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JP2010203311A - Control device for internal combustion engine - Google Patents

Control device for internal combustion engine Download PDF

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JP2010203311A
JP2010203311A JP2009049061A JP2009049061A JP2010203311A JP 2010203311 A JP2010203311 A JP 2010203311A JP 2009049061 A JP2009049061 A JP 2009049061A JP 2009049061 A JP2009049061 A JP 2009049061A JP 2010203311 A JP2010203311 A JP 2010203311A
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air
fuel ratio
variation
internal combustion
combustion engine
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JP5310102B2 (en
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Kenji Suzuki
健児 鈴木
Hitoshi Ishii
仁 石井
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Nissan Motor Co Ltd
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Abstract

【課題】多気筒内燃機関の各気筒の空燃比を正確に検出できる内燃機関の制御装置を提供する。
【解決手段】排気通路125に空燃比センサ126が設けられた多気筒内燃機関の制御装置において、予め取得された、前記空燃比センサの出力振幅ΔPaekに対する前記各気筒の空燃比ばらつきΔA/Fの関係を示す第1特性式と、各気筒の空燃比ばらつきに対する感度が前記第1特性式より低い第2特性式とを記憶した記憶手段11と、前記空燃比センサの出力から出力振幅を求め、前記第1の空燃比特性式を用いて空燃比ばらつきを求めるばらつき検出手段11を備える。
【選択図】 図1
A control device for an internal combustion engine capable of accurately detecting an air-fuel ratio of each cylinder of a multi-cylinder internal combustion engine.
In a control apparatus for a multi-cylinder internal combustion engine in which an air-fuel ratio sensor 126 is provided in an exhaust passage 125, an air-fuel ratio variation ΔA / F of each cylinder obtained in advance with respect to an output amplitude ΔPaek of the air-fuel ratio sensor is obtained. A storage means 11 storing a first characteristic expression indicating a relationship and a second characteristic expression having a sensitivity to variation in air-fuel ratio of each cylinder lower than that of the first characteristic expression; and determining an output amplitude from the output of the air-fuel ratio sensor; There is provided a variation detecting means 11 for obtaining an air-fuel ratio variation using the first air-fuel ratio characteristic equation.
[Selection] Figure 1

Description

本発明は、内燃機関の制御装置に関するものである。   The present invention relates to a control device for an internal combustion engine.

直噴式多気筒エンジンの各気筒の実空燃比を一つの空燃比センサ(酸素センサを含む)で検出する技術として、各気筒の燃焼間隔と空燃比センサに到達するまでの遅れ時間を考慮し、各気筒のサンプル周期に応じた空燃比センサの出力変化から実空燃比を推定するものが知られている(特許文献1)。 As a technique for detecting the actual air-fuel ratio of each cylinder of a direct injection multi-cylinder engine with one air-fuel ratio sensor (including an oxygen sensor), taking into account the combustion interval of each cylinder and the delay time until it reaches the air-fuel ratio sensor, An apparatus that estimates an actual air-fuel ratio from an output change of an air-fuel ratio sensor corresponding to a sampling period of each cylinder is known (Patent Document 1).

特開2000−220492号公報JP 2000-220492 A

しかしながら、各気筒のサンプル周期に対して空燃比センサの応答速度が不足すると、最もリーンな気筒と最もリッチな気筒との間の気筒の検出値は前後のピーク値の影響により不正確となる。   However, if the response speed of the air-fuel ratio sensor is insufficient with respect to the sampling period of each cylinder, the detected value of the cylinder between the leanest cylinder and the richest cylinder becomes inaccurate due to the influence of the front and rear peak values.

本発明が解決しようとする課題は、多気筒内燃機関の各気筒の空燃比を正確に検出できる内燃機関の制御装置を提供することである。 The problem to be solved by the present invention is to provide a control device for an internal combustion engine that can accurately detect the air-fuel ratio of each cylinder of a multi-cylinder internal combustion engine.

本発明は、空燃比センサの出力振幅に対する各気筒の空燃比ばらつきの関係を示す、互いに感度が異なる少なくとも2つの特性式を予め取得しておき、空燃比ばらつきを検出する場合は感度が高い特性式を用いることによって、上記課題を解決する。 The present invention obtains in advance at least two characteristic formulas having different sensitivities indicating the relationship of the air-fuel ratio variation of each cylinder with respect to the output amplitude of the air-fuel ratio sensor. The above problem is solved by using an equation.

本発明によれば、予め取得した2つの特性式のうち感度が高い特性式を用いて空燃比ばらつきを検出するので、空燃比センサの応答速度に拘らず正確な空燃比を検出することができる。   According to the present invention, since the air-fuel ratio variation is detected using the characteristic equation having high sensitivity of the two characteristic equations acquired in advance, the accurate air-fuel ratio can be detected regardless of the response speed of the air-fuel ratio sensor. .

本発明の一実施の形態を適用した内燃機関の制御装置を示すブロック図である。1 is a block diagram showing a control device for an internal combustion engine to which an embodiment of the present invention is applied. 図1の空燃比センサの出力の一例を示すグラフである。It is a graph which shows an example of the output of the air fuel ratio sensor of FIG. 図1のエンジンコントロールユニットに格納される特性式を示すグラフである。It is a graph which shows the characteristic formula stored in the engine control unit of FIG. 図3の特性式を取得する際に観察された空燃比センサの出力の類型を示すグラフである。It is a graph which shows the type of the output of the air fuel ratio sensor observed when acquiring the characteristic formula of FIG. 図1のエンジンコントローラで実行される空燃比補正の一例を示すグラフである。2 is a graph showing an example of air-fuel ratio correction executed by the engine controller of FIG. 1. 図1のエンジンコントローラで実行される空燃比補正において可変動弁機構による作動角との関係を示すグラフである。2 is a graph showing a relationship with an operating angle by a variable valve mechanism in air-fuel ratio correction executed by the engine controller of FIG. 1. 図1のエンジンコントローラで実行される制御手順を示すフローチャートである。It is a flowchart which shows the control procedure performed with the engine controller of FIG.

以下、本発明の実施形態を図面に基づいて説明する。   Hereinafter, embodiments of the present invention will be described with reference to the drawings.

図1は、本発明の一実施の形態を適用した直噴型多気筒エンジンEGを示すブロック図であり、エンジンEGの吸気通路111には、エアーフィルタ112、吸入空気流量を検出するエアフローメータ113、吸入空気流量を制御するスロットルバルブ114およびコレクタ115が設けられている。   FIG. 1 is a block diagram showing a direct injection multi-cylinder engine EG to which an embodiment of the present invention is applied. An air filter 112 and an air flow meter 113 for detecting an intake air flow rate are provided in an intake passage 111 of the engine EG. A throttle valve 114 and a collector 115 for controlling the intake air flow rate are provided.

スロットルバルブ114には、当該スロットルバルブ114の開度を調整するDCモータ等のアクチュエータ116が設けられている。このスロットルバルブアクチュエータ116は、運転者のアクセルペダル操作量等に基づき演算される要求トルクを達成するように、エンジンコントロールユニット11からの駆動信号に基づき、スロットルバルブ114の開度を電子制御する。また、スロットルバルブ114の開度を検出するスロットルセンサ117が設けられて、その検出信号をエンジンコントロールユニット1へ出力する。なお、スロットルセンサ117はアイドルスイッチとしても機能させることができる。   The throttle valve 114 is provided with an actuator 116 such as a DC motor that adjusts the opening of the throttle valve 114. The throttle valve actuator 116 electronically controls the opening of the throttle valve 114 based on the drive signal from the engine control unit 11 so as to achieve the required torque calculated based on the driver's accelerator pedal operation amount and the like. Further, a throttle sensor 117 for detecting the opening degree of the throttle valve 114 is provided, and the detection signal is output to the engine control unit 1. The throttle sensor 117 can also function as an idle switch.

燃料噴射バルブ118は、燃焼室123に臨ませて設けられている。燃料噴射バルブ118は、エンジンコントロールユニット11において設定される駆動パルス信号によって開弁駆動され、図外の燃料ポンプから圧送されてプレッシャレギュレータにより所定圧力に制御された燃料を筒内に直接噴射する。   The fuel injection valve 118 is provided facing the combustion chamber 123. The fuel injection valve 118 is driven to open by a drive pulse signal set in the engine control unit 11 and directly injects fuel, which is pumped from a fuel pump (not shown) and controlled to a predetermined pressure by a pressure regulator, into the cylinder.

シリンダ119と、当該シリンダ内を往復移動するピストン120の冠面と、吸気バルブ121及び排気バルブ122が設けられたシリンダヘッドとで囲まれる空間が燃焼室123を構成する。点火プラグ124は、各気筒の燃焼室123に臨んで装着され、エンジンコントロールユニット11からの点火信号に基づいて吸入混合気に対して点火を行う。   A space surrounded by the cylinder 119, the crown surface of the piston 120 that reciprocates within the cylinder, and the cylinder head provided with the intake valve 121 and the exhaust valve 122 constitutes a combustion chamber 123. The spark plug 124 is mounted facing the combustion chamber 123 of each cylinder, and ignites the intake air-fuel mixture based on an ignition signal from the engine control unit 11.

一方、排気通路125には、排気中の特定成分、たとえば酸素濃度を検出することにより排気、ひいては吸入混合気の空燃比を検出する空燃比センサ126が設けられ、その検出信号はエンジンコントロールユニット11へ出力される。この空燃比センサ126は、リッチ・リーン出力する酸素センサであっても良いし、空燃比をリニアに広域に亘って検出する広域空燃比センサであってもよい。   On the other hand, the exhaust passage 125 is provided with an air-fuel ratio sensor 126 for detecting an exhaust gas by detecting a specific component in the exhaust gas, for example, oxygen concentration, and thus an air-fuel ratio of the intake air-fuel mixture. Is output. The air-fuel ratio sensor 126 may be an oxygen sensor that performs rich / lean output, or a wide-area air-fuel ratio sensor that linearly detects the air-fuel ratio over a wide area.

また、排気通路125には、排気を浄化するための排気浄化触媒127が設けられている。この排気浄化触媒127としては、ストイキ(理論空燃比,λ=1、空気重量/燃料重量=14.7)近傍において排気中の一酸化炭素COと炭化水素HCを酸化するとともに、窒素酸化物NOxの還元を行って排気を浄化することができる三元触媒、或いは排気中の一酸化炭素COと炭化水素HCの酸化を行う酸化触媒を用いることができる。   The exhaust passage 125 is provided with an exhaust purification catalyst 127 for purifying the exhaust. The exhaust purification catalyst 127 oxidizes carbon monoxide CO and hydrocarbon HC in the exhaust in the vicinity of stoichiometric (theoretical air-fuel ratio, λ = 1, air weight / fuel weight = 14.7), and nitrogen oxide NOx. It is possible to use a three-way catalyst that can purify the exhaust gas by reducing the above, or an oxidation catalyst that oxidizes carbon monoxide CO and hydrocarbon HC in the exhaust gas.

排気通路125の排気浄化触媒127の下流側には、排気中の特定成分、たとえば酸素濃度を検出し、リッチ・リーン出力する酸素センサ128が設けられ、その検出信号はエンジンコントロールユニット11へ出力される。ここでは、酸素センサ128の検出値により、空燃比センサ126の検出値に基づく空燃比フィードバック制御を補正することで、空燃比センサ126の劣化等に伴う制御誤差を抑制する等のために(いわゆるダブル空燃比センサシステム採用のために)、下流側酸素センサ128を設けて構成したが、空燃比センサ126の検出値に基づく空燃比フィードバック制御を行なわせるだけで良い場合には、酸素センサ128を省略することができる。   On the downstream side of the exhaust purification catalyst 127 in the exhaust passage 125, there is provided an oxygen sensor 128 that detects a specific component in the exhaust, for example, oxygen concentration, and outputs a rich / lean output, and the detection signal is output to the engine control unit 11. The Here, by correcting the air-fuel ratio feedback control based on the detection value of the air-fuel ratio sensor 126 based on the detection value of the oxygen sensor 128, so as to suppress a control error associated with the deterioration of the air-fuel ratio sensor 126 (so-called) Although the downstream oxygen sensor 128 is provided (for the adoption of a double air-fuel ratio sensor system), if it is only necessary to perform air-fuel ratio feedback control based on the detection value of the air-fuel ratio sensor 126, the oxygen sensor 128 is Can be omitted.

なお、図1において129はマフラである。   In FIG. 1, reference numeral 129 denotes a muffler.

エンジンEGのクランク軸130にはクランク角センサ131が設けられ、エンジンコントロールユニット11は、クランク角センサ131から機関回転と同期して出力されるクランク単位角信号を一定時間カウントすることで、又は、クランク基準角信号の周期を計測することで、機関回転速度Neを検出することができる。   The crankshaft 130 of the engine EG is provided with a crank angle sensor 131, and the engine control unit 11 counts a crank unit angle signal output from the crank angle sensor 131 in synchronization with the engine rotation for a predetermined time, or By measuring the cycle of the crank reference angle signal, the engine speed Ne can be detected.

エンジンEGの冷却ジャケット132には、水温センサ133が当該冷却ジャケットに臨んで設けられ、冷却ジャケット131内の冷却水温度Twを検出し、これをエンジンコントロールユニット11へ出力する。   The cooling jacket 132 of the engine EG is provided with a water temperature sensor 133 facing the cooling jacket, detects the cooling water temperature Tw in the cooling jacket 131, and outputs this to the engine control unit 11.

図2は排気通路125に設けられた空燃比センサ126の出力の一例を示すグラフであり、V型6気筒エンジンの一方の排気通路に設けられた空燃比センサにより第1気筒(#1)、第3気筒(#3)及び第5気筒(#5)の空燃比(酸素濃度)出力信号を示す。   FIG. 2 is a graph showing an example of the output of the air-fuel ratio sensor 126 provided in the exhaust passage 125. The first cylinder (# 1) is provided by the air-fuel ratio sensor provided in one exhaust passage of the V-type six-cylinder engine. The air-fuel ratio (oxygen concentration) output signals of the third cylinder (# 3) and the fifth cylinder (# 5) are shown.

背景技術の欄で触れたとおり、同図の横軸に示すサンプル周期に対し空燃比センサは少なからず応答速度の遅れなどを含んでいるが、本発明者らが探求したところ以下の事項が判明した。   As mentioned in the Background Art section, the air-fuel ratio sensor has a considerable response speed delay with respect to the sample period shown on the horizontal axis of the figure. did.

図3は、上記V型6気筒エンジンの一方の排気通路125に空燃比センサ126を設け、種々の運転条件を設定することで3つの気筒、すなわち第1気筒(#1)、第3気筒(#3)及び第5気筒(#5)間に故意に空燃比ばらつきを生じさせ、そのときの空燃比センサ126の出力振幅ΔPeak(図2の最大出力と最小出力との長さ)をプロットしたものである。   FIG. 3 shows that an air-fuel ratio sensor 126 is provided in one exhaust passage 125 of the V-type six-cylinder engine and various operating conditions are set, so that three cylinders, that is, a first cylinder (# 1) and a third cylinder ( # 3) and the fifth cylinder (# 5) are intentionally caused to vary the air-fuel ratio, and the output amplitude ΔPeak (the length between the maximum output and the minimum output in FIG. 2) of the air-fuel ratio sensor 126 at that time is plotted. Is.

これによると、図4(A)および(B)に示すように3つの気筒のうち1つの気筒の空燃比が他の2つの気筒の空燃比に比べて異なる類型は、図3に示す第1特性式に従った。これに対し、3つの気筒の空燃比の差が互いに近似して極端に大きくなく、同図(C)に示すように徐々に増加するか、同図(D)に示すように徐々に減少するかといった類型は、図3に示す第2特性式に従った。   According to this, as shown in FIGS. 4A and 4B, the type in which the air-fuel ratio of one of the three cylinders is different from the air-fuel ratio of the other two cylinders is the first type shown in FIG. According to the characteristic formula. On the other hand, the difference between the air-fuel ratios of the three cylinders approximates each other and is not extremely large, and gradually increases as shown in FIG. 10C or gradually decreases as shown in FIG. Such a type follows the second characteristic equation shown in FIG.

すなわち、図4(A)に示すようにリーンな気筒#1とリッチな気筒#5との間の気筒#3や、同図(B)に示すようにリーンな気筒#1とリッチな気筒#3との間の気筒#5の検出値は、前後のピーク値の影響により不正確となりがちであるが、図3の結果から、同図(A)及び(B)に示すような類型であっても空燃比センサ126の出力振幅ΔPeakは空燃比ばらつきΔA/Fに対して感度が高いことが判明した。   That is, the cylinder # 3 between the lean cylinder # 1 and the rich cylinder # 5 as shown in FIG. 4A, or the lean cylinder # 1 and the rich cylinder # as shown in FIG. 4B. The detection value of cylinder # 5 between 3 and 3 tends to be inaccurate due to the influence of the front and rear peak values, but from the results of FIG. 3, the detected values are similar to those shown in FIGS. However, it has been found that the output amplitude ΔPeak of the air-fuel ratio sensor 126 is highly sensitive to the air-fuel ratio variation ΔA / F.

したがって、図3のように予めその内燃機関の各気筒間の空燃比ばらつきΔA/Fに対する空燃比センサ126の出力振幅ΔPeakの関係を実験やシミュレーションにより求め、これを制御マップとして利用すれば、空燃比センサ126の出力振幅ΔPeakから各気筒間の空燃比ばらつきΔA/Fを正確に求めることが可能となる。   Therefore, as shown in FIG. 3, if the relationship of the output amplitude ΔPeak of the air-fuel ratio sensor 126 to the air-fuel ratio variation ΔA / F between the cylinders of the internal combustion engine is obtained in advance by experiments and simulations and used as a control map, It is possible to accurately obtain the air-fuel ratio variation ΔA / F between the cylinders from the output amplitude ΔPeak of the fuel ratio sensor 126.

次に制御手順を説明する。   Next, the control procedure will be described.

図7は本例の制御手順を示すフローチャートであり、吸気バルブ121の作動角を可変とする可変動弁機構を備える内燃機関であるとして説明する。なお、可変動弁機構は作動角、リフト量、位相等を連続的に変更可能な公知の機構を採用することができる。   FIG. 7 is a flowchart showing the control procedure of this example, and will be described as an internal combustion engine provided with a variable valve mechanism that makes the operating angle of the intake valve 121 variable. As the variable valve mechanism, a known mechanism that can continuously change the operating angle, lift amount, phase, and the like can be employed.

ステップS1では、気筒別空燃比の検出を許可するか否かを判定する。許可条件としては、たとえばアイドルスイッチがON(アイドル状態である)または加速状態ではない、エンジン回転数が所定値以下、吸排気弁の作動角が所定範囲内、空燃比のλコントロール実行中、キャニスタからの燃料パージが非作動、および失火判定なし等の条件が全て成立したときに許可を出すことができる。   In step S1, it is determined whether or not the detection of the cylinder-by-cylinder air-fuel ratio is permitted. For example, the idling switch is ON (in an idling state) or is not in an accelerating state, the engine speed is equal to or less than a predetermined value, the intake / exhaust valve operating angle is within a predetermined range, the air-fuel ratio λ control is being executed, the canister Permission can be issued when all of the conditions such as non-operation of fuel purge from No. and no misfire determination are satisfied.

ステップS2では、図6に示すように可変動弁機構を駆動して吸気バルブ121の作動角を初期位置に設定する。この初期位置は作動角が相対的に大きい位置である。   In step S2, as shown in FIG. 6, the variable valve mechanism is driven to set the operating angle of the intake valve 121 to the initial position. This initial position is a position where the operating angle is relatively large.

ステップS3では、空燃比センサ126からの信号を取り込み、図2に示すようにその出力波形から出力振幅ΔPeakを算出する。   In step S3, the signal from the air-fuel ratio sensor 126 is captured, and the output amplitude ΔPeak is calculated from the output waveform as shown in FIG.

ステップS4では、ステップS3で算出された出力振幅ΔPeakを図3の第1特性式に代入することで気筒間の空燃比ばらつきΔA/Fを算出する。   In step S4, the output amplitude ΔPeak calculated in step S3 is substituted into the first characteristic equation of FIG. 3 to calculate the air-fuel ratio variation ΔA / F between the cylinders.

ステップS5では、ステップS4で算出されたΔA/Fが所定閾値αより小さいか否かを判定し、小さい場合はステップS6〜S9の空燃比補正をすることなくステップS10へ進む。   In step S5, it is determined whether or not ΔA / F calculated in step S4 is smaller than a predetermined threshold value α. If smaller, the process proceeds to step S10 without correcting the air-fuel ratio in steps S6 to S9.

ステップS5にてΔA/Fが所定閾値αより大きい場合はステップS6へ進み、ステップS3にて算出した出力振幅ΔPeakを図3に示す第2特性式に代入することで気筒間の空燃比ばらつきΔA/Fを算出する。   If ΔA / F is larger than the predetermined threshold value α in step S5, the process proceeds to step S6, and the output amplitude ΔPeak calculated in step S3 is substituted into the second characteristic equation shown in FIG. / F is calculated.

ステップS7では、点火プラグ124の点火タイミングと空燃比センサ126の出力タイミングとから補正すべき気筒を判定する。   In step S7, the cylinder to be corrected is determined from the ignition timing of the spark plug 124 and the output timing of the air-fuel ratio sensor 126.

ステップS8では、算出されたΔA/Fから補正すべき燃料量に相当するΔパルス幅を気筒ごとに算出し、ステップS9にて各気筒に対しパルス補正を加える。   In step S8, a Δ pulse width corresponding to the fuel amount to be corrected is calculated for each cylinder from the calculated ΔA / F, and pulse correction is applied to each cylinder in step S9.

このとき、図5に示すように、検出された空燃比ばらつきΔA/Fが目標A/Fに対してリーン側である場合は補正量の変化率を大きくして、できる限り短時間で目標A/Fに達するように制御する。これに対し、検出された空燃比ばらつきΔA/Fが目標A/Fに対してリッチ側である場合は補正量の変化率を相対的に小さくしてリーン側へのオーバーシュートを回避することが望ましい。   At this time, as shown in FIG. 5, when the detected air-fuel ratio variation ΔA / F is on the lean side with respect to the target A / F, the change rate of the correction amount is increased, and the target A is shortened as quickly as possible. Control to reach / F. On the other hand, when the detected air-fuel ratio variation ΔA / F is on the rich side with respect to the target A / F, the change rate of the correction amount can be made relatively small to avoid overshooting on the lean side. desirable.

以上により、図6に示す作動角が初期位置における空燃比の補正処理が終了するので、ステップS10にて作動角が目標値に達していなければステップS11へ進み、図6に第2学習で示すように作動角を減少させたのちステップS3へ戻り、以上の処理を繰り返す。   6 completes the air-fuel ratio correction process at the initial position of the operating angle shown in FIG. 6. If the operating angle has not reached the target value in step S10, the process proceeds to step S11, and the second learning is shown in FIG. After reducing the operating angle as described above, the process returns to step S3 and the above processing is repeated.

以上のとおり、本例によれば、既存の空燃比センサ126をそのまま利用して気筒毎の空燃比ばらつきを精度良く検出することができる。その結果、燃焼安定度および触媒転換率を改善することができる。   As described above, according to this example, the existing air-fuel ratio sensor 126 can be used as it is, and the air-fuel ratio variation for each cylinder can be accurately detected. As a result, combustion stability and catalyst conversion rate can be improved.

特に出力振幅ΔPaekに対して各気筒の空燃比ばらつきの感度が高い第1特性式を用いて空燃比ばらつきを検出するので、ばらつきの過小判定を抑制することができる。   In particular, since the variation in the air-fuel ratio is detected using the first characteristic equation in which the sensitivity of the variation in the air-fuel ratio of each cylinder with respect to the output amplitude ΔPaek is detected, it is possible to suppress the determination of the variation being too small.

一方で、出力振幅ΔPaekに対して各気筒の空燃比ばらつきの感度が低い第2特性式を用いて空燃比ばらつきを補正するので、過補正を抑制することができる。   On the other hand, since the air-fuel ratio variation is corrected using the second characteristic equation that is low in sensitivity of the air-fuel ratio variation of each cylinder with respect to the output amplitude ΔPaek, overcorrection can be suppressed.

また、ステップS9にて空燃比を補正する場合には、検出された空燃比ばらつきΔA/Fが補正目標値よりリッチ側である場合は、リーン側である場合に比べ、補正量の変化率を小さく設定する。これにより、空気量が少なく燃焼耐力が弱いリーン側へオーバーシュートさせないので、失火を防止することができる。   Further, when the air-fuel ratio is corrected in step S9, when the detected air-fuel ratio variation ΔA / F is on the rich side from the correction target value, the change rate of the correction amount is set as compared with the case on the lean side. Set smaller. Thereby, since it does not overshoot to the lean side where the amount of air is small and combustion resistance is weak, misfire can be prevented.

また、可変動弁機構を有する場合には、気筒別の空燃比判定を作動角が大きい方から段階的に実施する。これにより、空燃比ばらつきが大きい極小作動角から開始したときの失火を防止することができる。   In addition, when the variable valve mechanism is provided, the air-fuel ratio determination for each cylinder is performed step by step from the larger operating angle. As a result, misfire can be prevented when starting from a minimum operating angle where the variation in air-fuel ratio is large.

なお、本例のエンジンコントロールユニット11が、本発明の記憶手段、ばらつき検出手段、ばらつき補正手段に相当する。   The engine control unit 11 of this example corresponds to a storage unit, a variation detection unit, and a variation correction unit of the present invention.

EG…エンジン(内燃機関)
11…エンジンコントローラ
111…吸気通路
112…エアーフィルタ
113…エアフローメータ
114…スロットルバルブ
115…コレクタ
116…スロットルバルブアクチュエータ
117…スロットルセンサ
118…燃料噴射バルブ
119…シリンダ
120…ピストン
121…吸気バルブ
122…排気バルブ
123…燃焼室
124…点火プラグ
125…排気通路
126…空燃比センサ
127…排気浄化触媒
128…酸素センサ
129…マフラ
130…クランク軸
131…クランク角センサ
132…冷却ジャケット
133…水温センサ
134…温度センサ
EG ... Engine (internal combustion engine)
DESCRIPTION OF SYMBOLS 11 ... Engine controller 111 ... Intake passage 112 ... Air filter 113 ... Air flow meter 114 ... Throttle valve 115 ... Collector 116 ... Throttle valve actuator 117 ... Throttle sensor 118 ... Fuel injection valve 119 ... Cylinder 120 ... Piston 121 ... Intake valve 122 ... Exhaust Valve 123 ... Combustion chamber 124 ... Spark plug 125 ... Exhaust passage 126 ... Air-fuel ratio sensor 127 ... Exhaust purification catalyst 128 ... Oxygen sensor 129 ... Muffler 130 ... Crankshaft 131 ... Crank angle sensor 132 ... Cooling jacket 133 ... Water temperature sensor 134 ... Temperature Sensor

Claims (6)

排気通路に空燃比センサが設けられた多気筒内燃機関の制御装置において、
予め取得された、前記空燃比センサの出力振幅に対する前記各気筒の空燃比ばらつきの関係を示す第1特性式と、各気筒の空燃比ばらつきに対する感度が前記第1特性式より低い第2特性式とを記憶した記憶手段と、
前記空燃比センサの出力から出力振幅を求め、前記第1の空燃比特性式を用いて空燃比ばらつきを求めるばらつき検出手段を備えることを特徴とする内燃機関の制御装置。
In a control device for a multi-cylinder internal combustion engine provided with an air-fuel ratio sensor in an exhaust passage,
A first characteristic equation indicating the relationship of the air-fuel ratio variation of each cylinder with respect to the output amplitude of the air-fuel ratio sensor acquired in advance, and a second characteristic equation in which the sensitivity to the air-fuel ratio variation of each cylinder is lower than the first characteristic equation Storage means for storing
A control apparatus for an internal combustion engine, comprising: variation detection means for obtaining an output amplitude from an output of the air-fuel ratio sensor and obtaining an air-fuel ratio variation using the first air-fuel ratio characteristic equation.
請求項1に記載の内燃機関の制御装置において、
前記ばらつき検出手段による空燃比ばらつきが所定閾値より大きい場合は、前記第2特性式により空燃比ばらつきを求め、当該空燃比ばらつきに応じて空燃比の補正量を求めるばらつき補正手段、をさらに備えることを特徴とする内燃機関の制御装置。
The control apparatus for an internal combustion engine according to claim 1,
When the variation in air-fuel ratio by the variation detection means is larger than a predetermined threshold, the variation correction means further obtains the variation in air-fuel ratio by the second characteristic equation and obtains the correction amount of the air-fuel ratio according to the variation in air-fuel ratio. A control device for an internal combustion engine.
請求項1又は2に記載の内燃機関の制御装置において、
前記第1特性式及び前記第2特性式は、前記各気筒の配置と各空燃比ばらつきの大きさに相関することを特徴とする内燃機関の制御装置。
The control device for an internal combustion engine according to claim 1 or 2,
The control apparatus for an internal combustion engine, wherein the first characteristic equation and the second characteristic equation correlate with the arrangement of the cylinders and the magnitude of variation in the air-fuel ratio.
請求項1〜3のいずれか一項に記載の内燃機関の制御装置において、
前記ばらつき補正手段は、ばらつき検出手段により検出された空燃比ばらつきが補正目標値よりリッチ側である場合は、リーン側である場合に比べ、補正量の変化率を小さく設定することを特徴とする内燃機関の制御装置。
The control apparatus for an internal combustion engine according to any one of claims 1 to 3,
The variation correction unit sets the change rate of the correction amount to be smaller when the air-fuel ratio variation detected by the variation detection unit is richer than the correction target value compared to when the variation is on the lean side. Control device for internal combustion engine.
請求項1〜4のいずれか一項に記載の内燃機関の制御装置において、
前記内燃機関は吸気バルブ及び排気バルブの少なくとも一方の作動角を可変とする可変動弁機構を備え、
前記空燃比ばらつきの検出及び前記空燃比ばらつきの補正を、前記作動角を段階的に変化させながら実行する制御手段を備えることを特徴とする内燃機関の制御装置。
In the control device for an internal combustion engine according to any one of claims 1 to 4,
The internal combustion engine includes a variable valve mechanism that varies an operating angle of at least one of an intake valve and an exhaust valve,
A control device for an internal combustion engine, comprising: control means for executing detection of the air-fuel ratio variation and correction of the air-fuel ratio variation while gradually changing the operating angle.
請求項5に記載の内燃機関の制御装置において、
前記制御手段は、前記作動角を大きい方から小さい方へ段階的に変化させながら実行することを特徴とする内燃機関の制御装置。
The control apparatus for an internal combustion engine according to claim 5,
The control device for an internal combustion engine, wherein the control means is executed while gradually changing the operating angle from a larger one to a smaller one.
JP2009049061A 2009-03-03 2009-03-03 Control device for internal combustion engine Expired - Fee Related JP5310102B2 (en)

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