JP2007032378A - Control device for cylinder direct injection type spark ignition internal combustion engine - Google Patents

Control device for cylinder direct injection type spark ignition internal combustion engine Download PDF

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JP2007032378A
JP2007032378A JP2005215208A JP2005215208A JP2007032378A JP 2007032378 A JP2007032378 A JP 2007032378A JP 2005215208 A JP2005215208 A JP 2005215208A JP 2005215208 A JP2005215208 A JP 2005215208A JP 2007032378 A JP2007032378 A JP 2007032378A
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injection
dead center
top dead
fuel
compression top
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JP4525509B2 (en
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Hitoshi Ishii
仁 石井
Mitsuyasu Akagi
三泰 赤木
Yuuya Hakamata
雄哉 袴田
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Nissan Motor Co Ltd
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    • 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
    • Y02T10/12Improving ICE efficiencies
    • 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

<P>PROBLEM TO BE SOLVED: To materialize rise of exhaust gas temperature and reduction of HC emission at a time of cold engine by compatibly establishing large delay of ignition timing and combustion stability. <P>SOLUTION: Normal stratified combustion operation and homogeneous combustion operation are performed under warm up completion condition. Main fuel injection I1 is performed over top dead center to make injection start timing ITS before compression top dead center and injection end timing ITE after top dead center as a top dead center injection operation mode is performed for accelerating activation of a catalytic converter and HC emission reduction under a cold engine condition. Ignition timing ADV is after top dead center. Since swirl and tumble are attenuated at compression top dead center and minute turbulence is activated and position change of a piston is small at compression top dead center, stable combustion can be materialized. Part of fuel is injected as expansion stroke injection I2 for raise exhaust gas temperature further. <P>COPYRIGHT: (C)2007,JPO&INPIT

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。
特開2001−336467号公報
In Patent Document 1, when the exhaust gas-purifying catalytic converter is in an unwarmed state lower than the activation temperature, fuel is injected during the compression stroke, and the ignition timing is retarded from the compression top dead center. Technology is disclosed.
JP 2001-336467 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、例えば触媒コンバータの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とともに、この圧縮上死点を跨ぐ期間の主噴射から遅れて、上記の点火後に燃料の一部を膨張行程噴射として噴射することを特徴としている。上記膨張行程噴射は、望ましくは、上記主噴射による燃焼が終了した直後に行う。例えば、膨張行程噴射の噴射開始時期は、上記点火時期から50°CA〜100°CA程度遅れた時期となる。   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, such as when the engine is cold, the fuel injection is performed as the top dead center injection operation mode. 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, and the ignition is performed after the main injection in the period straddling the compression top dead center. A feature is that a part of the fuel is injected later as an expansion stroke injection. The expansion stroke injection is desirably performed immediately after the combustion by the main injection is completed. For example, the injection start timing of the expansion stroke injection is delayed by about 50 ° CA to 100 ° CA from the ignition timing.

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例示したものであり、図示するように、圧縮上死点を跨ぐ主噴射I1とこれから遅れた膨張行程噴射I2とが行われるが、本発明では、基本的に、主噴射I1によって燃焼が成立する。この主噴射I1は、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 exemplifies the fuel injection period and ignition timing in the top dead center injection operation mode of the present invention. As shown in FIG. 1, the main injection I1 straddling the compression top dead center and the expansion stroke injection I2 delayed from the main injection I1 However, in the present invention, combustion is basically established by the main injection I1. In the main injection I1, 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). 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.

そして、本発明では、さらに排気ガス温度の昇温を図るために、主噴射による燃料への点火後の膨張行程において、燃料の一部を膨張行程噴射I2として噴射する。この膨張行程噴射による燃料は、筒内の温度によって自着火し、排気ガス温度をさらに高める。なお、主噴射の燃焼中に次の膨張行程噴射の燃料が噴射されると、拡散燃焼となってスモークが増加するので、主噴射による燃焼が終了した直後に行うことが望ましい。本発明では、そもそもの主噴射による燃焼が上死点よりも遅れて行われることから、膨張行程噴射による燃料の燃焼が非常に遅い時期となり、排気ガス温度が効果的に上昇する。   In the present invention, in order to further raise the exhaust gas temperature, a part of the fuel is injected as the expansion stroke injection I2 in the expansion stroke after ignition of the fuel by the main injection. The fuel by the expansion stroke injection is self-ignited by the temperature in the cylinder, and further increases the exhaust gas temperature. In addition, if the fuel of the next expansion stroke injection is injected during the combustion of the main injection, it becomes diffusion combustion and the smoke increases. Therefore, it is desirable to carry out immediately after the completion of the combustion by the main injection. In the present invention, since the combustion by the main injection is performed after the top dead center, the combustion of the fuel by the expansion stroke injection becomes very late, and the exhaust gas temperature effectively rises.

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、燃料の一部を主噴射の点火後に膨張行程噴射として噴射することにより、排気ガス温度を最大限に高めることができる。   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 injecting a part of the fuel as an expansion stroke injection after ignition of the main injection, the exhaust gas temperature can be maximized.

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.

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。さらに、本実施例では、触媒コンバータ22の温度状態を検出するために、該触媒コンバータ22のモノリス型セラミックス触媒担体の長手方向中央部に配置された触媒温度センサ38を備えている。   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. Furthermore, in this embodiment, in order to detect the temperature state of the catalytic converter 22, a catalyst temperature sensor 38 is provided at the center in the longitudinal direction of the monolith ceramic catalyst carrier of the catalytic converter 22.

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においては、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, normal stratified combustion operation and homogeneous combustion operation are performed after the warm-up is completed.

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。   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.

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。   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.

これに対し、内燃機関の暖機が完了していない状態においては、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、基本的に、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、前述した図1に示したように、主噴射I1と膨張行程噴射I2とが行われ、主噴射I1は、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、主噴射I1の噴射開始時期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、主噴射I1の燃料噴射量は、平均的な空燃比が30前後となるように設定される。そして、膨張行程噴射I2は、主噴射I1による燃焼が終了した直後の時期に噴射される。例えば、上記点火時期ADVから50°CA〜100°CA程度遅れた時期に膨張行程噴射I2が開始される。この膨張行程噴射I2の噴射量は、主噴射I1と膨張行程噴射I2との総燃料量による平均空燃比が理論空燃比よりもややリーン、例えば16〜17程度となるように設定される。   On the other hand, in the state where the warm-up of the internal combustion engine is not completed, the top dead center injection operation mode is basically set in order to activate the catalytic converter 22, that is, promote the temperature rise and reduce the HC emission amount. . In this top dead center injection operation mode, as shown in FIG. 1 described above, main injection I1 and expansion stroke injection I2 are performed. In main injection I1, the injection start timing ITS is before compression top dead center (TDC). The injection end timing ITE is after the compression top dead center (TDC), and fuel injection is performed across the compression top dead center. The ignition timing ADV is after the compression top dead center (TDC), and is ignited at a timing delayed by 10 ° CA to 25 ° CA from the injection start timing ITS of the main injection I1. 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 of the main injection I1 is set so that the average air-fuel ratio is around 30. The expansion stroke injection I2 is injected at a time immediately after the combustion by the main injection I1 is completed. For example, the expansion stroke injection I2 is started at a time delayed by about 50 ° CA to 100 ° CA from the ignition timing ADV. The injection amount of the expansion stroke injection I2 is set so that the average air-fuel ratio based on the total fuel amount of the main injection I1 and the expansion stroke injection I2 is slightly leaner than the theoretical air-fuel ratio, for example, about 16 to 17.

なお、本実施例では、上記の主噴射I1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 the present embodiment, the fuel injection timing of the main injection I1 is controlled such 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。   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.

また主噴射I1の燃焼終了直後に噴射された膨張行程噴射I2の燃料は、筒内の温度によって自着火し、そのエネルギの多くが熱となって排気ガス温度の上昇に寄与する。特に、主噴射I1による燃焼が上死点TDCよりも遅れて行われ、その燃焼終了後に膨張行程噴射による燃焼が行われるので、非常に遅い時期となり、排気ガス温度が効果的に上昇する。また、膨張行程噴射I2が行われるタイミングでの筒内の温度変化が比較的緩やかであるので、膨張行程噴射I2の燃料の自着火が安定的に行われる。   Further, the fuel of the expansion stroke injection I2 injected immediately after the end of the combustion of the main injection I1 is self-ignited by the temperature in the cylinder, and most of the energy becomes heat and contributes to the increase of the exhaust gas temperature. In particular, the combustion by the main injection I1 is performed later than the top dead center TDC, and the combustion by the expansion stroke injection is performed after the end of the combustion, so that it becomes a very late time and the exhaust gas temperature effectively increases. Further, since the temperature change in the cylinder at the timing when the expansion stroke injection I2 is performed is relatively gradual, the self-ignition of the fuel in the expansion stroke injection I2 is stably performed.

図8は、上述した本発明の上死点噴射運転モードの場合の主噴射I1の燃焼による発生熱量(a1)および筒内温度(b1)を、一般的な圧縮行程噴射(図の主噴射I101)の燃焼による発生熱量(a2)および筒内温度(b2)と対比して示したものである。燃焼期間は発生熱量の変化によって表されるが、本発明では、燃焼終了直後に膨張行程噴射I2が行われ、このときの筒内温度は、符号t1で示す付近のものとなる。これに対し、仮に、一般的な圧縮行程噴射の燃焼終了直後に追加噴射I102を加えるとすると、このときの筒内温度は、符号t2で示す付近のものとなる。t1付近の温度とt2付近の温度とは、温度そのものはあまり変わらないが、単位クランク角当たりの温度低下は、t2付近の方が急激であり、t1付近の方が相対的に緩やかである。従って、本発明の膨張行程噴射I2の方がより確実に自着火に至る。また、図の追加噴射I102に比べて本発明の膨張行程噴射I2の方が遙かに遅い時期に燃焼するので、排気ガス温度の上昇の上で有利となる。   FIG. 8 shows the amount of heat generated by the combustion of the main injection I1 (a1) and the in-cylinder temperature (b1) in the above-described top dead center injection operation mode of the present invention. ) And the amount of heat generated by combustion (a2) and the in-cylinder temperature (b2). Although the combustion period is represented by a change in the amount of generated heat, in the present invention, the expansion stroke injection I2 is performed immediately after the end of the combustion, and the in-cylinder temperature at this time is in the vicinity indicated by the symbol t1. On the other hand, if the additional injection I102 is added immediately after the end of the combustion of the general compression stroke injection, the in-cylinder temperature at this time is in the vicinity indicated by reference numeral t2. Although the temperature itself does not change much between the temperature near t1 and the temperature near t2, the temperature decrease per unit crank angle is sharper near t2 and relatively gentle near t1. Therefore, the expansion stroke injection I2 of the present invention leads to self-ignition more reliably. Further, since the expansion stroke injection I2 of the present invention burns at a much later time than the additional injection I102 in the figure, it is advantageous in increasing the exhaust gas temperature.

次に、図9および図10は、上記実施例の内燃機関の始動直後におけるより具体的な運転モードの変化の一例を示している。この例では、始動後、時間経過に伴って、第1フェーズ,第2フェーズ,第3フェーズの3段階に順次移行する。すなわち、図9のフローチャートに示すように、始動後、所定時間(例えば数秒程度)経過するまでは、第1フェーズとする(ステップ1,2)。所定時間経過後は、触媒温度センサ38により検出される触媒温度Tcatの変化率ΔTcatを監視し、ある変化率a以上の急激な温度上昇の間は第1フェーズを継続し、変化率a未満となったら、第2フェーズへ移行する(ステップ3,4,5)。第2フェーズでは、触媒温度Tcatを監視し、これが所定温度bを越えたら、第3フェーズへ移行する(ステップ6,7)。   Next, FIG. 9 and FIG. 10 show an example of more specific operation mode changes immediately after the start of the internal combustion engine of the above embodiment. In this example, after the start, the three phases of the first phase, the second phase, and the third phase are sequentially shifted with time. That is, as shown in the flowchart of FIG. 9, the first phase is set until a predetermined time (for example, about several seconds) elapses after starting (steps 1 and 2). After a predetermined time has elapsed, the rate of change ΔTcat of the catalyst temperature Tcat detected by the catalyst temperature sensor 38 is monitored, and the first phase is continued during a rapid temperature rise above a certain rate of change a. If it becomes, it will transfer to a 2nd phase (step 3, 4, 5). In the second phase, the catalyst temperature Tcat is monitored, and when it exceeds the predetermined temperature b, the process proceeds to the third phase (steps 6 and 7).

前述した図1の上死点噴射運転モードは、第2フェーズに相当する。また、通常の均質燃焼運転モードが第3フェーズに相当する。これに対し、第1フェーズは、上記上死点噴射運転モードの主噴射I1のみの燃焼に相当するものであり、図10のタイムチャートに示すように、噴射開始時期が圧縮上死点(TDC)前で噴射終了時期が圧縮上死点(TDC)後となるように圧縮上死点を跨いで行われる1回の燃料噴射期間の間に、燃料の全量が噴射される。点火時期ADVは、圧縮上死点(TDC)後となり、やはり噴射開始時期から10°CA〜25°CA遅れた時期に点火される。空燃比は、第2フェーズと同じく、16〜17程度に維持される。   The above-described top dead center injection operation mode in FIG. 1 corresponds to the second phase. The normal homogeneous combustion operation mode corresponds to the third phase. On the other hand, the first phase corresponds to the combustion of only the main injection I1 in the top dead center injection operation mode, and as shown in the time chart of FIG. 10, the injection start timing is the compression top dead center (TDC). ) The entire amount of fuel is injected during one fuel injection period that is performed across the compression top dead center so that the injection end timing is after the compression top dead center (TDC). The ignition timing ADV is after compression top dead center (TDC), and is also ignited at a timing delayed by 10 ° CA to 25 ° CA from the injection start timing. The air-fuel ratio is maintained at about 16 to 17 as in the second phase.

この第1フェーズの燃焼形態では、第2フェーズの上死点噴射運転モードに比べると排気ガス温度は低いものの、通常の成層燃焼運転や均質燃料運転に比べると、十分に高い排気ガス温度が得られ、かつ第2フェーズの上死点噴射運転モードよりもHC生成量が少ないものとなる。つまり、触媒温度Tcatが非常に低い始動直後の間は、触媒作用に依存せずにHCを最小限とするように、膨張行程噴射I2を行わないで、燃料の全量を上死点を跨ぐ期間に噴射する。なお、図示例では、上死点前の噴射期間と上死点後の噴射期間とが等しくなっている。   In this first phase combustion mode, the exhaust gas temperature is lower than that in the second phase top dead center injection operation mode, but a sufficiently high exhaust gas temperature is obtained compared to the normal stratified combustion operation and homogeneous fuel operation. And the amount of HC generated is smaller than that in the second phase top dead center injection operation mode. That is, immediately after start-up where the catalyst temperature Tcat is very low, the expansion stroke injection I2 is not performed so that HC is minimized without depending on the catalytic action, and the entire amount of fuel is straddled over the top dead center. To spray. In the illustrated example, the injection period before top dead center is equal to the injection period after top dead center.

前述したフローチャートに従って第1フェーズから第2フェーズへ移行すると、燃料の一部が膨張行程噴射I2として噴射されるようになり、前述した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は、第1フェーズの燃焼形態よりも燃焼効率が低いので、同じトルクを維持するために電子制御スロットル弁25の開度がより大きく制御され、吸気量Qaが増加する。従って、総燃料量もこれに見合うように増加し、平均空燃比は第1フェーズから変化しない。なお、実際には、電子制御スロットル弁25の開度変化に対し吸気量Qaの変化は応答遅れを伴ったものとなるが、図10では、説明の簡略化のためにステップ的に変化するように示してある。   When shifting from the first phase to the second phase according to the flowchart described above, a part of the fuel is injected as the expansion stroke injection I2, and the above-described top dead center injection operation mode is set. In this top dead center injection operation mode, the combustion efficiency is lower than that of the combustion mode of the first phase. Therefore, in order to maintain the same torque, the opening degree of the electronic control throttle valve 25 is controlled to be larger, and the intake air amount Qa is increased. . Accordingly, the total amount of fuel also increases correspondingly, and the average air-fuel ratio does not change from the first phase. Actually, the change in the intake air amount Qa is accompanied by a response delay with respect to the change in the opening degree of the electronic control throttle valve 25. However, in FIG. It is shown in

その後、第3フェーズに移行すると、空燃比センサ23の検出に基づく空燃比制御が開始されるため、空燃比は、理論空燃比に維持される。また、第3フェーズでは、点火時期がMBT点に近づき、燃焼効率が高くなることから、同じトルクを維持するために電子制御スロットル弁25の開度は小さくなり、吸気量Qaが減少する。このように、冷間始動時に、第1〜第3フェーズと段階的に変化させることで、触媒が速やかに活性化し、外部へのHC等の排出を最小限にすることができる。   Thereafter, when the third phase is entered, air-fuel ratio control based on the detection of the air-fuel ratio sensor 23 is started, so that the air-fuel ratio is maintained at the stoichiometric air-fuel ratio. In the third phase, since the ignition timing approaches the MBT point and the combustion efficiency increases, the opening degree of the electronically controlled throttle valve 25 decreases to maintain the same torque, and the intake air amount Qa decreases. In this way, by changing in stages from the first to third phases at the time of cold start, the catalyst can be activated quickly and the discharge of HC or the like to the outside can be minimized.

なお、上記第1フェーズは必ずしも必須のものではなく、省略することも可能である。   Note that the first phase is not necessarily essential and can be omitted.

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. 主噴射I1の燃焼による発生熱量および筒内温度の変化を一般的な圧縮行程噴射と対比して示す特性図。The characteristic view which shows the amount of heat generated by combustion of the main injection I1 and the change in the in-cylinder temperature in comparison with general compression stroke injection. 冷間始動時の制御の流れを示すフローチャート。The flowchart which shows the flow of control at the time of cold start. 冷間始動時のフェーズの変化を示すタイムチャート。The time chart which shows the change of the phase at the time of cold start.

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 (8)

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に、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、この圧縮上死点を跨ぐ期間の主噴射から遅れて、上記の点火後に燃料の一部を膨張行程噴射として噴射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 a direct injection type spark ignition internal combustion engine that includes a fuel injection valve that directly injects fuel into a cylinder and includes an ignition plug, the fuel injection is performed at an injection start timing in a predetermined operating state. Is performed in a period straddling the compression top dead center so that the injection end timing is after the compression top dead center before the compression top dead center, and ignition is performed after the compression top dead center delayed from the injection start timing. A control apparatus for an in-cylinder direct injection spark ignition internal combustion engine, characterized in that a part of the fuel is injected as an expansion stroke injection after the ignition, delayed from the main injection in a period over the compression top dead center. 上記膨張行程噴射は、上記主噴射による燃焼が終了した直後に行う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 spark ignition internal combustion engine according to claim 1, wherein the expansion stroke injection is performed immediately after the combustion by the main injection is completed. 上記主噴射と上記膨張行程噴射との総燃料量による平均空燃比が16〜17程度である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。   The control device for a direct injection spark ignition internal combustion engine according to claim 1 or 2, wherein an average air-fuel ratio according to a total fuel amount of the main injection and the expansion stroke injection is about 16 to 17. 上記主噴射の燃料量による平均空燃比が30程度であることを特徴とする請求項3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 apparatus for a direct injection type spark ignition internal combustion engine according to claim 3, wherein an average air-fuel ratio according to the amount of fuel of the main injection is about 30. 点火時期が、圧縮上死点を跨ぐ主噴射の噴射開始時期から10°CA〜25°CA遅れた時期であることを特徴とする請求項1〜4のいずれかに記載の筒内直接噴射式火花点火内燃機関の制御装置。   The in-cylinder direct injection type according to any one of claims 1 to 4, wherein the ignition timing is a timing delayed by 10 ° CA to 25 ° CA from an injection start timing of main injection straddling the compression top dead center. Control device for spark ignition internal combustion engine. 圧縮上死点を跨ぐ主噴射の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ほぼ等しいことを特徴とする請求項1〜5のいずれかに記載の筒内直接噴射式火花点火内燃機関の制御装置。   The in-cylinder according to any one of claims 1 to 5, wherein a period before the compression top dead center and a period after the compression top dead center in the fuel injection period of the main injection straddling the compression top dead center are substantially equal. Control device for a direct injection spark ignition internal combustion engine. 上記膨張行程噴射の噴射開始時期が、上記点火時期から50°CA〜100°CA遅れた時期であることを特徴とする請求項5に記載の筒内直接噴射式火花点火内燃機関の制御装置。   6. The control apparatus for a direct injection type spark ignition internal combustion engine according to claim 5, wherein an injection start timing of the expansion stroke injection is a timing delayed by 50 [deg.] CA to 100 [deg.] CA from the ignition timing. 所定の運転状態として、排気ガス温度の昇温が要求されたときに、上記の噴射・点火を実行することを特徴とする請求項1〜7のいずれかに記載の筒内直接噴射式火花点火内燃機関の制御装置。
The in-cylinder direct injection spark ignition according to any one of claims 1 to 7, wherein the injection / ignition is performed when a temperature increase of the exhaust gas is required as a predetermined operation state. Control device for internal combustion engine.
JP2005215208A 2005-07-26 2005-07-26 In-cylinder direct injection spark ignition internal combustion engine controller Expired - Fee Related JP4525509B2 (en)

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