JPS5828550A - Electronically controlled fuel injector for multicylinder internal combustion engine with auxiliary intake passages - Google Patents

Electronically controlled fuel injector for multicylinder internal combustion engine with auxiliary intake passages

Info

Publication number
JPS5828550A
JPS5828550A JP56117148A JP11714881A JPS5828550A JP S5828550 A JPS5828550 A JP S5828550A JP 56117148 A JP56117148 A JP 56117148A JP 11714881 A JP11714881 A JP 11714881A JP S5828550 A JPS5828550 A JP S5828550A
Authority
JP
Japan
Prior art keywords
intake
fuel injection
fuel
cylinder
valves
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.)
Granted
Application number
JP56117148A
Other languages
Japanese (ja)
Other versions
JPH0245028B2 (en
Inventor
Hidetaka Nohira
野平 英隆
Hideaki Matsui
英昭 松井
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP56117148A priority Critical patent/JPS5828550A/en
Publication of JPS5828550A publication Critical patent/JPS5828550A/en
Publication of JPH0245028B2 publication Critical patent/JPH0245028B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/32Controlling fuel injection of the low pressure type
    • F02D41/36Controlling fuel injection of the low pressure type with means for controlling distribution
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

Abstract

PURPOSE:To improve the performance of an engine including auxiliary intake passages for conducting intake jets to the combustion chambers when the load on the engine is light, by operating the fuel injection valves of the cylinders in their ignition order to keep the distribution of fuel appropriate. CONSTITUTION:In a four-cylinder engine, auxiliary intake throttle valves 40a- 40d are provided in intake passages 15a-15d ramified from a surge tank 14 to the cylinders and auxiliary intake passages including jet ports 48a-48d opened near intak valves are provided detouring the auxiliary intake throttle valves. Fuel injection valves 34a-34d are installed downstream to the throttle valves 40a-40d. The injection valves 34a-34d are operated in prescribed ignition order by an injection valve drive circuit 62 which is regulated by an electronic controller 26 which determines an injected fuel quantity on the basis of an ignition signal and the air flow rate signal of an air flow meter 18 and sends out a fuel injection instructing signal.

Description

【発明の詳細な説明】 本vhW14は火花点火式内燃機関O燃料供給技術に係
り、よ1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 vhW14 relates to a spark ignition internal combustion engine O fuel supply technology, and more specifically, 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。
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 perspectives including exhaust gas countermeasures. .

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、各気筒の吸気ボートととに夫々−個の燃
料噴射弁を設は各噴射弁に#′i互いに畔量O憔料を噴
射させるととによシ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IIK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
シ稀薄(リーン)なII!鋳用混用混合物転することを
可能にしてHC。
That is, the main advantage of the fuel injection method in a spark-ignition internal combustion engine is that by providing two fuel injection valves in each cylinder's intake boat, each injection valve can inject a similar amount of fuel to each other. Since it is possible to equalize the amount of fuel supplied to each combustion chamber, the problem of fuel distribution between cylinders inherent in the carbureted IIK system is solved, and as a result, the engine becomes leaner. Na II! HC making it possible to convert foundry mixtures.

COのような有害な未燃成生物の発生を低減すゐことが
できることにある。燃料噴射弁の作1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ノイドは=般にマイクロコ
ンビエータを内蔵し次電子制御ユニットからのパルスの
形の噴射指令によって励起されるようになっている。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、411i
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壜っており(同時噴射
方式)、晴射の回数はエンジンの咎作動すイクル?!!
1シ1回屯しくFi2回である。
It is possible to reduce the generation of harmful unburned organisms such as CO. The first method of making a fuel injection valve is a continuous injection method that injects fuel continuously from the injector, and a pulse injection method that injects fuel intermittently. It is adapted to be excited by an injection command in the form of a pulse. This system is called an electronically controlled fuel injection system (EFI), and the technology to which the present invention is directed also belongs to this system. In the conventional electronically controlled fuel injection system, 411i
The fuel injection timing is set so that all fuel injection valves are injected at the same time (simultaneous injection method), and the number of injections depends on the engine operating cycle. ! !
Fi is twice once in a row.

他方、燃料噴射方式であゐ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
フィ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W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ととができない。低速低負荷運転
時Kll入会合気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ュラφド
弁を用いたシ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0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1.る1絞り弁とその下流に位置して低負荷時に
のみ全閉さnる補助絞り弁とを設けるとと%に、1絞り
弁と補助絞シ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K111口する副吸気通路
分校管を分枝せしめ、上P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放し、もって低
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O発生を促進して燃焼改善を行いつつ、高負荷時KF
i主吸気通viを全開として吸気抵抗を最小とすゐこと
Kよりて出力の低下を防止することが提案されている傘
(特開昭53137320入こO方式を本明細書では、
便宜上、副吸気通路式乱流発止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. ◎ However, if the intake port is shaped like this, sufficient turbulence will not be generated in the mixture sucked into the combustion chamber during low-speed, low-negative W operation. ,
If the flame propagation speed is increased, the flame cannot be sharpened. A method of generating a turbulent flow of Kll air intensity during low-speed, low-load operation is to forcibly generate a swirling flow in the combustion chamber by making the intake port a helical shape or by using a shroud valve. However, these methods have a problem in that the ventilation resistance to the intake air mixture flow increases, resulting in a decrease in filling efficiency during high-speed, high-load operation. Therefore, in a carburetor type engine, artificially operated 1. If a first throttle valve and an auxiliary throttle valve located downstream of the first throttle valve are fully closed only at low loads, the main intake passage between the first throttle valve and the auxiliary throttle valve can be connected by a pipe. A sub-intake passage branch pipe is led to the communication pipe, and is branched from the communication pipe to the K111 outlet near the intake port, and a sub-intake passage that bypasses the auxiliary throttle valve is created with the upper P pipe, the communication passage, and the branch pipe. 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 promote the generation of turbulent O in the combustion chamber to improve combustion, while at high load the KF
In this specification, an umbrella (Japanese Patent Laid-Open No. 53137320) is proposed to prevent a decrease in output by fully opening the main intake vent vi to minimize intake resistance.
For convenience, this method will be abbreviated as the sub-intake passage type turbulence generation method.

とζろで、従来O気化IlIを有するエンジンに上配調
款気過酪式tilI発生方式を応用する場合には、剛職
気過ysoh枝管は気化−の1絞)弁の下流にあ〕、気
化器において均質な混合気が形成1れゐため、混合気が
副吸気通路の各分校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O!分
校管又は個々O吸気ポー)Klil!を同時噴射する慣
科噴射方式と上記mI甑気aS式tII−生方式とを組
合せ為と、気筒間O儀科分配が悪化し、副吸気通路によ
為悌焼改善効果が気前聞O1!犠比O変動に減殺畜れて
エンジンOトルタ変−が増大するという不具合があった
・ 零*@は上記不具合tS消することII的とす、&40
であって、電子制御式燃料噴射システムを上配剛獣気通
−弐ti+ui垂方決と組会せ穴と自にも燃料分配の墨
化し壜い燃料供給装置を提供すゐことにようて、高速高
負荷運転時O出力を確保するとともに低速低負荷運転時
Oトルク蜜lI管防止し稀薄(1−ン)1に燃gl用混
合物でエンジンを運転すること管可能にして悌費O改善
と有害排出ガス成分O低減を実現することta的とする
もOであゐ◎ 本発明は、上記燃料分配の悪化は、一定時期に同時噴射
畜れ各気筒の吸気ポート内に@冑している燃料が成る気
筒が吸気性11になった時に連通管を介して廻〕込んで
その気筒Ka人されそO結果後続して順次吸気行llK
入ゐ他O丸部O眼入燃料量が爾滅するととに因1%ので
あるという知見に立脚するもOで、本発明はかか1事■
を防止するtめ、各気筒の燃料噴射弁を点火順序に従っ
て順次作−させる同期独立噴射方式とすることt−提案
すゐ40である0 以下、添附図Nt参照して実施例を説−する01111
1は零鞄110電子制御式燃料噴射システムtAtたエ
ンジンの金体配置を示す園、II意図は第t yaor
x −n断面図である。園は4気筒エンジンを示すもの
で、周知Oようにシリンダポア2a〜24管形成したシ
リンダブ四ツタ4の上には勘弁系と吸排気ポートを具え
たシリンダヘッド6が麹着してあ)、シリンダボア2七
その中で往復動するピストン8とシリンダヘッド6との
聞には燃鉤寵10が**されている。シリンダヘッド6
0侮藺KFi黴気マニホールド12およびサージタンク
1゛4が頴次KII着されており、この吸気マニホール
ド13嬬シリンダヘツドSKm!す墨基部13と数基m
から延長する4つの分校管15a〜15dとから成る0
黴入空気はエアクリーナ16、吸入空気流量を計橢する
友めOエアフローメータ18、ス曹ットルパルプ20f
具えたスロットルボデー22を経てサージタンク14に
導かれ、そζかも吸気マニホールド12!!介してシリ
ンダヘッド6内に形成さfした吸気ポート24を経て燃
鉤宣l0Kl1人され為ようになりている026はマイ
ク四コンビ具−タtP!蔵した周知の電子制御:Lエツ
ト(ECU)で、エアフロメータ18からの吸気貴信4
j、 St−”fフロメータに設けた吸気温竜ンナ28
からO吸気温信号、スaットルがデー22に設けたス冨
ットルポジシ璽ンセンサ30からの信号、冷却水温令ン
サ32からO信号、エンジン回転数竜ンナ(a!!l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40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〜34
(iが設置しである0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
イド管有する全知の電磁式噴射弁で、電子制御ヱニット
26からの噴射指令信号に応じて燃料を吸気ポート24
に向って噴射する。
When applying the upper adjustment air overflow type TIL generation system to an engine that has a conventional O vaporization IlI, the rigid air overflow ysoh branch pipe is located downstream of the vaporization (one throttle) valve. ] Since a homogeneous air-fuel mixture is formed in the carburetor, even if the air-fuel mixture is divided into the branch pipes of the auxiliary intake passage, the fuel distribution between the cylinders will not deteriorate. However, the intake manifold is O! Branch tube or individual O intake port) Klil! Due to the combination of the conventional injection system that simultaneously injects the mI air and the above-mentioned mI air aS type tII-generation system, the oxygen distribution between the cylinders deteriorates, and the sub-intake passage improves the combustion performance. ! There was a problem in which the engine torque change increased due to the decrease in sacrifice ratio O fluctuation. ・Zero*@ is intended to eliminate the above problem tS, &40
The idea is to combine the electronically controlled fuel injection system with the upper rigid ventilation hole and the two vertical holes to provide a fuel supply device with a blackened fuel distribution system. It secures O output during high-speed, high-load operation, and prevents O-torque during low-speed, low-load operation, making it possible to run the engine with a dilute (1-ton) fuel mixture, thereby improving operating costs. The present invention aims to reduce the harmful exhaust gas components O◎ The present invention solves the above deterioration of fuel distribution by simultaneously injecting the fuel at a certain period of time and causing a drop in the intake port of each cylinder. When the cylinder that contains the fuel reaches the intake capacity 11, it flows through the communication pipe and flows into that cylinder.As a result, the intake line is sequentially
Based on the knowledge that the amount of fuel entering the eye is destroyed by 1%, the present invention is based on the following points.
In order to prevent this, a synchronous independent injection system is proposed in which the fuel injection valves of each cylinder are activated in sequence according to the ignition order.Hereinafter, embodiments will be described with reference to the attached drawings. 01111
1 shows the metal body arrangement of the engine with zero bag 110 electronically controlled fuel injection system tAt, II intention is the th yaor
It is an x-n sectional view. The figure shows a four-cylinder engine, and as is well known, a cylinder head 6 equipped with a valve system and intake/exhaust ports is attached on top of the four cylinder tabs 4 in which cylinder pores 2a to 24 are formed. 27 A fuel hook 10 is installed between the piston 8 and the cylinder head 6 that reciprocate therein. cylinder head 6
0 Intake KFi mold air manifold 12 and surge tank 1-4 are attached to KII, and this intake manifold 13 cylinder head SKm! Ink base 13 and several m
0 consisting of four branch pipes 15a to 15d extending from
For the moldy air, there is an air cleaner 16, a friend O air flow meter 18 that measures the intake air flow rate, and a sutotle pulp 20f.
It is guided to the surge tank 14 through the throttle body 22 equipped with it, and the intake manifold 12! ! 026, which is designed to be used as a fuel hook, is inserted through the intake port 24 formed in the cylinder head 6. Well-known electronic control system: The L-ET (ECU) controls the intake air flow from the air flow meter 18.
j, St-"f Intake temperature dragon installed in the flow meter 28
From the O intake temperature signal, the signal from the throttle position sensor 30 installed on throttle day 22, the O signal from the cooling water temperature sensor 32, the signal from the engine rotational speed sensor (a!!l not shown). , etc., to calculate the fuel injection amount and output the fuel injection command signal.◎The intake manifold 12 has fuel injection valves 34a to 34 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 an omniscient electromagnetic injection system having a solenoid pipe. A valve injects fuel into the intake port 24 in response to an injection command signal from the electronically controlled Enit 26.
Spray toward.

各吸気マニホールド分校管15には補助絞り弁401〜
40dが設けてあり、これらは共通の軸4mKXり連動
されるようKfkっている0軸42はたとえばv#[@
 55−75531 KR示すf’Lfいゐ制御弁44
によ)制御するダイヤフラムV&鐙46の出力にりンク
されて>1.エンジンの低負荷運転時には補助絞〕弁4
0を回動して分校管15内O主空気通路を実質上値断じ
得るよう罠なっている0一方、シリンダヘッド6には、
吸気ポート24に略々平行に4−、径の噴流ポート48
a〜48dが各気筒ごとに形成されているC、これらO
噴流ポートは、第2図に新面を示しかつ第1図に点−で
示したところから明らかなように、吸気弁!5GOJI
IIK対して略々接線方向にポート24f)終端部近傍
に開口しており、9気がこれらの噴流ポートから吸入さ
れた時には@焼室内に乱流ないしスツールが斃生される
ようになっている。各噴流ポート48は吸気で二ホール
ド120基部13内に形成した長手方向に延長する連通
路52によって互いに連通されておシ、一方、こO連通
Sはたとえば吸気マニホールド分枝管IBeの壁中に1
1成し*、ii路54によって補助絞9弁401傭路し
てサージタンク14t)Pl*Wc連通されている◎通
路s4、連通9152%噴流ポート481〜4g4が1
llIl気通路を構成する0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〜40纏が
全閉された時には吸入空気は専ら剛吸気通路から供給さ
n1懲焼室内に乱fLt発生させ為・第1図下方に参照
番号s6で示したのけディストリビ息−夕で、その回転
軸には8つの突起を有する態動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が取付けてあり
、他方、ディストリビ二一夕のハウジングtQj上配各
−−タに対応する位置において点火パルス検出センサ5
8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 has an auxiliary throttle valve 401 to
40d are provided, and these are Kfk so as to be interlocked by a common axis 4mKX.The 0 axis 42 is, for example, v#[@
55-75531 KR indicating f'Lf control valve 44
>1. Auxiliary throttle valve 4 when operating the engine at low load
On the other hand, in the cylinder head 6,
A 4-diameter jet port 48 substantially parallel to the intake port 24
a to 48d are formed for each cylinder C, these O
As is clear from the new surface of the jet port shown in Fig. 2 and indicated by a dot in Fig. 1, the intake valve! 5GOJI
Ports 24f) are opened in the vicinity of the terminal end in a direction approximately tangential to IIK, so that when air is sucked in from these jet ports, a turbulent flow or a stool is created in the firing chamber. . Each jet port 48 is in communication with each other by a longitudinally extending communication passage 52 formed in the base 13 of the two-fold 120, while this communication S is connected, for example, to the wall of the intake manifold branch pipe IBe. 1
1 completed*, the auxiliary throttle 9 valve 401 is connected to the surge tank 14t) Pl*Wc through the ii passage 54 ◎Passage s4, communication 9152% Jet ports 481 to 4g4 are
With this configuration, when the auxiliary throttle valves 40a to 40 are fully closed during low-load operation of the engine, intake air is exclusively supplied from the rigid intake passage, and no turbulence fLt occurs in the combustion chamber. In order to generate the ignition pulse, there is a distributing valve shown by the reference number s6 at the bottom of Figure 1, and its rotating shaft has a rotor for generating ignition pulses with eight protrusions and a rotor for cylinder discrimination having one protrusion. On the other hand, the ignition pulse detection sensor 5 is installed at a position corresponding to each rotor on the housing tQj of the distributor.
8 and a cylinder discrimination sensor 60 are installed.

各燃料噴射弁34a〜34dは噴射弁駆動回路62によ
りて点火順序に従りて順次に作動せられる0第311は
この噴射弁駆動回路62を含む電子制御式懺科吠射装置
のブロック図で、ディストリビ具−タ56の点火パルス
検出センサ58(@1図mmN)は波形整形器64およ
びフリップフロップ6・を介して電子制御ユニット26
およびシフトレジスI68の一方の入力端子に接続され
て−る・一方、ディストリビ為−夕56に設けた気筒判
別センt60は他の波形整形器70に勘弁してシフトレ
ジメタロ8の他方の入力端子に接続されている0電子制
御ユニツト26の燃料噴射指令信号出力Sおよびシフト
レジスタ680出力部はANDゲートγ2a〜72aの
入力部に夫々接続されてい為・各ANDゲート72a〜
72dは抵抗を介してトランジスタ74m−74dのペ
ースKg続されている。各トランジスタ74a〜74d
のコレクタは各悌料噴射、弁のンレノイド76a〜76
dl介して電源に接続され、工建ツタは接地されている
。なおソレノイド76鳳はIN番気筒に、76bFi第
2番気筒Km 76 cは第3香気筒に、76dは1l
l4番気筒に夫々対応している。
Each of the fuel injection valves 34a to 34d is sequentially operated by an injection valve drive circuit 62 according to the ignition order. 311 is a block diagram of an electronically controlled injection device including this injection valve drive circuit 62. , the ignition pulse detection sensor 58 (@1 mmN) of the distributor 56 is connected to the electronic control unit 26 via the waveform shaper 64 and the flip-flop 6.
and one input terminal of the shift register I68. On the other hand, the cylinder discrimination center T60 provided in the distributor 56 is connected to the other input terminal of the shift register metal 8 in consideration of the other waveform shaper 70. The fuel injection command signal output S of the electronic control unit 26 and the output section of the shift register 680, which are connected to
72d is connected to the pace Kg of transistors 74m-74d via a resistor. Each transistor 74a to 74d
The collector is for each fuel injection, valve renoids 76a to 76.
It is connected to the power supply via dl, and the construction ivy is grounded. In addition, solenoid 76 is installed in the IN cylinder, 76bFi 2nd cylinder Km 76c is installed in the 3rd cylinder, and 76d is installed in the 1L cylinder.
Each corresponds to the 14th cylinder.

次に第4図以下の図面を参照してこの電子制御式I&料
噴射製置の作動を説明する。エンジンのクランク軸に連
動してディストリビ為−夕56の点火パルス発生用ロー
タが回転す石に伴い点火パルス検出センナ58は電気信
号を出力する。この電気償考を波形整形器64で整形し
て@4図(a)のパルス信号を得る。このパルス信号を
7リツプ70ツブ66で分周してIIE4図ら)のパル
ス信号を得てこれをシフ)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図ら)のパルス信号は順次右方にシフトさn
、シフトレジスタ68は各ANDゲート72に対して第
4図(c)〜(f)のいずれか対応するパルス信号を出
力する。他方、電子制御ユニット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って噴射量
を決定し、ANDゲート72に向ってI!4図(g)K
示しえ燃料噴射指令信号を出力してしる。したがって、
各ANDゲート72a〜72dは第4図(c)〜(f)
のパルスと同図−)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nて
各トランジスタ74a〜74dのコレクタとエミッタが
導通し、燃料噴射弁のツレノイド76&〜76dK電流
が流れて燃料が噴射される。第3図において燃料噴射弁
のソレノイドは上より第1.@3.第4、第2気筒のも
のく対応しており、各気筒の点火もこの順序で行われる
ので、燃料の噴射も点火順序に従って行われること[す
る。この状MIfi従来の方式による場合と対比して示
し友11E5Zの噴射タイミングチャートから明らかで
あろう。
Next, the operation of this electronically controlled I&fuel injection system will be explained with reference to FIG. 4 and the subsequent drawings. As the ignition pulse generation rotor of the distributor 56 rotates in conjunction with the engine crankshaft, the ignition pulse detection sensor 58 outputs an electrical signal. This electrical compensation is shaped by a waveform shaper 64 to obtain the pulse signal shown in Figure 4 (a). This pulse signal is frequency-divided by a 7-rip, 70-rub 66 to obtain a pulse signal of IIE4, etc., which is input to one terminal of a shift register 68. 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 signals in Fig. 4, etc.) are sequentially shifted to the right.
, the shift register 68 outputs a pulse signal corresponding to one of FIGS. 4(c) to 4(f) to each AND gate 72. On the other hand, as is well known, the electronic control unit 26 determines the injection amount based on the signal from the air flow meter 18 and the ignition signal, and sends the I! to AND gate 72. Figure 4 (g) K
A fuel injection command signal is output. therefore,
Each AND gate 72a to 72d is shown in FIG. 4(c) to (f).
%1 only when the pulse of and the pulse of -) in the same figure overlap.
Outputs # signal. Triggered by this output signal, the collector and emitter of each of the transistors 74a to 74d are brought into conduction, and the current of the fuel injection valve's trenoid 76 and 76dK flows to inject fuel. In Fig. 3, the solenoid of the fuel injection valve is No. 1 from the top. @3. The fourth and second cylinders correspond to each other, and the ignition of each cylinder is performed in this order, so fuel injection is also performed in accordance with the ignition order. This situation will be clear from the injection timing chart of the MIFI 11E5Z, which is shown in comparison with the conventional MIFI system.

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
lL欅−生方式を組合せ次場合には、副吸気通−の連通
IIt介して燃料が廻シ込むので各気筒O!儀比はII
@It(a)に示すように変動があった。
In the next case where the conventional electronically controlled fuel injection system is combined with the auxiliary intake passage type lL keyaki method, fuel flows in through the auxiliary intake passage communication IIt, so that each cylinder O! Gihi is II
There were fluctuations as shown in @It(a).

零−明は各気筒O燃料噴射弁を点火順序に従って順次外
−させるので或ゐ気筒が吸気行1iKあると暑他O気箇
0徴気ボートから噴流ボートおよび連aIIを介して1
ll)込んで来る混合気の条件はどの気筒についても岡
等の条件となる0このため、各気筒o!!燃比は鶴6図
(b)に示しtように均一とな!、低負荷這運転にトル
ク変動を最小にすゐことがで自る0
Zero light sequentially removes each cylinder's O fuel injector according to the ignition order, so if a certain cylinder has an intake line of 1iK, the hot and other O air injectors will be injected from the air intake boat to the jet boat and through the series a II.
ll) The condition of the incoming air-fuel mixture is the Oka et al. condition for every cylinder. Therefore, each cylinder o! ! The fuel ratio is uniform as shown in Figure 6 (b)! , it is possible to minimize torque fluctuation during low load crawling operation.

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

1111Q嬬電子制御式燃料噴射装置を備えた4気筒ニ
シジンO倉体配Ii図、l!2図はIN図の■−[1l
l1図、Sa図は噴射弁駆動回路のブロック図、11g
4園はパルス信号の経時変化を示す波形図・第2園は噴
射タイ々ングチャート、第6図は空燃比o*−を比較す
るグラフである0 12−・−吸気マ二ホールド、15−−−・吸気i二ホ
ールドO分技管、20−・・・・・スロットルノくルプ
、24・・・・・・吸気ボート、26・・・・・・電子
制御ユニット、34・・・・・・燃料噴射弁、40・・
・・・・補助絞り弁、48・・・・・・噴流ボート、5
0・・・・・・吸気弁、52・・・・・・連通路、54
・・・・・・通路、62・・・・・・噴射弁駆動a路、
66・−・・・フリップフロップ、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0特許出願人 トlり自動阜工業株式金社 特許出胆代理人 弁理士 背 木    朗 弁理士 西 舘 和 之 弁理士 吉 1)正 行 弁理士 山 口 昭 之 第4図 (9) 第5囚 第6図
1111Q 4-cylinder Nishijin O-kura layout with electronically controlled fuel injection system Ii diagram, l! Figure 2 shows the IN diagram ■-[1l
Diagram l1 and diagram Sa are block diagrams of the injection valve drive circuit, 11g
Figure 4 is a waveform diagram showing changes in pulse signals over time, Figure 2 is an injection timing chart, and Figure 6 is a graph comparing air-fuel ratios o*-. ---Intake i two-hold O division tube, 20--throttle knob, 24--intake boat, 26--electronic control unit, 34--・・Fuel injection valve, 40・・
... Auxiliary throttle valve, 48 ... Jet boat, 5
0...Intake valve, 52...Communication path, 54
... Passage, 62 ... Injection valve drive path a,
66...Flip-flop, 68...Shift register, 72...AND gate, 74...
... Transistor, 76 ... Injection valve solenoid 0 Patent applicant Tori Jidofu Kogyo Co., Ltd. Patent attorney Akira Seki Patent attorney Kazuyuki Nishidate Patent attorney Yoshi 1) Masayuki Patent Attorney Akiyuki Yamaguchi Figure 4 (9) Prisoner 5 Figure 6

Claims (1)

【特許請求の範囲】[Claims] 多気筒内燃機関の主吸気絞弁下流の各吸気通路に低負荷
運転時にほぼ全閉されb補助吸気絞弁を設け、主吸気絞
弁と補助吸気絞弁との間の吸気通路区間から補助吸気絞
弁をバイパスして吸気弁近傍に開口する副吸気通路t−
設け、機関の低負荷運転時K11ll吸気通路から吸気
噴流を噴出せしめるようkした、aWk気通路を備えた
多気筒内燃機関のための電子制御式燃料噴射麹酸におい
て、各気筒の燃料噴射弁は各気筒O点火順序に従って順
次に作−名せるようにしたことを¥#黴とする電子制御
式燃料噴射麹酸。
An auxiliary intake throttle valve is installed in each intake passage downstream of the main intake throttle valve of a multi-cylinder internal combustion engine, and the auxiliary intake throttle valve is almost fully closed during low-load operation. Sub-intake passage t- which bypasses the throttle valve and opens near the intake valve
In an electronically controlled fuel injection koji acid for a multi-cylinder internal combustion engine equipped with an aWK air passage, the fuel injection valve of each cylinder is designed to inject an intake jet from the K11ll intake passage during low load operation of the engine. Electronically controlled fuel injection koji acid that can be created sequentially according to the ignition order of each cylinder.
JP56117148A 1981-07-28 1981-07-28 Electronically controlled fuel injector for multicylinder internal combustion engine with auxiliary intake passages Granted JPS5828550A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP56117148A JPS5828550A (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
JP56117148A JPS5828550A (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
JPS5828550A true JPS5828550A (en) 1983-02-19
JPH0245028B2 JPH0245028B2 (en) 1990-10-08

Family

ID=14704645

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56117148A Granted JPS5828550A (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) JPS5828550A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04343084A (en) * 1991-05-20 1992-11-30 Fujitsu Ten Ltd Fm-cw radar device
JPH05142337A (en) * 1991-11-22 1993-06-08 Fujitsu Ten Ltd Millimeter wave radar distance and velocity measuring device
US8618710B2 (en) 2010-11-26 2013-12-31 Siemens Aktiengesellschaft Wedge for a stator of a generator with preformed coil windings

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53137320A (en) * 1977-04-14 1978-11-30 Yamaha Motor Co Ltd Air intake system in engine
JPS54152712A (en) * 1978-05-24 1979-12-01 Hitachi Ltd Injection type fuel feeder for 6-cylinder engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53137320A (en) * 1977-04-14 1978-11-30 Yamaha Motor Co Ltd Air intake system in engine
JPS54152712A (en) * 1978-05-24 1979-12-01 Hitachi Ltd Injection type fuel feeder for 6-cylinder engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04343084A (en) * 1991-05-20 1992-11-30 Fujitsu Ten Ltd Fm-cw radar device
JPH05142337A (en) * 1991-11-22 1993-06-08 Fujitsu Ten Ltd Millimeter wave radar distance and velocity measuring device
US8618710B2 (en) 2010-11-26 2013-12-31 Siemens Aktiengesellschaft Wedge for a stator of a generator with preformed coil windings

Also Published As

Publication number Publication date
JPH0245028B2 (en) 1990-10-08

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