JPS60122240A - Fuel injector of engine - Google Patents

Fuel injector of engine

Info

Publication number
JPS60122240A
JPS60122240A JP58232165A JP23216583A JPS60122240A JP S60122240 A JPS60122240 A JP S60122240A JP 58232165 A JP58232165 A JP 58232165A JP 23216583 A JP23216583 A JP 23216583A JP S60122240 A JPS60122240 A JP S60122240A
Authority
JP
Japan
Prior art keywords
fuel injection
injection
timing
fuel
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP58232165A
Other languages
Japanese (ja)
Other versions
JPH0467578B2 (en
Inventor
Hiroyuki Oda
博之 小田
Takashige Tokushima
徳島 孝成
Akio Nagao
長尾 彰士
Sadashichi Yoshioka
吉岡 定七
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.)
Mazda Motor Corp
Original Assignee
Mazda 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 Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP58232165A priority Critical patent/JPS60122240A/en
Publication of JPS60122240A publication Critical patent/JPS60122240A/en
Publication of JPH0467578B2 publication Critical patent/JPH0467578B2/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
    • F02D41/34Controlling fuel injection of the low pressure type with means for controlling injection timing or duration
    • F02D41/345Controlling injection timing
    • 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 prevent blow-by of injected fuel in a system wherein the fuel injection completion timing of a fuel injection valve disposed in an intake port is set to the proximity of an intake valve closing timing by compensating the fuel injection completion timing to a slower timing in the operating range where much fuel is injected. CONSTITUTION:In operation of an engine, CPU15 reads and stores each signal of a pressure sensor 8, a water temperature sensor 9, a crank angle sensor 10 and an ignitionn switch 11. If the operation is not made for engine start, CPU computes a reference injection quantity from an engine rpm and a suction negative pressure, and compensates the reference injection quantity according to the temperature of cooling water so as to redetermine the reference injection quantity as an actual injection quantity. From the actual fuel injection quantity an injection angle theta is determined and from both suction valve fully-closed timing and specified-injection completion timing compensatory quantity, an injection completion timing thetaic is determined so as to determine whether theta is larger than the crank angle made between thetaic and an exhaust valve fully-closed timing, or not. If determination of YES is obtained, an injection start timing thetaio according to the injection angle theta is determined based on the timing thetaic, so as to control a fuel injection valve 6.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、エンジンの燃料噴射装置に関するものであ
る。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a fuel injection device for an engine.

〔従来技術〕[Prior art]

従来、特開昭56−148636号公報に示されるよう
に、高エンジン出力をあまり必要としない部分負荷領域
等においては吸気行程のほぼ後半に燃料を噴射して点火
プラグが位置する燃焼室の上層部分に混合気を、下層部
分に空気をそれぞれ成屓させ、その状態で燃焼を行なう
ようにしたものがある。
Conventionally, as shown in Japanese Unexamined Patent Application Publication No. 56-148636, in partial load regions where high engine output is not required, fuel is injected almost in the latter half of the intake stroke and the fuel is injected into the upper layer of the combustion chamber where the spark plug is located. There is one in which the air-fuel mixture is formed in the upper part and the air is formed in the lower part, and combustion is carried out in that state.

この方式の燃料噴射装置では、上層の混合気は点火プラ
グによりこれを着火し得る空燃比にすればよ(、一方下
層は空気のみ又は、非常に希薄な混合気であるため、全
体としての空燃比は非常にリーンとなって燃費を大幅に
改善でき、又NOx。
In this type of fuel injection system, the air-fuel mixture in the upper layer only needs to be brought to an air-fuel ratio that can be ignited using a spark plug (on the other hand, the air-fuel mixture in the lower layer is only air or has a very lean mixture, so the air-fuel mixture as a whole is The fuel ratio becomes extremely lean, which greatly improves fuel efficiency and reduces NOx.

CO等の未燃焼成分を低減できるという利点を有する。This has the advantage that unburned components such as CO can be reduced.

さらには燃焼室内の混合気層の領域が点火プラグに近い
狭い領域に集中して、エントガスプーンが空気又は非常
に薄い混合気で占められることから、混合気の異品燃焼
が発生しにくく、ノッキングの発生が少ないという利点
をも自するものである。
Furthermore, the mixture layer in the combustion chamber is concentrated in a narrow area near the spark plug, and the gas spoon is occupied by air or a very thin mixture, making it difficult for foreign mixture combustion to occur. It also has the advantage of less occurrence of knocking.

ところでこのような成層化燃焼を行なうようにL7だエ
ンジンの燃料噴射装置においては、燃料噴射の終了タイ
ミングは吸気ブrの全閉タイミングと一致さゼ爆のが望
ましいが、実際には吸気弁の全閉(=J近では吸気J1
′、のリフト量が小さく、1−分な通路面積を確保でき
ないこと、及び燃料pll射出燃焼室との間には一定の
距離があり、燃料が燃料噴射弁から燃焼室に到達するま
でに時間遅れがあること等の理由により、燃料噴射終了
タイミングを吸気弁仝閉タイミングa前に設定する・ゼ
・要がある。。
By the way, in the fuel injection system of the L7 engine that performs such stratified combustion, it is desirable that the end timing of fuel injection coincides with the fully closing timing of the intake valve, but in reality it is Fully closed (= intake J1 near J
', the lift amount is small and it is not possible to secure a 1-minute passage area, and there is a certain distance between the fuel injection valve and the combustion chamber, so it takes a long time for the fuel to reach the combustion chamber from the fuel injection valve. Due to reasons such as a delay, it is necessary to set the fuel injection end timing before the intake valve closing timing a. .

そして1.記従来公報記載の装置では、燃料噴射終了タ
イミングを吸気弁全閉タイミング以前の一定のクランク
角付;??に固定し、この噴射終了クランク角4−+7
置に基いて噴射開始クランク角位置を演算し、エンジン
の運転状態に応じた量の燃料を噴射供給するようζこし
ていた。
And 1. In the device described in the conventional publication, the fuel injection end timing is set to a certain crank angle before the intake valve fully closed timing; ? This injection end crank angle is 4-+7.
The injection start crank angle position was calculated based on the engine position, and the amount of fuel was injected and supplied according to the operating state of the engine.

しかしながらこの従来分轄記載の燃料噴射装置では、噴
射すべき燃料惜が増大すると、燃料噴射開始時期が早く
なゲ(吸気、 1〕1気弁のオーバラップ域内(吸、1
)F気jflのバルブリフ1−呈を示す第4図の1; 
各1:、R)の、7シ゛/り角()7置になることがあ
り、その場合には噴射燃料がそのまま排気系に吹き抜け
てしまい、燃焼性が悪化してエンジン出力が低下し、又
排気ガス中の未燃焼成分が増大してエミッションが悪化
するという問題があった。また燃料流量が多いことから
、燃料の気化n化が悪くなり、これによっても燃焼性が
iu(化するという問題があった。
However, in this conventional fuel injection device, when the amount of fuel to be injected increases, the fuel injection start timing becomes earlier (intake, 1) within the overlap region of the 1st valve (intake, 1st).
) 1 in Fig. 4 showing the valve rift 1 of F air jfl;
Each 1:, R) may be 7 degrees/angle () 7 positions, in which case the injected fuel will directly flow into the exhaust system, worsening combustibility and reducing engine output. There is also the problem that unburned components in the exhaust gas increase, resulting in worsening of emissions. Further, since the fuel flow rate is large, the vaporization of the fuel becomes poor, and this also causes the problem that the combustibility changes to IU().

〔発明の目的〕[Purpose of the invention]

この発明は、かかる問題点に泥ミ、燃料噴射♀の多い運
転領域において噴射燃料の吹き抜+Jを防止でき、又燃
料の気化霧化を促進できるエンジンの燃料噴射装置を提
供せんとするものである。
SUMMARY OF THE INVENTION The present invention aims to solve such problems by providing a fuel injection device for an engine that can prevent blow-out of injected fuel in an operating region where there is a lot of dirt and fuel injection, and can promote vaporization and atomization of fuel. be.

〔発明の構成〕[Structure of the invention]

そこでこの発明は、燃料噴射量の多い運転領域において
は、燃料噴射開始時期を所定クランク角位置より前には
進めないようにし、これにより噴射燃料の吹き抜けを防
止し、燃料噴射路rIL’1期を遅れ側に補正し、これ
により不足分の燃料を確保するとともに、燃料の一部を
次の吸気行程の最初に吸入させ吸気弁の熱及び吸気の乱
流を利用してlP料の気化n化を促進するようにしたも
のである。
Therefore, the present invention prevents the fuel injection start timing from advancing beyond a predetermined crank angle position in an operating range where the amount of fuel injection is large, thereby preventing the injected fuel from blowing through and is corrected to the delayed side, thereby securing the fuel shortage, and at the same time, a part of the fuel is taken in at the beginning of the next intake stroke, and the heat of the intake valve and the turbulent flow of intake air are used to vaporize the lP charge. It was designed to promote the

〔実施例〕〔Example〕

以下、本発明の実h(G例を図について説明する。 Hereinafter, practical examples of the present invention will be explained with reference to the drawings.

第1図は本発明の−・実施例によるエンジンの燃料噴射
装置を示す。図において、1は第1〜第4の4・つの気
筒(但し、図中には1つの気筒のみが示されている)を
有するエンジンで、)−記音気筒にはそれぞれ吸、排気
管2,3が接続され、上記吸気管2の年金部にはスロ7
トル弁4a、4bが配設され、吸気管2の−1,流bm
は:Lアクリ−す5に至っている。そし−ζ上記各吸気
管2には吸気ボー1−に近接して燃料噴射弁6がそれぞ
れ配設され、該各燃料噴射弁6はレギプーレークを介し
゛C燃料タンク(図示・lず)に接続されており、上記
燃料噴射弁6には1記レギゴーレークを介して吸気管圧
力との差圧が常に一定とな【)ような燃圧が供給される
よ−)になっている。
FIG. 1 shows a fuel injection system for an engine according to an embodiment of the present invention. In the figure, 1 is an engine having four cylinders, first to fourth (however, only one cylinder is shown in the figure), and each cylinder has an intake pipe and an exhaust pipe. , 3 are connected, and a slot 7 is connected to the pension part of the intake pipe 2.
Torque valves 4a and 4b are provided, and -1 of the intake pipe 2, the flow bm
Has reached: L Clear 5. A fuel injection valve 6 is disposed in each intake pipe 2 in the vicinity of the intake bow 1-, and each fuel injection valve 6 is connected to a C fuel tank (not shown) via a leg pulley. The fuel injector 6 is supplied with fuel pressure such that the differential pressure with the intake pipe pressure is always constant () through the Regigo rake.

また図中、8は吸気管2のスロノ1ヘルド流の圧力を検
出する月−カセンザ、9はエンジン1の冷却水ll!i
1度を検出する水温センサ、10はディストリビュータ
の回転角からエンジンのクランク角と第1気筒のピスト
ン上死点T D Cとを検出するクランク角センザ、1
1はイグニッションスイッチ、12はスタータモータ、
13はインタフェース14、CPU15及びメモリ16
からなる燃料噴射制御回路であり、」二記メモリ16内
には第2図にフローチャートで示すCPU15の演算処
理のプログラム等が格納されている。そして−1−記C
P U15は、エンジンの始動時は所定量の燃料が噴射
されるように始動噴射パルスを燃料噴射弁に6に加え、
一方エンジンの始動後はエンジンの運転状態に応じて実
際燃料噴射量をめ、これが設定91以下の場合にはほぼ
吸気弁全閉時期の所定の噴射終了時期に基いて噴射開始
時期をめ、設定呈以トの場合には噴射開始時期を1ノ1
気弁の全閉クランク角位置に設定するとともにそれにノ
1チいて上記噴射終了時期を遅れ側に補止し、これより
燃料噴射弁6に上記実際燃料噴射量に応した燃料噴射パ
ルスを加えるという燃料噴射制御を行な・)、1、・う
になっている。なお7Gよ排気系に設りられた触媒であ
る。
Also, in the figure, 8 is the moon-kasenza that detects the pressure of the air flow in the intake pipe 2, and 9 is the cooling water for the engine 1! i
10 is a crank angle sensor that detects the engine crank angle and the piston top dead center TDC of the first cylinder from the rotation angle of the distributor;
1 is the ignition switch, 12 is the starter motor,
13 is an interface 14, a CPU 15 and a memory 16
The memory 16 stores programs for arithmetic processing of the CPU 15 as shown in a flowchart in FIG. 2. And -1-C
P U15 applies a starting injection pulse to the fuel injection valve 6 so that a predetermined amount of fuel is injected when starting the engine;
On the other hand, after starting the engine, determine the actual fuel injection amount according to the engine operating condition, and if this is less than the setting 91, determine the injection start timing based on the predetermined injection end time of the intake valve fully closed timing, and set the In this case, set the injection start time to 1 no 1.
The fuel injection valve is set to the fully closed crank angle position, and the above-mentioned injection end timing is corrected to the delayed side by notching it, and from this, a fuel injection pulse corresponding to the above-mentioned actual fuel injection amount is applied to the fuel injection valve 6. The fuel injection control is performed.), 1,. Note that 7G is a catalyst installed in the exhaust system.

そして以上のような構成において、CPUI 5が、燃
料噴射開始時期が所定のクランク角位置に達したことを
検出して検出信号を出力する検出手段、及び燃料噴射開
始時期が所定のクランク角位置に達した以後は燃料噴射
終了時期を遅れ側に補正する燃料噴射終了時期補正手段
を構成している。
In the above configuration, the CPUI 5 includes a detection means for detecting that the fuel injection start timing has reached a predetermined crank angle position and outputting a detection signal, and a detection means that outputs a detection signal when the fuel injection start timing has reached a predetermined crank angle position. After the fuel injection end timing is reached, the fuel injection end timing correction means is configured to correct the fuel injection end timing to the delayed side.

次に第2図ないし第4図を用いて動作について説明する
。ここで第3図(al (blはそれぞれ燃料噴射量の
少ない運転時及び多い運転時におりる吸気弁の開閉タイ
ミングと燃料噴射タイミングとの関係を、第4図は吸、
 JJI気弁のバルブリフト量と吸。
Next, the operation will be explained using FIGS. 2 to 4. Here, Figure 3 (al (bl) shows the relationship between the opening/closing timing of the intake valve and the fuel injection timing during operation with a small amount of fuel injection and during operation with a large amount of fuel injection, respectively.
JJI valve lift amount and suction.

排気弁の開閉タイミングとの関係を示す。なお図中、F
、O,IOはIJト気弁、吸気弁の開弁タイミング、E
 CハJJi気弁の全開タイミング、EX、INは排気
弁、吸気弁のバルブリフト特性である。
The relationship with the opening/closing timing of the exhaust valve is shown. In the figure, F
, O, IO are IJ air valve, intake valve opening timing, E
The fully open timing of the C-JJi air valve, EX, and IN are the valve lift characteristics of the exhaust valve and intake valve.

エンジンが作動すると、CPU15はクランク角センサ
Io、圧力センサ8及び水温センサ9の各信号を読み込
んでぞの各値をレジスタT、B。
When the engine starts, the CPU 15 reads the signals from the crank angle sensor Io, pressure sensor 8, and water temperature sensor 9, and stores the respective values in registers T and B.

Wlに記憶するとともに(ステップ20〜22)、イグ
ニッションスイッチ11からのスタータ信号を読み込ん
でそれをレジスタSに記憶しくステップ23)、次にレ
ジスタSの配備内容からエンジンの始動時か否かを判定
する(ステップ24)。
Wl (steps 20 to 22), reads the starter signal from the ignition switch 11 and stores it in the register S (step 23), and then determines whether or not it is time to start the engine from the contents of the register S. (Step 24).

そしてエンジンの始動時にはCPU15はステップ24
においてYESと判定してステップ25に進み、そこで
レジスタIに所定の始動噴射量βを記憶し、レジスタI
の値に基いて始動噴射パルスを作成してそれを第1気筒
のT D C信号に応じて判別した噴射すべき気筒の燃
料噴射弁6に加え(ステップ26)、ステップ2oに戻
り、上述の処理を繰り返す。なおエンジンの始動時にお
いて、予め設定した始動噴射パルスを発生ずるようにし
ているのは、この始動時には吸入空気量に基いて燃料噴
射量を算出できないからである。
When the engine starts, the CPU 15 performs step 24.
If YES is determined in step 25, the process proceeds to step 25, where the predetermined starting injection amount β is stored in register I.
A starting injection pulse is created based on the value of , and is applied to the fuel injection valve 6 of the cylinder to be injected, which is determined according to the TDC signal of the first cylinder (step 26), and the process returns to step 2o, where the above-mentioned Repeat the process. The reason why a preset starting injection pulse is generated when the engine is started is because the fuel injection amount cannot be calculated based on the intake air amount at this starting time.

そしてエンジンが始動すると、CP U 15は上記ス
テップ24においてNoと判定してステップ27に進み
、そこでレジスタT内のクランク角を用いてエンジン回
転数を演算してそれをレジスタRに記憶し、次にレジス
タR,B内のエンジン回転数と吸気負圧とでもって基本
燃料噴射量を演算してそれをレジスタ1に記1.Oする
(ステップ28)。
When the engine starts, the CPU 15 makes a negative determination in step 24 and proceeds to step 27, where the engine speed is calculated using the crank angle in the register T and stored in the register R. 1. Calculate the basic fuel injection amount using the engine speed and intake negative pressure in registers R and B, and record it in register 1. O (step 28).

次にCPU15ば、レジスタW1内のエンジン冷却水温
を設定値W、例えば60℃と比較して冷却水温が設定値
W以下であれば、両者の差(W−Wl>と補正係数01
とを乗算し、これを温度補正量としてレジスフI内の基
本燃料噴射量に加算して実際燃料噴射♀をめ、その値1
 +CI (W−Wl)をレジスタ■に記憶しくステッ
プ29)、該レジスタI内の実際燃料噴射量から噴射角
θ(第3図(al参照)を決定してそれをレジスタθに
記憶しくステップ30)、さらに吸気弁全閉時期θvc
(第3図(al参照)と所定噴射終了時期補正殴Δθと
でもって噴射終了時期θ1c−(第3図(al参照)を
決定しくステップ31)、次に噴射角θが噴射終了時期
θicとill気ブ1′!仝閉全閉EC間のクランク角
γより大きいか否かを判定するくステップ32)。
Next, the CPU 15 compares the engine coolant temperature in the register W1 with a set value W, for example 60°C, and if the coolant temperature is below the set value W, the difference between the two (W-Wl> and the correction coefficient 01
Multiply by
+CI (W-Wl) is stored in the register (Step 29), the injection angle θ (see FIG. 3 (al)) is determined from the actual fuel injection amount in the register I, and it is stored in the register θ (Step 30). ), and the intake valve fully closed timing θvc
(Determine the injection end time θ1c-(see FIG. 3 (al)) using the predetermined injection end time correction punch Δθ and the injection end time θic (step 31), and then the injection angle θ is set to the injection end time θic. Step 32).

ここで吸気弁の仝閉時期OvCは基準となるエンジン回
転数、例えば最大トルクとなる3000 rpmにおい
て吸気の吹き返しが発生しないクランク角位置に設定す
ればよく、その1例を示すと、第4図の吸気弁のバルブ
リフト特性図において、吸気行程終期のランプ部分Aの
初期のクランク角位置となる。
Here, the closing timing OvC of the intake valve may be set at a crank angle position that does not cause intake air to blow back at a reference engine speed, for example, 3000 rpm, which is the maximum torque. In the valve lift characteristic diagram of the intake valve, this is the initial crank angle position of the ramp portion A at the end of the intake stroke.

そして燃料噴射量が少なく、噴射角θが設定(Iへγよ
り小さい場合は、CPU15はステップ32においてN
oと判定してステップ33に進んで上記噴射終了時期θ
icに基いてレジスタθ内の実際噴射量θに応じた噴射
開始時期θio(第3図+8+参照)を決定し、噴射開
始時期θioになるまでステップ34に待機し、噴射開
始時期θioになると、ステップ35で燃料噴射弁6に
“1”信号を加え、該弁6を駆動し続ける間ステップ3
6に待機し、噴射終了時期θicになると“1”信号の
出力を停止しくステップ37)、このようにして燃料噴
射パルスを加えた後、上記ステップ20に戻る。
Then, if the fuel injection amount is small and the injection angle θ is set (I is smaller than γ, the CPU 15 sets N at step 32).
It is determined that the injection end time θ is determined as o, and the process proceeds to step 33.
ic, determines the injection start time θio (see Figure 3 +8+) according to the actual injection amount θ in the register θ, waits in step 34 until the injection start time θio is reached, and when the injection start time θio is reached, In step 35, a "1" signal is applied to the fuel injection valve 6, and while the valve 6 continues to be driven, step 3
6, and when the injection end time θic is reached, the output of the "1" signal is stopped (step 37). After applying the fuel injection pulse in this way, the process returns to step 20.

このようにエンジンの始動後で、かつ噴射開始時期が排
気弁全閉クランク角位置に達しない場合にはエンジンの
運転状態に応じて噴射開始時期を進ま−l1、−の噴射
開始時期から設定噴射終了時期の間燃料噴射パルスを加
えるという制御が行なわれることとなる。
In this way, after the engine has started, and if the injection start time does not reach the exhaust valve fully closed crank angle position, the injection start time is advanced according to the engine operating condition, and the set injection starts from the injection start time of -l1, -. Control is performed to apply fuel injection pulses during the end period.

次に燃料噴射量が多くなって噴射角θが設定値γより大
きくなると、CPU15ば上記ステップ32においてY
 E Sと判定してステップ38に進んで噴射開始時期
θIOを排気弁全開クランク角位置EC(第3図(11
)参照)に設定するとともに、θ−γ−八〇とへう式を
用いて噴射終了時期補正9八〇° (第3図(t、+l
参照)をめる(ステップ39)。こごで八〇は燃料噴射
量が小ない領域において上記設定噴射終了時期θicを
めるためのクランク角である。次にCP tJ 15は
上記求めた噴射終了時期補正9八〇”を用いて上記設定
噴射終了時期θicを遅れ側に補iEしてこの場合の実
際の噴射終了時期θic’(第3図(l+)参照)をめ
(ステップ40 ’) 1.、j−記ステップ34〜3
7の経路を進む。
Next, when the fuel injection amount increases and the injection angle θ becomes larger than the set value γ, the CPU 15 executes Y in step 32.
It is determined that E S, and the process proceeds to step 38, where the injection start timing θIO is changed to the exhaust valve fully open crank angle position EC (Fig. 3 (11).
)), and use the equation θ-γ-80 to correct the injection end timing to 980° (see Figure 3 (t, +l
(see step 39). Here, 80 is a crank angle for adjusting the set injection end time θic in a region where the fuel injection amount is small. Next, CP tJ 15 corrects the set injection end time θic to the delayed side using the injection end time correction 980'' obtained above, and calculates the actual injection end time θic' in this case (Fig. 3 (l+ )) (step 40') 1., j-steps 34 to 3
Follow route 7.

このようにエンジンの始動後で、かつ噴射開始時期がI
lY気弁全弁全閉位置する場合には、噴射開始時期を排
気弁全閉クランク角位置に設定するとともに、それによ
って不足する燃料分噴射終了時期を遅れ側に補正すると
いう制御が行なわれる。
In this way, after the engine has started and the injection start timing is I
When the exhaust valve is in the fully closed position, control is performed to set the injection start timing to the exhaust valve fully closed crank angle position and thereby correct the injection end timing for the insufficient fuel to the delayed side.

ところでこのように燃料噴射終了時期を遅れ側に補正す
るようにすると、燃料の−91が次の吸気行程に持ち込
まれ、成層化燃焼が<J゛れることとなるが、このよ・
うに多量の燃料を供給する運転状態では、燃料が吸気行
程のほぼ全期間にわたて吸入され、上述の成層化燃焼に
よる利点はほとんど期待できないことから、成層化燃焼
がくずれたとしても別設の支陳は生しないものである。
By the way, if the fuel injection end timing is corrected to the delayed side in this way, -91 of the fuel will be carried into the next intake stroke, and the stratified combustion will be delayed.
Under operating conditions in which a large amount of fuel is supplied, fuel is inhaled over almost the entire period of the intake stroke, and the benefits of stratified combustion described above cannot be expected. Therefore, even if stratified combustion breaks down, a separate Support is ineffective.

以上のような本実施例の装置では、燃料噴射開始時期を
排気弁全閉クランク角位置より前に進めないようにした
ので、噴射燃料の吹き抜&ノが発生することはなく、そ
の結果燃焼性及びエミッションの悪化を防止できる。ま
た燃料噴射終了時期を遅らせるようにしたので、燃料噴
射開始時期の規制に起因する不足分の燃料を確保できる
。さらに燃料の一部は吸気行程終了後の吸気ボー1−に
残り、該燃料は吸気弁の熱によって気化霧化されるとと
もに、次の吸気行程の最初に急激に吸入され7、そのと
きの吸気の乱流によって空気とよく混合されるので、良
好な燃焼性がUIN保される。
In the device of this embodiment as described above, the fuel injection start timing is prevented from advancing beyond the exhaust valve fully closed crank angle position, so blow-out of the injected fuel does not occur, and as a result, the combustion This can prevent deterioration of performance and emissions. Furthermore, since the fuel injection end timing is delayed, it is possible to secure fuel for the shortage caused by restrictions on the fuel injection start timing. Further, a part of the fuel remains in the intake valve 1- after the intake stroke, and this fuel is vaporized and atomized by the heat of the intake valve, and is rapidly inhaled at the beginning of the next intake stroke 7, and the fuel is inhaled at the beginning of the next intake stroke. Good combustibility is maintained because the turbulence of the UIN mixes well with the air.

なコ・辷1−記実施例では燃料噴射開始時)す」を排気
弁全閉クランク角位置より前に進ませなG1ようQこし
7たが、これは1ノド気弁全閉クランク角位置より遅れ
側の所定のクランク角位置であゲζもよし)。まノ、二
本発明は全運転↑1f1威で成層化燃焼を省jなうよう
Gにし7ノコものに限らず、一部の運転領域、例えば部
分性1rj ′ian域で成Ji化燃焼を行なうものに
ついても同様に通用できる。さらに本発明は、燃料咄”
射終了時期をlσr定クランク角位置に固定し7たもの
に限らず、例えば運転状態に応じて可変制御するよう心
こしたものに・ついても同様に通用できる。
In the example described above, when starting fuel injection, G1 should not be advanced beyond the fully closed crank angle position of the exhaust valve. (Gage ζ is also acceptable at a predetermined crank angle position on the more delayed side). Mano, two, the present invention uses G to avoid stratified combustion in full operation ↑ 1f1 power, and reduces stratified combustion in some operating ranges, for example, in the partial 1rj ′ian range, not only in the 7-speed engine. The same applies to what you do. Furthermore, the present invention provides fuel
The present invention is not limited to one in which the injection end timing is fixed at a constant lσr crank angle position, but can similarly be applied to one in which it is variably controlled depending on the operating condition, for example.

〔発明のりJ果〕[Invention glue J fruit]

以上のよ〜)に本発明によれば、吸気行程の終rj);
1に炉別噴射終了1l)I!llを設定し、噴射量の増
加に伴ゲc +Pa *、を噴射量kt)時期を進める
ようにしノココーンジンの燃料1+i則装置において、
燃料噴射量の多い場合は、噴8・1開9f)時期を8す
i定りランク角位置より前には進ませないようにし、噴
射終了時期を遅らせるようにしたので、噴射燃料の吹き
抜ζノを防止でき、これにより燃焼性及びエミッション
を大幅に改善でき、又燃料の気化霧化を1だ進でき、こ
れによっても燃焼性を向」二できる効果がある。
According to the present invention, the end of the intake stroke rj);
Finished injection by furnace at 11) I! ll is set, and as the injection amount increases, the timing of the injection amount kt) is advanced.
When the amount of fuel injected is large, the injection timing (8/1 open 9f) is prevented from advancing beyond the 8s fixed rank angle position, and the injection end timing is delayed, so that the injection ζ can be prevented, thereby significantly improving combustibility and emissions, and further accelerating vaporization and atomization of fuel, which also has the effect of improving combustibility.

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

第1図は本発明の一実施例によるエンジンの燃料噴射装
置の概略構成図、第2図はL記装置におけるCPU15
の演算処理のフローチャートを示す図、第3図+8)及
びtb)はそれぞれL記装置における燃料噴射量の少な
い運転時及び多い運転時での吸気弁の開閉タイミングと
燃1パ1噴躬タイミングとの関係を示す図、第4し1は
吸、排気弁のバルブリフト量と吸、排気弁の開閉タイミ
ングとの関係を示す図である。 6・・・燃料噴射弁、15・・・C))tJ(検出手段
、燃料噴射終了時期補正手段)。 特許出願人 東洋工業株式会社 代理人 弁理士 リ 瀬 憲 − 第3図 (b) l:IUシ
FIG. 1 is a schematic configuration diagram of an engine fuel injection device according to an embodiment of the present invention, and FIG. 2 is a CPU 15 in the L device.
Fig. 3+8) and tb) are flowcharts of the calculation processing of the L device, respectively. The fourth figure 1 is a diagram showing the relationship between the valve lift amount of the intake and exhaust valves and the opening/closing timing of the intake and exhaust valves. 6...Fuel injection valve, 15...C))tJ (detection means, fuel injection end timing correction means). Patent Applicant Toyo Kogyo Co., Ltd. Agent Patent Attorney Ken Rise - Figure 3 (b) l: IU Si

Claims (1)

【特許請求の範囲】[Claims] (1) 吸気弁を介して燃焼室に通ずる吸気通路内に燃
料噴射弁を設&J、該燃料噴射弁の燃料噴射終了時期を
ほぼ吸気弁閉弁時期に設定するとともに、燃料噴射量の
増大に伴って燃料噴射開始時期を早めるようにしたエン
ジンの燃料噴射装置において、−上記燃料噴射弁の燃料
噴射開始時期が所定のクランク角位置に達したことを検
出して検出信号を出力する検出手段と、該検出手段の検
出信号を受けて燃料噴射開始時期が所定のクランク角位
置に達した以後は−に記燃料噴射弁の燃料噴射終了時期
を遅れ側に補正する燃料噴射終了時期補正手段とを設け
たことを特徴とするエンジンの燃料噴射装置。
(1) A fuel injection valve is installed in the intake passage leading to the combustion chamber via the intake valve, and the fuel injection end time of the fuel injection valve is set to approximately the intake valve closing time, and the fuel injection amount is increased. Accordingly, in the fuel injection device for an engine which advances the fuel injection start timing, there is provided a detection means for detecting that the fuel injection start timing of the fuel injection valve has reached a predetermined crank angle position and outputting a detection signal; , after the fuel injection start time reaches a predetermined crank angle position in response to the detection signal of the detection means, the fuel injection end time correction means corrects the fuel injection end time of the fuel injection valve to the delayed side after the fuel injection start time reaches a predetermined crank angle position. A fuel injection device for an engine, characterized in that:
JP58232165A 1983-12-07 1983-12-07 Fuel injector of engine Granted JPS60122240A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58232165A JPS60122240A (en) 1983-12-07 1983-12-07 Fuel injector of engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58232165A JPS60122240A (en) 1983-12-07 1983-12-07 Fuel injector of engine

Publications (2)

Publication Number Publication Date
JPS60122240A true JPS60122240A (en) 1985-06-29
JPH0467578B2 JPH0467578B2 (en) 1992-10-28

Family

ID=16935010

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58232165A Granted JPS60122240A (en) 1983-12-07 1983-12-07 Fuel injector of engine

Country Status (1)

Country Link
JP (1) JPS60122240A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60212654A (en) * 1984-04-07 1985-10-24 Toyota Motor Corp Fuel injection controller for internal-combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60212654A (en) * 1984-04-07 1985-10-24 Toyota Motor Corp Fuel injection controller for internal-combustion engine

Also Published As

Publication number Publication date
JPH0467578B2 (en) 1992-10-28

Similar Documents

Publication Publication Date Title
US7841316B2 (en) Controller for direct injection engine
US7096853B2 (en) Direct fuel injection/spark ignition engine control device
JP4013594B2 (en) Engine idling control device
US20170292462A1 (en) Control system for internal combustion engine
US4811231A (en) Apparatus for controlling fuel injection and swirl motion of air in internal combustion engine
JP3677876B2 (en) Engine ignition timing control device
KR100269839B1 (en) Control device of cylinder injection type spark ignition internal combustion engine
JP2005214102A (en) Control device of cylinder injection internal combustion engine
JP2003013784A (en) Control device of direct injection spark ignition type internal combustion engine
JPH0512543B2 (en)
JP4075638B2 (en) Engine valve timing control device
JP4066796B2 (en) Internal combustion engine with variable valve timing mechanism
JP2003013785A (en) Control device of direct injection spark ignition type internal combustion engine
JPS60122240A (en) Fuel injector of engine
JP3985419B2 (en) Control device for internal combustion engine
JPS60230554A (en) Knocking suppressor for engine
JP2929781B2 (en) Fuel injection timing control stratified combustion internal combustion engine
JP3959784B2 (en) Combustion stabilization system for direct injection spark ignition engine
JP2007077842A (en) Control device for internal combustion engine
JPS60230543A (en) Engine equipped with fuel injector
JP2005098186A (en) Operation area control device of internal combustion engine
JPS6116248A (en) Fuel injection device for engine
JP2000213392A (en) Direct injection spark ignition internal combustion engine
JPH11218036A (en) Cylinder injection type internal combustion engine
JPH09287525A (en) Combustion controller for internal combustion engine