
The OR circuit (OR circuit) 7 sequentially opens the gates in accordance with the signal from the binary-decimal converter 6, and when the simultaneous injection signal D 2 is input from the CPU 4, all the gates are opened.

論理積回路(AND回路)8は論理和回路7のゲートが開
いている間、対応するゲートがCPU4から送られる噴射パ
ルス信号Tにより開かれ、その噴射パルス信号Tを開閉
用のパワートランジスタ9〜12に出力する。
The AND gate 8 is opened by the ejection pulse signal T sent from the CPU 4 while the gate of the OR circuit 7 is opened, and the ejection pulse signal T is opened and closed by the power transistors 9 to. Output to 12.

順次噴射の場合、CPU4は要求燃料量に応じた幅の噴射パ
ルス信号T1を各気筒の吸気行程直前毎に出力し、パワー
トランジスタ9〜12を介して対応する燃料噴射弁A〜D
が順次開閉される。
In the case of sequential injection, the CPU 4 outputs the injection pulse signal T 1 having a width corresponding to the required fuel amount immediately before the intake stroke of each cylinder, and the corresponding fuel injection valves A to D via the power transistors 9 to 12.
Are opened and closed sequentially.

同時噴射の場合、CPU4は論理和回路7に同時噴射信号D2
を出力すると共に、要求燃料量の半分の幅の噴射パルス
信号T2を機関1回転毎に所定の吸気行程直前に出力し、
燃料噴射弁A〜Dが同時開閉される。
In the case of simultaneous injection, the CPU 4 sends the simultaneous injection signal D 2 to the OR circuit 7.
And an injection pulse signal T 2 having a width half the required fuel amount is output immediately before a predetermined intake stroke for each engine revolution,
The fuel injection valves A to D are simultaneously opened and closed.

そして、順次噴射から同時噴射に切換える場合、CPU4は
まず順次噴射の状態で論理積回路8に出力する噴射パル
ス信号T1の幅を半分に設定し、最後の順次噴射となる燃
料噴射弁の開弁時間を短縮する。
When switching from the sequential injection to the simultaneous injection, the CPU 4 first sets the width of the injection pulse signal T 1 output to the AND circuit 8 to half in the state of the sequential injection, and opens the fuel injection valve to be the final sequential injection. Reduce valve time.

例えば、燃料噴射弁Aによる噴射終了後に同時噴射に切
換えようとすると、順次噴射では2進−10進変換器6の
出力に応じて論理和回路7のゲートが切換り、次に燃料
噴射弁Bから噴射が行なわれるが、この燃料噴射弁Bの
開弁時間が半減される。
For example, if an attempt is made to switch to simultaneous injection after the injection by the fuel injection valve A is completed, in sequential injection, the gate of the OR circuit 7 is switched in accordance with the output of the binary-decimal converter 6, and then the fuel injection valve B. However, the valve opening time of the fuel injection valve B is halved.

この後、さらに2進−10進変換器6の出力が切換り燃料
噴射弁Cの噴射タイミングになると、CPU4は半分の幅の
噴射パルス信号T2を出力すると共に、論理和回路7に同
時噴射信号D2を出力し、燃料噴射弁A〜Dを同時に開閉
する。
After this, when the output of the binary-decimal converter 6 is further switched to the injection timing of the fuel injection valve C, the CPU 4 outputs the injection pulse signal T 2 having a half width and the simultaneous injection to the OR circuit 7. The signal D 2 is output and the fuel injection valves A to D are simultaneously opened and closed.

そして、この噴射後、CPU4は2進−10進変換器6の出力
が切換るまで、同時噴射信号D2を遮断すると共に、その
噴射終了に応答して同じく半分の幅の単一パルス信号T3
を出力し、この場合燃料噴射弁Cを再度開閉する。
Then, after this injection, the CPU 4 blocks the simultaneous injection signal D 2 until the output of the binary-decimal converter 6 is switched, and in response to the completion of the injection, the single pulse signal T of half the width is also provided. 3
Is output, and in this case, the fuel injection valve C is opened and closed again.

なお、この開閉を終了すると、以降は前述した機関1回
転毎の同時噴射が行なわれる。
When this opening and closing is completed, the above-mentioned simultaneous injection for every one revolution of the engine is performed thereafter.

次に作用を第4図、第5図のフローチャートに基づいて
説明する。
Next, the operation will be described based on the flowcharts of FIGS. 4 and 5.

クランク角180゜毎の割込みに伴い、S1にて噴射気筒カ
ウンタCOUNT1のインクリメント(値は0〜3)がなされ
ると共に、S2にて機関1/4回転周期に対する噴射パルス
信号Tの幅がヒステリシスを考慮した所定値K1、K2と比
較され、Tの幅が小さいときはS3,S4の順次噴射ルーチ
ンに入る。
The injection cylinder counter COUNT1 is incremented (the value is 0 to 3) in S1 due to the interruption every 180 ° of the crank angle, and the width of the injection pulse signal T with respect to the engine 1/4 rotation cycle has hysteresis in S2. It is compared with the predetermined values K 1 and K 2 considered, and when the width of T is small, the sequential injection routine of S3 and S4 is started.

S3では噴射パルス信号Tがそのまま選択され、S4では図
外の噴射実行フローのフラグF1=1、F2=0、F3=1を
選択する。
In S3, the injection pulse signal T is selected as it is, and in S4, flags F1 = 1, F2 = 0, and F3 = 1 of the injection execution flow (not shown) are selected.

ただし、F1:1 順次噴射 0 同時噴射 F2:1 順次→同時噴射に切換え 0 順次または同時噴射 F3:1 噴射実行 0 噴射せず したがって、噴射パルス信号T1とF1、F2、F3に応じてク
ランク角度180゜毎に燃料噴射弁A〜Dが順々に開閉さ
れ、各気筒で吸気行程直前に要求量の燃料が噴射され
る。
However, F1: 1 successively jetting 0 coinjected F2: 1 successively → coinjected into switching 0 sequentially or simultaneously injected F3: therefore without 1 injection execution 0 injection, a crank in accordance with the injection pulse signal T 1 and F1, F2, F3 The fuel injection valves A to D are sequentially opened and closed at every angle of 180 °, and the required amount of fuel is injected into each cylinder immediately before the intake stroke.

なお、S5では噴射気筒をCOUNT1にセットする。In S5, the injection cylinder is set to COUNT1.

そして、この順次噴射から機関1/4回転周期に対する噴
射パルス信号Tの幅が所定値K1、K2よりも大きくなる
と、S2、S6からS7〜S9の減量ルーチンに入る。
When the width of the injection pulse signal T with respect to the engine 1/4 rotation cycle from this sequential injection becomes larger than the predetermined values K 1 and K 2 , the reduction routine from S2, S6 to S7 to S9 is started.

S7では噴射パルス信号Tの幅が減少され(第2図の場合
K3=0.5)、S8でフラグF1=0、F2=1、F3=1が選択
される。
In S7, the width of the injection pulse signal T is reduced (in the case of FIG. 2
K 3 = 0.5) and the flags F1 = 0, F2 = 1 and F3 = 1 are selected in S8.

したがって、このとき開閉される燃料噴射弁は、噴射パ
ルス信号T1の幅が短いため開弁時間が短縮され、噴射量
が減少される。
Therefore, the fuel injection valve that is opened and closed at this time has a short width of the injection pulse signal T 1 , so that the valve opening time is shortened and the injection amount is reduced.

また、S9では割込み噴射気筒がCOUNT2にストア、つまり
燃料増量気筒が次の180゜割込み時の気筒に定められ
る。
In S9, the interrupt injection cylinder is stored in COUNT2, that is, the fuel increase cylinder is set to the cylinder at the next 180 ° interruption.

そして、次の180゜割込みが入ると、このときF1=0で
あるからS6からS10〜S14の同時噴射ルーチンに入る。
When the next 180 ° interrupt is entered, since F1 = 0 at this time, the simultaneous injection routine from S6 to S10 to S14 is started.

このルーチンの始めはF3=1となり、S11で噴射パルス
信号Tの幅が半分に設定される。また、S12でF1=0、F
3=0が選択され、S13で噴射気筒を全気筒に設定され
る。
At the beginning of this routine, F3 = 1, and the width of the injection pulse signal T is set to half in S11. Also, in S12, F1 = 0, F
3 = 0 is selected and the injection cylinders are set to all cylinders in S13.

したがって、180゜割込みにより噴射パルス信号T2が全
燃料噴射弁A〜Dに送られ、同時噴射が行なわれる。
Therefore, the injection pulse signal T 2 is sent to all the fuel injection valves A to D by the 180 ° interruption, and the simultaneous injection is performed.

そして、この噴射終了と同時に第5図の噴射終了割込み
に入り、このときF2=1であるからU1からU2〜U4の割込
み噴射ルーチンに進む。
Upon completion of this injection, the injection end interrupt shown in FIG. 5 is entered. Since F2 = 1 at this time, the routine advances from U1 to U2 to U4.

U2ではTの幅の半分(第2図の場合K5=0.5)の噴射パ
ルス信号T3が選出され、U3で噴射気筒をCOUNT2にセット
する。
Half the width of U2 in T (the case of FIG. 2 K 5 = 0.5) of the injection pulse signal T 3 is selected, sets the injection cylinder in COUNT2 in U3.

したがって、上記噴射終了後、噴射パルス信号T3により
S9にて定めた気筒の燃料噴射弁のみが再度開弁され、燃
料が増量される。
Therefore, after the end of the injection, the injection pulse signal T 3
Only the fuel injection valve of the cylinder determined in S9 is opened again, and the fuel amount is increased.

また、U4ではこの割込み噴射を終了するようにF2=0に
切換る。
Further, in U4, it switches to F2 = 0 so as to end this interrupt injection.

この後、次の180゜割込みが入ると、第4図の同時噴射
ルーチンでS10からS14に行き、さらに180゜割込みが入
ると、S10からS1〜S13に進む。
After this, when the next 180 ° interrupt is entered, the process proceeds from S10 to S14 in the simultaneous injection routine of FIG. 4, and when another 180 ° interrupt is entered, the process proceeds from S10 to S1 to S13.

これにより、機関1回転毎に所定気筒の吸気行程直前に
全燃料噴射弁A〜Dが開閉され、同時噴射に移行する。
As a result, all the fuel injection valves A to D are opened and closed immediately before the intake stroke of the predetermined cylinder for each engine revolution, and the simultaneous injection is performed.

この順次噴射から同時噴射に切換るときのタイミングチ
ャートを示すと第6図のようになり、このため順次噴射
の最後に燃料が噴射される気筒(例えば#1)で燃料が
過剰となったり、同時噴射の直後に吸気行程がくる気筒
(#3)で燃料が否定したりすることはなく、常に要求
量の燃料を供給することが可能となる。
A timing chart when switching from this sequential injection to the simultaneous injection is shown in FIG. 6, and therefore, the fuel is excessive in the cylinder (for example, # 1) where the fuel is injected at the end of the sequential injection, The fuel is not denied in the cylinder (# 3) where the intake stroke comes immediately after the simultaneous injection, and the required amount of fuel can always be supplied.

この結果、切換時でも各気筒で正常な燃焼を維持するこ
とができ、トルク変動等を防止して、特に低速低負荷か
ら高速高負荷への移行時に良好な運転性を確保すること
ができる。
As a result, normal combustion can be maintained in each cylinder even during switching, torque fluctuations, etc. can be prevented, and good drivability can be ensured particularly when shifting from low speed low load to high speed high load.

第7図は本発明の他の実施例を示すタイミングチャート
で、前記順次噴射の代わりに各気筒#1〜#4を吸気行
程が近い気筒#1、#2と気筒#3、#4のグループに
分け、グループ毎に所定のタイミングで燃料噴射を行な
うものに適用した例である。
FIG. 7 is a timing chart showing another embodiment of the present invention. Instead of the sequential injection, the cylinders # 1 to # 4 are arranged in groups of cylinders # 1 and # 2 and cylinders # 3 and # 4 having a close intake stroke. In this example, the fuel injection is performed for each group at a predetermined timing.

このグループ噴射は機関2回転に1回行なわれるが、同
時に噴射に切換える場合、第6図と同様に最後に行なわ
れるグループ噴射による噴射量が所定量減量され、同時
噴射後に他のグループ側の噴射量が所定量増量される。
なお、この場合、噴射量の減量割合および増量割合は少
なくて良い。
This group injection is performed once every two revolutions of the engine, but when switching to injection at the same time, the injection amount by the last group injection is reduced by a predetermined amount as in FIG. 6, and after the simultaneous injection, the injection on the other group side is performed. The amount is increased by a predetermined amount.
In this case, the reduction rate and the increase rate of the injection amount may be small.

(発明の効果) 以上のように本発明によれば、燃料噴射期間に基づいて
順次噴射と同時噴射とを直ちに切り換えるように図る一
方、順次噴射から同時噴射へと切り換える際に、同時噴
射の直前に噴射を行う燃料噴射弁の噴射量を減量すると
共に、同時噴射の直後に吸気行程が到来する気筒の燃料
噴射弁の噴射量を1回限り増量するようにしたので、急
速な運転状態の変化があっても順次噴射から同時噴射へ
の切換に伴う燃料量の過不足を確実に補償して適切な空
燃比を維持し、これにより良好な燃焼状態を保つことが
できるという効果が得られる。
As described above, according to the present invention, the sequential injection and the simultaneous injection are immediately switched based on the fuel injection period, while the sequential injection and the simultaneous injection are switched immediately before the simultaneous injection. In addition to reducing the injection amount of the fuel injection valve that injects into the cylinder, the injection amount of the fuel injection valve of the cylinder in which the intake stroke arrives immediately after the simultaneous injection is increased only once. Even if there is, the excess and deficiency of the fuel amount due to the switching from the sequential injection to the simultaneous injection can be surely compensated to maintain an appropriate air-fuel ratio, and thereby an effect that a good combustion state can be maintained can be obtained.

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

第1図は本発明の構成図、第2図は実施例の制御ブロッ
ク図、第3図は2進−10進変換器の機能を示す表図、第
4図、第5図はフローチャート、第6図はタイミングチ
ャート、第7図は他の実施例のタイミングチャート、第
8図は従来のタイミングチャートである。 1……エアフローメータ、2……クランク角センサ、3
……制御回路、4……CPU、5……ROM
FIG. 1 is a block diagram of the present invention, FIG. 2 is a control block diagram of an embodiment, FIG. 3 is a table showing the functions of a binary-decimal converter, FIGS. 4 and 5 are flowcharts, and FIG. FIG. 6 is a timing chart, FIG. 7 is a timing chart of another embodiment, and FIG. 8 is a conventional timing chart. 1 ... Air flow meter, 2 ... Crank angle sensor, 3
...... Control circuit, 4 ... CPU, 5 ... ROM

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】各気筒毎に燃料噴射弁を備えると共に、機
関の回転角を検出する手段と、機関の運転条件を検出す
る手段と、これらの検出信号に基づき前記燃料噴射弁か
ら各気筒の点火順序にしたがって順次燃料を噴射させる
順次噴射駆動回路と、この順次噴射の代わり所定の運転
条件下で燃料噴射弁から所定回転数毎に回転同期で各気
筒同時に燃料を噴射させる同時噴射駆動回路とを備えた
内燃機関の燃料噴射制御装置において、燃料噴射期間を
判定する手段と、該燃料噴射期間が所定値よりも短い場
合には直ちに順次噴射を、所定値よりも長い場合には直
ちに同時噴射をそれぞれ前記対応する駆動回路に指令す
る手段と、順次噴射から同時噴射に切換える際、同時噴
射の直前に噴射を行なう燃料噴射弁の噴射量を所定量減
量する噴射量減量回路と、同時噴射の直後に吸気行程が
くる気筒の燃料噴射弁の噴射量を1回限り所定量増量す
る噴射量増量回路とを設けたことを特徴とする内燃機関
の燃料噴射制御装置。
1. A fuel injection valve is provided for each cylinder, and means for detecting a rotation angle of the engine, means for detecting an operating condition of the engine, and a means for detecting the operating condition of the engine from the fuel injection valve to each cylinder are provided. A sequential injection drive circuit for sequentially injecting fuel in accordance with the ignition order, and a simultaneous injection drive circuit for injecting fuel simultaneously from the fuel injection valve at predetermined rotational speeds in each cylinder simultaneously under predetermined operating conditions instead of this sequential injection In a fuel injection control device for an internal combustion engine, the means for determining a fuel injection period and sequential injection immediately when the fuel injection period is shorter than a predetermined value, and simultaneous injection immediately when the fuel injection period is longer than the predetermined value. And a means for instructing the corresponding drive circuits, and an injection amount reduction for reducing the injection amount of the fuel injection valve that performs injection immediately before simultaneous injection when switching from sequential injection to simultaneous injection by a predetermined amount. Road and, a fuel injection control apparatus for an internal combustion engine, characterized by comprising the injection amount increasing circuit for a predetermined amount increasing one-time injection amount of the fuel injection valve in the intake stroke comes cylinder immediately after the simultaneous injection.
JP60070340A 1985-04-03 1985-04-03 Fuel injection control device for internal combustion engine Expired - Lifetime JPH076436B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60070340A JPH076436B2 (en) 1985-04-03 1985-04-03 Fuel injection control device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60070340A JPH076436B2 (en) 1985-04-03 1985-04-03 Fuel injection control device for internal combustion engine

Publications (2)

Publication Number Publication Date
JPS61229956A JPS61229956A (en) 1986-10-14
JPH076436B2 true JPH076436B2 (en) 1995-01-30

Family

ID=13428586

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60070340A Expired - Lifetime JPH076436B2 (en) 1985-04-03 1985-04-03 Fuel injection control device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH076436B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01294937A (en) * 1988-05-20 1989-11-28 Mazda Motor Corp Control device for fuel injection type engine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0674768B2 (en) * 1983-06-16 1994-09-21 日本電装株式会社 Fuel injection control method for internal combustion engine

Also Published As

Publication number Publication date
JPS61229956A (en) 1986-10-14

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