JPH0245027B2 - - Google Patents
Info
- Publication number
- JPH0245027B2 JPH0245027B2 JP56117145A JP11714581A JPH0245027B2 JP H0245027 B2 JPH0245027 B2 JP H0245027B2 JP 56117145 A JP56117145 A JP 56117145A JP 11714581 A JP11714581 A JP 11714581A JP H0245027 B2 JPH0245027 B2 JP H0245027B2
- Authority
- JP
- Japan
- Prior art keywords
- intake
- cylinder
- fuel injection
- throttle valve
- fuel
- 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
燃料供給量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. This eliminates the fuel distribution problems inherent in carburetor systems, allowing the engine to run with a leaner combustion mixture. to
It is possible to reduce the generation of harmful unburned organisms such as HC and CO. 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. In the latter system, an electromagnetic fuel injection valve is used which is opened and closed by a solenoid, which is energized by injection commands in the form of pulses from an electronic control unit, typically 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および低速高
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、主吸気絞弁の下流において吸気マニホルドの
各分枝管内の各吸気通路に第2の吸気絞弁を個々
に設けると共に、吸気弁近傍において各気筒の吸
気ポート内に開口する小径の噴流ポートを各気筒
ごとに設け、上記噴流ポートを共通の連通管によ
つて互いに連通し、もつて機関の低速運転時にお
いて或る気筒が吸気行程になつた時には吸気行程
にない他の気筒の吸気ポートから吸気を誘引して
該吸気行程にある気筒の吸気ポートに該噴流ポー
トから空気を噴出せしめて燃焼室内に強度の乱流
を発生させ、これによつて低速運転時の燃焼改善
を行いつつ高速運転時の出力を確保することが提
案されている(特開昭55−25547)。この方式を以
下では便宜上強誘引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 has a straight vent to maximize power output during high-load, high-speed operation. Designed to have a low resistance shape. 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 and low-speed, high-load operation, which increases the flame propagation speed. I can't. 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 second intake throttle valve is individually provided in each intake passage in each branch pipe of the intake manifold downstream of the main intake throttle valve, and a second intake throttle valve is individually provided in each intake passage in each branch pipe of the intake manifold, and a second intake throttle valve is installed in each intake port of each cylinder near the intake valve. Each cylinder is provided with a small-diameter jet port that opens into the cylinder, and the jet ports are communicated with each other through a common communication pipe, so that when a certain cylinder enters the intake stroke during low-speed operation of the engine, the jet port enters the intake stroke. Intake air is induced from the intake ports of other cylinders that are currently in the intake stroke, and the air is jetted from the jet ports to the intake ports of the cylinders that are in the intake stroke, thereby generating strong turbulence in the combustion chamber, thereby causing a strong turbulent flow during low-speed operation. It has been proposed to secure output during high-speed operation while improving combustion of the engine (Japanese Patent Laid-Open No. 55-25547). For convenience, this method will be abbreviated as the forcible attraction turbulence generation method hereinafter.
ところで、従来の気化器を有するエンジンに上
記強誘引乱流発生方式を応用する場合には、噴流
ポート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
が各噴流ポート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強誘引乱流発生方式と
を組合せると、気筒間の燃料分配が悪化し、誘引
乱流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 forced turbulence generation method to an engine with a conventional carburetor, the jet port is located downstream of the main throttle valve of the carburetor, and a homogeneous air-fuel mixture is formed in the carburetor. , even if the air-fuel mixture is divided into each jet port, the fuel distribution between the cylinders will not deteriorate. However, when a fuel injection method that simultaneously injects fuel into each branch pipe of the intake manifold or individual intake ports is combined with the above-mentioned forced turbulence generation method, the fuel distribution between the cylinders deteriorates and the induced turbulence There was a problem in that the combustion improvement effect was attenuated by the fluctuations in the air-fuel ratio between cylinders, resulting in increased 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
上記強誘引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および低速高負荷運転時の
トルク変動を防止しより稀薄(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。 SUMMARY OF THE INVENTION An object of the present invention is to solve the above-mentioned problems, and to provide a fuel supply device that does not cause deterioration in fuel distribution even when an electronically controlled fuel injection system is combined with the above-mentioned forcibly induced turbulent flow generation method. This ensures output during high-speed, high-load operation, prevents torque fluctuations during low-speed, low-load operation, and low-speed, high-load operation, and enables the engine to operate with a leaner combustion mixture. The aim is to improve fuel efficiency and 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噴流ポ
ートならび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
かる事態を防止するため、多気筒内燃機関の主吸
気絞弁の下流において各吸気通路に第2の吸気絞
弁をそれぞれ設けると共に、吸気弁近傍において
各気筒の吸気ポート内に開口する小径の噴流ポー
トを各気筒ごとに設け、上記噴流ポートを共通の
連通管によつて互いに連通し、もつて上記第2の
吸気絞弁をほぼ全閉とする機関の低速運転時にお
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ポートから吸気を誘引し
て上記吸入行程にある気筒の吸気ポートに上記噴
流ポートから吸気を噴出させるようにし、さら
に、各気筒の上記吸気ポート内の上記第2の吸気
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、上記各気筒の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 deterioration in fuel distribution is caused by fuel that is injected simultaneously at a certain time and remains in the intake port of each cylinder, and when a certain cylinder enters the intake stroke, it circulates through the jet port and the communication pipe. This is based on the knowledge that this is due to the fact that the amount of fuel sucked into that cylinder gradually decreases as a result, the amount of fuel sucked into the other cylinders that subsequently enter the intake stroke sequentially, and the present invention aims to prevent such a situation. , a second intake throttle valve is provided in each intake passage downstream of the main intake throttle valve of a multi-cylinder internal combustion engine, and a small diameter jet port that opens into the intake port of each cylinder near the intake valve is provided for each cylinder. and the jet ports are communicated with each other through a common communication pipe, so that when a certain cylinder enters the intake stroke during low-speed operation of the engine with the second intake throttle valve substantially fully closed, the second intake throttle valve is substantially fully closed. Intake air is induced from the intake ports of other cylinders that are not in the intake stroke, and the intake air is jetted from the jet port to the intake ports of the cylinders that are in the intake stroke, and further, the second intake air in the intake ports of each cylinder is A fuel injection valve is provided for each cylinder so as to open between the throttle valve and the opening of the jet port, and the fuel injection valves of each cylinder are divided into two groups each having half the number of cylinders. The present invention proposes an electronically controlled fuel injection system for a multi-cylinder internal combustion engine, characterized in that a group of fuel injection valves is configured to operate at predetermined ignition timing intervals according to the ignition order.
以下、添付図面を参照して実施例を説明する。 Hereinafter, embodiments will be described 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ールド付きサージタンク12
が装着されている。このサージタンク12は本体
部分から各吸気ポートに向つて延長する4本の吸
気マニホールド分枝管14を一体に備えている。
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12に導かれ、そこから吸気マニホ
ールド14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、エンジン回転センサ
(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。吸気マニホールド分枝管14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3
8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26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 a cylinder head 6 is provided between the cylinder bore 2, the piston 8 that reciprocates therein, and the cylinder head 6. A combustion chamber 10 is formed. A surge tank 12 with an intake manifold is located on the side of the cylinder head 6.
is installed. This surge tank 12 is integrally equipped with four intake manifold branch pipes 14 extending from the main body toward each intake port.
Intake air is led to the surge tank 12 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 14. The air is sucked into the combustion chamber 10 through an intake port 24 which has been opened. 26 is a well-known electronic control unit (ECU) with a built-in microcomputer.
The intake air amount signal from the air flow meter 18, the intake temperature signal from the intake temperature sensor 28 provided on the air flow meter, the signal from the throttle position sensor 30 provided on the throttle body 22, the signal from the cooling water temperature sensor 32, and the engine. This is for inputting signals from a rotation sensor (not shown), etc., calculating the fuel injection amount, and outputting a fuel injection command signal. Fuel injection valves 34a to 34d are installed in the intake manifold branch pipe 14 for each cylinder. Each fuel injection valve 34 is connected to a fuel hose 36 and a delivery pipe 3 from a fuel pump (not shown).
Fuel is supplied via step 8. The fuel injection valve 34 is a known electromagnetic injection valve having a solenoid, and injects fuel toward the intake port 24 in response to an injection command signal from the electronic control unit 26.
各吸気マニホールド分枝管14には第2の吸気
絞り弁40a〜40dが設けてあり、これらはリ
ンク機構42により連動されるようになつてい
る。リンク機構42はたとえば特開昭55−75531
に開示されているような制御弁44により制御す
るダイヤフラム装置46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第2絞り弁4
0を回動して分枝管14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には吸気ポート24に略々平行に小径の噴流
ポート48a〜48d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図に点線したところから明らかなよう
に、吸気弁50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48から噴射された時には
燃焼室内に強度の乱流が発生せられるようになつ
ている。第2図から明らかなように、各噴流ポー
ト48は吸気マニホールド付きサージタンク12
の下部に形成した長手方向に延長する連通路52
によつて互いに連通している。このような構成で
あるから、エンジンの低速運転時に第2絞弁40
a〜40dが全閉された時において或る気筒が吸
気行程に入つた時には、その気筒の噴流ポート4
8には連通路52ならびに吸気行程にない他の気
筒の噴流ポートを経由して当該他の気筒の吸気ポ
ートから混合気が誘引され、吸気行程にある気筒
の吸気ポートにその噴流ポートから噴出せられ
る。このため、その気筒の燃焼室内には強度の乱
流が発生する。この関係は他の気筒が順次吸気行
程に入つた時も同様である。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ロー
タが取付けてあり、他方、デイストリビユータ5
6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 14 is provided with second intake throttle valves 40a to 40d, which are linked by a link mechanism 42. The link mechanism 42 is, for example, disclosed in Japanese Patent Application Laid-Open No. 55-75531.
The second throttle valve 4 is linked to the output shaft of a diaphragm device 46 which is controlled by a control valve 44 as disclosed in .
0 can be rotated to substantially block the main air passage within the branch pipe 14. On the other hand, small diameter jet ports 48a to 48d are formed in the cylinder head 6 approximately parallel to the intake port 24 for each cylinder. As is clear from the cross section shown in FIG. 2 and the dotted line in FIG. 1, these jet ports open near the terminal end of the intake port 24 in a direction substantially tangential to the periphery of the intake valve 50. When air is injected from these jet ports 48, strong turbulence is generated within the combustion chamber. As is clear from FIG. 2, each jet port 48 is connected to a surge tank 12 with an intake manifold.
A communication path 52 extending in the longitudinal direction formed at the bottom of the
are connected to each other by. With such a configuration, the second throttle valve 40 is closed during low-speed operation of the engine.
When a certain cylinder enters the intake stroke when a to 40d are fully closed, the jet port 4 of that cylinder
8, the air-fuel mixture is induced from the intake port of the other cylinder via the communication passage 52 and the jet port of the other cylinder that is not in the intake stroke, and is ejected from the jet port to the intake port of the cylinder that is in the intake stroke. It will be done. Therefore, strong turbulence occurs within the combustion chamber of that cylinder. This relationship holds true even when the other cylinders sequentially enter their intake strokes. At the bottom of FIG. 1, the reference number 56 indicates 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, the data distributor 5
An ignition pulse detection sensor 58 and a cylinder discrimination sensor 60 are installed in the housing 6 at positions corresponding to the respective rotors.
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によつて点火順序に従い所定の点火
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、
76d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,
76d corresponds to the fuel injection valve of No. 4 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1
8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弁の
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
の割合いで、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 1 as is well known.
The injection amount is determined based on the signal from 8 and the ignition signal, and the fuel injection command signal shown in FIG. 4e is outputted to the AND gates 72 and 72'. Therefore, each AND gate 72, 72' is
A signal of "1" is output only when the pulse shown in FIG. 1 overlaps with the pulse shown in FIG. Triggered by this output signal, the collector and emitter of each transistor 74, 74' are brought into conduction, and current flows through solenoids 76a to 76d of the fuel injection valves 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 half of the fuel injection amount for one cycle at a rate of once per crankshaft revolution.
The fuel is injected separately.
従来の電子制御式燃料噴射システムに上記強誘
引乱流発生方式を組合せた場合には、噴流ポート
および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に比較して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 above-mentioned forcibly induced turbulent flow generation method is combined with a conventional electronically controlled fuel injection system, the cylinder (fifth
cylinders where the intake stroke occurs within a period of approximately 180° from the start of fuel injection, such as those at crank angles of 180°, 540°, and 900° illustrated in Figure a), and cylinders in which fuel does not circulate (Fig. 5a). As shown in Fig. 6a, the air-fuel ratio with the cylinder whose intake stroke comes approximately 180° or more after the start of fuel injection fluctuated 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 contribution from the air mixture flowing around through the communication pipe is reduced. The conditions are the same for all cylinders. Therefore, the air-fuel ratio of each cylinder is
As shown in comparison with FIG. b, the torque becomes uniform, 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…吸気マニホールド付きサージタンク、1
4…吸気マニホールド分枝管、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…第2吸気絞り
弁、48…噴流ポート、50…吸気弁、52…連
通路、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...Surge tank with intake manifold, 1
4... Intake manifold branch pipe, 20... Throttle valve, 24... Intake port, 26... Electronic control unit, 34... Fuel injection valve, 40... Second intake throttle valve, 48... Jet port, 50... Intake valve, 52 ...Communication path, 62...Injection valve drive circuit, 66...Flip-flop, 68...Shift register, 72...AND gate, 74...Transistor, 76...Injection valve solenoid.
Claims (1)
各吸気通路に第2の吸気絞弁をそれぞれ設けると
共に、吸気弁近傍において各気筒の吸気ポート内
に開口する小径の噴流ポートを各気筒ごとに設
け、上記噴流ポートを共通の連通管によつて互い
に連通し、もつて上記第2の吸気絞弁をほぼ全閉
とする機関の低速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
吸気ポートから吸気を誘引して上記吸入行程にあ
る気筒の吸気ポートに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
ポート内の上記第2の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、上記各気筒の
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. A second intake throttle valve is provided in each intake passage downstream of the main intake throttle valve of a multi-cylinder internal combustion engine, and a small diameter jet port that opens into the intake port of each cylinder near the intake valve is provided for each cylinder. and the jet ports are communicated with each other through a common communication pipe, so that when a certain cylinder enters the intake stroke during low-speed operation of the engine with the second intake throttle valve substantially fully closed, the second intake throttle valve is substantially fully closed. Intake air is induced from the intake ports of other cylinders that are not in the intake stroke, and the intake air is jetted from the jet port to the intake ports of the cylinders that are in the intake stroke, and further, the second intake air in the intake ports of each cylinder is A fuel injection valve is provided for each cylinder so as to open between the throttle valve and the opening of the jet port, and the fuel injection valves of each cylinder are divided into two groups each having half the number of cylinders. An electronically controlled fuel injection system for a multi-cylinder internal combustion engine, characterized in that a group of fuel injection valves is configured to operate at predetermined ignition timing intervals according to the ignition order.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56117145A JPS5828548A (en) | 1981-07-28 | 1981-07-28 | Electronically controlled fuel injector for multicylinder internal-conbustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56117145A JPS5828548A (en) | 1981-07-28 | 1981-07-28 | Electronically controlled fuel injector for multicylinder internal-conbustion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5828548A JPS5828548A (en) | 1983-02-19 |
| JPH0245027B2 true JPH0245027B2 (en) | 1990-10-08 |
Family
ID=14704569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP56117145A Granted JPS5828548A (en) | 1981-07-28 | 1981-07-28 | Electronically controlled fuel injector for multicylinder internal-conbustion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5828548A (en) |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| JPS5525547A (en) * | 1978-08-10 | 1980-02-23 | Toyota Motor Corp | Suction device of multicylinder internal combustion engine |
-
1981
- 1981-07-28 JP JP56117145A patent/JPS5828548A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5828548A (en) | 1983-02-19 |
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