JP4207866B2 - In-cylinder direct injection spark ignition internal combustion engine controller - Google Patents

In-cylinder direct injection spark ignition internal combustion engine controller Download PDF

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JP4207866B2
JP4207866B2 JP2004234972A JP2004234972A JP4207866B2 JP 4207866 B2 JP4207866 B2 JP 4207866B2 JP 2004234972 A JP2004234972 A JP 2004234972A JP 2004234972 A JP2004234972 A JP 2004234972A JP 4207866 B2 JP4207866 B2 JP 4207866B2
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injection
fuel
fuel injection
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top dead
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匡聡 日高
仁 石井
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Nissan Motor Co Ltd
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Description

この発明は、筒内に燃料を直接に噴射する筒内直接噴射式火花点火内燃機関に関し、特に、その噴射時期および点火時期の制御に関する。   The present invention relates to an in-cylinder direct injection spark ignition internal combustion engine that directly injects fuel into a cylinder, and more particularly to control of the injection timing and ignition timing.

特許文献1には、排気浄化用の触媒コンバータが活性温度よりも低い未暖機状態にあるときに、圧縮行程中に燃料噴射を行い、かつ、点火時期を圧縮上死点よりも遅角させる技術が開示されている。   Patent Document 1 discloses that when an exhaust purification catalytic converter is in an unwarmed state lower than an activation temperature, fuel is injected during the compression stroke, and the ignition timing is retarded from the compression top dead center. Technology is disclosed.

なお、特許文献2には、燃料噴射率(単位時間当たりの噴射量)を可変制御することができる可変噴射率燃料噴射弁の一例が開示されている。
特開2001−336467号公報 特開2000−274331号公報
Patent Document 2 discloses an example of a variable injection rate fuel injection valve that can variably control the fuel injection rate (injection amount per unit time).
JP 2001-336467 A JP 2000-274331 A

内燃機関冷機時の触媒の早期活性化を図るべく排気ガス温度を昇温させるとともにHCを低減するためには、点火時期をなるべく大きく遅角させることが望ましいが、点火時期を大幅に遅角すると、燃焼安定度が悪化するため、燃焼安定度の観点から定まるある限界よりも遅角することはできない。特許文献1のような従来の技術では、特に冷機時のような条件下において、安定した燃焼の確保が難しく、燃焼安定度から定まる点火時期の遅角限界が比較的進み側にあり、十分な点火時期の遅角を実現することができない。   In order to raise the exhaust gas temperature and reduce HC in order to achieve early activation of the catalyst when the internal combustion engine is cold, it is desirable to retard the ignition timing as much as possible, but if the ignition timing is significantly retarded Since the combustion stability deteriorates, it cannot be retarded from a certain limit determined from the viewpoint of combustion stability. In the conventional technique such as Patent Document 1, it is difficult to ensure stable combustion, particularly under conditions such as cold, and the retard limit of the ignition timing determined from the combustion stability is relatively advanced, which is sufficient. The ignition timing delay cannot be realized.

本発明は、筒内に直接燃料を噴射する燃料噴射弁を備えるとともに、点火プラグを備えてなる筒内直接噴射式火花点火内燃機関の制御装置において、所定の運転状態のとき、例えば冷機時のような排気ガス温度の昇温が必要な場合などに、上死点噴射運転モードとして、燃料噴射を、噴射開始時期が圧縮上死点前で噴射終了時期が圧縮上死点後となるように圧縮上死点を跨ぐ期間に行い、かつ、上記噴射開始時期から遅れた圧縮上死点後に点火を行うことを特徴としている。そして、さらに、燃料噴射期間の長さをより適切なものとするために、上記燃料噴射弁として燃料噴射率を可変制御可能な可変噴射率燃料噴射弁を用いている。   The present invention provides a control device for an in-cylinder direct injection spark ignition internal combustion engine that includes a fuel injection valve that directly injects fuel into a cylinder and that includes an ignition plug. When it is necessary to raise the exhaust gas temperature, the fuel injection is performed as the top dead center injection operation mode so that the injection start timing is before the compression top dead center and the injection end timing is after the compression top dead center. The ignition is performed in a period straddling the compression top dead center, and ignition is performed after the compression top dead center delayed from the injection start timing. Further, in order to make the length of the fuel injection period more appropriate, a variable injection rate fuel injection valve capable of variably controlling the fuel injection rate is used as the fuel injection valve.

従って、上記上死点噴射運転モードのときに、圧縮上死点前に点火を行う通常の成層燃焼運転モードでの燃料噴射率よりも燃料噴射率を低く制御することで、圧縮上死点を跨ぐ燃料噴射期間をより長く確保することができる。 Therefore, by controlling the fuel injection rate lower than the fuel injection rate in the normal stratified combustion operation mode in which ignition is performed before the compression top dead center in the top dead center injection operation mode, the compression top dead center is reduced. It is possible to secure a longer fuel injection period.

本発明の一つの態様では、吸気行程中に燃料噴射を行う均質燃焼運転モードを備えており、この均質燃焼運転モードにおける燃料噴射率よりも、上記上死点噴射運転モードにおける燃料噴射率が相対的に低く制御されるようになっている。   In one aspect of the present invention, a homogeneous combustion operation mode in which fuel is injected during the intake stroke is provided, and the fuel injection rate in the top dead center injection operation mode is relative to the fuel injection rate in the homogeneous combustion operation mode. It is designed to be controlled low.

図1は、本発明の上死点噴射運転モードにおける燃料噴射期間および点火時期を筒内圧変化とともに例示したものであり、噴射開始時期ITSが圧縮上死点(TDC)前、噴射終了時期ITEが圧縮上死点(TDC)後となる。その間の噴射期間Tの長さは、噴射量に相当する。点火時期ADVは、圧縮上死点(TDC)後であり、噴射開始時期ITSから所定クランク角(例えば10°CA〜25°CA)遅れた時期となる。この遅れ期間Dは、一般に、燃料噴射弁から点火プラグまでの距離に相関する。   FIG. 1 illustrates the fuel injection period and ignition timing in the top dead center injection operation mode of the present invention together with the change in the in-cylinder pressure. The injection start timing ITS is before the compression top dead center (TDC), and the injection end timing ITE is After compression top dead center (TDC). The length of the injection period T during that time corresponds to the injection amount. The ignition timing ADV is after compression top dead center (TDC), and is a timing delayed by a predetermined crank angle (for example, 10 ° CA to 25 ° CA) from the injection start timing ITS. This delay period D generally correlates with the distance from the fuel injection valve to the spark plug.

なお、圧縮上死点(TDC)を中心として前半の圧縮上死点前の期間と後半の圧縮上死点後の期間とがほぼ等しくなるように、噴射開始時期ITSおよび噴射終了時期ITEを制御するようにしてもよい。   The injection start timing ITS and the injection end timing ITE are controlled so that the period before the compression top dead center in the first half and the period after the compression top dead center in the second half are substantially equal with the compression top dead center (TDC) as the center. You may make it do.

図2は、内燃機関の1サイクル中のピストンストロークによるピストン位置変化量と燃焼室の体積変化量とを示したものである。図示するように、単位クランク角当たりの変化量は、ストロークの中間位置付近で最も大きく、下死点(BDC)付近ならびに上死点(TDC)付近では、非常に小さい。従って、本発明で燃料噴射を行う圧縮上死点付近は、ピストン位置変化や体積変化が非常に小さく、ピストンの動き等に影響されない安定した場が形成され得る。   FIG. 2 shows the piston position change amount and the combustion chamber volume change amount due to the piston stroke in one cycle of the internal combustion engine. As shown in the figure, the amount of change per unit crank angle is the largest near the middle position of the stroke, and is very small near the bottom dead center (BDC) and near the top dead center (TDC). Therefore, in the vicinity of the compression top dead center where the fuel injection is performed in the present invention, the piston position change and volume change are very small, and a stable field that is not affected by the piston movement or the like can be formed.

また、筒内には、吸気行程において、スワール流やタンブル流といった比較的大きな流れのガス流動が発生し、圧縮行程においても残存しているが、このようなスワール流やタンブル流といった大きな流れは、ピストンが圧縮上死点付近に達して燃焼室が狭小なものとなると、急激に崩壊する。図3は、種々の機関回転数の下での燃焼室内の大きな流れの流速変化を示したものであり、図示するように、回転数に応じた強さのスワール流ないしタンブル流が発生するが、圧縮上死点(360°CA)に達する前に、急激に崩壊する。従って、本発明において圧縮上死点付近で噴射された燃料噴霧は、スワール流やタンブル流のような大きな流れにより動かされることがなく、点火プラグに対し、常に安定した形で噴霧を形成することが可能である。   In the cylinder, a relatively large gas flow such as a swirl flow or a tumble flow is generated in the intake stroke and remains in the compression stroke. However, a large flow such as a swirl flow or a tumble flow is When the piston reaches near the compression top dead center and the combustion chamber becomes narrow, it collapses rapidly. FIG. 3 shows a change in flow velocity of a large flow in the combustion chamber under various engine speeds. As shown in the figure, a swirl flow or a tumble flow having a strength corresponding to the rotation speed is generated. Collapses rapidly before reaching compression top dead center (360 ° CA). Therefore, in the present invention, the fuel spray injected near the compression top dead center is not moved by a large flow such as a swirl flow or a tumble flow, and always forms a spray in a stable manner on the spark plug. Is possible.

一方、上記のスワール流やタンブル流といった比較的大きな流れのエネルギは、その流れの崩壊に伴って、微小な乱れへと遷移する。従って、燃焼室内の微小な乱れは、圧縮上死点の直前に、急激に増大する。図4は、図3に示した流れの崩壊に伴って生じる微小な乱れの強さを、流速に換算していわゆる乱れ流速として示したものであり、図示するように、圧縮上死点直前に、乱れが大きく増加する。このような微小な乱れは、燃焼場の活性化に寄与し、燃焼改善作用が得られる。   On the other hand, the energy of a relatively large flow such as the swirl flow or the tumble flow described above transitions to minute turbulence as the flow collapses. Therefore, the minute disturbance in the combustion chamber increases rapidly just before the compression top dead center. FIG. 4 shows the intensity of the minute turbulence caused by the collapse of the flow shown in FIG. 3 as a so-called turbulent flow rate converted to a flow velocity, and as shown in the figure, immediately before the compression top dead center. , Disturbances increase greatly. Such minute disturbances contribute to the activation of the combustion field, and a combustion improving action is obtained.

つまり、燃料が噴射される圧縮上死点付近での燃焼室内の場は、噴霧を動かしてしまうような大きな流れが存在せず、かつ燃焼を活発化させる微小な乱れが多く存在し、しかも、ピストンの動きに対し非常に安定した場となる。従って、圧縮上死点よりも遅角した点火時期でもって、安定した燃焼が可能であり、燃焼安定度の上で制限される点火時期の遅角限界が、より遅角側となる。そのため、点火時期の大幅な遅角により、排気ガス温度を大幅に昇温させることができ、かつHC排出量が低減する。   In other words, the field in the combustion chamber near the compression top dead center where the fuel is injected does not have a large flow that moves the spray, and there are many minute disturbances that activate the combustion, It is a very stable place against the movement of the piston. Therefore, stable combustion is possible with the ignition timing retarded from the compression top dead center, and the retard limit of the ignition timing that is limited in terms of combustion stability is on the retard side. For this reason, the exhaust gas temperature can be raised significantly by a large retardation of the ignition timing, and the HC emission amount is reduced.

ここで、上記のように圧縮上死点付近で高い筒内圧に対抗して燃料を噴射するためには、燃料噴射系の燃圧を比較的高く設定する必要があり、従って、同じ燃料噴射量であれば燃料噴射期間が短くなる傾向となる。しかし、圧縮上死点を跨いで噴射される燃料噴射期間が短いと、点火プラグ近傍に可燃混合気が形成されるタイミングが微妙なものとなって不安定化しやすい。つまり、最適な点火時期が狭い範囲でしか得られず、何らかの要因で実際に可燃混合気が形成されるタイミングがずれると、着火が不安定化なものとなる。一方、燃料噴射期間を長くすべく燃料噴射弁として燃料噴射率が低いものを用いたとすると、上死点噴射運転モード以外のときに、燃料噴射期間が過度に長くなる場合が生じてしまう。   Here, in order to inject fuel against a high in-cylinder pressure near the compression top dead center as described above, it is necessary to set the fuel pressure of the fuel injection system to be relatively high. If so, the fuel injection period tends to be shorter. However, if the fuel injection period in which the fuel is injected over the compression top dead center is short, the timing at which the combustible air-fuel mixture is formed in the vicinity of the spark plug becomes subtle and tends to become unstable. In other words, the optimum ignition timing can be obtained only within a narrow range, and if the timing at which the combustible air-fuel mixture is actually formed deviates for some reason, the ignition becomes unstable. On the other hand, if a fuel injection valve having a low fuel injection rate is used to lengthen the fuel injection period, the fuel injection period may become excessively long in a mode other than the top dead center injection operation mode.

本発明では、可変噴射率燃料噴射弁を用いることにより、上死点噴射運転モード以外のときの燃料噴射期間を過度に長くすることなく、上死点噴射運転モードの際に、燃料噴射率を低くすることで、圧縮上死点を跨いで噴射される燃料噴射期間を十分に長くすることができる。これにより、上述したように大きな流れが存在しない安定した場の中で、点火プラグ近傍に適切な可燃混合気が留まる時間がより長くなり、最適な点火時期を比較的広い範囲に得ることができる。つまり、例えばサイクル毎の変動等に対し、より確実な着火燃焼が得られる。   In the present invention, by using the variable injection rate fuel injection valve, the fuel injection rate can be set in the top dead center injection operation mode without excessively extending the fuel injection period in a mode other than the top dead center injection operation mode. By making it low, the fuel injection period that is injected across the compression top dead center can be made sufficiently long. As a result, in a stable field where there is no large flow as described above, the time for the appropriate combustible mixture to remain in the vicinity of the spark plug becomes longer, and the optimal ignition timing can be obtained in a relatively wide range. . That is, for example, more reliable ignition combustion can be obtained with respect to fluctuations in each cycle.

また、例えば高負荷域での均質燃焼運転モードでは、燃料噴射率を高くすることで、燃料噴射を短期間に完了することができ、燃料噴射期間の長期化による燃焼の悪化を回避することが可能である。   Further, for example, in the homogeneous combustion operation mode in a high load region, by increasing the fuel injection rate, the fuel injection can be completed in a short period of time, and deterioration of combustion due to the prolonged fuel injection period can be avoided. Is possible.

この発明によれば、点火時期を圧縮上死点よりも大幅に遅角させた状態で安定した燃焼を得ることができ、例えば内燃機関の冷機時に、排気ガス温度を昇温させて触媒の早期活性化を図ることができるとともに、HC排出量の低減が可能となる。特に、この上死点噴射運転モードの際に燃料噴射率を低くすることで、圧縮上死点を跨いで噴射される燃料噴射期間を十分に長く確保することができ、種々の変動に対し、より確実な点火が可能となる。   According to the present invention, stable combustion can be obtained in a state where the ignition timing is significantly retarded from the compression top dead center. For example, when the internal combustion engine is cold, the exhaust gas temperature is raised and the catalyst is accelerated. Activation can be achieved and HC emissions can be reduced. In particular, by lowering the fuel injection rate during this top dead center injection operation mode, it is possible to ensure a sufficiently long fuel injection period that is injected across the compression top dead center. More reliable ignition is possible.

以下、この発明の一実施例を図面に基づいて詳細に説明する。   Hereinafter, an embodiment of the present invention will be described in detail with reference to the drawings.

図5〜図7は、この発明が適用される筒内直接噴射式火花点火内燃機関の一実施例を示しており、特に、図5,図6は、一つの気筒の構成を示し、図7は機関全体のシステム構成を示している。   5 to 7 show an embodiment of a direct injection type spark ignition internal combustion engine to which the present invention is applied. In particular, FIGS. 5 and 6 show the configuration of one cylinder. Indicates the system configuration of the entire organization.

図5,図6に示すように、シリンダブロック1に形成されたシリンダ2にピストン3が摺動可能に配置されているとともに、シリンダブロック1上面に固定されたシリンダヘッド4と上記ピストン3との間に、燃焼室5が形成されている。上記シリンダヘッド4には、吸気弁6によって開閉される吸気ポート7と、排気弁8によって開閉される排気ポート9と、が形成されている。1つの気筒に対し、一対の吸気弁6と一対の排気弁8とが設けられており、これらの4つの弁に囲まれた燃焼室5天井面中心部に、点火プラグ10が配置されている。また、この実施例では、運転状態によってタンブル流を強化することができるように、吸気ポート7内に、該吸気ポート7内を上下2つの流路に区画する隔壁11が設けられているとともに、その下側の流路を上流端で開閉するタンブル制御弁12が設けられている。当業者には容易に理解できるように、タンブル制御弁12によって下側の流路を閉塞した状態ではタンブル流が強化され、タンブル制御弁12を開いた状態ではタンブル流が弱まる。なお、このタンブル制御弁12は本発明において必ずしも必須のものではなく、省略することも可能であり、また、これに代えて、公知のスワール制御弁を設けるようにしてもよい。   As shown in FIGS. 5 and 6, a piston 3 is slidably disposed in a cylinder 2 formed in the cylinder block 1, and a cylinder head 4 fixed to the upper surface of the cylinder block 1 and the piston 3 A combustion chamber 5 is formed between them. The cylinder head 4 is formed with an intake port 7 that is opened and closed by an intake valve 6 and an exhaust port 9 that is opened and closed by an exhaust valve 8. A pair of intake valves 6 and a pair of exhaust valves 8 are provided for one cylinder, and an ignition plug 10 is disposed at the center of the ceiling surface of the combustion chamber 5 surrounded by these four valves. . Further, in this embodiment, the intake port 7 is provided with a partition wall 11 that divides the intake port 7 into two upper and lower flow paths so that the tumble flow can be strengthened depending on the operating state. A tumble control valve 12 that opens and closes the lower flow path at the upstream end is provided. As can be easily understood by those skilled in the art, the tumble flow is strengthened when the lower flow path is closed by the tumble control valve 12, and the tumble flow is weakened when the tumble control valve 12 is opened. The tumble control valve 12 is not necessarily essential in the present invention, and can be omitted. Alternatively, a known swirl control valve may be provided.

上記シリンダヘッド4の吸気ポート7の下側、より詳しくは一対の吸気ポート7の中間部の位置には、筒内へ燃料を直接噴射する燃料噴射弁15が配置されている。つまり、この燃料噴射弁15は、燃焼室5の吸気弁6側の側部に位置し、平面図上において図示せぬピストンピンと直交する方向に沿って燃料を噴射するように配置されているとともに、図5の断面図上において、斜め下方を指向して配置されている。但し、下方への傾斜角は比較的小さく、つまり水平に近い方向へ燃料を噴射する。   A fuel injection valve 15 for directly injecting fuel into the cylinder is disposed below the intake port 7 of the cylinder head 4, more specifically at a position between the pair of intake ports 7. That is, the fuel injection valve 15 is located on the side of the combustion chamber 5 on the intake valve 6 side, and is disposed so as to inject fuel along a direction orthogonal to a piston pin (not shown) on the plan view. In the cross-sectional view of FIG. However, the downward inclination angle is relatively small, that is, the fuel is injected in a direction close to the horizontal.

ここで、上記燃料噴射弁15としては、燃料噴射率(単位時間当たりの噴射量)を可変制御可能な可変噴射率燃料噴射弁が用いられている。なお、前述した特許文献2のものでは、燃圧を変えることで燃料噴射率を変化させる構成となっているが、本実施例の可変噴射率燃料噴射弁15は、燃圧と無関係に燃料噴射率を可変制御し得る構成となっている。   Here, a variable injection rate fuel injection valve capable of variably controlling the fuel injection rate (injection amount per unit time) is used as the fuel injection valve 15. In the above-mentioned Patent Document 2, the fuel injection rate is changed by changing the fuel pressure. However, the variable injection rate fuel injection valve 15 of this embodiment has a fuel injection rate that is independent of the fuel pressure. The configuration can be variably controlled.

一方、ピストン3の頂部は、ペントルーフ型をなす燃焼室5天井面の傾斜に沿った凸部形状をなしているとともに、その中央部に、平面図上において略矩形をなす凹部16が形成されている。この凹部16の底面は、タンブル流に沿うように、所定の曲率半径の円弧面ないしは円弧に近似した湾曲面をなしている。   On the other hand, the top of the piston 3 has a convex shape along the inclination of the ceiling surface of the combustion chamber 5 that forms a pent roof type, and a concave portion 16 having a substantially rectangular shape in plan view is formed at the center. Yes. The bottom surface of the recess 16 forms an arc surface having a predetermined radius of curvature or a curved surface approximating an arc so as to follow the tumble flow.

図7に示すように、この実施例の内燃機関は、例えば直列4気筒機関であり、各気筒の排気ポート9が接続された排気通路21に、排気浄化用の触媒コンバータ22が設けられており、その上流側に、酸素センサ等の空燃比センサ23が配置されている。また、各気筒の吸気ポート7が接続された吸気通路24は、その入口側に、制御信号により開閉される電子制御スロットル弁25を備えている。上記排気通路21と上記吸気通路24との間には、排気還流通路26が設けられており、その途中に、排気還流制御弁27が介装されている。また、各気筒のタンブル制御弁12は、ソレノイドバルブ28を介して導入される吸入負圧により動作する負圧式タンブル制御アクチュエータ29によって、一斉に開閉される構成となっている。   As shown in FIG. 7, the internal combustion engine of this embodiment is, for example, an in-line four-cylinder engine, and a catalytic converter 22 for purifying exhaust gas is provided in an exhaust passage 21 to which an exhaust port 9 of each cylinder is connected. An air-fuel ratio sensor 23 such as an oxygen sensor is disposed on the upstream side. The intake passage 24 to which the intake port 7 of each cylinder is connected is provided with an electronically controlled throttle valve 25 that is opened and closed by a control signal on the inlet side. An exhaust gas recirculation passage 26 is provided between the exhaust passage 21 and the intake air passage 24, and an exhaust gas recirculation control valve 27 is interposed in the middle. Further, the tumble control valves 12 of the respective cylinders are configured to be simultaneously opened and closed by a negative pressure type tumble control actuator 29 that is operated by a suction negative pressure introduced via a solenoid valve 28.

また、上記燃料噴射弁15には、燃料ポンプ31およびプレッシャレギュレータ32によって所定圧力に調圧された燃料が、燃料ギャラリ33を介して供給されている。従って、各気筒の燃料噴射弁15が制御パルスにより開弁することで、その開弁期間に応じた量の燃料が噴射される。なお、本実施例では、燃圧は常に一定に維持される。また、各気筒の点火プラグ10は、イグニッションコイル34に接続されている。   The fuel injection valve 15 is supplied with the fuel adjusted to a predetermined pressure by the fuel pump 31 and the pressure regulator 32 via the fuel gallery 33. Therefore, when the fuel injection valve 15 of each cylinder is opened by the control pulse, an amount of fuel corresponding to the valve opening period is injected. In this embodiment, the fuel pressure is always kept constant. The ignition plug 10 of each cylinder is connected to an ignition coil 34.

上記内燃機関の燃料噴射時期や噴射量、噴射率、点火時期等は、コントロールユニット35によって制御される。このコントロールユニット35には、アクセルペダル踏み込み量を検出するアクセル開度センサ30の検出信号や、クランク角センサ36の検出信号、空燃比センサ23の検出信号、冷却水温を検出する水温センサ37の検出信号、等が入力されている。   The fuel injection timing, injection amount, injection rate, ignition timing, etc. of the internal combustion engine are controlled by the control unit 35. The control unit 35 includes a detection signal of an accelerator opening sensor 30 that detects the amount of depression of an accelerator pedal, a detection signal of a crank angle sensor 36, a detection signal of an air-fuel ratio sensor 23, and a detection of a water temperature sensor 37 that detects a cooling water temperature. Signals, etc. are input.

上記のように構成された内燃機関においては、暖機が完了した後の状態、例えば冷却水温が80℃を越えているときには、通常の成層燃焼運転および均質燃焼運転が行われる。   In the internal combustion engine configured as described above, when the warm-up is completed, for example, when the cooling water temperature exceeds 80 ° C., normal stratified combustion operation and homogeneous combustion operation are performed.

すなわち、低速低負荷側の所定の領域では、通常の成層燃焼運転モードとして、基本的にタンブル制御弁12を閉じた状態の下で、圧縮行程の適宜な時期に燃料噴射が行われ、かつ圧縮上死点前の時期に点火が行われる。なお、この運転モードでは、圧縮上死点前に必ず燃料噴射が終了する。圧縮行程中にピストン3へ向けて噴射された燃料は、凹部16に沿って旋回するタンブル流を利用して点火プラグ10近傍へ集められ、ここで点火される。そのため、平均的な空燃比がリーンとなった成層燃焼が実現される。このとき、燃料噴射弁15の噴射率は、中間的な噴射率に制御される。   That is, in a predetermined region on the low speed and low load side, as a normal stratified combustion operation mode, fuel injection is performed at an appropriate time in the compression stroke, with the tumble control valve 12 basically closed. Ignition is performed before the top dead center. In this operation mode, fuel injection always ends before compression top dead center. The fuel injected toward the piston 3 during the compression stroke is collected in the vicinity of the spark plug 10 using a tumble flow swirling along the recess 16 and ignited there. Therefore, stratified combustion with an average air-fuel ratio lean is realized. At this time, the injection rate of the fuel injection valve 15 is controlled to an intermediate injection rate.

また、暖機完了後の高速高負荷側の所定の領域では、通常の均質燃焼運転モードとして、基本的にタンブル制御弁12を開いた状態の下で、吸気行程中に燃料噴射が行われ、かつ圧縮上死点前のMBT点において点火が行われる。この場合は、燃料は筒内で均質な混合気となり、基本的に理論空燃比近傍で運転が行われる。また燃料噴射弁15の噴射率は、高い噴射率に制御される。従って、燃料噴射量が多い高負荷時にも、燃料噴射期間が比較的短くなり、短期間で良好に混合した状態となって、良好な燃焼が確保できる。   Further, in a predetermined region on the high speed and high load side after the warm-up is completed, fuel injection is performed during the intake stroke under the condition that the tumble control valve 12 is basically opened as a normal homogeneous combustion operation mode. And ignition is performed at the MBT point before the compression top dead center. In this case, the fuel becomes a homogeneous air-fuel mixture in the cylinder and is basically operated near the stoichiometric air-fuel ratio. The injection rate of the fuel injection valve 15 is controlled to a high injection rate. Therefore, even during a high load with a large amount of fuel injection, the fuel injection period is relatively short, and the fuel is mixed well in a short period of time, thus ensuring good combustion.

これに対し、内燃機関の冷却水温が80℃以下のとき、つまり暖機が完了していない状態では、触媒コンバータ22の活性化つまり温度上昇の促進とHC排出量低減のために、上死点噴射運転モードとなる。この上死点噴射運転モードでは、燃料噴射期間が十分に長く得られるように、噴射率が低く制御される。そして、前述した図1に示したように、噴射開始時期ITSが圧縮上死点(TDC)前、噴射終了時期ITEが圧縮上死点(TDC)後となり、圧縮上死点を跨いで燃料噴射が行われる。点火時期ADVは、圧縮上死点(TDC)後となり、噴射開始時期ITSから10°CA〜25°CA遅れた時期に点火される。この遅れ期間の間に、燃料噴霧がちょうど点火プラグ10付近に到達し、点火プラグ10付近に可燃混合気を形成するので、確実に着火燃焼に至り、成層燃焼が行われる。このとき、燃料噴射量は、平均的な空燃比が理論空燃比となるように制御される。   On the other hand, when the cooling water temperature of the internal combustion engine is 80 ° C. or lower, that is, when the warm-up is not completed, the top dead center is used to activate the catalytic converter 22, that is, promote the temperature rise and reduce the HC emissions. It becomes the injection operation mode. In this top dead center injection operation mode, the injection rate is controlled to be low so that the fuel injection period is sufficiently long. Then, as shown in FIG. 1 described above, the injection start timing ITS is before the compression top dead center (TDC), and the injection end timing ITE is after the compression top dead center (TDC). Is done. The ignition timing ADV is after compression top dead center (TDC), and is ignited at a timing delayed by 10 ° CA to 25 ° CA from the injection start timing ITS. During this delay period, the fuel spray just reaches the vicinity of the spark plug 10 and forms a combustible air-fuel mixture in the vicinity of the spark plug 10, so that ignition combustion is surely performed and stratified combustion is performed. At this time, the fuel injection amount is controlled so that the average air-fuel ratio becomes the stoichiometric air-fuel ratio.

本実施例では、上記の燃料噴射時期は、噴射開始時期ITSが所定のクランク角となるように制御され、噴射終了時期ITEは、この噴射開始時期ITSと燃料噴射量(噴射時間)とによって定まる。なお、燃料噴射期間における圧縮上死点前の期間と圧縮上死点後の期間とが等しくなるように、燃料噴射量に基づき、噴射開始時期ITSと噴射終了時期ITEとを求めるようにすることも可能である。   In this embodiment, the fuel injection timing is controlled so that the injection start timing ITS becomes a predetermined crank angle, and the injection end timing ITE is determined by the injection start timing ITS and the fuel injection amount (injection time). . The injection start timing ITS and the injection end timing ITE are obtained based on the fuel injection amount so that the period before the compression top dead center and the period after the compression top dead center in the fuel injection period are equal. Is also possible.

前述したように、この上死点噴射運転モードにおいて燃料が噴射される圧縮上死点付近での燃焼室内の場は、大きな流れの崩壊により噴霧を動かしてしまうような大きな流れが存在せず、かつ大きな流れの崩壊に伴い、燃焼を活発化させる微小な乱れが多く存在し、しかも、ピストンの動きに対し非常に安定した場となる。従って、圧縮上死点よりも遅角した点火時期でもって、安定した燃焼が可能であり、燃焼安定度の上で制限される点火時期の遅角限界が、より遅角側となる。そのため、点火時期の大幅な遅角により、排気ガス温度を大幅に昇温させることができ、かつHC排出量が低減する。特に、上死点噴射運転モードの際に噴射率を低くし、圧縮上死点を跨いで噴射される燃料噴射期間を十分に長くすることにより、タンブルのような大きな流れが存在しない安定した場の中で、点火プラグ10近傍に適切な可燃混合気が留まる時間をより長くすることができ、最適な点火時期を比較的広い範囲に得ることができる。これにより、例えばサイクル毎の変動等に対し、より確実な着火燃焼が得られる。   As described above, the field in the combustion chamber near the compression top dead center where fuel is injected in this top dead center injection operation mode does not have a large flow that causes the spray to move due to the collapse of the large flow, Along with the collapse of the large flow, there are many minute disturbances that activate the combustion, and the field becomes very stable against the movement of the piston. Therefore, stable combustion is possible with the ignition timing retarded from the compression top dead center, and the retard limit of the ignition timing that is limited in terms of combustion stability is on the retard side. For this reason, the exhaust gas temperature can be raised significantly by a large retardation of the ignition timing, and the HC emission amount is reduced. In particular, by reducing the injection rate during the top dead center injection operation mode and sufficiently lengthening the fuel injection period that is injected across the compression top dead center, a stable field where there is no large flow such as tumble exists. Among these, the time during which an appropriate combustible mixture remains in the vicinity of the spark plug 10 can be made longer, and the optimal ignition timing can be obtained in a relatively wide range. Thereby, for example, more reliable ignition combustion can be obtained with respect to fluctuation or the like for each cycle.

図8は、上記の上死点噴射運転モードにおける点火プラグ10近傍の局所的な空燃比と点火時期との関係を模式的に示した特性図であって、点火プラグ10近傍の空燃比は、燃料噴射開始から若干の遅れの後、徐々に濃くなっていき、点火可能な空燃比域に達する。そして、その後、燃料噴射が終了すると、若干の遅れの後、徐々に薄くなっていき、点火可能な空燃比域から外れる。従って、本実施例では、図のΔ1の期間が点火可能な時期となり、例えばこのΔ1の期間内に適宜な余裕を見込んで点火時期を設定すれば、サイクル変動等種々の要因により実際の空燃比変化のタイミングが多少ずれたとしても、確実な点火が可能である。   FIG. 8 is a characteristic diagram schematically showing the relationship between the local air-fuel ratio in the vicinity of the spark plug 10 and the ignition timing in the top dead center injection operation mode, and the air-fuel ratio in the vicinity of the spark plug 10 is After a slight delay from the start of fuel injection, it gradually increases and reaches an air-fuel ratio range that can be ignited. After that, when the fuel injection is completed, after a slight delay, the fuel gradually becomes thinner and deviates from the ignitable air-fuel ratio range. Therefore, in the present embodiment, the period Δ1 in the figure is a timing at which ignition is possible. For example, if the ignition timing is set with an appropriate margin within the period Δ1, the actual air-fuel ratio is caused by various factors such as cycle fluctuations. Even if the timing of the change slightly deviates, reliable ignition is possible.

これに対し、仮に、噴射率が高い状態で燃料噴射を行ったとすると、圧縮上死点を跨いで設定される燃料噴射期間が短くなり、点火プラグ10近傍の空燃比の変化は比較例として示す破線のようになる。つまり点火可能な空燃比域に留まる期間が燃料噴射期間の短縮に伴って短くなり、点火可能な時期が、図のΔ2の期間内に制限されてしまう。従って、適切な点火時期の設定が難しくなり、サイクル変動等の何らかの要因により実際の空燃比変化のタイミングが僅かでもずれると、着火が不安定なものとなり易い。   On the other hand, if fuel injection is performed with a high injection rate, the fuel injection period set across the compression top dead center is shortened, and the change in the air-fuel ratio in the vicinity of the spark plug 10 is shown as a comparative example. It looks like a dashed line. That is, the period during which the air-fuel ratio can be ignited is shortened as the fuel injection period is shortened, and the ignition timing is limited within the period Δ2. Accordingly, it becomes difficult to set an appropriate ignition timing, and if the actual air-fuel ratio change timing slightly shifts due to some factor such as cycle fluctuation, the ignition tends to become unstable.

なお、上記実施例では、燃料噴射弁15が燃焼室5の側部に配置され、水平に近い方向に燃料を噴射する構成となっているが、これに代えて、燃料噴射弁15が、一対の吸気弁6と一対の排気弁8とに囲まれた燃焼室5天井面中心部に配置され、垂直に近い角度でピストン3頂面へ向けて燃料を噴射するようにした所謂直上噴射形式の構成とすることも可能である。   In the above-described embodiment, the fuel injection valve 15 is disposed on the side of the combustion chamber 5 and is configured to inject fuel in a direction close to horizontal. Instead, the fuel injection valve 15 includes a pair of fuel injection valves 15. Of the combustion chamber 5 surrounded by the intake valve 6 and the pair of exhaust valves 8 in the center of the ceiling surface of the combustion chamber 5 so as to inject fuel toward the top surface of the piston 3 at an angle close to vertical. A configuration is also possible.

また、上記実施例では、燃圧は常に一定に維持されるが、負荷の上昇(つまり燃料噴射量の増加)に対し燃料噴射期間が過度に長くならないように、負荷が高いほど燃圧が高くなるように燃圧制御を行っても良い。   In the above embodiment, the fuel pressure is always maintained constant. However, the fuel pressure increases as the load increases so that the fuel injection period does not become excessively long with respect to the increase in load (that is, increase in fuel injection amount). Alternatively, fuel pressure control may be performed.

本発明の燃料噴射期間および点火時期の一例を示した特性図。The characteristic view which showed an example of the fuel-injection period and ignition timing of this invention. サイクル中のピストン位置変化量と体積変化量の特性図。The characteristic figure of the piston position change amount and volume change amount during a cycle. 大きな流れのサイクル中の変化を示す特性図。The characteristic figure which shows the change in the cycle of a big flow. 微小な乱れのサイクル中の変化を示す特性図。The characteristic view which shows the change in the cycle of a minute disturbance. 筒内直接噴射式火花点火内燃機関の一実施例を示す断面図。Sectional drawing which shows one Example of a direct injection type spark ignition internal combustion engine. 同じく平面図。FIG. この内燃機関全体のシステム構成を示す構成説明図。FIG. 2 is a configuration explanatory view showing the system configuration of the entire internal combustion engine. 点火プラグ近傍の局所的な空燃比と点火時期との関係を示す特性図。The characteristic view which shows the relationship between the local air fuel ratio in the vicinity of a spark plug, and ignition timing.

符号の説明Explanation of symbols

3…ピストン
5…燃焼室
10…点火プラグ
15…燃料噴射弁
3 ... Piston 5 ... Combustion chamber 10 ... Spark plug 15 ... Fuel injection valve

Claims (4)

筒内に直接燃料を噴射する燃料噴射弁を備えるとともに、点火プラグを備えてなる筒内直接噴射式火花点火内燃機関の制御装置において、排気ガス温度の昇温が要求されたときに、上死点噴射運転モードとして、燃料噴射を、噴射開始時期が圧縮上死点前で噴射終了時期が圧縮上死点後となるように圧縮上死点を跨ぐ期間に行い、かつ、上記噴射開始時期から遅れた圧縮上死点後に点火を行うとともに、上記燃料噴射弁として燃料噴射率を可変制御可能な可変噴射率燃料噴射弁を用い、上記上死点噴射運転モードのときに、圧縮上死点前に点火を行う通常の成層燃焼運転モードでの燃料噴射率よりも燃料噴射率を低く制御することを特徴とする筒内直接噴射式火花点火内燃機関の制御装置。 In a control device for an in-cylinder direct-injection spark-ignition internal combustion engine that includes a fuel injection valve that directly injects fuel into the cylinder and that includes an ignition plug, when the exhaust gas temperature is required to rise, As the point injection operation mode, fuel injection is performed in a period spanning the compression top dead center so that the injection start time is before the compression top dead center and the injection end time is after the compression top dead center, and from the injection start time The ignition is performed after the delayed compression top dead center, and the variable injection rate fuel injection valve capable of variably controlling the fuel injection rate is used as the fuel injection valve. A control device for an in-cylinder direct injection spark ignition internal combustion engine, wherein the fuel injection rate is controlled to be lower than the fuel injection rate in a normal stratified combustion operation mode in which ignition is performed . 点火時期が、噴射開始時期から10°CA〜25°CA遅れた時期であることを特徴とする請求項1に記載の筒内直接噴射式火花点火内燃機関の制御装置。   2. The control apparatus for a direct injection type spark ignition internal combustion engine according to claim 1, wherein the ignition timing is a time delayed by 10 [deg.] CA to 25 [deg.] CA from the injection start timing. 吸気行程中に燃料噴射を行う均質燃焼運転モードを備え、この均質燃焼運転モードにおける燃料噴射率よりも、上記上死点噴射運転モードにおける燃料噴射率が相対的に低いことを特徴とする請求項1または2に記載の筒内直接噴射式火花点火内燃機関の制御装置。 A homogeneous combustion operation mode in which fuel is injected during an intake stroke is provided, and the fuel injection rate in the top dead center injection operation mode is relatively lower than the fuel injection rate in the homogeneous combustion operation mode. 3. A control apparatus for an in-cylinder direct injection spark ignition internal combustion engine according to 1 or 2 . 上記均質燃焼運転モードと上記上死点噴射運転モードとで燃圧が変化しないことを特徴とする請求項に記載の筒内直接噴射式火花点火内燃機関の制御装置。 4. The control device for a direct injection spark ignition internal combustion engine according to claim 3 , wherein the fuel pressure does not change between the homogeneous combustion operation mode and the top dead center injection operation mode.
JP2004234972A 2004-08-12 2004-08-12 In-cylinder direct injection spark ignition internal combustion engine controller Expired - Fee Related JP4207866B2 (en)

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