JPH07217478A - Fuel injection control device for internal combustion engine - Google Patents

Fuel injection control device for internal combustion engine

Info

Publication number
JPH07217478A
JPH07217478A JP853694A JP853694A JPH07217478A JP H07217478 A JPH07217478 A JP H07217478A JP 853694 A JP853694 A JP 853694A JP 853694 A JP853694 A JP 853694A JP H07217478 A JPH07217478 A JP H07217478A
Authority
JP
Japan
Prior art keywords
fuel injection
fuel
cylinder
control device
injection
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.)
Pending
Application number
JP853694A
Other languages
Japanese (ja)
Inventor
Hiroaki Nihei
裕昭 仁平
Kenichi Nomura
憲一 野村
Shigeki Miyashita
茂樹 宮下
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 JP853694A priority Critical patent/JPH07217478A/en
Publication of JPH07217478A publication Critical patent/JPH07217478A/en
Pending legal-status Critical Current

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

Abstract

PURPOSE:To restrain a knock without causing any deterioration in fuel consumption, upon occurrence thereof in the fuel injection control device of an internal combustion engine. CONSTITUTION:This fuel injection control control device of an internal combustion engine is equipped with a fuel injection valve 6 at the side of an intake valve 2 on the peripheral surface of the upper section of a cylinder, so as to conically inject fuel toward the crown of a piston 7 nearing the end of intake stroke. Also, the device begins to inject a necessary amount of fuel on optimum timing after intermediate intake stroke. Regarding this control device, a part of the required fuel amount is injected in advance at the early stage of intake stroke, when a knock takes place.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、特に常時均一燃焼を実
行する筒内噴射式火花点火機関において、ノッキングを
抑制するための燃料噴射制御装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel injection control device for suppressing knocking, particularly in a cylinder injection type spark ignition engine which always performs uniform combustion.

【0002】[0002]

【従来の技術】気筒上部のシリンダヘッドの温度は、吸
気により冷却される吸気弁側に比較して排気弁側が高く
維持される。点火時点における混合気温度もこのシリン
ダヘッドの熱によって同様な傾向を示し、点火時にまず
高温の排気弁側の混合気が着火燃焼して膨張し、吸気弁
側の混合気が圧縮されて温度上昇する。この上昇温度が
発火温度に達しなければ、火炎は吸気弁側の混合気に伝
播され良好な燃焼が実現されるが、発火温度に達する
と、吸気弁側の混合気は自発火し、ノッキングが発生す
る。
2. Description of the Related Art The temperature of a cylinder head above a cylinder is maintained higher on the exhaust valve side than on the intake valve side cooled by intake air. The temperature of the air-fuel mixture at the time of ignition also shows a similar tendency due to the heat of this cylinder head.At the time of ignition, the hot air-fuel mixture on the exhaust valve side ignites and burns to expand, and the air-fuel mixture on the intake valve side is compressed and rises in temperature. To do. If this rising temperature does not reach the ignition temperature, the flame is propagated to the air-fuel mixture on the intake valve side to achieve good combustion, but when it reaches the ignition temperature, the air-fuel mixture on the intake valve side ignites spontaneously and knocks. Occur.

【0003】特開平4−183951号公報には、常時
成層燃焼を実行する筒内噴射式火花点火機関において、
ノッキング発生時には、点火時期を遅角すると共に圧縮
行程における燃料噴射の時期を遅角するものが記載され
ている。これは、ノッキング発生時に点火時期を遅角す
ることにより、点火時点の混合気圧力が下がると共に混
合気温度が下がり、それにより、吸気弁側の混合気の自
発火、すなわちノッキングを抑制するものである。
Japanese Unexamined Patent Publication (Kokai) No. 4-183951 discloses a cylinder injection type spark ignition engine which always performs stratified combustion.
When knocking occurs, the ignition timing is retarded and the fuel injection timing in the compression stroke is retarded. This is to suppress ignition of the air-fuel mixture on the intake valve side, that is, knocking, by retarding the ignition timing when knocking occurs, thereby lowering the air-fuel mixture pressure at the time of ignition and lowering the air-fuel mixture temperature. is there.

【0004】[0004]

【発明が解決しようとする課題】点火時期遅角は、もち
ろん、常時均一燃焼を実行する筒内噴射式火花点火機関
におけるノッキング抑制にも有効であるが、圧縮上死点
後に燃焼が開始され、すなわち燃焼の等容度が低くなる
ために出力が低下し、所望の出力を得るためには燃料を
増量しなければならず、燃費が悪化する。
The ignition timing retard is, of course, effective for suppressing knocking in a direct injection spark ignition engine that always performs uniform combustion, but combustion is started after compression top dead center, That is, the equal volume of combustion is lowered, so the output is reduced, and in order to obtain a desired output, it is necessary to increase the amount of fuel, which deteriorates fuel efficiency.

【0005】従って、本発明の目的は、常時均一燃焼を
実行する筒内噴射式火花点火機関において、燃費を悪化
させることなくノッキングを抑制することができる燃料
噴射制御装置を提供することである。
Therefore, an object of the present invention is to provide a fuel injection control device capable of suppressing knocking without deteriorating fuel consumption in a cylinder injection type spark ignition engine which always performs uniform combustion.

【0006】[0006]

【課題を解決するための手段】本発明による筒内噴射式
火花点火機関の燃料噴射制御装置は、気筒上部周囲の吸
気弁側に配置され、燃料を円錐状に吸気行程末期のピス
トン頂面に向けて噴射する燃料噴射弁を具備し、吸気行
程中期以降の最適時期から必要燃料量の噴射を開始する
筒内噴射式火花点火機関の燃料噴射制御装置において、
ノッキング発生時には、必要燃料量の一部を吸気行程初
期に前もって噴射することを特徴とする。
A fuel injection control device for a cylinder injection type spark ignition engine according to the present invention is arranged on the intake valve side around the upper part of a cylinder and conically forms fuel on the piston top surface at the end of the intake stroke. In a fuel injection control device for a cylinder injection type spark ignition engine, which is equipped with a fuel injection valve for injecting toward, and starts injection of a required fuel amount from an optimum timing after the middle of the intake stroke,
When knocking occurs, a part of the required fuel amount is injected in advance in the early stage of the intake stroke.

【0007】[0007]

【作用】前述の筒内噴射式火花点火機関の燃料噴射制御
装置は、気筒上部周囲の吸気弁側に配置され、燃料を円
錐状に吸気行程末期のピストン頂面に向けて噴射する燃
料噴射弁を具備し、通常時は、噴射された燃料があまり
ピストン頂面に付着しないように吸気行程中期以降の最
適時期から必要燃料量の噴射を開始し、ノッキング発生
時には、必要燃料量の一部を吸気行程初期に前もって噴
射し、この燃料を積極的にピストン頂面の吸気弁側に衝
突させる。
The above-described fuel injection control device for a cylinder injection type spark ignition engine is arranged on the intake valve side around the upper part of the cylinder and injects fuel conically toward the top surface of the piston at the end of the intake stroke. In normal times, the injection of the required fuel amount is started from the optimum timing after the middle of the intake stroke so that the injected fuel does not adhere much to the piston top surface, and when knocking occurs, a portion of the required fuel amount is The fuel is injected in advance at the beginning of the intake stroke, and this fuel is positively collided with the intake valve side of the piston top surface.

【0008】[0008]

【実施例】図1は、本発明による燃料噴射制御装置が取
り付けられた筒内噴射式火花点火機関の概略縦断面図で
あり、図2はその概略平面図である。これらの図におい
て、1は気筒上部略中心に位置する点火栓であり、その
回りには互いに隣接する各二つの吸気弁2及び排気弁3
が配置されている。4は吸気弁2を介して気筒内へ通じ
る二つの吸気通路であり、5は排気弁3を介して気筒内
へ通じる二つの排気通路である。
1 is a schematic longitudinal sectional view of a cylinder injection type spark ignition engine to which a fuel injection control device according to the present invention is attached, and FIG. 2 is a schematic plan view thereof. In these drawings, reference numeral 1 denotes an ignition plug located substantially in the center of the upper portion of the cylinder, around which two intake valves 2 and exhaust valves 3 adjacent to each other are provided.
Are arranged. Reference numeral 4 is two intake passages communicating with the inside of the cylinder via the intake valve 2, and 5 is two exhaust passages communicating with the inside of the cylinder via the exhaust valve 3.

【0009】6は気筒内へ直接燃料を噴射する燃料噴射
弁であり、気筒上部周囲の吸気弁2側に取り付けられて
いる。7はピストンであり、その頂面には浅い凹部7a
が形成されている。
Reference numeral 6 denotes a fuel injection valve for directly injecting fuel into the cylinder, which is mounted on the intake valve 2 side around the upper part of the cylinder. Reference numeral 7 is a piston, and a shallow recess 7a is formed on the top surface thereof.
Are formed.

【0010】本実施例の筒内噴射式火花点火機関は、常
時、高出力が得られる均一燃焼を実行するものであり、
そのために燃料噴射弁6は、燃料を円錐状に微粒化して
噴射するものであり、その噴射方向は、吸気下死点のピ
ストン7頂面に向けられている。このように燃料噴射方
向が設定させることで、噴射された燃料は、図1に示す
ように、いずれのピストン7位置においても直接気筒内
壁に付着することはなく、またピストン7の凹部7aに
付着する燃料は流動しても気筒内壁に達することがな
い。それにより、気筒内壁に付着した燃料が、潤滑油膜
に取り込まれて未燃燃料として排出されることは防止さ
れる。
The in-cylinder injection type spark ignition engine of the present embodiment always performs uniform combustion capable of obtaining high output,
Therefore, the fuel injection valve 6 atomizes the fuel in a conical shape and injects it, and the injection direction is directed to the top surface of the piston 7 at the intake bottom dead center. By setting the fuel injection direction in this manner, the injected fuel does not directly adhere to the inner wall of the cylinder at any piston 7 position and adheres to the recess 7a of the piston 7 as shown in FIG. Even if the fuel flowing flows, it does not reach the inner wall of the cylinder. This prevents the fuel adhering to the inner wall of the cylinder from being taken up by the lubricating oil film and discharged as unburned fuel.

【0011】燃料噴射弁6による燃料噴射制御は、図3
に示すフローチャートに従って行われる。本フローチャ
ートは、所定時間又は所定クランク角度毎に実行される
ものである。まず、ステップ101において、例えば、
吸気通路1のスロットル弁(図示せず)上流に設けられ
たエアフローメータ(図示せず)によって吸入空気重量
Gaが測定され、ステップ102において、各気筒への
吸入空気重量Ga’が所望空燃比A/Fで割られ、必要
燃料噴射量Qfが算出される。次にステップ103にお
いて回転センサにより機関回転数Neが検出され、ステ
ップ104に進む。
The fuel injection control by the fuel injection valve 6 is shown in FIG.
It is performed according to the flowchart shown in. This flowchart is executed every predetermined time or every predetermined crank angle. First, in step 101, for example,
The intake air weight Ga is measured by an air flow meter (not shown) provided upstream of the throttle valve (not shown) in the intake passage 1, and in step 102, the intake air weight Ga ′ to each cylinder is the desired air-fuel ratio A. The required fuel injection amount Qf is calculated by dividing by / F. Next, at step 103, the engine speed Ne is detected by the rotation sensor, and the routine proceeds to step 104.

【0012】ステップ104において、例えば、気筒外
壁に取り付けられ、音又は振動によってノッキングを検
出するノッキングセンサ(図示せず)により、少なくと
もいずれか一つの気筒でノッキングが発生しているかど
うかが判断される。この判断が肯定される時、すなわち
ノッキング発生時には、ステップ105に進み、フラグ
Fが1であるかどうかが判断される。このフラグFは機
関停止と共に0にリセットされるものであり、当初、こ
の判断は否定されステップ106に進む。
In step 104, for example, a knocking sensor (not shown) mounted on the outer wall of the cylinder and detecting knocking by sound or vibration determines whether knocking has occurred in at least one cylinder. . When this determination is affirmative, that is, when knocking occurs, the routine proceeds to step 105, where it is determined whether the flag F is 1. This flag F is reset to 0 when the engine is stopped, and this determination is initially denied and the routine proceeds to step 106.

【0013】ステップ106においてフラグFは1とさ
れ、ステップ107に進み、予備燃料噴射量Q1が最小
燃料噴射量Qminとされ、ステップ114に進む。最
小燃料噴射量Qminとは、燃料噴射弁6の特性により
決定される噴射可能な最小燃料噴射量である。フラグF
は、後述されるステップ112において、予備燃料噴射
量Q1が0とされた時にステップ113において0にリ
セットされ、すなわち予備燃料噴射が実行される限り1
に維持されるものである。ステップ114において、予
備燃料噴射の噴射期間Tinj1、すなわち機関回転数
Neを考慮して予備燃料噴射量Q1を噴射するのに必要
なクランク角度範囲が算出され、ステップ115におい
て吸気行程開始直後の所定クランク角度θ1に固定され
ている予備燃料噴射の噴射開始時期SOI1に噴射期間
Tinj1が加えられ予備燃料噴射の噴射終了時期EO
I1が算出される。
At step 106, the flag F is set to 1, and the routine proceeds to step 107, where the preliminary fuel injection amount Q1 is set to the minimum fuel injection amount Qmin, and the routine proceeds to step 114. The minimum fuel injection amount Qmin is the minimum injectable fuel injection amount that is determined by the characteristics of the fuel injection valve 6. Flag F
Is reset to 0 in step 113 when the preliminary fuel injection amount Q1 is set to 0 in step 112 described later, that is, 1 as long as the preliminary fuel injection is executed.
Is maintained at. In step 114, the crank angle range necessary to inject the preliminary fuel injection amount Q1 is calculated in consideration of the injection period Tinj1 of the preliminary fuel injection, that is, the engine speed Ne, and in step 115, the predetermined crank angle immediately after the start of the intake stroke. The injection start timing SOI1 of the preliminary fuel injection fixed at the angle θ1 is added with the injection period Tinj1 to end the injection EO of the preliminary fuel injection.
I1 is calculated.

【0014】次にステップ116において、必要燃料噴
射量Gfから予備燃料噴射量G1が引かれ主燃料噴射量
Q2が算出され、ステップ117において、主燃料噴射
の噴射期間Tinj2、すなわち機関回転数Neを考慮
して主燃料噴射量Q2を噴射するのに必要なクランク角
度範囲が算出される。次にステップ118において、吸
気行程中期前半の所定クランク角度θ2と予備燃料噴射
の噴射終了時期EOI1との差が間隔I(Ne)以上で
あるかどうかが判断される。間隔I(Ne)は、燃料噴
射弁6が閉弁指令を受けてから次の開弁指令を正常に受
けることができる最低時間を現在の機関回転数Neを基
にクランク角度範囲で表したものであり、予備燃料噴射
量Q1が最小燃料噴射量Qminである時は、機関回転
数Neが高くてもこの判断は肯定され、主燃料噴射は所
定クランク角度θ2から噴射可能であるために、ステッ
プ119において、主燃料噴射の噴射開始時期SOI2
は、正常燃焼時において、噴射された燃料がピストン7
頂面に多量に付着して未燃燃料として排出されることを
防止すると共に均一混合気形成に有利なように噴射終了
時期をできる限り早めるために、燃料噴射弁6の噴口と
ピストン7頂面との間にある程度の距離がある吸気行程
中期前半の最適クランク角度θ2とされ、ステップ12
1に進む。
Next, at step 116, the main fuel injection amount Q2 is calculated by subtracting the preliminary fuel injection amount G1 from the required fuel injection amount Gf, and at step 117, the injection period Tinj2 of the main fuel injection, that is, the engine speed Ne. Considering this, the crank angle range required to inject the main fuel injection amount Q2 is calculated. Next, at step 118, it is judged if the difference between the predetermined crank angle θ2 in the first half of the intake stroke and the injection end timing EOI1 of the preliminary fuel injection is the interval I (Ne) or more. The interval I (Ne) is the minimum time during which the fuel injection valve 6 can normally receive the next valve opening command after receiving the valve closing command in the crank angle range based on the current engine speed Ne. When the preliminary fuel injection amount Q1 is the minimum fuel injection amount Qmin, this judgment is affirmed even if the engine speed Ne is high, and the main fuel injection can be performed from the predetermined crank angle θ2. At 119, the injection start timing SOI2 of the main fuel injection
In the normal combustion, the injected fuel is
The injection port of the fuel injection valve 6 and the top surface of the piston 7 are provided in order to prevent a large amount of the fuel from adhering to the top surface and be discharged as unburned fuel and to advance the injection end timing as early as possible in order to form a uniform mixture. Is set to the optimum crank angle θ2 in the first half of the middle of the intake stroke, and step 12
Go to 1.

【0015】ステップ121において、噴射開始時期S
OI2にステップ117において算出された噴射期間T
inj2が加えられ主燃料噴射の噴射終了時期EOI2
が算出される。
In step 121, the injection start timing S
The injection period T calculated in step 117 for OI2
inj2 is added and injection end timing EOI2 of main fuel injection
Is calculated.

【0016】従って、ノッキング発生直後の燃料噴射
は、図4に実線で示すように、必要燃料噴射量Gfのう
ち吸気行程初期に最小燃料噴射量Qminでの予備燃料
噴射が実行され、この時、その残りが主燃料噴射として
吸気行程中期前半のクランク角度θ2から噴射される。
Therefore, as shown by the solid line in FIG. 4, the fuel injection immediately after the knocking occurs is the preliminary fuel injection with the minimum fuel injection amount Qmin at the beginning of the intake stroke of the required fuel injection amount Gf. The remainder is injected as the main fuel from the crank angle θ2 in the first half of the middle stage of the intake stroke.

【0017】ノッキングは、前述したように、排気弁側
の混合気の着火燃焼による膨張に伴う吸気弁側の混合気
の圧縮による温度上昇が発火温度以上となる時に起きる
ものである。本実施例の燃料噴射制御によれば、前述し
たように、ノッキング発生当初、吸気行程初期において
最小燃料噴射量Qminでの予備燃料噴射を実行するよ
うになっており、この時に噴射された燃料は燃料噴射弁
5の噴口からピストン7頂面までの距離が小さいため
に、大きな貫徹力を持ってピストン7頂面に衝突し、ピ
ストン7頂面の吸気弁2側に付着すると共に気筒上部の
シリンダヘッドの吸気弁2側に跳ね返ってそこに付着す
る。これらの付着燃料は、ピストン7頂面及び気筒上部
のシリンダヘッドの吸気弁側から熱を奪い気化するため
に、これらの部分を冷却し、点火直後に吸気弁側の混合
気が圧縮されてもその温度が発火温度以上になり難くな
り、ノッキングを抑制することができる。
As described above, knocking occurs when the temperature rise due to the compression of the air-fuel mixture on the intake valve side due to the expansion of the air-fuel mixture on the exhaust valve side due to the ignition and combustion exceeds the ignition temperature. According to the fuel injection control of the present embodiment, as described above, at the beginning of knocking, the preliminary fuel injection with the minimum fuel injection amount Qmin is executed at the beginning of the intake stroke, and the fuel injected at this time is Since the distance from the injection port of the fuel injection valve 5 to the top surface of the piston 7 is small, it collides with the top surface of the piston 7 with a large penetrating force and adheres to the intake valve 2 side of the top surface of the piston 7 and at the same time as the cylinder above the cylinder. It bounces to the intake valve 2 side of the head and adheres there. These adhering fuels take heat from the top surface of the piston 7 and the intake valve side of the cylinder head above the cylinder to be vaporized, so that these parts are cooled and even if the air-fuel mixture on the intake valve side is compressed immediately after ignition. It becomes difficult for the temperature to exceed the ignition temperature, and knocking can be suppressed.

【0018】もし、予備燃料噴射量Q1が最小燃料噴射
量Qminではピストン7頂面及び気筒上部のシリンダ
ヘッドの吸気弁側を十分に冷却できずにノッキングが持
続する時には、ステップ105における判断は、すでに
フラグFが1であるために肯定されてステップ108に
進み、予備燃料噴射量Q1は、前回の量(当初は最小燃
料噴射量Qmin)に所定量Δqだけ増加され、ステッ
プ114以降の処理が行われる。この流れが繰り返され
る毎に予備燃料噴射量Q1は所定量Δqづつ増加され、
ステップ118における判断が否定されれば、ステップ
120に進み、図4に一点鎖線で示すように、主燃料噴
射の噴射開始時期SOI2は、この燃料噴射を可能とす
るために予備燃料噴射の噴射終了時期EOI1から間隔
I(Ne)だけ遅らされたクランク角度とされ、ステッ
プ121に進み、噴射終了時期EOI2が決定される。
If the preliminary fuel injection amount Q1 is the minimum fuel injection amount Qmin and the knocking continues because the top face of the piston 7 and the intake valve side of the cylinder head above the cylinder cannot be sufficiently cooled, the determination in step 105 is as follows. Since the flag F has already been set to 1, the determination is affirmative and the routine proceeds to step 108, where the preliminary fuel injection amount Q1 is increased by a predetermined amount Δq from the previous amount (initially the minimum fuel injection amount Qmin), and the processing after step 114 is executed. Done. Each time this flow is repeated, the preliminary fuel injection amount Q1 is increased by a predetermined amount Δq,
If the determination in step 118 is negative, the routine proceeds to step 120, where the injection start timing SOI2 of the main fuel injection is the end of injection of the preliminary fuel injection to enable this fuel injection, as indicated by the alternate long and short dash line in FIG. The crank angle is delayed from the timing EOI1 by the interval I (Ne), the routine proceeds to step 121, where the injection end timing EOI2 is determined.

【0019】図4における実線及び一点鎖線での燃料噴
射は、同じ機関回転数で同じ必要燃料噴射量の場合を示
しており、このように予備燃料噴射量Q1の増加に伴い
主燃料噴射の噴射開始時期SOI2が遅らされても、そ
の分、主燃料噴射量Q2が減少されるために、その噴射
終了時期EOI2が遅くなることなく、均一混合気形成
に不利となることはない。予備燃料噴射によりノッキン
グが発生しなくなれば、ステップ104における判断が
否定されてステップ109に進み、ステップ105と同
様にフラグFが1であるかどうかが判断され、この判断
は肯定され、ステップ110に進む。
The solid line and the alternate long and short dash line in FIG. 4 show the case of the same engine speed and the same required fuel injection amount, and thus the injection of the main fuel injection as the preliminary fuel injection amount Q1 increases. Even if the start timing SOI2 is delayed, the main fuel injection amount Q2 is reduced accordingly, so that the injection end timing EOI2 is not delayed and there is no disadvantage in forming a homogeneous mixture. If knocking does not occur due to the preliminary fuel injection, the determination at step 104 is denied and the routine proceeds to step 109. As at step 105, it is determined whether or not the flag F is 1, and this determination is affirmative and the routine proceeds to step 110. move on.

【0020】ステップ110において、予備燃料噴射量
Q1は前回の量から所定量Δqだけ減少され、ステップ
111において、今回の予備燃料噴射量Q1が最小燃料
噴射量Qmin未満であるかどうかが判断され、当初、
この判断は否定されてステップ114以降の処理が実行
される。このように、ノッキング抑制に必要な最少の予
備燃料噴射量Q1が選択されるために、この時に噴射さ
れピストン7頂面及びシリンダヘッドに付着する燃料
は、全て点火時点において気化され、液状のまま未燃燃
料として排出されることにより排気エミッションを悪化
させることはない。前述の流れを繰り返すうちにステッ
プ111における判断が肯定されると、現実的に最小燃
料噴射量Qmin未満の燃料噴射は不可能であるため
に、ステップ112に進み、予備燃料噴射量Q1は0と
され、ステップ113においてフラグFは0にリセット
され、ステップ114以降の処理が実行される。この
時、ステップ114において予備燃料噴射の噴射期間T
inj1は0°クランク角度範囲となり、従って、ステ
ップ115において算出される予備燃料噴射の噴射終了
時期EOI1は噴射開始時期θ1と同じとなり、予備燃
料噴射は行われず、またステップ118における判断
は、当然肯定され、燃料噴射開始時期SOI2をθ2と
する必要燃料噴射量Qfでの主燃料噴射が行われる。
In step 110, the preliminary fuel injection amount Q1 is reduced by a predetermined amount Δq from the previous amount, and in step 111, it is judged whether or not the current preliminary fuel injection amount Q1 is less than the minimum fuel injection amount Qmin. Initially,
This determination is denied and the processing from step 114 onward is executed. As described above, since the minimum preliminary fuel injection amount Q1 required for suppressing knocking is selected, all the fuel injected at this time and adhering to the top surface of the piston 7 and the cylinder head is vaporized at the time of ignition and remains liquid. Exhaust emissions are not deteriorated by being discharged as unburned fuel. If the determination in step 111 is affirmed while repeating the above-described flow, it is practically impossible to inject less than the minimum fuel injection amount Qmin, so the routine proceeds to step 112, where the preliminary fuel injection amount Q1 is 0. Then, in step 113, the flag F is reset to 0, and the processing of step 114 and subsequent steps is executed. At this time, in step 114, the injection period T of the preliminary fuel injection
Since inj1 is in the 0 ° crank angle range, the injection end timing EOI1 of the preliminary fuel injection calculated in step 115 is the same as the injection start timing θ1, no preliminary fuel injection is performed, and the determination in step 118 is naturally affirmative. Then, the main fuel injection is performed at the required fuel injection amount Qf with the fuel injection start timing SOI2 being θ2.

【0021】予備燃料噴射を行わなくてもノッキングが
発生しない時には、ステップ109における判断が否定
されてステップ112に進み、予備燃料噴射量Q1を0
とすると共に、ステップ113においてフラグFは0に
維持され、ステップ114以降の処理を実行し、前述同
様、必要燃料噴射量Qfでの主燃料噴射を行う。
When knocking does not occur even if the preliminary fuel injection is not performed, the determination in step 109 is denied and the routine proceeds to step 112, where the preliminary fuel injection amount Q1 is set to 0.
At the same time, the flag F is maintained at 0 in step 113, the processes of step 114 and the subsequent steps are executed, and the main fuel injection with the required fuel injection amount Qf is performed as described above.

【0022】本実施例において、予備燃料噴射の開始時
期SOI1は、吸気行程初期の所定クランク角度θ1に
固定されているが、予備燃料噴射量Q1の増加に伴い吸
気上死点側に早めるように可変とすることもでき、それ
により、予備燃料噴射量Q1がある程度多くなっても機
関回転数Neを考慮して主燃料噴射を吸気行程中期前半
の所定クランク角度θ2から噴射することができる機会
が増加し、その分、主燃料噴射の噴射終了時期EOI2
が早まり、均一混合気形成に有利となる。
In the present embodiment, the start timing SOI1 of the preliminary fuel injection is fixed to the predetermined crank angle θ1 at the beginning of the intake stroke, but it may be advanced to the intake top dead center side as the preliminary fuel injection amount Q1 increases. It is possible to make it variable, so that even if the preliminary fuel injection amount Q1 increases to some extent, there is an opportunity to inject the main fuel injection from the predetermined crank angle θ2 in the first half of the middle of the intake stroke in consideration of the engine speed Ne. Increased by that amount, injection end timing EOI2 of main fuel injection
Becomes faster, which is advantageous for forming a uniform mixture.

【0023】[0023]

【発明の効果】このように、本発明による筒内噴射式火
花点火機関の燃料噴射制御装置によれば、気筒上部周囲
の吸気弁側に配置され、燃料を円錐状に吸気行程末期の
ピストン頂面に向けて噴射する燃料噴射弁を具備し、通
常時は、噴射された燃料があまりピストン頂面に付着し
ないように吸気行程中期以降の最適時期から必要燃料量
の噴射を開始し、ノッキング発生時には、必要燃料量の
一部を吸気行程初期に前もって噴射し、この燃料を積極
的にピストン頂面の吸気弁側に衝突させてピストン頂面
の吸気弁側に付着させると共に、シリンダヘッドの気筒
上部の吸気弁側に跳ね返させてそこに付着させ、燃料の
気化熱によりこれらを冷却し、吸気弁側の混合気が排気
弁側の混合気の燃焼膨張により圧縮されても発火温度ま
で温度上昇することは防止され、ノッキングを抑制する
ことができる。この時、点火時期を遅らせる必要はな
く、高い等容度での燃焼が可能であるために、出力向上
のための燃料増量は不要となり、燃費が悪化することは
防止される。
As described above, according to the fuel injection control device for a cylinder injection type spark ignition engine of the present invention, the fuel is conically arranged on the intake valve side around the upper part of the cylinder and the fuel is conically shaped at the piston top at the end of the intake stroke. It is equipped with a fuel injection valve that injects toward the surface, and normally, in order to prevent the injected fuel from adhering too much to the top surface of the piston, injection of the required amount of fuel is started from the optimum timing after the middle of the intake stroke, causing knocking. Sometimes, a portion of the required fuel quantity is injected in advance in the early stage of the intake stroke, and this fuel is positively collided with the intake valve side of the piston top surface to adhere to the intake valve side of the piston top surface, and the cylinder of the cylinder head Even if the air-fuel mixture on the intake valve side is compressed by combustion expansion of the air-fuel mixture on the exhaust valve side, the temperature rises to the ignition temperature by making it bounce back to the upper intake valve side and adhering to it, cooling them by the heat of vaporization of the fuel. To do Is prevented, it is possible to suppress the knocking. At this time, it is not necessary to delay the ignition timing, and since combustion can be performed with a high degree of equality, it is unnecessary to increase the amount of fuel for improving the output, and it is possible to prevent deterioration of fuel efficiency.

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

【図1】本発明による燃料噴射制御装置が取り付けられ
た筒内噴射式火花点火機関の概略縦断面図である。
FIG. 1 is a schematic vertical sectional view of a direct injection spark ignition engine to which a fuel injection control device according to the present invention is attached.

【図2】図1の概略平面図である。FIG. 2 is a schematic plan view of FIG.

【図3】燃料噴射制御のためのフローチャートである。FIG. 3 is a flowchart for fuel injection control.

【図4】特定機関運転状態における燃料噴射を示す図で
ある。
FIG. 4 is a diagram showing fuel injection in a specific engine operating state.

【符号の説明】[Explanation of symbols]

1…点火栓 2…吸気弁 3…排気弁 4…吸気通路 5…排気通路 6…燃料噴射弁 7…ピストン 1 ... Spark plug 2 ... Intake valve 3 ... Exhaust valve 4 ... Intake passage 5 ... Exhaust passage 6 ... Fuel injection valve 7 ... Piston

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 気筒上部周囲の吸気弁側に配置され、燃
料を円錐状に吸気行程末期のピストン頂面に向けて噴射
する燃料噴射弁を具備し、吸気行程中期以降の最適時期
から必要燃料量の噴射を開始する筒内噴射式火花点火機
関の燃料噴射制御装置において、ノッキング発生時に
は、必要燃料量の一部を吸気行程初期に前もって噴射す
ることを特徴とする筒内噴射式火花点火機関の燃料噴射
制御装置。
1. A fuel injection valve, which is arranged on the intake valve side around the upper part of a cylinder and injects fuel conically toward the top surface of the piston at the end of the intake stroke, is equipped with a required fuel from the optimum timing after the middle of the intake stroke. In a fuel injection control device for a cylinder injection type spark ignition engine that starts injection of an amount of fuel, a cylinder injection type spark ignition engine characterized in that when knocking occurs, a part of the required fuel quantity is injected in advance in the early stage of the intake stroke. Fuel injection control device.
JP853694A 1994-01-28 1994-01-28 Fuel injection control device for internal combustion engine Pending JPH07217478A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP853694A JPH07217478A (en) 1994-01-28 1994-01-28 Fuel injection control device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP853694A JPH07217478A (en) 1994-01-28 1994-01-28 Fuel injection control device for internal combustion engine

Publications (1)

Publication Number Publication Date
JPH07217478A true JPH07217478A (en) 1995-08-15

Family

ID=11695880

Family Applications (1)

Application Number Title Priority Date Filing Date
JP853694A Pending JPH07217478A (en) 1994-01-28 1994-01-28 Fuel injection control device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH07217478A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0919714A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Control system for a direct injection spark ignition engine
EP0919709A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Control system for an engine equipped with exhaust gas recirculation system
EP0919711A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Control system for a direct injection spark ignition engine
EP0919713A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Controlsystem for a direct injection-spark ignition engine
US6055956A (en) * 1998-09-29 2000-05-02 Mazda Motor Corporation Control system for an engine equipped with exhaust gas recirculation system
US6085718A (en) * 1998-09-29 2000-07-11 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6116208A (en) * 1998-09-29 2000-09-12 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6257197B1 (en) 1998-09-29 2001-07-10 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6325040B1 (en) 1999-03-02 2001-12-04 Suzuki Motor Corporation Cylinder direct injection engine
JP2003013784A (en) * 2001-06-28 2003-01-15 Nissan Motor Co Ltd Control device of direct injection spark ignition type internal combustion engine
US6513320B1 (en) 1998-09-29 2003-02-04 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
JP2008196387A (en) * 2007-02-13 2008-08-28 Toyota Motor Corp Control device for cylinder injection type internal combustion engine
JP2009138655A (en) * 2007-12-07 2009-06-25 Hitachi Ltd Control device for spark ignition type internal combustion engine

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0919714A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Control system for a direct injection spark ignition engine
EP0919709A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Control system for an engine equipped with exhaust gas recirculation system
EP0919711A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Control system for a direct injection spark ignition engine
EP0919713A2 (en) 1997-11-26 1999-06-02 Mazda Motor Corporation Controlsystem for a direct injection-spark ignition engine
US6116208A (en) * 1998-09-29 2000-09-12 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6085718A (en) * 1998-09-29 2000-07-11 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6055956A (en) * 1998-09-29 2000-05-02 Mazda Motor Corporation Control system for an engine equipped with exhaust gas recirculation system
US6257197B1 (en) 1998-09-29 2001-07-10 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6513320B1 (en) 1998-09-29 2003-02-04 Mazda Motor Corporation Control system for a direct injection-spark ignition engine
US6325040B1 (en) 1999-03-02 2001-12-04 Suzuki Motor Corporation Cylinder direct injection engine
JP2003013784A (en) * 2001-06-28 2003-01-15 Nissan Motor Co Ltd Control device of direct injection spark ignition type internal combustion engine
JP2008196387A (en) * 2007-02-13 2008-08-28 Toyota Motor Corp Control device for cylinder injection type internal combustion engine
JP2009138655A (en) * 2007-12-07 2009-06-25 Hitachi Ltd Control device for spark ignition type internal combustion engine

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