JPH0245029B2 - - Google Patents
Info
- Publication number
- JPH0245029B2 JPH0245029B2 JP56117149A JP11714981A JPH0245029B2 JP H0245029 B2 JPH0245029 B2 JP H0245029B2 JP 56117149 A JP56117149 A JP 56117149A JP 11714981 A JP11714981 A JP 11714981A JP H0245029 B2 JPH0245029 B2 JP H0245029B2
- Authority
- JP
- Japan
- Prior art keywords
- intake
- cylinder
- fuel injection
- throttle valve
- auxiliary
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/32—Controlling fuel injection of the low pressure type
- F02D41/36—Controlling fuel injection of the low pressure type with means for controlling distribution
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine 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】
本発明は火花点火式内燃機関の燃料供給技術に
係り、より詳しくは、多気筒内燃機関の電子制御
式燃料噴射システムに関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fuel supply technology for a spark-ignition internal combustion engine, and more particularly to an electronically controlled fuel injection system for a multi-cylinder internal combustion engine.
火花点火式内燃機関の燃料供給方式には大別し
て気化器による方式と燃料噴射弁による方式があ
る。後者は比較的最近開発された技術で、排気ガ
ス対策その他諸種の見地から近年注目されてい
る。すなわち、火花点火式内燃機関における燃料
噴射方式の主たる利点は、各気筒の吸気ポートご
とに夫々一個の燃料噴射弁を設け各噴射弁には互
いに等量の燃料を噴射させることにより各燃焼室
への燃料供給料を均一化することができるので、
気化器による方式に固有の燃料の気筒間分配の問
題が解決され、その結果エンジンをより稀薄(リ
ーン)な燃焼用混合物で運転することを可能にし
てHC、COのような有害な未燃成生物の発生を低
減することができることにある。燃料噴射弁の作
動方式には噴射弁から連続的に燃料を噴出させる
連続噴射方式と間欠的に噴射を行わせるパルス噴
射方式とがある。後者の方式においてはソレノイ
ドにより開閉する電磁式燃料噴射弁が使用され、
このソレノイドは一般にマイクロコンピユータを
内蔵した電子制御ユニツトからのパルスの形の噴
射指令によつて励起されるようになつている。か
かる方式は電子制御式燃料噴射方式(EFI)とい
われているもので、本発明が対象とする技術もこ
れに属する。従来の電子制御式燃料噴射方式にお
いては、燃料噴射時期はすべての燃料噴射弁につ
いて同時、すなわち燃料が一斉に噴射されるよう
になつており(同時噴射方式)、噴射の回数はエ
ンジンの各作動サイクル当り1回もしくは2回で
ある。 Fuel supply methods for spark ignition internal combustion engines can be roughly divided into two types: a method using a carburetor and a method using a fuel injection valve. The latter is a relatively recently developed technology that has been attracting attention in recent years from various viewpoints including exhaust gas countermeasures. In other words, the main advantage of the fuel injection method in spark-ignition internal combustion engines is that one fuel injection valve is provided for each intake port of each cylinder, and each injection valve injects the same amount of fuel into each combustion chamber. Because it is possible to equalize the fuel supply of
The problem of fuel distribution between cylinders inherent in carburetor systems is resolved, allowing the engine to operate with a leaner combustion mixture and eliminating harmful unburned compounds such as HC and CO. The reason is that it can reduce the occurrence of living organisms. There are two types of operating methods for fuel injection valves: a continuous injection method in which fuel is continuously injected from the injector, and a pulse injection method in which fuel is injected intermittently. The latter method uses an electromagnetic fuel injection valve that is opened and closed by a solenoid.
This solenoid is generally energized by injection commands in the form of pulses from an electronic control unit containing a microcomputer. Such a method is called an electronically controlled fuel injection method (EFI), and the technology to which the present invention is directed also belongs to this. In conventional electronically controlled fuel injection systems, the fuel injection timing is set at the same time for all fuel injection valves, that is, the fuel is injected all at once (simultaneous injection system), and the number of injections depends on each engine operation. Once or twice per cycle.
他方、燃料噴射方式であるか気化器方式である
かを問わず今日のエンジンにおいては、高負荷高
速運転時における出力をできるだけ大きくするた
めに吸気ポートのプロフイルは一般に比較的直径
が大きくて真直ぐな通気抵抗の小さい形状に設計
されている。ところが、吸気ポートの形状をこの
ようにした場合には低速低負荷運転時に燃焼室内
に吸入される混合気中に十分な乱流が発生せず、
火炎伝播速度を高めることができない。低速低負
荷運転時に吸入混合気に強度の乱流を発生させる
手法としては、吸気ポートをヘリカル形状にした
り或いはシユラウド弁を用いたりして燃焼室内に
強制的に旋回流を発生させる手法があるが、これ
らの手法においては吸入混合気流に対する通気抵
抗が増大するため高速高負荷運転時における充填
効率が低下するという問題がある。そこで、気化
器方式のエンジンにおいて、主吸気通路内に人為
的に操作される主絞リ弁とその下流に位置して低
負荷時にのみ全閉される補助絞り弁とを設けると
ともに、主絞り弁と補助絞り弁との間の主吸気通
路を管路で連通管に導き、該連通管から吸気口近
傍に開口する副吸気通路分枝管を分枝せしめ、上
記管路と連通路と分枝管とで補助絞り弁をバイパ
スする副吸気通路を構成し、もつて低負荷時には
補助絞り弁を閉じ又は閉じ気味として該副吸気通
路から強い混合気噴流を噴出せしめて燃焼室内に
乱れの発生を促進して燃焼改善を行いつつ、高負
荷時には主吸気通路を全開として吸気抵抗を最小
とすることによつて出力の低下を防止することが
提案されている(特開昭53−137320)。この方式
を本明細書では、便宜上、副吸気通路式乱流発生
方式と略称することとする。 On the other hand, in today's engines, whether fuel-injected or carburetor-based, the intake port profile is generally relatively large in diameter and straight in order to maximize power output during high-load, high-speed operation. Designed to have a shape with low ventilation resistance. However, when the intake port is shaped like this, sufficient turbulence is not generated in the air-fuel mixture sucked into the combustion chamber during low-speed, low-load operation.
Unable to increase flame propagation velocity. Methods of generating strong turbulence in the intake air-fuel mixture during low-speed, low-load operation include creating a helical intake port or using a shroud valve to forcibly generate a swirling flow within the combustion chamber. However, these methods have a problem in that the charging efficiency during high-speed, high-load operation decreases because the ventilation resistance to the intake air mixture increases. Therefore, in a carburetor type engine, a main throttle valve that is artificially operated in the main intake passage and an auxiliary throttle valve that is located downstream of the main throttle valve and is fully closed only at low load are installed. A main intake passage between the and the auxiliary throttle valve is led to a communication pipe by a pipe, and a sub-intake passage branch pipe that opens near the intake port is branched from the communication pipe, and the pipe and the communication passage are connected to each other. A sub-intake passage that bypasses the auxiliary throttle valve is formed with the pipe, and when the load is low, the auxiliary throttle valve is closed or slightly closed, and a strong mixture jet is ejected from the auxiliary intake passage to prevent turbulence from occurring in the combustion chamber. It has been proposed to prevent a decrease in output by minimizing intake resistance by fully opening the main intake passage during high loads while promoting combustion improvement (Japanese Patent Application Laid-Open No. 137320/1983). In this specification, for convenience, this method will be abbreviated as a sub-intake passage type turbulence generation method.
ところで、従来の気化器を有するエンジンに上
記副吸気通路式乱流発生方式を応用する場合に
は、副吸気通路の分枝管は気化器の主絞り弁の下
流にあり、気化器において均質な混合気が形成さ
れるため、混合気が副吸気通路の各分枝管に分流
しても各気筒間の燃料分配の悪化は生じない。と
ころが、吸気マニホールドの各分枝管又は個々の
吸気ポートに燃料を同時噴射する燃料噴射方式と
上記副吸気通路式乱流発生方式とを組合せると、
気筒間の燃料分配が悪化し、副吸気通路による燃
焼改善効果が気筒間の空燃比の変動に減殺されて
エンジンのトルク変動が増大するという不具合が
あつた。 By the way, when applying the above auxiliary intake passage type turbulence generation system to an engine with a conventional carburetor, the branch pipe of the auxiliary intake passage is located downstream of the main throttle valve of the carburetor, and a homogeneous flow is generated in the carburetor. Since the air-fuel mixture is formed, even if the air-fuel mixture is divided into the branch pipes of the auxiliary intake passage, fuel distribution between the cylinders will not deteriorate. However, when the fuel injection method in which fuel is simultaneously injected into each branch pipe of the intake manifold or each intake port is combined with the auxiliary intake passage type turbulence generation method,
There was a problem in that the fuel distribution between the cylinders deteriorated, and the combustion improvement effect of the auxiliary intake passage was offset by the fluctuations in the air-fuel ratio between the cylinders, resulting in an increase in engine torque fluctuations.
本発明は上記不具合を解消することを目的とす
るものであつて、電子制御式燃料噴射システムを
上記副吸気通路式乱流発生方法と組合せたときに
も燃料分配の悪化しない燃料供給装置を提供する
ことによつて、高速高負荷運転時の出力を確保す
るとともに低速低負荷運転時のトルク変動を防止
し稀薄(リーン)な燃焼用混合物でエンジンを運
転することを可能にして燃費の改善と有害排出ガ
ス成分の低減を実現することを目的とするもので
ある。 The present invention aims to eliminate the above-mentioned problems, and provides a fuel supply device that does not deteriorate fuel distribution even when an electronically controlled fuel injection system is combined with the above-mentioned auxiliary intake passage type turbulence generation method. By doing so, it secures output during high-speed, high-load operation, prevents torque fluctuations during low-speed, low-load operation, and enables the engine to operate with a lean combustion mixture, improving fuel efficiency. The purpose is to reduce harmful exhaust gas components.
本発明は、上記燃料分配の悪化は、一定時期に
同時噴射された各気筒の吸気ポート内に滞留して
いる燃料が或る気筒が吸気行程になつた時に連通
管を介して廻り込んでその気筒に吸入されその結
果後続して順次吸気行程に入る他の気筒の吸入燃
料量が漸減することに因るものであるという知見
に立脚するもので、本発明はかゝる事態を防止す
るため、多気筒内燃機関の主吸気絞弁下流の各気
筒の吸気通路に低負荷運転時にほぼ全閉される補
助吸気絞弁をそれぞれ設けると共に、上記主吸気
絞弁と上記補助吸気絞弁との間の吸気通路区間か
ら分岐し上記補助吸気絞弁をバイパスして各気筒
の吸気弁近傍に開口する噴流ポートを相互に連通
状態として副吸気通路を形成し、機関の低負荷運
転時において或る気筒が吸入行程になつたときに
は吸入行程にない他の気筒の吸気通路から上記副
吸気通路を通じて吸気を誘引して上記吸入行程に
ある気筒の上記吸気通路へ上記噴流ポートから吸
気を噴出させるようにし、さらに、各気筒の上記
吸気通路内の上記補助吸気絞弁と上記噴流ポート
の開口との間に開口するように、各気筒のための
燃料噴射弁をそれぞれ設けると共に、各気筒の上
記燃料噴射弁を気筒数の半数ずつの2グループに
分割し、各グループの上記燃料噴射弁が点火順序
に従つて所定の点火時期間隔で作動するように構
成したことを特徴とする多気筒内燃機関の電子制
御式燃料噴射装置を提案するものである。 According to the present invention, the above-mentioned deterioration in fuel distribution is caused by fuel remaining in the intake ports of each cylinder that has been injected at the same time at a certain time flowing around through a communication pipe when a certain cylinder enters its intake stroke. The present invention is based on the knowledge that this is due to the fact that the amount of fuel sucked into a cylinder gradually decreases as a result of the amount of fuel sucked into other cylinders that subsequently enter the intake stroke, and the present invention aims to prevent such a situation. , an auxiliary intake throttle valve that is substantially fully closed during low-load operation is provided in the intake passage of each cylinder downstream of the main intake throttle valve of the multi-cylinder internal combustion engine, and between the main intake throttle valve and the auxiliary intake throttle valve. A sub-intake passage is formed by connecting jet ports that branch from the intake passage section of the engine and bypass the auxiliary intake throttle valve and open near the intake valves of each cylinder to form an auxiliary intake passage. When in the intake stroke, intake air is induced from the intake passages of other cylinders not in the intake stroke through the auxiliary intake passage, and the intake air is jetted from the jet port to the intake passage of the cylinder in the intake stroke, Further, a fuel injection valve for each cylinder is provided so as to open between the auxiliary intake throttle valve in the intake passage of each cylinder and the opening of the jet port, and the fuel injection valve for each cylinder is electronic control for a multi-cylinder internal combustion engine, characterized in that the engine is divided into two groups each having half the number of cylinders, and the fuel injection valves of each group are configured to operate at predetermined ignition timing intervals according to the ignition order. This paper proposes a type fuel injection system.
以下、添附図面を参照して実施例を説明する。 Embodiments will be described below with reference to the accompanying drawings.
第1図は本発明の電子制御式燃料噴射システム
を具えたエンジンの全体配置を示す図、第2図は
第1図の−断面図である。図は4気筒エンジ
ンを示すもので、周知のようにシリンダボア2a
〜2dを形成したシリンダブロツク4の上には動
弁系と吸排気ポートを具えたシリンダヘツド6が
装着してあり、シリンダボア2と、その中で往復
動するピストン8とシリンダヘツド6との間には
燃焼室10が形成されている。シリンダヘツド6
の側面には吸気マニホルド12およびサージタン
ク14が順次に固着されており、この吸気マニホ
ールド12はシリンダヘツド6およびサージタン
ク14に夫々接する一体のフランジ13と中間の
4つの分枝管15a〜15dとから成る。吸入空
気はエアクリーナ16、吸入空気流量を計測する
ためのエアフローメータ18、スロツトルバルブ
20を具えたスロツトルボデー22を経てサージ
タンク14に導かれ、そこから吸気マニホールド
12を介してシリンダヘツド6内に形成された吸
気ポート24を経て燃焼室10に吸入されるよう
になつている。26はマイクロコンピユータを内
蔵した周知の電子制御ユニツト(ECU)で、エ
アフローメータ18からの吸気量信号、エアフロ
ーメータに設けた吸気温センサ28からの吸気温
信号、スロツトルボデー22に設けたスロツトル
ポジシヨンセンサ30からの信号、冷却水温セン
サ32からの信号、エンジンの回転数センサ(図
示せず)からの信号、等を入力して燃料噴射量を
演算し燃料噴射指令信号を出力するためのもので
ある。吸気マニホールド12には各気筒ごとに燃
料噴射弁34a〜34dが設置してある。各燃料
噴射弁34には燃料ポンプ(図示せず)から燃料
ホース36およびデリベリパイプ38を経て燃料
が供給される。燃料噴射弁34はソレノイドを有
する公知の電磁式噴射弁で、電子制御ユニツト2
6からの噴射指令信号に応じて燃料を吸気ポート
24に向つて噴射する。 FIG. 1 is a diagram showing the overall arrangement of an engine equipped with an electronically controlled fuel injection system according to the present invention, and FIG. 2 is a sectional view taken along the line taken from FIG. 1. The figure shows a four-cylinder engine, and as is well known, cylinder bore 2a
A cylinder head 6 equipped with a valve train and an intake/exhaust port is mounted on the cylinder block 4 forming the cylinder bore 2, and the cylinder head 6 is connected between the cylinder bore 2, the piston 8 that reciprocates therein, and the cylinder head 6. A combustion chamber 10 is formed in the combustion chamber 10 . cylinder head 6
An intake manifold 12 and a surge tank 14 are sequentially fixed to the side surface of the intake manifold 12, and the intake manifold 12 has an integral flange 13 that contacts the cylinder head 6 and the surge tank 14, respectively, and four intermediate branch pipes 15a to 15d. Consists of. Intake air is led to a surge tank 14 via an air cleaner 16, an air flow meter 18 for measuring the intake air flow rate, and a throttle body 22 equipped with a throttle valve 20, and from there is formed in the cylinder head 6 via an intake manifold 12. The air is sucked into the combustion chamber 10 through an intake port 24 which has been opened. Reference numeral 26 denotes a well-known electronic control unit (ECU) with a built-in microcomputer, which controls the intake air amount signal from the air flow meter 18, the intake air temperature signal from the intake temperature sensor 28 provided in the air flow meter, and the throttle position provided in the throttle body 22. It inputs signals from the sensor 30, the coolant temperature sensor 32, the engine rotation speed sensor (not shown), etc., calculates the fuel injection amount, and outputs the fuel injection command signal. be. Fuel injection valves 34a to 34d are installed in the intake manifold 12 for each cylinder. Each fuel injection valve 34 is supplied with fuel from a fuel pump (not shown) via a fuel hose 36 and a delivery pipe 38. The fuel injection valve 34 is a known electromagnetic injection valve having a solenoid, and is controlled by the electronic control unit 2.
The fuel is injected toward the intake port 24 in response to an injection command signal from 6.
各吸気マニホールド分枝管15には補助絞り弁
40a〜40dが設けてあり、これらは共通の軸
42により連動されるようになつている。軸42
はダイヤフラム装置44の出力軸にリンクされて
おり、エンジンの低負荷運転時には補助絞り弁4
0を回動して分枝管15内の主空気通路を実質上
遮断し得るようになつている。一方、シリンダヘ
ツド6および吸気マニホルド12には、吸気通路
に略々平行に小径の噴流ポート46a〜46dが
各気筒ごとに形成されている。これらの噴流ポー
トは、第2図に断面を示しかつ第1図に点線で示
したところから明らかなように、吸気弁48の周
縁に対して略々接線方向に吸気ポート24の終端
部近傍に開口しており、空気がこれらの噴流ポー
トから吸入された時には燃焼室内に乱流ないしス
ワールが発生されるようになつている。各噴流ポ
ート46はサージタンク14の下部に形成した連
通管50によつて互いに連通されており、一方、
この連通管50は開口52を介して補助絞り弁4
0を側路してサージタンク14の内部に連通され
ている。開口52、連通管50、噴流ポート46
a〜46dが副吸気通路を構成する。このような
構成であるから、エンジンの低負荷運転時に補助
絞り弁40a〜40dが全閉された時には吸入空
気は専ら副吸気通路から供給され、燃焼室内に乱
れを発生させる。第1図下方に参照番号56で示
したのはデイストリビユータで、その回転軸には
4つの突起を有する星形の点火パルス発生用ロー
タと1つの突起を有する気筒判別用ロータを取付
けてあり、他方、デイストリビユータのハウジン
グには上記各ロータに対応する位置において点火
パルス検出センサ58および気筒判別センサ60
が設置されている。 Each intake manifold branch pipe 15 is provided with auxiliary throttle valves 40a to 40d, which are linked by a common shaft 42. shaft 42
is linked to the output shaft of the diaphragm device 44, and when the engine is operating at low load, the auxiliary throttle valve 4 is
0 can be rotated to substantially block the main air passage within the branch pipe 15. On the other hand, in the cylinder head 6 and the intake manifold 12, small-diameter jet ports 46a to 46d are formed for each cylinder, substantially parallel to the intake passage. As is clear from the cross section shown in FIG. 2 and the dotted line in FIG. These jet ports are open so that when air is drawn in through these jet ports, turbulence or swirl is generated within the combustion chamber. Each of the jet ports 46 communicates with each other through a communication pipe 50 formed at the bottom of the surge tank 14.
This communication pipe 50 is connected to the auxiliary throttle valve 4 through an opening 52.
0 is bypassed and communicated with the inside of the surge tank 14. Opening 52, communication pipe 50, jet port 46
a to 46d constitute a sub-intake passage. With this configuration, when the auxiliary throttle valves 40a to 40d are fully closed during low-load operation of the engine, intake air is supplied exclusively from the auxiliary intake passage, causing turbulence within the combustion chamber. The number 56 shown at the bottom of Figure 1 is a distributor, and its rotating shaft has a star-shaped ignition pulse generation rotor with four protrusions and a cylinder discrimination rotor with one protrusion. On the other hand, an ignition pulse detection sensor 58 and a cylinder discrimination sensor 60 are installed in the housing of the distributor at positions corresponding to the respective rotors.
is installed.
本発明に従い、各燃料噴射弁34a〜34dは
たとえば、奇数番号の気筒と偶数番号の気筒とを
組合わせて1つのグループとし、4つの気筒を2
つのグループに分割する。すなわち、エンジンの
前方つまり第1図の右方より数えて第1番目の気
筒の燃料噴射弁34aと第4番気筒の燃料噴射弁
34dをグループとし、第2番気筒と第3番気
筒の燃料噴射弁34b,34cをグループとす
る。そして、これら2グループの噴射弁は噴射弁
駆動回路62によつて点火順次に従い所定の点火
時期間隔をもつて作動させる。 According to the present invention, each fuel injector 34a-34d is configured, for example, by combining odd-numbered cylinders and even-numbered cylinders into one group, and by combining four cylinders into two groups.
into two groups. That is, the fuel injection valve 34a of the first cylinder and the fuel injection valve 34d of the fourth cylinder counted from the front of the engine, that is, from the right side of FIG. The injection valves 34b and 34c are grouped. These two groups of injection valves are operated by the injection valve drive circuit 62 at predetermined ignition timing intervals according to the ignition order.
第3図はこの噴射弁駆動回路62を含む電子制
御式燃料噴射装置のブロツク図で、デイストリビ
ユータ56の点火パルス検出センサ58(第1図
参照)は波形整形器64およびフリツプフロツプ
66を介して電子制御ユニツト26およびシフト
レジスタ68の一方の入力端子に接続されてい
る。一方、デイストリビユータ56に設けた気筒
判別センサ60は他の波形整形器70を介してシ
フトレジスタ68の他方の入力端子に接続されて
いる。電子制御ユニツト26の燃料噴射指令信号
出力部およびシフトレジスタ68の出力部は
ANDゲート72,72′の入力部に夫々接続され
ている。各ANDゲート72,72′は抵抗を介し
てトランジスタ74,74′のベースに接続され
ている。各トランジスタ74,74′のコレクタ
は各燃料噴射弁のソレノイド76a〜76dを介
して電源に接続され、エミツタは接地されてい
る。なお、ソレノイド76aは第1番気筒に、7
6bは第2番気筒に、76cは第3番気筒に、7
6dは第4番気筒の燃料噴射弁に夫々対応してい
る。 FIG. 3 is a block diagram of an electronically controlled fuel injection system including this injection valve drive circuit 62, in which the ignition pulse detection sensor 58 (see FIG. 1) of the distributor 56 is connected via a waveform shaper 64 and a flip-flop 66. It is connected to one input terminal of electronic control unit 26 and shift register 68. On the other hand, the cylinder discrimination sensor 60 provided in the distributor 56 is connected to the other input terminal of the shift register 68 via another waveform shaper 70. The fuel injection command signal output section of the electronic control unit 26 and the output section of the shift register 68 are
They are connected to the inputs of AND gates 72 and 72', respectively. Each AND gate 72, 72' is connected to the base of a transistor 74, 74' via a resistor. The collector of each transistor 74, 74' is connected to a power source via a solenoid 76a-76d of each fuel injection valve, and the emitter is grounded. Note that the solenoid 76a is connected to the No. 1 cylinder.
6b is for the second cylinder, 76c is for the third cylinder, 7
6d corresponds to the fuel injection valve of the fourth cylinder.
次に第4図以下の図面を参照してこの電子制御
式燃料噴射装置の作動を説明する。エンジンのク
ランク軸に連動してデイストリビユータ56の点
火パルス発生用ロータが回転するに伴い点火パル
ス検出センサ58は電気信号を出力する。この電
気信号を波形整形器64で整形して第4図aのパ
ルス信号を得る。このパルス信号をフリツプフロ
ツプ66で分周して第4図bのパルス信号を得て
これをシフトレジスタ68の一方の端子に入力す
る。シフトレジスタの他方の端子には気筒判別セ
ンサ60からの信号をシフトパルスとして入力す
る。このため第4図bのパルス信号は順次右方に
シフトされ、シフトレジスタ68は各ANDゲー
ト72,72′に対して第4図c,dのいずれか
対応するパルス信号を出力する。他方、電子制御
ユニツト26は周知の如くエアフローメータ18
からの信号と点火信号によつて噴射量を決定し、
ANDゲート72,72′に向つて第4図eに示し
た燃料噴射指令信号を出力している。したがつ
て、各ANDゲート72,72′は第4図c,dの
パルスと同図eのパルスが重複する時期にのみ
“1”の信号を出力する。この出力信号にトリツ
ガされて各トランジスタ74,74′のコレクタ
とエミツタが導通し、各グループの燃料噴射系の
ソレノイド76a〜76dに電流が流れて燃料が
噴射される。トランジスタ74が導通した時には
グループすなわち第1、第4気筒の噴射弁34
a,34dが作動し、トランジスタ74′が導通
した時にはグループすなわち第2、第3気筒の
噴射弁34b,34cが作動する。この状態は従
来の方式による場合と対比して示した第5図の噴
射タイミングチヤートから明らかであろう。第5
図aは従来の方式による場合で、360゜間隔の同じ
時期に全気筒に対して一斉に燃料噴射を行つてい
るが、本発明の図示実施例の場合は、第5図bの
ように、2つのグループを交互に180゜間隔で作動
させて、各燃料噴射弁はクランク軸1回転に1度
の割合で、1サイクルの燃料噴射量の2分の1ず
つの燃料の噴射を行つている。 Next, the operation of this electronically controlled fuel injection system will be explained with reference to the drawings from FIG. 4 onwards. As the ignition pulse generation rotor of the distributor 56 rotates in conjunction with the crankshaft of the engine, the ignition pulse detection sensor 58 outputs an electrical signal. This electrical signal is shaped by a waveform shaper 64 to obtain the pulse signal shown in FIG. 4a. This pulse signal is frequency-divided by a flip-flop 66 to obtain the pulse signal shown in FIG. A signal from the cylinder discrimination sensor 60 is input as a shift pulse to the other terminal of the shift register. Therefore, the pulse signal of FIG. 4b is sequentially shifted to the right, and the shift register 68 outputs the corresponding pulse signal of either FIG. 4c or d to each AND gate 72, 72'. On the other hand, the electronic control unit 26 controls the air flow meter 18 as is well known.
The injection amount is determined by the signal from the ignition signal and the ignition signal.
A fuel injection command signal shown in FIG. 4e is outputted to the AND gates 72 and 72'. Therefore, each AND gate 72, 72' outputs a signal of "1" only when the pulses c and d in FIG. 4 overlap with the pulses e in the same figure. Triggered by this output signal, the collector and emitter of each transistor 74, 74' become conductive, and current flows through the solenoids 76a to 76d of the fuel injection system of each group to inject fuel. When the transistor 74 is conductive, the injection valves 34 of the group, that is, the first and fourth cylinders
When the injectors a and 34d are activated and the transistor 74' is conductive, the injection valves 34b and 34c of the group, that is, the second and third cylinders are activated. This condition will be clear from the injection timing chart in FIG. 5, which is shown in comparison with the conventional method. Fifth
Figure a shows a conventional system in which fuel is injected to all cylinders at the same time at 360° intervals, but in the illustrated embodiment of the present invention, as shown in Figure 5b, The two groups are operated alternately at 180° intervals, and each fuel injection valve injects one-half of the fuel injection amount for one cycle at a rate of once per crankshaft revolution. .
従来の電子制御式燃料噴射システムに上記副吸
気通路式乱流発生方式を組合せた場合には、副吸
気通路の連通路を介して燃料が廻りこむ気筒(第
5図aに例示したクランク角180゜、540゜、900゜の
ように、燃料噴射開始からおよそ180゜の期間内に
吸気行程が来る気筒)と、燃料の廻りこみのない
気筒(第5図aに例示したクランク角360゜、720゜
のように、燃料噴射開始からおよそ180゜以上の期
間経過後に吸気行程が来る気筒)との空燃比は、
第6図aに示すように変動があつた。本発明は各
気筒の燃料噴射弁を2グループに分割し、各グル
ープの燃料噴射弁を点火順序に従つて所定の点火
時期間隔で作動させるので、連通管50を介して
廻り込む混合気流による寄与がどの気筒について
も同等の条件となる。このため、各気筒の空燃比
は第6図bに示したように均一となり、低負荷運
転時にトルク変動を最小にすることができる。 When the conventional electronically controlled fuel injection system is combined with the auxiliary intake passage type turbulence generation system, the cylinders (crank angle 180 as shown in FIG. cylinders whose intake stroke occurs within a period of approximately 180° from the start of fuel injection, such as cylinders with a crank angle of 360°, 540°, and 900°; The air-fuel ratio with a cylinder whose intake stroke comes after a period of approximately 180° or more after the start of fuel injection, such as 720°, is
There were fluctuations as shown in Figure 6a. In the present invention, the fuel injection valves of each cylinder are divided into two groups, and the fuel injection valves of each group are operated at predetermined ignition timing intervals according to the ignition order, so that the air-fuel mixture flow circulating through the communication pipe 50 contributes. is the same condition for all cylinders. Therefore, the air-fuel ratio of each cylinder becomes uniform as shown in FIG. 6b, and torque fluctuations can be minimized during low-load operation.
第1図は電子制御式燃料噴射装置を備えた4気
筒エンジンの全体配置図、第2図は第1図の−
断面図、第3図は噴射弁駆動回路のブロツク
図、第4図はパルス信号の経時変化を示す波形
図、第5図は噴射タイミングチヤート、第6図は
空燃比の変動を比較するグラフである。
12……吸気マニホールド、15……吸気マニ
ホールドの分枝管、20……スロツトルバルブ、
24……吸気ポート、26……電子制御ユニツ
ト、34……燃料噴射弁、40……補助絞り弁、
46……噴流ポート、48……吸気弁、50……
連通管、52……開口、62……噴射弁駆動回
路、66……フリツプフロツプ、68……シフト
レジスタ、72……ANDゲート、74……トラ
ンジスタ、76……噴射弁のソレノイド。
Figure 1 is an overall layout of a four-cylinder engine equipped with an electronically controlled fuel injection system, and Figure 2 is the same as in Figure 1.
Figure 3 is a block diagram of the injection valve drive circuit, Figure 4 is a waveform diagram showing changes in pulse signals over time, Figure 5 is an injection timing chart, and Figure 6 is a graph comparing air-fuel ratio fluctuations. be. 12... Intake manifold, 15... Branch pipe of intake manifold, 20... Throttle valve,
24...Intake port, 26...Electronic control unit, 34...Fuel injection valve, 40...Auxiliary throttle valve,
46... Jet port, 48... Intake valve, 50...
Communication pipe, 52...Opening, 62...Injection valve drive circuit, 66...Flip-flop, 68...Shift register, 72...AND gate, 74...Transistor, 76...Injection valve solenoid.
Claims (1)
吸気通路に低負荷運転時にほぼ全閉される補助吸
気絞弁をそれぞれ設けると共に、上記主吸気絞弁
と上記補助吸気絞弁との間の吸気通路区間から分
岐し上記補助吸気絞弁をバイパスして各気筒の吸
気弁近傍に開口する噴流ポートを相互に連通状態
として副吸気通路を形成し、機関の低負荷運転時
において或る気筒が吸入行程になつたときには吸
入行程にない他の気筒の吸気通路から上記副吸気
通路を通じて吸気を誘引して上記吸入行程にある
気筒の上記吸気通路へ上記噴流ポートから吸気を
噴出させるようにし、さらに、各気筒の上記吸気
通路内の上記補助吸気絞弁と上記噴流ポートの開
口との間に開口するように、各気筒のための燃料
噴射弁をそれぞれ設けると共に、各気筒の上記燃
料噴射弁を気筒数の半数ずつの2グループに分割
し、各グループの上記燃料噴射弁が点火順序に従
つて所定の点火時期間隔で作動するように構成し
たことを特徴とする多気筒内燃機関の電子制御式
燃料噴射装置。1. An auxiliary intake throttle valve that is almost fully closed during low-load operation is provided in the intake passage of each cylinder downstream of the main intake throttle valve of a multi-cylinder internal combustion engine, and an auxiliary intake throttle valve is provided between the main intake throttle valve and the auxiliary intake throttle valve. A sub-intake passage is formed by connecting jet ports that branch from the intake passage section of the engine and bypass the auxiliary intake throttle valve and open near the intake valves of each cylinder to form an auxiliary intake passage. When the engine enters the intake stroke, intake air is induced through the auxiliary intake passage from the intake passages of other cylinders that are not in the intake stroke, and the intake air is jetted from the jet port to the intake passage of the cylinder that is in the intake stroke; Further, a fuel injection valve for each cylinder is provided so as to open between the auxiliary intake throttle valve in the intake passage of each cylinder and the opening of the jet port, and the fuel injection valve for each cylinder is electronic control for a multi-cylinder internal combustion engine, characterized in that the engine is divided into two groups each having half the number of cylinders, and the fuel injection valves of each group are configured to operate at predetermined ignition timing intervals according to the ignition order. type fuel injection device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56117149A JPS5828551A (en) | 1981-07-28 | 1981-07-28 | Electronically controlled fuel injector for multicylinder internal combustion engine with auxiliary intake passages |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56117149A JPS5828551A (en) | 1981-07-28 | 1981-07-28 | Electronically controlled fuel injector for multicylinder internal combustion engine with auxiliary intake passages |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5828551A JPS5828551A (en) | 1983-02-19 |
| JPH0245029B2 true JPH0245029B2 (en) | 1990-10-08 |
Family
ID=14704670
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP56117149A Granted JPS5828551A (en) | 1981-07-28 | 1981-07-28 | Electronically controlled fuel injector for multicylinder internal combustion engine with auxiliary intake passages |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5828551A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0720974U (en) * | 1991-04-23 | 1995-04-18 | 株式会社徳安 | Earpick |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0528362Y2 (en) * | 1985-06-03 | 1993-07-21 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6041210B2 (en) * | 1977-04-14 | 1985-09-14 | ヤマハ発動機株式会社 | engine intake system |
| JPS6011211B2 (en) * | 1978-05-24 | 1985-03-23 | 株式会社日立製作所 | Fuel injection system for even-numbered cylinder engines |
-
1981
- 1981-07-28 JP JP56117149A patent/JPS5828551A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0720974U (en) * | 1991-04-23 | 1995-04-18 | 株式会社徳安 | Earpick |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5828551A (en) | 1983-02-19 |
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