JP4529832B2 - 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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JP4529832B2
JP4529832B2 JP2005215207A JP2005215207A JP4529832B2 JP 4529832 B2 JP4529832 B2 JP 4529832B2 JP 2005215207 A JP2005215207 A JP 2005215207A JP 2005215207 A JP2005215207 A JP 2005215207A JP 4529832 B2 JP4529832 B2 JP 4529832B2
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internal combustion
direct injection
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泰三 堀込
全幸 富田
太朗 酒井
智之 武田
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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、排気系の触媒コンバータの早期昇温(早期活性化)が要求される冷間始動時などにおける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 type spark ignition internal combustion engine that directly injects fuel into a cylinder, and in particular, at a cold start in which early temperature rise (early activation) of an exhaust system catalytic converter is required. It relates to control of injection timing and ignition timing.

特許文献1には、筒内直接噴射式火花点火内燃機関の触媒暖機方法として、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のときに、吸気行程から点火時期にかけての期間内で、部分的な空燃比の濃淡を有する混合気を燃焼室内に形成する後期噴射と、この後期噴射より前に燃料を噴射して、後期噴射の燃料と後期噴射の燃焼とで延焼可能な、理論空燃比よりもリーンな空燃比の混合気を燃焼室内に生成する早期噴射と、の少なくとも2回の分割噴射を行い、かつ点火時期をMBT点より所定量リタードさせるとともに、機関の無負荷領域では点火時期を圧縮上死点よりも前に設定し、無負荷領域を除く低速低負荷領域では点火時期を圧縮上死点以降までリタードさせる技術が記載されている。上記後期噴射は、圧縮行程の中期以降、例えば120°BTDC〜45°BTDCに行われる。
特許第3325230号公報
In Patent Document 1, as a catalyst warm-up method for a direct injection spark ignition internal combustion engine, a period from an intake stroke to an ignition timing when the exhaust gas catalytic converter is in an unwarmed state lower than an activation temperature. In this case, it is possible to spread the fuel by the late injection in which the air-fuel mixture having a partial air-fuel ratio concentration is formed in the combustion chamber, the fuel is injected before this late injection, and the fuel of the late injection and the combustion of the late injection And at least two split injections of early injection for generating an air-fuel mixture leaner than the stoichiometric air-fuel ratio in the combustion chamber, and retarding the ignition timing by a predetermined amount from the MBT point, and no engine load A technique is described in which the ignition timing is set before the compression top dead center in the region, and the ignition timing is retarded until the compression top dead center in the low speed and low load region excluding the no-load region. The latter-stage injection is performed after the middle of the compression stroke, for example, at 120 ° BTDC to 45 ° BTDC.
Japanese Patent No. 3325230

内燃機関の冷機時における触媒の早期活性化および後燃えによるHC低減のためには、点火時期の遅角が有効であり、より大きな効果を得るためには、圧縮上死点以降の点火(ATDC点火)が望ましい。ATDC点火で安定した燃焼を行わせるためには、燃焼期間を短縮する必要があり、そのために、筒内の乱れを強化して、燃焼速度(火炎伝播速度)を上昇させることが必要である。   For early activation of the catalyst when the internal combustion engine is cold and HC reduction due to afterburning, retarding the ignition timing is effective. To obtain a greater effect, ignition after compression top dead center (ATDC) Ignition) is desirable. In order to perform stable combustion by ATDC ignition, it is necessary to shorten the combustion period. For this reason, it is necessary to increase the combustion speed (flame propagation speed) by strengthening the turbulence in the cylinder.

このような乱れの強化のために、筒内に高圧で噴射される燃料噴霧のエネルギにより筒内に乱れを生成することが考えられる。   In order to strengthen such disturbance, it is conceivable that the disturbance is generated in the cylinder by the energy of the fuel spray injected at a high pressure in the cylinder.

しかしながら、特許文献1では、主に、1回目の燃料噴射(早期噴射)を吸気行程中に行い、2回目の燃料噴射(後期噴射)を圧縮行程中の120°BTDC〜45°BTDCに行っている。このように最後の燃料噴射が圧縮上死点よりも前では、その噴霧により筒内に乱れを生成しても、圧縮上死点以降はその乱れが減衰してしまい、ATDC点火での火炎伝播速度上昇には寄与しない。   However, in Patent Document 1, the first fuel injection (early injection) is performed during the intake stroke, and the second fuel injection (late injection) is performed from 120 ° BTDC to 45 ° BTDC during the compression stroke. Yes. As described above, before the last fuel injection is before the compression top dead center, even if the spray generates turbulence in the cylinder, the turbulence is attenuated after the compression top dead center, and the flame propagation in ATDC ignition Does not contribute to speed increase.

例えば、図6は、吸気ポート内に設けたガス流動制御弁(例えばタンブル制御弁)を作動させた場合とこのようなガス流動制御弁を具備しない場合とについて、筒内の乱れの大きさを示したものであるが、ガス流動制御弁を作動させることで吸気行程中に生成した乱れ(符号Aの部分)は、圧縮行程の進行とともに減衰し、圧縮行程後期のタンブル流の崩壊に伴い一時的に乱れが大きくなる(符号Bの部分)ものの、圧縮上死点以降は符号Cで示すように急速に減衰してしまい、その乱れを用いた燃焼改善(火炎伝播向上)はあまり期待できない。燃料噴霧による乱れについても同様であり、圧縮上死点より前の燃料噴射により乱れが生成されたとしても、圧縮上死点以降の点火燃焼には寄与しない。   For example, FIG. 6 shows the magnitude of turbulence in a cylinder when a gas flow control valve (for example, a tumble control valve) provided in an intake port is operated and when such a gas flow control valve is not provided. As shown, the turbulence (part A) generated during the intake stroke by operating the gas flow control valve attenuates with the progress of the compression stroke, and is temporarily accompanied by the collapse of the tumble flow in the latter half of the compression stroke. Although the turbulence increases (the portion indicated by reference symbol B), after the compression top dead center, as shown by the reference symbol C, it rapidly attenuates, and combustion improvement (improving flame propagation) using the turbulence cannot be expected so much. The same applies to turbulence caused by fuel spray, and even if turbulence is generated by fuel injection before compression top dead center, it does not contribute to ignition combustion after compression top dead center.

このため、ATDC点火の方が排温上昇やHC低減に有利であるが、燃焼安定性が成立しないため、特許文献1では、無負荷領域では点火時期を圧縮上死点前(BTDC点火)としている。   Therefore, ATDC ignition is more advantageous for exhaust temperature rise and HC reduction, but combustion stability is not established. Therefore, in Patent Document 1, the ignition timing is set to before compression top dead center (BTDC ignition) in the no-load region. Yes.

本発明は、このような実状を踏まえて、触媒の早期活性化およびHC低減などのためのATDC点火での燃焼安定性を改善することを目的としている。   The present invention aims to improve the combustion stability in ATDC ignition for early activation of the catalyst, reduction of HC, and the like based on such a situation.

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、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に、点火時期を圧縮上死点後に設定するとともに、この点火時期前でかつ圧縮上死点後に燃料を噴射する超リタード燃焼を行うことを特徴としている。なお、NOxを吸着するNOxトラップ触媒においては、硫黄成分(SOx)が触媒に付着することによりNOx吸着性能が低下するので、触媒を強制的に高温化してSOxを放出するSOx放出処理(硫黄被毒解除)を行う必要があるが、このSOx放出処理の際の排気ガス温度の昇温を、上記の超リタード燃焼を利用して行うことも可能である。そして、本発明では、アイドル時の機関回転数を点火時期のフィードバック制御によって目標アイドル回転数に維持するようになっているが、特に、上記の超リタード燃焼でのアイドル運転中に機関回転数が低下したときには該超リタード燃焼を解除するようにしている。 The present invention is provided with a fuel injection valve for injecting fuel directly into the cylinder, the control apparatus for a cylinder direct injection spark ignition internal combustion engine comprising comprises a spark plug, such as during cold catalytic converter if example embodiment the exhaust the Atsushi Nobori if required for the gas temperature, and sets after the compression top dead center of the ignition timing, is characterized by performing the super-retard combustion for injecting fuel after and compression top dead center before the ignition timing. In the NOx trap catalyst that adsorbs NOx, the sulfur component (SOx) adheres to the catalyst, so that the NOx adsorption performance deteriorates. However, it is also possible to raise the temperature of the exhaust gas during the SOx release process using the above-mentioned super retard combustion. In the present invention, the engine speed at idling is maintained at the target idling speed by feedback control of the ignition timing. In particular, the engine speed during the idling operation in the super retard combustion is particularly high. When it decreases, the super retard combustion is canceled.

すなわち、圧縮上死点以降では、吸気行程や圧縮行程で生成された乱れは減衰してしまうが、圧縮上死点以降の膨張行程中になされる燃料噴射によって、筒内の乱れを生成・強化することができ、ATDC点火での火炎伝播が促進される。従って、点火時期を圧縮上死点後とした超リタード燃焼が安定的に成立する。   In other words, after the compression top dead center, the turbulence generated in the intake stroke and the compression stroke is attenuated, but the in-cylinder turbulence is generated and strengthened by the fuel injection performed during the expansion stroke after the compression top dead center. Flame propagation with ATDC ignition is facilitated. Therefore, super retard combustion with the ignition timing after the compression top dead center is established stably.

一方、アイドル状態において、補機負荷(例えば空調装置のコンプレッサ)や自動変速機のレンジ位置の切換などによってアイドル回転数が大きく低下した場合、目標アイドル回転数を維持すべく点火時期フィードバック制御によって点火時期がMBT点に近づくように補正されることになるが、圧縮上死点後に燃料を噴射する超リタード燃焼を継続したまま点火時期をMBT点へ向けて進角補正すると、排気ガス温度が低下し、それに伴って排気中のスモークが増加する。   On the other hand, in the idle state, when the idling engine speed greatly decreases due to an auxiliary load (for example, a compressor of an air conditioner) or a range position change of the automatic transmission, ignition is performed by ignition timing feedback control to maintain the target idling engine speed. The timing will be corrected to approach the MBT point, but if the ignition timing is advanced toward the MBT point while continuing the super retard combustion that injects fuel after the compression top dead center, the exhaust gas temperature decreases. As a result, smoke in the exhaust gas increases.

そこで、本発明では、超リタード燃焼でのアイドル運転中に機関回転数が比較的大きく低下した場合には、超リタード燃焼を解除するようにしている。これにより、スモークの増加が回避される。 Therefore, in the present invention, when the engine speed is relatively lowered during the idling operation in the super retard combustion, the super retard combustion is canceled. This avoids an increase in smoke.

本発明の一つの態様では、実際の機関回転数が所定の下限回転数よりも低下したときに超リタード燃焼を解除する。そして、望ましくは、機関回転数の低下速度が大きいほど上記下限回転数が高く設定される。これにより、急激に機関回転数が低下した場合にも、機関停止に至ることがない。   In one aspect of the present invention, the super retard combustion is released when the actual engine speed falls below a predetermined lower limit speed. Desirably, the lower limit engine speed is set higher as the engine speed decreases. As a result, even when the engine speed rapidly decreases, the engine does not stop.

この発明によれば、点火時期を圧縮上死点後に設定した超リタード燃焼の燃焼安定性を十分に確保することができ、例えば冷間始動の際に、触媒の早期活性化および後燃えによるHC低減を達成することができる。そして、超リタード燃焼でのアイドル運転中に回転数が大きく低下した場合には、超リタード燃焼が解除されるので、点火時期のフィードバック制御によるスモークの増加を回避することができる。 According to the present invention, it is possible to sufficiently ensure the combustion stability of the super retard combustion in which the ignition timing is set after the compression top dead center. For example, at the time of cold start, the catalyst is activated early and the HC due to the afterburning. Reduction can be achieved. Then, when the rotational speed is greatly reduced during the idling operation in the super retard combustion, the super retard combustion is canceled, so that an increase in smoke due to the feedback control of the ignition timing can be avoided.

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1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システム構成を示す構成説明図である。   FIG. 1 is a configuration explanatory view showing a system configuration of a direct injection type spark ignition internal combustion engine to which the present invention is applied.

この内燃機関1のピストン2により形成される燃焼室3には、吸気弁(図示せず)を介して吸気通路4が接続され、かつ排気弁(図示せず)を介して排気通路5が接続されている。上記吸気通路4には、吸入空気量を検出するエアフロメータ6が配設されているとともに、制御信号によりアクチュエータ8を介して開度制御される電子制御スロットル弁7が配設されている。排気通路5には、排気浄化用の触媒コンバータ10が配設されているとともに、その上流側および下流側にそれぞれ空燃比センサ11,12が設けられており、さらに、上流側の空燃比センサ11と並んで、触媒コンバータ10入口側での排気温度を検出する排気温度センサ13が設けられている。   An intake passage 4 is connected to the combustion chamber 3 formed by the piston 2 of the internal combustion engine 1 via an intake valve (not shown), and an exhaust passage 5 is connected via an exhaust valve (not shown). Has been. The intake passage 4 is provided with an air flow meter 6 for detecting the amount of intake air, and an electronically controlled throttle valve 7 whose opening degree is controlled via an actuator 8 by a control signal. The exhaust passage 5 is provided with a catalytic converter 10 for purifying exhaust gas, and air-fuel ratio sensors 11 and 12 are provided on the upstream side and the downstream side, respectively. Further, the upstream air-fuel ratio sensor 11 is provided. Is provided with an exhaust gas temperature sensor 13 for detecting the exhaust gas temperature at the inlet side of the catalytic converter 10.

燃焼室3の中央頂上部には、点火プラグ14が配置されている。また、燃焼室3の吸気通路4側の側部に、該燃焼室3内に燃料を直接噴射する燃料噴射弁15が配置されている。この燃料噴射弁15には、高圧燃料ポンプ16およびプレッシャレギュレータ17によって所定圧力に調圧された燃料が、高圧燃料通路18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、19は、燃圧を検出する燃圧センサ、20は、上記高圧燃料ポンプ16へ燃料を送る低圧燃料ポンプである。   A spark plug 14 is disposed at the central top of the combustion chamber 3. A fuel injection valve 15 that directly injects fuel into the combustion chamber 3 is disposed on the side of the combustion chamber 3 on the intake passage 4 side. The fuel that has been regulated to a predetermined pressure by the high-pressure fuel pump 16 and the pressure regulator 17 is supplied to the fuel injection valve 15 via the high-pressure fuel passage 18. 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. Reference numeral 19 denotes a fuel pressure sensor that detects the fuel pressure, and 20 denotes a low-pressure fuel pump that sends fuel to the high-pressure fuel pump 16.

また内燃機関1には、機関冷却水温を検出する水温センサ21が設けられているとともに、クランク角を検出するクランク角センサ22が設けられている。さらに、運転者による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23が設けられている。   In addition, the internal combustion engine 1 is provided with a water temperature sensor 21 for detecting the engine cooling water temperature and a crank angle sensor 22 for detecting a crank angle. Further, an accelerator opening sensor 23 is provided for detecting the amount of depression of the accelerator pedal by the driver.

上記内燃機関1の燃料噴射量や噴射時期、点火時期、等は、コントロールユニット25によって制御される。このコントロールユニット25には、上述した各種のセンサ類の検出信号が入力されている。コントロールユニット25は、これらの入力信号により検出される機関運転条件に応じて、燃焼方式つまり均質燃焼とするか成層燃焼とするかを決定するとともに、これに合わせて、電子制御スロットル弁7の開度、燃料噴射弁15の燃料噴射時期および燃料噴射量、点火プラグ14の点火時期、等を制御する。なお、暖機完了後においては、低速低負荷側の所定の領域では、通常の成層燃焼運転として、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。燃料噴霧は点火プラグ14近傍に層状に集められ、これにより、空燃比を30〜40程度とした極リーンの成層燃焼が実現される。また、高速高負荷側の所定の領域では、通常の均質燃焼運転として、吸気行程中に燃料噴射が行われ、かつ圧縮上死点前のMBT点近傍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る。この均質燃焼運転としては、運転条件に応じて、空燃比を理論空燃比とした均質ストイキ燃焼と、空燃比を20〜30程度のリーンとした均質リーン燃焼と、がある。   The fuel injection amount, injection timing, ignition timing, etc. of the internal combustion engine 1 are controlled by the control unit 25. The control unit 25 receives detection signals from the various sensors described above. The control unit 25 determines the combustion method, that is, the homogeneous combustion or the stratified combustion, in accordance with the engine operating conditions detected by these input signals, and according to this, the electronic control throttle valve 7 is opened. The fuel injection timing and fuel injection amount of the fuel injection valve 15, the ignition timing of the spark plug 14, and the like are controlled. After the warm-up is completed, in a predetermined region on the low-speed and low-load side, as normal stratified combustion operation, fuel injection is performed at an appropriate time in the compression stroke, and ignition is performed before the compression top dead center. Done. The fuel spray is collected in the vicinity of the spark plug 14, thereby achieving extremely lean stratified combustion with an air-fuel ratio of about 30 to 40. Further, in a predetermined region on the high speed and high load side, as normal homogeneous combustion operation, fuel injection is performed during the intake stroke, and ignition is performed in the vicinity of the MBT point before the compression top dead center. In this case, the fuel becomes a homogeneous mixture in the cylinder. As the homogeneous combustion operation, there are homogeneous stoichiometric combustion in which the air-fuel ratio is the stoichiometric air-fuel ratio and homogeneous lean combustion in which the air-fuel ratio is lean about 20 to 30 depending on the operating conditions.

本発明は、触媒コンバータ10の早期昇温が要求される内燃機関1の冷間始動時において、排気温度を高温とするように、超リタード燃焼を行うものであり、以下、この超リタード燃焼の燃料噴射時期および点火時期を図2に基づいて説明する。   The present invention performs super retard combustion so that the exhaust gas temperature becomes high at the time of cold start of the internal combustion engine 1 where early temperature rise of the catalytic converter 10 is required. The fuel injection timing and ignition timing will be described with reference to FIG.

図2は、超リタード燃焼の3つの実施例を示しており、実施例1では、点火時期を15°〜30°ATDC(例えば20°ATDC)とし、燃料噴射時期(詳しくは燃料噴射開始時期)を、圧縮上死点以降でかつ点火時期前に設定する。なお、このとき、空燃比は、理論空燃比ないしはこれよりも若干リーン(16〜17程度)に設定される。   FIG. 2 shows three examples of super retard combustion. In Example 1, the ignition timing is set to 15 ° to 30 ° ATDC (for example, 20 ° ATDC), and the fuel injection timing (specifically, the fuel injection start timing) is shown. Is set after the compression top dead center and before the ignition timing. At this time, the air-fuel ratio is set to the stoichiometric air-fuel ratio or slightly lean (about 16 to 17).

すなわち、触媒暖機促進ならびにHC低減のためには、点火時期遅角が有効であり、上死点以降の点火(ATDC点火)が望ましいが、ATDC点火で安定した燃焼を行わせるためには、燃焼期間を短縮する必要があり、そのためには、乱れによる火炎伝播を促進しなければならない。前述したように、圧縮上死点以降では、吸気行程や圧縮行程で生成された乱れは減衰してしまうが、本発明では、圧縮上死点以降の膨張行程中になされる高圧の燃料噴射によって、ガス流動が生じ、これにより筒内の乱れを生成・強化することができる。従って、ATDC点火での火炎伝播が促進され、安定した燃焼が可能となる。   That is, in order to promote catalyst warm-up and reduce HC, ignition timing retardation is effective, and ignition after top dead center (ATDC ignition) is desirable, but in order to perform stable combustion with ATDC ignition, It is necessary to shorten the combustion period, and for this purpose, flame propagation due to turbulence must be promoted. As described above, after the compression top dead center, the turbulence generated in the intake stroke and the compression stroke is attenuated, but in the present invention, by the high pressure fuel injection performed during the expansion stroke after the compression top dead center. The gas flow is generated, and thereby the turbulence in the cylinder can be generated and strengthened. Therefore, flame propagation by ATDC ignition is promoted and stable combustion is possible.

図2の実施例2は、燃料噴射を2回に分割した例であり、1回目の燃料噴射を吸気行程中に行い、2回目の燃料噴射を圧縮上死点以降に行う。なお、点火時期および空燃比(2回の噴射を合わせた空燃比)は実施例1と同様である。   The second embodiment in FIG. 2 is an example in which the fuel injection is divided into two, and the first fuel injection is performed during the intake stroke, and the second fuel injection is performed after the compression top dead center. The ignition timing and the air-fuel ratio (the air-fuel ratio obtained by combining the two injections) are the same as those in the first embodiment.

このように、圧縮上死点後の燃料噴射(膨張行程噴射)に先立ち、吸気行程中に燃料噴射(吸気行程噴射)を行うと、吸気行程噴射の燃料噴霧による乱れは圧縮行程後半で減衰してしまい、圧縮上死点後におけるガス流動強化には殆ど影響を与えないが、噴射燃料が燃焼室全体に拡散していて、ATDC点火によるHCの後燃えの促進に寄与するので、HC低減および排温上昇には有効である。   Thus, if fuel injection (intake stroke injection) is performed during the intake stroke prior to fuel injection after compression top dead center (expansion stroke injection), the disturbance due to fuel spray in the intake stroke injection is attenuated in the latter half of the compression stroke. However, since the injected fuel is diffused throughout the combustion chamber and contributes to the promotion of HC afterburning by ATDC ignition, the HC reduction and It is effective for raising the exhaust temperature.

また、図2の実施例3は、燃料噴射を2回に分割し、1回目の燃料噴射を圧縮行程にて行い、2回目の燃料噴射を圧縮上死点以降に行う。このように、圧縮上死点後の燃料噴射(膨張行程噴射)に先立ち、圧縮行程中に燃料噴射(圧縮行程噴射)を行うと、実施例2の吸気行程噴射に比べれば、圧縮行程噴射の方が、その燃料噴霧による乱れの減衰が遅くなるため、この1回目の燃料噴射による乱れが残り、圧縮上死点以降に2回目の燃料噴射を行うことで、1回目の燃料噴射で生成した乱れを助長するように乱れを強化でき、圧縮上死点付近における更なるガス流動強化が図れる。   In the third embodiment of FIG. 2, the fuel injection is divided into two, the first fuel injection is performed in the compression stroke, and the second fuel injection is performed after the compression top dead center. As described above, when the fuel injection (compression stroke injection) is performed during the compression stroke prior to the fuel injection after the compression top dead center (expansion stroke injection), the compression stroke injection is compared with the intake stroke injection of the second embodiment. However, since the disturbance of the turbulence due to the fuel spray is delayed, the turbulence due to the first fuel injection remains, and the second fuel injection is performed after the compression top dead center, which is generated by the first fuel injection. The turbulence can be strengthened to promote the turbulence, and the gas flow can be further strengthened near the compression top dead center.

この実施例3の場合に、1回目の圧縮行程噴射は、圧縮行程前半でもよいが、圧縮行程後半(90°BTDC以降)に設定すると、上死点付近での乱れをより高めることができる。特に、この1回目の圧縮行程噴射を、45°BTDC以降、より望ましくは20°BTDC以降とすると、圧縮上死点以降のガス流動をより強化することができる。   In the case of Example 3, the first compression stroke injection may be in the first half of the compression stroke, but if it is set in the second half of the compression stroke (after 90 ° BTDC), the disturbance near the top dead center can be further increased. In particular, if the first compression stroke injection is 45 ° BTDC or later, more desirably 20 ° BTDC or later, the gas flow after compression top dead center can be further enhanced.

このように、実施例1〜3の超リタード燃焼によれば、点火の直前に燃料噴霧により筒内の乱れを生成・強化することができ、火炎伝播を促進して、安定した燃焼を行わせることができる。特に、点火時期を15°〜30°ATDCまで遅角させることにより、触媒の早期活性化およびHC低減のための十分な後燃え効果を得ることができる。換言すれば、このように点火時期を大きく遅らせても、その直前まで燃料噴射を遅らせて、乱れの生成時期も遅らせることで、火炎伝播向上による燃焼改善を達成できるのである。   As described above, according to the super retarded combustion of the first to third embodiments, the turbulence in the cylinder can be generated and strengthened by the fuel spray immediately before the ignition, and the flame propagation is promoted to perform stable combustion. be able to. In particular, by retarding the ignition timing from 15 ° to 30 ° ATDC, a sufficient afterburning effect for early activation of the catalyst and reduction of HC can be obtained. In other words, even if the ignition timing is greatly delayed in this way, the fuel injection is delayed until just before that, and the generation time of the turbulence is also delayed, so that the combustion improvement by improving the flame propagation can be achieved.

一方、アクセルペダル踏み込み量ないしは電子制御スロットル弁7の開度が0であることを示すアイドルスイッチ信号がONである場合には、通常の均質燃焼運転や成層燃焼運転であるか超リタード燃焼であるかにかかわらず、点火時期のフィードバック制御による公知のアイドル回転数制御が実行される。つまり、目標アイドル回転数と実回転数との回転数偏差に応じてトルクが増加もしくは減少するように点火時期を補正するのであるが、超リタード燃焼の下では、点火時期が圧縮上死点後であるので、回転数の低下に対してはMBT点に近づくように点火時期を進角補正し、逆に回転数の上昇に対しては点火時期を遅角補正することになる。なお、このアイドルスイッチ信号は、必ずしも物理的なスイッチでなくともよく、例えばアクセル開度センサ23の検出信号から生成される。   On the other hand, when the depression amount of the accelerator pedal or the opening amount of the electronically controlled throttle valve 7 is ON, the normal homogeneous combustion operation, the stratified combustion operation or the super retard combustion is performed. Regardless, known idle speed control by feedback control of ignition timing is executed. In other words, the ignition timing is corrected so that the torque increases or decreases according to the rotational speed deviation between the target idle speed and the actual rotational speed, but under super retard combustion, the ignition timing is after the compression top dead center. Therefore, the ignition timing is corrected to advance so as to approach the MBT point when the rotational speed decreases, and conversely, the ignition timing is retarded when the rotational speed increases. The idle switch signal is not necessarily a physical switch, and is generated from a detection signal of the accelerator opening sensor 23, for example.

ここで、上記の超リタード燃焼によるアイドル運転中に、補機負荷(例えば空調装置のコンプレッサ)や自動変速機のレンジ位置の切換(NレンジからDレンジへの切換)などによってアイドル回転数が大きく低下した場合、上記のアイドル回転数制御によって目標アイドル回転数を維持すべく点火時期が進角補正されるが、図3に示すように、点火時期の進角に伴ってトルクは上昇するものの、排気ガス温度が低下し、それに伴って排気中のスモークが増加する。   Here, during the idling operation by the super retard combustion, the idling speed is increased by switching the auxiliary machine load (for example, the compressor of the air conditioner) or the range position of the automatic transmission (switching from the N range to the D range). In the case of a decrease, the ignition timing is advanced to correct the target idle speed by the idle speed control described above, but as shown in FIG. 3, although the torque increases with the advance of the ignition timing, As the exhaust gas temperature decreases, the smoke in the exhaust increases.

そこで、本発明では、超リタード燃焼でのアイドル運転中に機関回転数が所定の下限回転数NLよりも低下した場合には、超リタード燃焼を解除する。特に、この実施例では、上記下限回転数NLは、回転数低下時の回転数低下速度ΔNeに基づいて設定される。すなわち、図4に示すように、応答遅れを考慮して、回転数低下速度ΔNeが大きいほど下限回転数NLが高く設定される。従って、急激な回転数低下であれば、より高い回転数において超リタード燃焼が解除される。   Therefore, in the present invention, when the engine speed falls below the predetermined lower limit speed NL during idling operation with super retard combustion, super retard combustion is canceled. In particular, in this embodiment, the lower limit rotational speed NL is set based on the rotational speed decrease speed ΔNe when the rotational speed is decreased. That is, as shown in FIG. 4, considering the response delay, the lower limit rotational speed NL is set higher as the rotational speed decrease speed ΔNe is larger. Therefore, if the engine speed is rapidly decreased, the super retard combustion is released at a higher engine speed.

図5は、上記の処理の流れをフローチャートとして示したものであり、超リタード燃焼でのアイドル運転中に回転数低下が検出されたら、ステップ1において回転数低下速度ΔNeから下限回転数NLを決定し、ステップ2で、そのときの機関回転数Neを下限回転数NLと比較する。機関回転数Neが下限回転数NL以上であれば、ステップ3へ進んで、超リタード燃焼を継続する。これに対し、下限回転数NLを下回っていれば、ステップ4へ進んで、超リタード燃焼を解除し、通常の燃焼、つまり上述した通常の成層燃焼運転もしくは均質燃焼運転とする。これにより、スモークの増加を伴わずにトルクの上昇が可能となり、機関回転数Neの過度の低下による機関停止が回避される。   FIG. 5 is a flowchart showing the above-described processing flow. When a decrease in the rotation speed is detected during the idling operation in the super retard combustion, the lower limit rotation speed NL is determined from the rotation speed decrease speed ΔNe in step 1. In step 2, the engine speed Ne at that time is compared with the lower limit speed NL. If the engine speed Ne is equal to or higher than the lower limit speed NL, the routine proceeds to step 3 where the super retard combustion is continued. On the other hand, if it is below the lower limit rotational speed NL, the routine proceeds to step 4 where super retard combustion is canceled and normal combustion, that is, normal stratified combustion operation or homogeneous combustion operation described above is performed. Thereby, the torque can be increased without increasing the smoke, and the engine stop due to the excessive decrease in the engine speed Ne is avoided.

なお、本発明の超リタード燃焼は、排気系の触媒コンバータ10としてNOxトラップ触媒を用いた場合の硫黄被毒解除のためにも利用することができる。NOxトラップ触媒は、流入する排気の排気空燃比がリーンであるときにNOxを吸着し、流入する排気の排気空燃比がリッチであると、吸着していたNOxを放出して触媒作用により浄化処理するものであるが、燃料中の硫黄成分(SOx)が触媒に結合するとNOx吸着性能が低下する。そのため、適当な時期に、触媒を強制的に高温化してSOxを放出除去する処理(いわゆる硫黄被毒解除)が必要である。本発明の超リタード燃焼は、非常に高い排気温度を得られるので、このNOxトラップ触媒の硫黄被毒解除処理に適したものとなる。   The super retarded combustion of the present invention can also be used for releasing sulfur poisoning when a NOx trap catalyst is used as the exhaust system catalytic converter 10. The NOx trap catalyst adsorbs NOx when the exhaust air-fuel ratio of the inflowing exhaust gas is lean, and releases the adsorbed NOx when the exhaust air-fuel ratio of the inflowing exhaust gas is rich, and purifies by catalytic action. However, when the sulfur component (SOx) in the fuel is bound to the catalyst, the NOx adsorption performance is lowered. For this reason, it is necessary to perform a process (so-called sulfur poisoning release) for forcibly raising the temperature of the catalyst and releasing SOx at an appropriate time. The super retarded combustion according to the present invention can obtain a very high exhaust temperature, and therefore is suitable for the sulfur poisoning release processing of this NOx trap catalyst.

本発明に係る内燃機関全体のシステム構成を示す構成説明図。BRIEF DESCRIPTION OF THE DRAWINGS The structure explanatory drawing which shows the system structure of the whole internal combustion engine which concerns on this invention. 本発明の超リタード燃焼の燃料噴射時期および点火時期を示す特性図。The characteristic view which shows the fuel injection timing and ignition timing of the super retard combustion of this invention. 点火時期に対する、トルク、排温、スモークの変化を示す特性図。The characteristic view which shows the change of a torque, exhaust temperature, and smoke with respect to ignition timing. 回転数低下速度ΔNeに対する下限回転数NLの特性を示す特性図。The characteristic view which shows the characteristic of the minimum rotation speed NL with respect to rotation speed fall speed (DELTA) Ne. 処理の流れを示すフローチャート。The flowchart which shows the flow of a process. 従来技術における筒内の乱れの変化を示す説明図。Explanatory drawing which shows the change of the disturbance in a cylinder in a prior art.

符号の説明Explanation of symbols

3…燃焼室
10…触媒コンバータ
14…点火プラグ
15…燃料噴射弁
25…コントロールユニット
3 ... Combustion chamber 10 ... Catalytic converter 14 ... Spark plug 15 ... Fuel injection valve 25 ... Control unit

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、かつアイドル時の機関回転数を点火時期のフィードバック制御によって目標アイドル回転数に維持す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、点火時期を圧縮上死点後に設定するとともに、この点火時期前でかつ圧縮上死点後に燃料を噴射する超リタード燃焼を行う一方、この超リタード燃焼でのアイドル運転中に機関回転数が低下したときに該超リタード燃焼を解除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-cylinder direct injection spark-ignition internal combustion engine having a fuel injection valve that directly injects fuel into the cylinder, an ignition plug, and maintaining the engine speed during idling at the target idle speed by feedback control of ignition timing In this control device, when the temperature of the exhaust gas is required to be raised , the ignition timing is set after the compression top dead center, and super retard combustion is performed in which fuel is injected before the ignition timing and after the compression top dead center. On the other hand, a control device for a direct injection spark ignition internal combustion engine, characterized in that the super retard combustion is canceled when the engine speed decreases during idling in the super retard combustion. 所定の下限回転数よりも低下したときに超リタード燃焼を解除す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 spark ignition internal combustion engine according to claim 1, wherein the super retard combustion is canceled when the engine speed falls below a predetermined lower limit rotational speed. 機関回転数の低下速度が大きいほど上記下限回転数が高く設定されることを特徴とする請求項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。   3. The control device for a direct injection type spark ignition internal combustion engine according to claim 2, wherein the lower limit rotational speed is set higher as the decrease speed of the engine rotational speed is larger. 超リタード燃焼における点火時期は、圧縮上死点後15°〜30°CAであることを特徴とする請求項1〜3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 control device for a direct injection spark ignition internal combustion engine according to any one of claims 1 to 3, wherein the ignition timing in the super retard combustion is 15 ° to 30 ° CA after compression top dead center. 超リタード燃焼においては、圧縮上死点後の燃料噴射に先だって、吸気行程中もしくは圧縮行程中に、さらに燃料噴射を行う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 according to any one of claims 1 to 4, wherein in super retard combustion, fuel injection is further performed during an intake stroke or a compression stroke prior to fuel injection after compression top dead center. A control device for an injection spark ignition internal combustion engine. 超リタード燃焼における空燃比は、理論空燃比もしくは若干リーンである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 control device for a direct injection spark ignition internal combustion engine according to any one of claims 1 to 5, wherein the air-fuel ratio in the super retard combustion is a stoichiometric air-fuel ratio or slightly lean. 排気系の触媒コンバータの早期昇温が要求される内燃機関の冷間始動時に、上記の排気ガス温度の昇温が要求されることを特徴とする請求項1〜6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 cylinder according to any one of claims 1 to 6, wherein the temperature of the exhaust gas is required to be raised during a cold start of the internal combustion engine that requires an early temperature increase of the exhaust system catalytic converter. Control device for internal direct injection spark ignition internal combustion engine. 排気系の触媒コンバータのSOx放出処理を行うときに、上記の排気ガス温度の昇温が要求されることを特徴とする請求項1〜6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。 When performing the SOx release process of a catalytic converter in the exhaust system, cylinder direct injection spark ignition internal combustion according to any one of claims 1 to 6, characterized in that heating of the exhaust gas temperature is required Engine control device.
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