JP2002327673A - Combustion control device of internal combustion engine - Google Patents

Combustion control device of internal combustion engine

Info

Publication number
JP2002327673A
JP2002327673A JP2001131912A JP2001131912A JP2002327673A JP 2002327673 A JP2002327673 A JP 2002327673A JP 2001131912 A JP2001131912 A JP 2001131912A JP 2001131912 A JP2001131912 A JP 2001131912A JP 2002327673 A JP2002327673 A JP 2002327673A
Authority
JP
Japan
Prior art keywords
cylinder
ignition timing
specific cylinder
stability limit
effective pressure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2001131912A
Other languages
Japanese (ja)
Other versions
JP3882525B2 (en
Inventor
Keiji Okada
圭司 岡田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP2001131912A priority Critical patent/JP3882525B2/en
Publication of JP2002327673A publication Critical patent/JP2002327673A/en
Application granted granted Critical
Publication of JP3882525B2 publication Critical patent/JP3882525B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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

PROBLEM TO BE SOLVED: To minimize the deterioration of operability in finding the stability limit in a structure for correcting the ignition timing in the lag nearly to the stability limit in order to activate a catalyst in an early stage. SOLUTION: When the catalyst is in the inactive state, only the ignition period of a specific cylinder is gradually corrected in the lag. Then, when the difference DLTPI between the average vale PIAVE of the indicated average effective pressure of cylinders other than the specific one and the indicated average effective pressure PIR of the specific cylinder exceeds the threshold DLTPILMT, it is judged that the specific cylinder exceeds the stability limit. When it is judged that the specific cylinder exceeds the stability limit, the ignition timing ADVR of the specific cylinder at the time is corrected in advance only by a specific angle DADV to find the ignition timing ADVi just before the stability limit, which is set as the ignition timing of each cylinder for promoting the activation of the catalyst.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、内燃機関の燃焼制
御装置に関し、詳しくは、点火時期を安定度限界にまで
遅角補正する技術に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustion control apparatus for an internal combustion engine, and more particularly, to a technique for retarding ignition timing to a stability limit.

【0002】[0002]

【従来の技術】従来から、内燃機関の始動直後におい
て、触媒装置を早期に活性化させるべく、点火時期を遅
角補正することで機関の排気温度を上昇させる制御が行
われる場合があった(特開平6−257546号公報参
照)。しかし、点火時期を遅角補正すると燃焼安定度が
悪化するため、排温の上昇効果を最大限に得るには、機
関の燃焼安定度を監視しながら、安定度限界内で点火時
期を最大限に遅角補正することが望まれる。
2. Description of the Related Art Conventionally, immediately after the start of an internal combustion engine, control for raising the exhaust gas temperature of the engine by retarding the ignition timing in order to activate the catalyst device early has been performed in some cases. See JP-A-6-257546). However, if the ignition timing is retarded, the combustion stability deteriorates.Therefore, in order to maximize the effect of increasing the exhaust temperature, the ignition timing must be maximized within the stability limit while monitoring the combustion stability of the engine. It is desired that the angle be corrected for the delay time.

【0003】点火時期を安定度限界内で最大限に遅角補
正する技術としては、従来、特開平9−068080号
公報に開示される方法があった。このものは、各気筒に
筒内圧センサを設けて、気筒毎に筒内圧積分値及び該筒
内圧積分値の変動率を演算し、前記変動率が所定値より
も小さいときに当該気筒の点火時期を遅角補正すること
で、各気筒それぞれが安定度限界内の点火時期で運転さ
れるようにする構成である。
As a technique for maximally retarding the ignition timing within the stability limit, there has been a method disclosed in Japanese Patent Application Laid-Open No. 9-0668080. In this apparatus, an in-cylinder pressure sensor is provided for each cylinder to calculate an in-cylinder pressure integrated value and a variation rate of the in-cylinder pressure integrated value for each cylinder. When the variation rate is smaller than a predetermined value, the ignition timing of the cylinder is determined. Is retarded so that each cylinder is operated at an ignition timing within the stability limit.

【0004】[0004]

【発明が解決しようとする課題】ところで、上記のよう
に、各気筒の点火時期を同時並行で遅角補正して、各気
筒の安定度限界を同時に探る構成の場合、例えば複数気
筒で安定度限界を超える状況となったときに、フィード
バック制御によって点火時期が進角側に戻されて、全気
筒が安定度限界内に復帰するまでの間、安定度限界を超
える点火時期での運転が複数気筒で行われることにな
り、機関の運転性が悪化するという問題があった。
By the way, as described above, in the case where the ignition timing of each cylinder is simultaneously retarded and the ignition timing of each cylinder is corrected simultaneously to find the stability limit of each cylinder, for example, the stability of a plurality of cylinders is determined. When the situation exceeds the limit, the ignition timing is returned to the advanced side by the feedback control, and until the all cylinders return to within the stability limit, multiple operations with the ignition timing exceeding the stability limit are performed. Since the operation is performed in the cylinder, there is a problem that the operability of the engine is deteriorated.

【0005】また、安定度限界への収束性を向上させる
べく、点火時期のフィードバック制御におけるゲインを
大きくすると、オーバーシュートによる運転性の悪化が
大きくなってしまうという問題があった。本発明は上記
問題点に鑑みなされたものであり、安定度限界付近に相
当する点火時期を探るときの運転性の悪化を小さく抑え
ることができる内燃機関の燃焼制御装置を提供すること
を目的とする。
Further, when the gain in the feedback control of the ignition timing is increased to improve the convergence to the stability limit, there is a problem that the operability is greatly deteriorated due to the overshoot. The present invention has been made in view of the above problems, and has as its object to provide a combustion control device for an internal combustion engine that can minimize deterioration in drivability when searching for an ignition timing corresponding to a vicinity of a stability limit. I do.

【0006】[0006]

【課題を解決するための手段】そのため、請求項1記載
の発明は、各気筒の図示平均有効圧をそれぞれ検出する
図示平均有効圧検出手段と、この図示平均有効圧検出手
段に基づき、特定気筒の図示平均有効圧と前記特定気筒
以外の気筒における図示平均有効圧の平均値との偏差を
演算すると共に、前記偏差と閾値とを比較することで前
記特定気筒の安定度限界を判定する安定度限界判定手段
と、この安定度限界判定手段で前記特定気筒が安定度限
界であると判定されるように、前記特定気筒の点火時期
を補正する点火時期補正手段と、安定度限界判定手段で
前記特定気筒が安定度限界であると判定された時点での
前記特定気筒の点火時期に基づいて、前記特定気筒以外
の気筒の点火時期を設定する点火時期設定手段と、を含
んで構成した。
According to the present invention, an indicated mean effective pressure detecting means for detecting the indicated mean effective pressure of each cylinder and a specific cylinder based on the indicated mean effective pressure detecting means are provided. And calculating a deviation between the indicated average effective pressure of the cylinder and the average value of the indicated average effective pressures of the cylinders other than the specific cylinder, and comparing the deviation with a threshold to determine a stability limit of the specific cylinder. Limit determination means, ignition timing correction means for correcting the ignition timing of the specific cylinder, and the stability limit determination means, so that the stability limit determination means determines that the specific cylinder is at the stability limit. Ignition timing setting means for setting the ignition timing of a cylinder other than the specific cylinder based on the ignition timing of the specific cylinder at the time when the specific cylinder is determined to be at the stability limit.

【0007】かかる構成によると、特定気筒の点火時期
のみを補正し、特定気筒の図示平均有効圧と特定気筒以
外の気筒における図示平均有効圧の平均値との偏差を閾
値と比較して、特定気筒の安定度限界が判定されると、
その時点での特定気筒の点火時期に基づいて、他の気筒
における安定度限界相当の点火時期を設定する。請求項
2記載の発明では、前記図示平均有効圧検出手段が、ク
ランク軸の角加速度に基づいて各気筒の図示平均有効圧
を検出する構成とした。
With this configuration, only the ignition timing of the specified cylinder is corrected, and the deviation between the indicated mean effective pressure of the specified cylinder and the mean value of the indicated mean effective pressure of the cylinders other than the specified cylinder is compared with the threshold value to determine the specified value. When the stability limit of the cylinder is determined,
Based on the ignition timing of the specific cylinder at that time, the ignition timing corresponding to the stability limit in other cylinders is set. In the invention according to claim 2, the indicated mean effective pressure detecting means detects the indicated mean effective pressure of each cylinder based on the angular acceleration of the crankshaft.

【0008】かかる構成によると、各気筒の燃焼行程に
おける角加速度が図示平均有効圧に比例することに基づ
き、それぞれの気筒における図示平均有効圧が検出され
る。請求項3記載の発明では、前記安定度限界判定手段
が、前記閾値を、前記特定気筒以外の気筒における図示
平均有効圧の平均値に応じて設定する構成とした。かか
る構成によると、点火時期を補正しない特定気筒以外の
気筒における図示平均有効圧の平均値に基づいて、特定
気筒における点火時期の補正による図示平均有効圧の低
下代を判断する閾値が決定される。
According to this configuration, the indicated average effective pressure in each cylinder is detected based on the fact that the angular acceleration in the combustion stroke of each cylinder is proportional to the indicated average effective pressure. According to a third aspect of the present invention, the stability limit determining means sets the threshold value in accordance with an average value of indicated mean effective pressures in cylinders other than the specific cylinder. According to this configuration, the threshold value for determining the margin of decrease in the indicated average effective pressure due to the correction of the ignition timing in the specific cylinder is determined based on the average value of the indicated average effective pressure in the cylinders other than the specific cylinder whose ignition timing is not corrected. .

【0009】請求項4記載の発明では、前記安定度限界
判定手段が、前記閾値を、通常の点火時期制御状態での
各気筒間における図示平均有効圧のばらつきに応じて設
定する構成とした。かかる構成によると、特定気筒にお
ける点火時期の補正による図示平均有効圧の低下代を判
断する閾値、換言すれば、特定気筒における安定度限界
の判定レベルが、気筒間における点火時期の補正可能範
囲の違いを示す気筒間での図示平均有効圧のばらつきに
応じて設定される。
According to a fourth aspect of the present invention, the stability limit determining means sets the threshold value in accordance with a variation in the indicated mean effective pressure among the cylinders in a normal ignition timing control state. According to this configuration, the threshold value for determining the decrease in the indicated mean effective pressure due to the correction of the ignition timing in the specific cylinder, in other words, the determination level of the stability limit in the specific cylinder is determined by the correction range of the ignition timing between the cylinders. The setting is made in accordance with the variation of the indicated mean effective pressure among the cylinders indicating the difference.

【0010】請求項5記載の発明では、通常の点火時期
制御状態での各気筒の図示平均有効圧に基づいて前記特
定気筒を設定する特定気筒設定手段を設ける構成とし
た。かかる構成によると、通常の点火時期制御状態での
図示平均有効圧が高い気筒ほど、より大きく点火時期を
補正することが可能となるので、この点火時期の補正可
能範囲の大小関係から、実際に点火時期を補正する特定
気筒を決定する。
According to a fifth aspect of the present invention, there is provided a specific cylinder setting means for setting the specific cylinder based on the indicated average effective pressure of each cylinder in a normal ignition timing control state. According to such a configuration, the cylinder having a higher indicated average effective pressure in a normal ignition timing control state can more greatly correct the ignition timing. A specific cylinder for which the ignition timing is to be corrected is determined.

【0011】請求項6記載の発明では、前記特定気筒設
定手段が、通常の点火時期制御状態で図示平均有効圧が
最も低い気筒を前記特定気筒として設定する構成とし
た。かかる構成によると、通常の点火時期制御状態での
図示平均有効圧が最も低く、点火時期の補正できる幅が
最も狭い気筒を特定気筒として設定し、この特定気筒で
安定度限界であると判定されたときの点火時期に基づい
て、他気筒の安定度限界に相当する点火時期を決定す
る。
According to a sixth aspect of the present invention, the specific cylinder setting means sets the cylinder having the lowest indicated average effective pressure in the normal ignition timing control state as the specific cylinder. According to this configuration, the indicated average effective pressure in the normal ignition timing control state is the lowest, and the cylinder in which the ignition timing can be corrected is set as the specific cylinder as the specific cylinder, and it is determined that the stability limit is reached in this specific cylinder. The ignition timing corresponding to the stability limit of the other cylinder is determined based on the ignition timing at the time of the ignition.

【0012】請求項7記載の発明では、前記特定気筒設
定手段が、所定の運転条件毎に前記特定気筒を学習する
構成とした。かかる構成によると、通常の点火時期制御
状態での各気筒における図示平均有効圧の大小関係が機
関毎に異なり、また、経時的に変化するのに対応して、
特定気筒が所定の運転条件毎に更新学習される。
In the invention described in claim 7, the specific cylinder setting means learns the specific cylinder for each predetermined operating condition. According to such a configuration, the magnitude relationship of the indicated average effective pressure in each cylinder in the normal ignition timing control state differs from engine to engine, and in response to the temporal change,
The specific cylinder is updated and learned for each predetermined operating condition.

【0013】[0013]

【発明の効果】請求項1記載の発明によると、特定気筒
が安定度限界であると判定された時点での特定気筒の点
火時期に基づいて、特定気筒以外の気筒の点火時期を設
定するので、安定度限界に達したときの運転性の悪化を
小さく抑えることができるという効果がある。
According to the first aspect of the present invention, the ignition timing of the cylinders other than the specific cylinder is set based on the ignition timing of the specific cylinder at the time when it is determined that the specific cylinder is at the stability limit. In addition, there is an effect that deterioration in drivability when the stability limit is reached can be suppressed.

【0014】請求項2記載の発明によると、各気筒それ
ぞれに筒内圧センサなどの燃焼センサを設けることな
く、各気筒の図示平均有効圧をそれぞれ検出することが
できるという効果がある。請求項3記載の発明による
と、点火時期が遅角補正されない特定気筒以外の図示平
均有効圧を基準に、安定度限界に相当する図示平均有効
圧の低下代を的確に設定でき、安定度限界を精度良く判
定できるという効果がある。
According to the second aspect of the invention, the indicated average effective pressure of each cylinder can be detected without providing a combustion sensor such as an in-cylinder pressure sensor for each cylinder. According to the third aspect of the present invention, the amount of decrease in the indicated mean effective pressure corresponding to the stability limit can be accurately set based on the indicated mean effective pressure other than the specific cylinder whose ignition timing is not retarded, and the stability limit Can be determined with high accuracy.

【0015】請求項4記載の発明によると、各気筒間に
おける図示平均有効圧のばらつきから、特定気筒におけ
る安定度限界判定の余裕代を設定した上で、特定気筒の
安定度限界に相当する点火時期を他気筒に適用すること
により、他気筒で安定度限界を超えることを回避するこ
とが可能となる。請求項5記載の発明によると、図示平
均有効圧の低下代に基づき安定度限界を判定する構成に
おいて、たとえ安定度限界判定の余裕代が小さくても、
他気筒で安定度限界を超えることを回避できる特定気筒
を選定することが可能になるという効果がある。
According to the present invention, the margin corresponding to the stability limit of the specific cylinder is set based on the variation of the indicated mean effective pressure among the cylinders, and then the margin corresponding to the stability limit of the specific cylinder is set. By applying the timing to the other cylinders, it is possible to avoid exceeding the stability limit in the other cylinders. According to the fifth aspect of the present invention, in the configuration in which the stability limit is determined based on the reduction allowance of the indicated mean effective pressure, even if the margin of the stability limit determination is small,
There is an effect that it is possible to select a specific cylinder that can avoid exceeding the stability limit in another cylinder.

【0016】請求項6記載の発明によると、図示平均有
効圧の最も低い気筒を特定気筒とするので、たとえ安定
度限界判定の余裕代が小さくても、他気筒における余裕
代を確保でき、他気筒で安定度限界を超えることを回避
できるという効果がある。請求項7記載の発明による
と、機関毎のばらつきや経時変化による図示平均有効圧
のばらつきの違いに対応して、常に最適な特定気筒を選
定できるという効果がある。
According to the sixth aspect of the present invention, the cylinder having the lowest indicated average effective pressure is set as the specific cylinder. Therefore, even if the margin for determining the stability limit is small, the margin for other cylinders can be secured. There is an effect that it is possible to avoid exceeding the stability limit in the cylinder. According to the seventh aspect of the present invention, there is an effect that an optimum specific cylinder can always be selected in response to a difference in the indicated mean effective pressure due to a difference between engines or a change with time.

【0017】[0017]

【発明の実施の形態】以下に本発明の実施の形態を図に
基づいて説明する。図1は実施形態における車両用の内
燃機関を示す。図1に示す内燃機関1において、吸気管
2に燃料噴射弁3が介装され、前記燃料噴射弁3から噴
射される燃料とスロットルバルブ4を介して吸引される
空気とによって混合気が形成される。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 shows an internal combustion engine for a vehicle according to the embodiment. In the internal combustion engine 1 shown in FIG. 1, a fuel injection valve 3 is interposed in an intake pipe 2, and a fuel-air mixture is formed by fuel injected from the fuel injection valve 3 and air sucked through a throttle valve 4. You.

【0018】機関1の燃焼室5内の混合気は、点火プラ
グ6による火花点火によって着火燃焼する。燃焼排気
は、途中に触媒装置7が介装される排気管8を介して大
気中に排出される。前記燃料噴射弁3及び点火プラグ6
は、マイクロコンピュータを内蔵するコントロールユニ
ット10によって制御される。
The air-fuel mixture in the combustion chamber 5 of the engine 1 is ignited and burned by spark ignition by a spark plug 6. The combustion exhaust is discharged into the atmosphere via an exhaust pipe 8 on which a catalyst device 7 is interposed. The fuel injection valve 3 and the spark plug 6
Is controlled by a control unit 10 incorporating a microcomputer.

【0019】前記コントロールユニット10には、クラ
ンク角を検出するクランク角センサ11,冷却水温度を
検出する水温センサ12,スロットルバルブ4上流側の
吸気管2に設けられ機関1の吸入空気流量を検出するエ
アフローメータ13、スロットルバルブ4の開度を検出
するスロットルセンサ14、触媒装置7上流側の排気管
8に設けられ排気中の酸素濃度を検出する酸素センサ1
5などからの検出信号が入力される。
The control unit 10 includes a crank angle sensor 11 for detecting a crank angle, a water temperature sensor 12 for detecting a coolant temperature, and a suction air flow rate of the engine 1 which is provided in the intake pipe 2 upstream of the throttle valve 4. Air flow meter 13, a throttle sensor 14 for detecting the opening of the throttle valve 4, and an oxygen sensor 1 provided in the exhaust pipe 8 on the upstream side of the catalyst device 7 for detecting the oxygen concentration in the exhaust gas
5 and the like.

【0020】前記クランク角センサ11は、図2に示す
ように、各気筒の爆発間隔(本実施形態の4気筒機関で
は180°CA)毎に、各気筒の圧縮上死点(TDC)
前の所定角度位置(例えば110°BTDC)でハイレ
ベルのパルスとなる基準信号REFを出力すると共に、
単位クランク角(例えば1°CA)毎にハイレベルとな
る単位信号POSを出力する。
As shown in FIG. 2, the crank angle sensor 11 detects the compression top dead center (TDC) of each cylinder every explosion interval of each cylinder (180 ° CA in the four-cylinder engine of this embodiment).
Outputs a reference signal REF that becomes a high-level pulse at a previous predetermined angular position (for example, 110 ° BTDC),
It outputs a unit signal POS which becomes a high level every unit crank angle (for example, 1 ° CA).

【0021】前記コントロールユニット10は、前記点
火プラグ6による点火時期を、機関負荷・機関回転速度
などに基づいて通常に制御すると共に、機関1の始動直
後で触媒装置7が非活性状態であるときには、排気温度
を積極的に上昇させて触媒装置7を早期に活性化すべ
く、前記通常の点火時期を補正する機能を有している。
以下では、上記触媒活性のための点火時期制御の詳細
を、図3のフローチャートに従って説明する。
The control unit 10 controls the ignition timing of the ignition plug 6 normally based on the engine load and the engine speed, and when the catalyst device 7 is inactive immediately after the start of the engine 1. In order to activate the catalytic converter 7 early by positively increasing the exhaust gas temperature, the normal ignition timing is corrected.
Hereinafter, details of the ignition timing control for the catalyst activity will be described with reference to the flowchart of FIG.

【0022】図3のフローチャートにおいて、ステップ
S1では、前記触媒装置7が活性化しているか否か(活
性温度に達しているか否か)を判別する。前記触媒装置
7の活性・非活性判断は、水温センサ12で検出される
冷却水温度が閾値以上であるか否かに基づいて行わせ
る。但し、活性・非活性の判断方法を上記のものに限定
するものではなく、公知の活性判断方法のいずれを用い
ても良い。
In the flowchart of FIG. 3, in step S1, it is determined whether or not the catalyst device 7 has been activated (whether or not the activation temperature has been reached). The determination as to whether the catalyst device 7 is active or inactive is made based on whether the coolant temperature detected by the coolant temperature sensor 12 is equal to or higher than a threshold value. However, the method of determining the activation / inactivation is not limited to the above, and any of the known activity determination methods may be used.

【0023】例えば、精度良く活性・非活性を判断させ
る場合には、触媒装置7の温度を検出する触媒温度セン
サを設け、該触媒温度センサで検出される触媒温度が活
性温度以上であるか否かを判断させるようにすれば良
い。ステップS1で触媒装置7が活性状態であると判別
されると、ステップS2へ進んで、通常の点火時期制御
を行わせると共に、ステップS10へ進んで、フラグF
LGRTDに0をセットする。
For example, in order to accurately determine whether the catalyst is active or inactive, a catalyst temperature sensor for detecting the temperature of the catalyst device 7 is provided, and whether the catalyst temperature detected by the catalyst temperature sensor is equal to or higher than the activation temperature is determined. What is necessary is just to make it judge. If it is determined in step S1 that the catalyst device 7 is in the active state, the routine proceeds to step S2, where normal ignition timing control is performed, and the routine proceeds to step S10, where the flag F
Set LGRTD to 0.

【0024】前記フラグFLGRTDは、イグニッショ
ンスイッチのON時に0にリセットされると共に、後述
するように、全気筒が安定度限界直前での点火時期制御
状態になったときに、1がセットされるようになってい
る。一方、ステップS1で、触媒装置7が非活性状態で
あると判別されると、ステップS3へ進む。
The flag FLGRTD is reset to 0 when the ignition switch is turned on, and is set to 1 when all cylinders are in the ignition timing control state immediately before the stability limit, as described later. It has become. On the other hand, if it is determined in step S1 that the catalyst device 7 is in the inactive state, the process proceeds to step S3.

【0025】ステップS3では、前記フラグFLGRT
Dに1がセットされているか否かを判別する。前記フラ
グFLGRTD=1であれば、既に安定度限界直前の点
火時期が設定され、この点火時期に基づいて各気筒の点
火プラグ6が制御されている状態であると判断し、その
まま本ルーチンを終了させる。
In step S3, the flag FLGRT
It is determined whether 1 is set in D. If the flag FLGRTD = 1, the ignition timing immediately before the stability limit has already been set, and it is determined that the ignition plug 6 of each cylinder is being controlled based on this ignition timing, and this routine is terminated as it is. Let it.

【0026】前記フラグFLGRTD=0であるときに
は、安定度限界の見極めが完了していない状態であると
判断し、ステップS4へ進む。ステップS4では、特定
の1気筒の点火時期ADVR(点火進角値)のみを、所
定角度DADVだけ遅角補正する(点火時期補正手
段)。 ADVR←ADVR−DADV ステップS5では、点火時期が補正される前記特定気
筒、及び、その他の気筒の図示平均有効圧をそれぞれに
算出する(図示平均有効圧検出手段)。
When the flag FLGRTD = 0, it is determined that the determination of the stability limit has not been completed, and the process proceeds to step S4. In step S4, only the ignition timing ADVR (ignition advance value) of a specific one cylinder is retarded by a predetermined angle DADV (ignition timing correction means). ADVR ← ADVR−DADV In step S5, the indicated average effective pressures of the specific cylinder and the other cylinders whose ignition timings are to be corrected are calculated (illustrated average effective pressure detection means).

【0027】前記ステップS5は、特開平9−3032
43号公報に開示されるように、クランク軸の角加速度
に基づいて図示平均有効圧Piを算出する構成であり、
その概略を以下に説明する。各気筒気筒の図示平均有効
圧Piは、下式に示すように、クランク軸の角加速度Δ
ωに比例する。
The step S5 is described in Japanese Patent Application Laid-Open No. 9-3032.
As disclosed in Japanese Patent Publication No. 43-43, a configuration for calculating an indicated average effective pressure Pi based on an angular acceleration of a crankshaft,
The outline will be described below. The indicated mean effective pressure Pi of each cylinder is represented by an angular acceleration Δ
It is proportional to ω.

【0028】[0028]

【数1】 Pi:図示平均有効圧 dω:角速度差 dt:微小時間 ここで、図2に示すように、同一燃焼行程内において予
め決められた2箇所の角度位置(基準信号REFからθ
1及びθ2の位置)毎に、それぞれ所定の角度幅K1,
K2での経過時間t1,t2を測定し、この経過時間t
1,t2及び角度幅K1,K2から、前記2箇所におけ
る角速度ω1,ω2をそれぞれ算出し、これらの偏差と
して前記角速度差dωが求められる。
(Equation 1) Pi: indicated mean effective pressure dω: angular velocity difference dt: minute time Here, as shown in FIG. 2, two predetermined angular positions within the same combustion stroke (from the reference signal REF to θ
1 and θ2), a predetermined angular width K1,
The elapsed times t1 and t2 at K2 are measured, and the elapsed time t
1, t2 and the angular widths K1, K2, the angular velocities ω1, ω2 at the two locations are calculated, respectively, and the angular velocity difference dω is obtained as a deviation between them.

【0029】また、前記微小時間dtは、前記2箇所の
角度位置間の時間間隔である。図4のフローチャート
は、上記ステップS5における処理内容を詳細に示すも
のであり、前記基準信号REFの発生毎に実行される。
ステップS101では、角速度を求める2個所の角度位
置における所定角度幅K1,K2の経過時間t1i,t
2i(iは気筒番号を示す)を読み込む。
The minute time dt is a time interval between the two angular positions. The flowchart of FIG. 4 shows the details of the processing in step S5, and is executed every time the reference signal REF is generated.
In step S101, the elapsed times t1i and t of the predetermined angular widths K1 and K2 at the two angular positions for obtaining the angular velocities.
2i (i indicates a cylinder number) is read.

【0030】ステップS102では、2個所の角度位置
における角速度ω1i,ω2i(iは気筒番号を示す)
を算出する。 ω1i=K1/t1i ω2i=K2/t2i ステップS103では、角加速度DOMGi(iは気筒
番号を示す)を算出する。
In step S102, angular velocities ω1i and ω2i at two angular positions (i indicates a cylinder number).
Is calculated. ω1i = K1 / t1i ω2i = K2 / t2i In step S103, an angular acceleration DOMGi (i indicates a cylinder number) is calculated.

【0031】DOMGi=(ω2i−ω1i)/dt ステップS104では、図5に示す関係に基づいて、前
記角加速度DOMGiを図示平均有効圧Piに変換す
る。ステップS5で、上記のようにして各気筒の図示平
均有効圧Piを算出すると、ステップS6へ進む。
DOMGi = (ω2i−ω1i) / dt In step S104, the angular acceleration DOMGi is converted into the indicated mean effective pressure Pi based on the relationship shown in FIG. After calculating the indicated mean effective pressure Pi of each cylinder as described above in step S5, the process proceeds to step S6.

【0032】ステップS6では、点火時期が遅角補正さ
れる特定の1気筒以外の気筒における図示平均有効圧の
平均値PIAVEと、前記特定の1気筒の図示平均有効
圧PIRとの差DLTPIを算出する。 DLTPI←PIAVE−PIR ステップS7では、前記DLTPI、即ち、点火時期の
遅角補正による図示平均有効圧の低下代が、閾値DLT
PILMTよりも大きいか否かを判別する(安定度限界
判定手段)。
In step S6, the difference DLTPI between the average value PIAVE of the indicated average effective pressure in cylinders other than the specific one cylinder whose ignition timing is to be retarded and the indicated average effective pressure PIR of the specific cylinder is calculated. I do. DLTPI ← PIAVE-PIR In step S7, the DLTPI, that is, the decrease in the indicated average effective pressure due to the ignition timing retard correction is determined by the threshold value DLT.
It is determined whether it is larger than PILMT (stability limit determining means).

【0033】点火時期を遅角補正すると図示平均有効圧
PIRが低下し、点火時期が補正されない気筒における
図示平均有効圧に対する特定気筒の図示平均有効圧の低
下代DLTPIは、特定気筒における遅角補正量が大き
くなるに従って増大する。そこで、前記低下代DLTP
Iが閾値DLTPILMTよりも大きくなったときに、
特定気筒における点火時期が、安定度限界を超えて遅角
されたものと判断する(図6参照)。
When the ignition timing is retarded, the indicated mean effective pressure PIR decreases, and the decrease DLTPI of the indicated mean effective pressure of the specific cylinder with respect to the indicated mean effective pressure of the cylinder for which the ignition timing is not corrected is determined by the delay correction in the particular cylinder. It increases as the amount increases. Therefore, the lowering allowance DLTP
When I becomes larger than the threshold DLTPILMT,
It is determined that the ignition timing in the specific cylinder has been retarded beyond the stability limit (see FIG. 6).

【0034】尚、点火時期を遅角補正しない状態での図
示平均有効圧が高いときほど、安定度を維持できる図示
平均有効圧の低下代が大きくなるので、前記閾値DLT
PILMTは、図7に示すように、特定気筒以外の気筒
における図示平均有効圧の平均値PIAVEが大きいと
きほど大きな値に設定される。前記低下代DLTPIが
閾値DLTPILMT以下であるときには、特定気筒の
点火時期が安定度限界にまで遅角されていないと判断さ
れるので、ステップS10へ進んで、前記フラグFLG
RTDに0をセットしてから本ルーチンを終了させ、本
ルーチンの次回実行時に更に点火時期が遅角補正される
ようにする。
It should be noted that the higher the indicated mean effective pressure in the state where the ignition timing is not retarded, the greater the decrease in the indicated mean effective pressure that can maintain the stability, so the threshold value DLT
As shown in FIG. 7, PILMT is set to a larger value as the average value PIAVE of the indicated mean effective pressures in the cylinders other than the specific cylinder increases. When the decrease allowance DLTPI is equal to or less than the threshold value DLTPILMT, it is determined that the ignition timing of the specific cylinder has not been retarded to the stability limit, and the routine proceeds to step S10, where the flag FLG is set.
After the RTD is set to 0, the present routine is terminated, and the ignition timing is further retarded at the next execution of the present routine.

【0035】一方、特定気筒の点火時期を徐々に遅角補
正した結果、ステップS7で、前記低下代DLTPIが
閾値DLTPILMTを超えていると判断されるように
なると、特定気筒において安定度限界を超えて点火時期
が遅角補正されたものと判断し、ステップS8へ進む。
ステップS8では、前記低下代DLTPIが閾値DLT
PILMTを超えたと判断されたときの特定気筒の点火
時期ADVRに、所定角度DADVを加算して進角補正
することで、低下代DLTPIが閾値DLTPILMT
を超える直前、即ち、特定気筒が安定度限界を超える直
前の点火時期ADViを求め、この点火時期ADViを
全気筒の点火時期として設定する(点火時期設定手
段)。
On the other hand, as a result of the ignition timing of the specific cylinder being gradually retarded, if it is determined in step S7 that the decrease allowance DLTPI exceeds the threshold DLTPILMT, the stability limit in the specific cylinder is exceeded. It is determined that the ignition timing has been retarded, and the process proceeds to step S8.
In step S8, the decrease DLTPI is equal to the threshold value DLT.
By adding a predetermined angle DADV to the ignition timing ADVR of the specific cylinder when it is determined that the value exceeds PILMT and performing advance correction, the decrease DLTPI becomes equal to the threshold value DLTPILMT.
, Ie, immediately before the specific cylinder exceeds the stability limit, the ignition timing ADVi is determined, and this ignition timing ADVi is set as the ignition timing of all cylinders (ignition timing setting means).

【0036】即ち、特定の1気筒の点火時期のみを徐々
に遅角補正していって、特定気筒において安定度限界直
前の点火時期を求め、これを他の気筒にも適用させて、
全気筒で安定度限界直前にまで遅角された点火時期で点
火を行わせるものである。このステップS8における処
理により、各気筒が安定度限界直前にまで遅角された点
火時期で燃焼されるので、排気温度が上昇し、触媒装置
7の早期活性化が図られる。
That is, only the ignition timing of one specific cylinder is gradually retarded, and the ignition timing immediately before the stability limit is obtained in the specific cylinder, and the ignition timing is applied to other cylinders.
The ignition is performed in all cylinders at the ignition timing delayed until just before the stability limit. By the processing in step S8, each cylinder is burned at the ignition timing delayed to just before the stability limit, so that the exhaust gas temperature rises and the catalyst device 7 is activated early.

【0037】ここで、安定度限界の点火時期を探るとき
に、特定の1気筒の点火時期のみを徐々に遅角補正する
から、安定度限界を超えて燃焼安定性が悪化しても、安
定度限界を超えるのが特定の1気筒に限られるため、運
転性の悪化を小さく抑えることができる。ところで、前
記特定の1気筒は予め固定された気筒としても良いが、
気筒間の図示平均有効圧のばらつきによって、特定気筒
以外の気筒に、図示平均有効圧が特定気筒よりも低く、
遅角補正量の許容代が特定気筒よりも小さい気筒が存在
すると、特定気筒で求められた安定度限界直前の点火時
期を適用したときに、安定度限界を超えてしまう可能性
がある。
Here, when searching for the ignition timing of the stability limit, only the ignition timing of a specific one cylinder is gradually retarded, so that even if the combustion stability exceeds the stability limit and the combustion stability deteriorates, the stable Since the degree exceeding the degree limit is limited to a specific one cylinder, deterioration in drivability can be suppressed to a small extent. By the way, the specific one cylinder may be a fixed cylinder in advance,
Due to the variation of the indicated average effective pressure between the cylinders, the indicated average effective pressure is lower than the specific cylinder in the cylinders other than the specific cylinder,
If there is a cylinder in which the allowable amount of the delay correction amount is smaller than the specific cylinder, there is a possibility that the stability limit will be exceeded when the ignition timing immediately before the stability limit obtained for the specific cylinder is applied.

【0038】そこで、通常の点火時期の制御状態で予め
図示平均有効圧の最も低い気筒を検出し、この気筒を、
点火時期の遅角補正を行わせる特定の1気筒として設定
する(特定気筒設定手段)。図示平均有効圧の最も低い
気筒を特定気筒とすれば、他の気筒は、より図示平均有
効圧が高く、特定気筒以上に遅角させることが可能であ
るから、特定気筒で安定度限界直前であると判断された
点火時期を適用したときに、安定度限界を超えることが
ない。
Therefore, the cylinder having the lowest indicated average effective pressure is detected in advance under the normal ignition timing control state, and this cylinder is determined as follows.
It is set as a specific one cylinder for which the ignition timing is to be retarded (specific cylinder setting means). If the cylinder having the lowest indicated average effective pressure is a specific cylinder, the other cylinders have a higher indicated average effective pressure and can be retarded more than the specific cylinder. When the ignition timing determined to be present is applied, the stability limit is not exceeded.

【0039】また、図示平均有効圧の最も低い気筒は、
個々の機関毎に異なり、また、経時的にも変化すること
がある。そこで、所定の運転条件(冷却水温度が所定
値、かつ、機関負荷・機関回転速度が所定値)であると
きに、各気筒の図示平均有効圧を算出して、その中で最
小の図示平均有効圧を示す気筒を検出し、これを次回始
動時における特定気筒として学習する。
The cylinder having the lowest indicated average effective pressure is
It varies from one institution to another and may change over time. Therefore, under predetermined operating conditions (the cooling water temperature is a predetermined value and the engine load / engine speed is a predetermined value), the indicated mean effective pressure of each cylinder is calculated, and the smallest indicated mean effective pressure is calculated. The cylinder indicating the effective pressure is detected and learned as the specific cylinder at the next start.

【0040】尚、上記では、特定気筒の選択によって他
の気筒で安定度限界を超えることがないようにしたが、
特定気筒を固定し、前記閾値DLTPILMTの設定に
よって、特定気筒以外で安定度限界を超えることを回避
することが可能である。即ち、予め気筒間の図示平均有
効圧のばらつきを想定し、最も図示平均有効圧の高い気
筒が特定気筒として選択され、最も図示平均有効圧の低
い気筒に前記特定気筒での安定度限界の判定結果を適用
しても、安定度限界を超える燃焼性の悪化が発生するこ
とがないように、前記閾値DLTPILMTを、予め大
きな余裕代を見込んで設定する構成とすれば良い。
In the above description, the stability limit is not exceeded in other cylinders by selecting a specific cylinder.
By fixing the specific cylinder and setting the threshold value DLTPILMT, it is possible to avoid exceeding the stability limit other than the specific cylinder. That is, the cylinder having the highest indicated average effective pressure is selected as the specific cylinder, assuming the variation of the indicated average effective pressure among the cylinders in advance, and the determination of the stability limit in the specific cylinder is performed for the cylinder having the lowest indicated average effective pressure. Even if the result is applied, the threshold DLTPILMT may be set in advance in consideration of a large margin so that the deterioration of the flammability exceeding the stability limit does not occur.

【0041】但し、上記構成では、点火時期の遅角補正
量が大きく制限される場合が生じるので、気筒間の図示
平均有効圧のばらつきに応じて前記閾値DLTPILM
Tを学習設定させることがより好ましい。具体的には、
点火時期を遅角補正しない通常の点火時期制御状態で、
かつ、所定の運転条件になったときに、各気筒の図示平
均有効圧のばらつき、即ち、特定気筒として予め設定さ
れた気筒の図示平均有効圧と、他の気筒の中で最も低い
図示平均有効圧との差を検出し、特定気筒の図示平均有
効圧が他の気筒よりも大きいときほど、前記閾値DLT
PILMTをより小さく補正するようにすれば良い。
However, in the above configuration, since the amount of retard correction of the ignition timing may be greatly limited, the threshold value DLTPILM may be changed according to the variation of the indicated mean effective pressure between the cylinders.
More preferably, T is set by learning. In particular,
In the normal ignition timing control state where the ignition timing is not retarded,
Further, when a predetermined operating condition is reached, the variation of the indicated average effective pressure of each cylinder, that is, the indicated average effective pressure of a cylinder set in advance as a specific cylinder and the lowest indicated average effective pressure of the other cylinders And when the indicated average effective pressure of the specific cylinder is higher than the other cylinders, the threshold value DLT
What is necessary is just to correct PILMT smaller.

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

【図1】内燃機関のシステム構成図。FIG. 1 is a system configuration diagram of an internal combustion engine.

【図2】クランク角センサの出力信号の特性及び図示平
均有効圧の算出処理を示すタイムチャート。
FIG. 2 is a time chart showing a characteristic of an output signal of a crank angle sensor and a process of calculating an indicated mean effective pressure.

【図3】触媒活性のための点火時期の遅角補正制御を示
すフローチャート。
FIG. 3 is a flow chart showing ignition timing retard correction control for catalyst activation.

【図4】各気筒の図示平均有効圧の算出処理を示すフロ
ーチャート。
FIG. 4 is a flowchart showing a process for calculating an indicated average effective pressure of each cylinder.

【図5】角加速度DOMGと図示平均有効圧Piとの相
関を示すグラフ。
FIG. 5 is a graph showing a correlation between the angular acceleration DOMG and the indicated mean effective pressure Pi.

【図6】図示平均有効圧の偏差DLTPIと安定度との
相関を示すグラフ。
FIG. 6 is a graph showing a correlation between a deviation DLTPI of an indicated mean effective pressure and stability.

【図7】遅角補正気筒以外の気筒における図示平均有効
圧の平均値PIAVEと閾値DLTPILMTとの相関
を示すグラフ。
FIG. 7 is a graph showing a correlation between an average value PIAVE of indicated mean effective pressure and a threshold value DLTPILMT in a cylinder other than the retard correction cylinder.

【符号の説明】[Explanation of symbols]

1…内燃機関 2…吸気管 3…燃料噴射弁 4…スロットルバルブ 5…燃焼室 6…点火プラグ 7…触媒装置 8…排気管 10…コントロールユニット 11…クランク角センサ 12…水温センサ 13…エアフローメータ 14…スロットルセンサ 15…酸素センサ DESCRIPTION OF SYMBOLS 1 ... Internal combustion engine 2 ... Intake pipe 3 ... Fuel injection valve 4 ... Throttle valve 5 ... Combustion chamber 6 ... Spark plug 7 ... Catalyst device 8 ... Exhaust pipe 10 ... Control unit 11 ... Crank angle sensor 12 ... Water temperature sensor 13 ... Air flow meter 14 ... Throttle sensor 15 ... Oxygen sensor

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】各気筒の図示平均有効圧をそれぞれ検出す
る図示平均有効圧検出手段と、 特定気筒の図示平均有効圧と前記特定気筒以外の気筒に
おける図示平均有効圧の平均値との偏差を演算し、該偏
差と閾値とを比較して、前記特定気筒の安定度限界を判
定する安定度限界判定手段と、 該安定度限界判定手段で前記特定気筒が安定度限界であ
ると判定されるように、前記特定気筒の点火時期を補正
する点火時期補正手段と、 前記安定度限界判定手段で前記特定気筒が安定度限界で
あると判定された時点での前記特定気筒の点火時期に基
づいて、前記特定気筒以外の気筒の点火時期を設定する
点火時期設定手段と、 を含んで構成されたことを特徴とする内燃機関の燃焼制
御装置。
An indicated average effective pressure detecting means for detecting an indicated average effective pressure of each cylinder, and a deviation between an indicated average effective pressure of a specific cylinder and an average value of indicated average effective pressures of cylinders other than the specific cylinder. Calculating and comparing the deviation with a threshold to determine a stability limit of the specific cylinder, and a stability limit determining means for determining the stability limit of the specific cylinder; and determining that the specific cylinder is at the stability limit by the stability limit determining means. As described above, ignition timing correction means for correcting the ignition timing of the specific cylinder, based on the ignition timing of the specific cylinder at the time when the specific cylinder is determined to be the stability limit by the stability limit determining means And an ignition timing setting means for setting an ignition timing of a cylinder other than the specific cylinder.
【請求項2】前記図示平均有効圧検出手段が、クランク
軸の角加速度に基づいて各気筒の図示平均有効圧を検出
することを特徴とする請求項1記載の内燃機関の燃焼制
御装置。
2. The combustion control apparatus for an internal combustion engine according to claim 1, wherein said indicated mean effective pressure detecting means detects the indicated mean effective pressure of each cylinder based on an angular acceleration of a crankshaft.
【請求項3】前記安定度限界判定手段が、前記閾値を、
前記特定気筒以外の気筒における図示平均有効圧の平均
値に応じて設定することを特徴とする請求項1又は2記
載の内燃機関の燃焼制御装置。
3. The stability limit determining means sets the threshold value as
3. The combustion control device for an internal combustion engine according to claim 1, wherein the setting is performed in accordance with an average value of the indicated average effective pressures in cylinders other than the specific cylinder.
【請求項4】前記安定度限界判定手段が、前記閾値を、
通常の点火時期制御状態での各気筒間における図示平均
有効圧のばらつきに応じて設定することを特徴とする請
求項1又は2記載の内燃機関の燃焼制御装置。
4. The stability limit judging means sets the threshold as:
3. The combustion control device for an internal combustion engine according to claim 1, wherein the setting is made in accordance with a variation in the indicated mean effective pressure among the cylinders in a normal ignition timing control state.
【請求項5】通常の点火時期制御状態での各気筒の図示
平均有効圧に基づいて前記特定気筒を設定する特定気筒
設定手段を設けたことを特徴とする請求項1〜4のいず
れか1つに記載の内燃機関の燃焼制御装置。
5. A specific cylinder setting means for setting the specific cylinder based on the indicated average effective pressure of each cylinder in a normal ignition timing control state. A combustion control device for an internal combustion engine according to any one of the first to third aspects.
【請求項6】前記特定気筒設定手段が、通常の点火時期
制御状態で図示平均有効圧が最も低い気筒を前記特定気
筒として設定することを特徴とする請求項5記載の内燃
機関の燃焼制御装置。
6. A combustion control apparatus for an internal combustion engine according to claim 5, wherein said specific cylinder setting means sets a cylinder having the lowest indicated average effective pressure in said normal ignition timing control state as said specific cylinder. .
【請求項7】前記特定気筒設定手段が、所定の運転条件
毎に前記特定気筒を学習することを特徴とする請求項5
又は6記載の内燃機関の燃焼制御装置。
7. The specific cylinder setting means learns the specific cylinder for each predetermined operating condition.
Or a combustion control apparatus for an internal combustion engine according to 6.
JP2001131912A 2001-04-27 2001-04-27 Combustion control device for internal combustion engine Expired - Fee Related JP3882525B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2001131912A JP3882525B2 (en) 2001-04-27 2001-04-27 Combustion control device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2001131912A JP3882525B2 (en) 2001-04-27 2001-04-27 Combustion control device for internal combustion engine

Publications (2)

Publication Number Publication Date
JP2002327673A true JP2002327673A (en) 2002-11-15
JP3882525B2 JP3882525B2 (en) 2007-02-21

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Link
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Publication number Publication date
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