JPH0571381A - Fuel supply control device for internal combustion engine - Google Patents

Fuel supply control device for internal combustion engine

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Publication number
JPH0571381A
JPH0571381A JP3233132A JP23313291A JPH0571381A JP H0571381 A JPH0571381 A JP H0571381A JP 3233132 A JP3233132 A JP 3233132A JP 23313291 A JP23313291 A JP 23313291A JP H0571381 A JPH0571381 A JP H0571381A
Authority
JP
Japan
Prior art keywords
fuel ratio
air
fuel
switching
cylinder
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
JP3233132A
Other languages
Japanese (ja)
Other versions
JP2696444B2 (en
Inventor
Naomi Tomizawa
尚己 冨澤
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.)
Hitachi Ltd
Original Assignee
Japan Electronic Control Systems 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 Japan Electronic Control Systems Co Ltd filed Critical Japan Electronic Control Systems Co Ltd
Priority to JP3233132A priority Critical patent/JP2696444B2/en
Publication of JPH0571381A publication Critical patent/JPH0571381A/en
Application granted granted Critical
Publication of JP2696444B2 publication Critical patent/JP2696444B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

(57)【要約】 【目的】燃料制御における設定空燃比の切り換え時にお
けるトルク段差の発生を抑止する。 【構成】運転条件に基づき理論空燃比付近の通常空燃比
と理論空燃比よりも大幅にリーンな空燃比とに切り換え
て燃料噴射量を制御するシステムであって、各気筒毎に
燃料噴射弁を備えたシステムを対象とする。ここで、前
記設定空燃比の切り換え条件が判別されたときに、n回
の噴射で段階的に設定空燃比A/Fが切り換えられるよ
うに、各気筒への噴射毎に、設定空燃比の段差をnで除
算して得られる変化幅ΔA/F(S6)ずつ設定空燃比
を変化させ(S10)、該設定空燃比に基づいて燃料噴射
量Tiを演算させる(S12)。
(57) [Summary] [Purpose] To suppress the occurrence of a torque step when switching the set air-fuel ratio in fuel control. [Configuration] A system for controlling a fuel injection amount by switching between a normal air-fuel ratio near the stoichiometric air-fuel ratio and an air-fuel ratio significantly leaner than the stoichiometric air-fuel ratio based on operating conditions, and controlling a fuel injection valve for each cylinder. Intended for equipped systems. Here, when the set air-fuel ratio switching condition is determined, the set air-fuel ratio step is changed for each injection into each cylinder so that the set air-fuel ratio A / F can be switched stepwise by n injections. Is divided by n to change the set air-fuel ratio by a change width ΔA / F (S6) (S10), and the fuel injection amount Ti is calculated based on the set air-fuel ratio (S12).

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は内燃機関の燃料供給制御
装置に関し、詳しくは、機関吸入混合気の空燃比設定を
切り換えるときの燃料供給制御の改善に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel supply control device for an internal combustion engine, and more particularly to improvement of fuel supply control when switching the air-fuel ratio setting of an engine intake air-fuel mixture.

【0002】[0002]

【従来の技術】近年、燃費の向上を目的として、理論空
燃比(14.7)よりも極めて高い空燃比(例えば20〜25)
で燃焼を行わせるようにしたリーン燃焼機関が提案され
ている。かかるリーン燃焼機関では、例えば低回転・低
負荷時で運転しているときに前記リーン空燃比で燃焼さ
せることで燃費の向上を図り、加速時や高負荷時にはト
ルク性能を重視して理論空燃比よりもややリッチ側の空
燃比として、燃費の向上と出力トルクの確保とを両立さ
せている。
2. Description of the Related Art In recent years, for the purpose of improving fuel efficiency, an air-fuel ratio (for example, 20-25) that is extremely higher than the theoretical air-fuel ratio (14.7).
A lean-burn engine is proposed which is designed to burn at. In such a lean combustion engine, for example, when operating at low rotation speed and low load, fuel efficiency is improved by burning at the lean air-fuel ratio, and torque performance is emphasized during acceleration and high load to give a theoretical air-fuel ratio. As an air-fuel ratio on the slightly rich side, both improved fuel efficiency and secured output torque are achieved.

【0003】[0003]

【発明が解決しようとする課題】ところで、上記のよう
に理論空燃比よりも極めて大きな空燃比(リーン空燃
比)と、理論空燃比よりも小さな空燃比(リッチ空燃
比)とに切り換えられる機関においては、運転条件に基
づき上記空燃比間での切り換え設定を行うときに、図5
に示すように同一運転条件でも設定空燃比が大きく変化
すると発生トルクが大きく異なるから、設定空燃比の切
り換え時に大きなトルク段差が発生し運転性を悪化させ
ることがあった。特に加速途中でリーン空燃比からリッ
チ空燃比に切り換えられると、リーン空燃比燃焼時の運
転感覚から予測される加速性と、リッチ空燃比に切り換
えられた後の加速性とに大きな隔たりがあるために、運
転者に違和感を与えてしまう惧れがあった。
By the way, as described above, in an engine in which the air-fuel ratio (lean air-fuel ratio) extremely larger than the stoichiometric air-fuel ratio and the air-fuel ratio (rich air-fuel ratio) smaller than the stoichiometric air-fuel ratio can be switched. 5 when the switching setting between the air-fuel ratios is performed based on the operating conditions.
Even if the set air-fuel ratio changes significantly even under the same operating conditions, the generated torque greatly differs, so that a large torque step may occur at the time of switching the set air-fuel ratio, which may deteriorate drivability. In particular, if the lean air-fuel ratio is switched to the rich air-fuel ratio during acceleration, there is a large gap between the acceleration that is predicted from the driving sensation during lean air-fuel ratio combustion and the acceleration after switching to the rich air-fuel ratio. In addition, there was a fear that the driver would feel uncomfortable.

【0004】本発明は上記問題点に鑑みなされたもので
あり、設定空燃比の切り換え時におけるトルク段差の発
生を抑止し、設定空燃比の切り換えに伴う運転性の悪化
を防止することを目的とする。
The present invention has been made in view of the above problems, and an object thereof is to suppress the occurrence of a torque step when switching the set air-fuel ratio and prevent the deterioration of drivability associated with the switching of the set air-fuel ratio. To do.

【0005】[0005]

【課題を解決するための手段】そのため本発明にかかる
内燃機関の燃料供給制御装置は、図1に示すように構成
される。図1において、運転条件検出手段は、機関の吸
入空気量に関与するパラメータを少なくとも含む機関運
転条件を検出する。燃料供給量演算手段は、前記検出さ
れた機関運転条件に基づいて機関吸入混合気の空燃比が
所定値となるように燃料供給量を演算する。
Therefore, a fuel supply control device for an internal combustion engine according to the present invention is constructed as shown in FIG. In FIG. 1, the operating condition detecting means detects an engine operating condition including at least a parameter relating to the intake air amount of the engine. The fuel supply amount calculation means calculates the fuel supply amount based on the detected engine operating condition so that the air-fuel ratio of the engine intake air-fuel mixture becomes a predetermined value.

【0006】燃料供給制御手段は、燃料供給量演算手段
で演算された燃料供給量に基づいて各気筒毎に設けられ
た燃料供給手段を個別に制御する。一方、空燃比切り換
え判別手段は、機関吸入混合気の空燃比設定を切り換え
る機関運転条件を判別する。そして、空燃比切り換え制
御手段は、空燃比切り換え設定手段により空燃比設定を
切り換える機関運転条件が判別されたときに、切り換え
前の空燃比から切り換え後の空燃比にまで各気筒の吸気
行程毎に段階的に変化するように前記燃料供給量演算手
段における空燃比の所定値を段階的に変化させる。
The fuel supply control means individually controls the fuel supply means provided for each cylinder based on the fuel supply quantity calculated by the fuel supply quantity calculation means. On the other hand, the air-fuel ratio switching determination means determines the engine operating condition for switching the air-fuel ratio setting of the engine intake air-fuel mixture. Then, the air-fuel ratio switching control means, when the engine operating conditions for switching the air-fuel ratio setting are determined by the air-fuel ratio switching setting means, from the air-fuel ratio before switching to the air-fuel ratio after switching for each intake stroke of each cylinder. The predetermined value of the air-fuel ratio in the fuel supply amount calculation means is changed stepwise so as to change stepwise.

【0007】ここで、前記空燃比切り換え制御手段によ
り空燃比を段階的に変化させる最初の気筒が、前記空燃
比切り換え判別手段による判別毎に異なるように制御す
る切り換え開始気筒制御手段を設けることが好ましい。
Here, there is provided switching start cylinder control means for controlling so that the first cylinder whose air-fuel ratio is changed stepwise by the air-fuel ratio switching control means is different for each judgment by the air-fuel ratio switching judgment means. preferable.

【0008】[0008]

【作用】かかる構成によると、空燃比切り換え判別手段
によって機関吸入混合気の空燃比設定を切り換える機関
運転条件が判別されたときに、空燃比を切り換え前の空
燃比から切り換え後の空燃比へオン・オフ的に変化さ
せ、切り換え判別がなされた時点から全ての気筒の空燃
比を切り換え後の空燃比とするのではなく、切り換え前
の空燃比から切り換え後の空燃比にまで各気筒の吸気行
程毎に段階的に変化させるようにした。
With this configuration, when the air-fuel ratio switching determination means determines the engine operating conditions for switching the air-fuel ratio setting of the engine intake air-fuel mixture, the air-fuel ratio is switched from the air-fuel ratio before switching to the air-fuel ratio after switching. -The intake stroke of each cylinder is changed from the air-fuel ratio before switching to the air-fuel ratio after switching, instead of changing the air-fuel ratio of all cylinders to the air-fuel ratio after switching from the time when switching is changed to OFF. It was changed step by step.

【0009】また、空燃比を各気筒の吸気行程毎に段階
的に変化させるときに、前回の空燃比切り換え時と同じ
気筒から開始されることがないように構成した。
Further, when the air-fuel ratio is changed stepwise for each intake stroke of each cylinder, the cylinder is not started from the same cylinder as when the air-fuel ratio was switched last time.

【0010】[0010]

【実施例】以下に本発明の実施例を説明する。一実施例
を示す図2において、内燃機関1にはエアクリーナ2か
ら吸気ダクト3,スロットル弁4及び吸気マニホールド
5を介して空気が吸入される。吸気マニホールド5の各
ブランチ部には、各気筒別に燃料供給手段としての燃料
噴射弁6が設けられている。この燃料噴射弁6は、ソレ
ノイドに通電されて開弁し、通電停止されて閉弁する電
磁式燃料噴射弁であって、後述するコントロールユニッ
ト12からの駆動パルス信号により個別に通電制御されて
開弁し、図示しない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の圧力に調整された燃料を、
各気筒の吸気行程に合わせて間欠的に噴射供給する。
EXAMPLES Examples of the present invention will be described below. In FIG. 2 showing an embodiment, air is drawn into an internal combustion engine 1 from an air cleaner 2 through an intake duct 3, a throttle valve 4 and an intake manifold 5. At each branch portion of the intake manifold 5, a fuel injection valve 6 as a fuel supply means is provided for each cylinder. The fuel injection valve 6 is an electromagnetic fuel injection valve that is opened by energizing a solenoid and is opened by stopping energization, and is opened by individually controlling energization by a drive pulse signal from a control unit 12 described later. The fuel, which is pumped from a fuel pump (not shown) and adjusted to a predetermined pressure by a pressure regulator,
The injection is intermittently supplied according to the intake stroke of each cylinder.

【0011】機関1の各燃焼室には点火栓7が設けられ
ていて、これにより火花点火して混合気を着火燃焼させ
る。そして、機関1からは、排気マニホールド8,排気
ダクト9,触媒10及びマフラー11を介して排気が排出さ
れる。コントロールユニット12は、CPU,ROM,R
AM,A/D変換器及び入出力インタフェイス等を含ん
で構成されるマイクロコンピュータを備え、各種のセン
サからの入力信号を受け、後述の如く演算処理して、燃
料噴射弁6の作動を制御する。
A spark plug 7 is provided in each combustion chamber of the engine 1 to spark-ignite and ignite and burn the air-fuel mixture. Then, the exhaust gas is discharged from the engine 1 through the exhaust manifold 8, the exhaust duct 9, the catalyst 10 and the muffler 11. The control unit 12 includes a CPU, ROM, R
A microcomputer including an AM, A / D converter, an input / output interface, etc. is provided, input signals from various sensors are received, arithmetic processing is performed as described later, and the operation of the fuel injection valve 6 is controlled. To do.

【0012】前記各種のセンサとしては、吸気ダクト3
中にエアフローメータ13が設けられていて、機関1の吸
入空気流量Qに応じた信号を出力する。また、クランク
角センサ14が設けられていて、燃料噴射制御の基準とな
る例えば4気筒機関で180 °毎(例えばBTDC70°
毎)の基準角度信号REFと、1°又は2°毎の単位角
度信号POSとを出力する。ここで、前記基準角度信号
REFの周期、或いは、所定時間内における前記単位角
度信号POSの発生数を計測することにより、機関回転
速度Neを算出できる。
As the various sensors, the intake duct 3 is used.
An air flow meter 13 is provided therein and outputs a signal according to the intake air flow rate Q of the engine 1. In addition, a crank angle sensor 14 is provided, for example, in a 4-cylinder engine that serves as a reference for fuel injection control, every 180 ° (for example, BTDC 70 °).
For each) and a unit angle signal POS for every 1 ° or 2 °. Here, the engine rotation speed Ne can be calculated by measuring the cycle of the reference angle signal REF or the number of generated unit angle signals POS within a predetermined time.

【0013】また、機関1のウォータジャケットの冷却
水温度Twを検出する水温センサ15が設けられている。
上記のエアフローメータ13及びクランク角センサ14の検
出信号に基づいてシリンダ吸入空気量を検出できるもの
で、本実施例における運転条件検出手段は、前記エアフ
ローメータ13,クランク角センサ14,水温センサ15が相
当する。
A water temperature sensor 15 for detecting the cooling water temperature Tw of the water jacket of the engine 1 is also provided.
The cylinder intake air amount can be detected based on the detection signals of the air flow meter 13 and the crank angle sensor 14, and the operating condition detecting means in the present embodiment includes the air flow meter 13, the crank angle sensor 14, and the water temperature sensor 15. Equivalent to.

【0014】ここにおいて、コントロールユニット12に
内蔵されたマイクロコンピュータのCPUは、図3のフ
ローチャートに示すROM上のプログラムに従って演算
処理を行い、機関吸入混合気の空燃比(A/F)が設定
空燃比に一致するように燃料噴射量Ti(燃料供給量)
を演算し、機関1の各気筒への燃料噴射を個別に制御す
る。
Here, the CPU of the microcomputer incorporated in the control unit 12 performs arithmetic processing in accordance with the program on the ROM shown in the flowchart of FIG. 3, and the air-fuel ratio (A / F) of the engine intake air-fuel mixture is set to the empty value. Fuel injection amount Ti (fuel supply amount) to match the fuel ratio
Is calculated and the fuel injection into each cylinder of the engine 1 is individually controlled.

【0015】尚、本実施例において、燃料供給量演算手
段,燃料供給制御手段,空燃比切り換え判別手段,空燃
比切り換え制御手段,切り換え開始気筒制御手段として
の機能は、前記図3のフローチャートに示すようにコン
トロールユニット12がソフトウェア的に備えている。図
3のフローチャートに示すプログラムは、クランク角セ
ンサ14から燃料噴射制御の基準となる基準角度信号RE
Fが出力される毎に実行されるものであり、このプログ
ラムに従って基準角度信号REF毎に次に吸気行程とな
る気筒に対する燃料噴射が行われるようになっている。
尚、以下の説明において、空燃比のリッチ・リーンは理
論空燃比を基準として表すものとする。
In the present embodiment, the functions of the fuel supply amount calculation means, the fuel supply control means, the air-fuel ratio switching determination means, the air-fuel ratio switching control means, and the switching start cylinder control means are shown in the flow chart of FIG. As described above, the control unit 12 is equipped with software. The program shown in the flow chart of FIG.
It is executed every time F is output, and fuel is injected into the cylinder that will be in the next intake stroke for each reference angle signal REF according to this program.
In the following description, the air-fuel ratio rich / lean is expressed based on the theoretical air-fuel ratio.

【0016】まず、ステップ1(図中ではS1としてあ
る。以下同様)では、理論空燃比よりも大きくリーン化
させた設定空燃比に基づいて燃料供給量Tiを演算させ
るリーン運転条件が成立しているか否かを判別する。本
実施例では、リーン空燃比(空燃比=20〜25)で燃焼さ
せるリーン領域と、理論空燃比(=14.7)又は僅かにリ
ッチな空燃比(例えば13程度)で燃焼させるリッチ領域
との2つ領域に大きく分けられており、例えば機関回転
速度Neと機関負荷を代表する基本燃料噴射量Tpとに
基づいて判別される所定の低負荷・低回転領域をリーン
領域として、かかるリーン領域では理論空燃比よりも大
きくリーン化させた設定空燃比に基づいて燃料噴射量T
iを演算させ、燃費の向上を図るようにしてあり、前記
リーン領域を除く高負荷・高回転領域であるリッチ領域
では、理論空燃比又は僅かにリッチな空燃比で燃焼させ
て、トルク性能を確保できるようにしてある。
First, in step 1 (denoted as S1 in the drawing; the same applies hereinafter), a lean operating condition is established in which the fuel supply amount Ti is calculated based on the set air-fuel ratio which is made leaner than the stoichiometric air-fuel ratio. It is determined whether or not there is. In this embodiment, there are a lean region where combustion is performed at a lean air-fuel ratio (air-fuel ratio = 20 to 25) and a rich region where combustion is performed at a stoichiometric air-fuel ratio (= 14.7) or a slightly rich air-fuel ratio (for example, about 13). Is divided into two regions, and for example, a predetermined low load / low rotation region that is determined based on the engine speed Ne and the basic fuel injection amount Tp representing the engine load is set as the lean region, and in this lean region, the theoretical Based on the set air-fuel ratio that is made leaner than the air-fuel ratio, the fuel injection amount T
i is calculated to improve fuel efficiency. In the rich region, which is a high load / high rotation region excluding the lean region, combustion is performed at a theoretical air-fuel ratio or a slightly rich air-fuel ratio to improve torque performance. I am able to secure it.

【0017】但し、本実施例では、後述するように、リ
ーン領域,リッチ領域内において運転条件によって設定
空燃比を細かく変化させて、運転条件毎に適正空燃比で
燃焼させることができるようにしてある。ステップ1で
リーン運転条件が成立していると判別されたときには、
ステップ2へ進み、予めリーン領域内の設定空燃比を機
関回転速度Neと基本燃料噴射量Tpとに対応させて記
憶させてあるリーン領域マップ(リーンA/Fマップ)
を参照し、現在の運転条件に見合ったリーン空燃比を検
索して求める。
However, in this embodiment, as will be described later, the set air-fuel ratio is finely changed depending on the operating conditions in the lean region and the rich region so that combustion can be performed at an appropriate air-fuel ratio for each operating condition. is there. When it is determined in step 1 that the lean operation condition is satisfied,
Proceeding to step 2, the lean region map (lean A / F map) in which the set air-fuel ratio in the lean region is stored in advance in association with the engine rotation speed Ne and the basic fuel injection amount Tp.
Refer to to find the lean air-fuel ratio that matches the current operating conditions.

【0018】一方、ステップ1でリーン運転条件が成立
していないと判別されたときには、ステップ3へ進み、
予めリッチ領域内の設定空燃比を機関回転速度Neと基
本燃料噴射量Tpとに対応させて記憶させてあるリッチ
領域マップ(通常A/Fマップ)を参照し、現在の運転
条件に見合ったリッチ空燃比を検索して求める。次にス
テップ4では、前記リーン領域マップとリッチ領域マッ
プとの切り換え初回からn回の噴射が行われるまでの間
であるか否か、換言すれば、リッチ空燃比とリーン空燃
比との切り換え初期であるか否かを判別する。
On the other hand, when it is judged in step 1 that the lean operating condition is not satisfied, the routine proceeds to step 3,
By referring to a rich region map (normal A / F map) in which the set air-fuel ratio in the rich region is stored in advance in association with the engine rotation speed Ne and the basic fuel injection amount Tp, the rich air condition corresponding to the current operating condition is referred to. Search for the air-fuel ratio to obtain it. Next, at step 4, it is determined whether or not it is between the first switching of the lean region map and the rich region map until the injection is performed n times, in other words, the initial stage of switching between the rich air-fuel ratio and the lean air-fuel ratio. Or not.

【0019】リッチ・リーンの切り換え初期でない場合
には、ステップ11へ進み、マップから検索して求めた設
定空燃比MA/Fを、燃料噴射量Tiの演算に用いる設
定空燃比A/Fとして設定する。次にステップ12へ進
み、理論空燃比に見合うように演算された基本燃料噴射
量Tp(=Q/Ne×K;Kは定数)に、理論空燃比
(=14.7)と前記設定空燃比A/Fとの比を乗算して、
設定空燃比A/F相当の基本燃料噴射量Tpに補正する
と共に、燃料噴射弁6のバッテリ電圧の変化による有効
噴射時間の変化を補正するための補正分Tsを加算し
て、最終的な燃料噴射量Tiを演算する。
When the rich / lean switching is not the initial stage, the routine proceeds to step 11, where the set air-fuel ratio MA / F obtained by searching from the map is set as the set air-fuel ratio A / F used in the calculation of the fuel injection amount Ti. To do. Next, the routine proceeds to step 12, where the theoretical air-fuel ratio (= 14.7) and the set air-fuel ratio A / are added to the basic fuel injection amount Tp (= Q / Ne × K; K is a constant) calculated to match the theoretical air-fuel ratio. Multiply the ratio with F,
The final fuel is corrected by correcting the basic fuel injection amount Tp corresponding to the set air-fuel ratio A / F and adding a correction amount Ts for correcting the change in the effective injection time due to the change in the battery voltage of the fuel injection valve 6. The injection amount Ti is calculated.

【0020】尚、燃料噴射量Tiの演算においては、こ
の他、水温センサ15で検出される冷却水温度Twに基づ
く補正係数や始動後増量などを加味しても良く、上記の
燃料噴射量Tiの演算は最も簡便な例を示したものであ
る。燃料噴射量Tiが演算されると、次のステップ13で
は、次に吸気行程となる気筒の燃料噴射弁6に対して前
記燃料噴射量Tiに相当するパルス幅の駆動信号を出力
し、前記吸気行程の気筒に対して燃料を噴射供給する。
In addition, in calculating the fuel injection amount Ti, in addition to this, a correction coefficient based on the cooling water temperature Tw detected by the water temperature sensor 15 and an increase after the start may be taken into consideration. The calculation of is the simplest example. When the fuel injection amount Ti is calculated, in the next step 13, a drive signal having a pulse width corresponding to the fuel injection amount Ti is output to the fuel injection valve 6 of the cylinder having the next intake stroke to perform the intake Fuel is injected and supplied to the cylinder in the stroke.

【0021】一方、ステップ4でリッチ・リーン空燃比
の切り換え初期であると判別されたときには、ステップ
5へ進み、切り換え初回であるか否かを判別する。そし
て、リッチ・リーンの切り換え初回であるときには、ス
テップ6へ進み、切り換え前の設定空燃比A/Fから今
回他方のマップから検索して求めた設定空燃比MA/F
を減算して、変化させるべき設定空燃比の段差を求め、
更に、この設定空燃比の段差(A/F−MA/F)を噴
射回数nで除算することにより、噴射回数n回で切り換
え前の空燃比から切り換え後の空燃比にまで変化させる
ために必要な1回噴射当たりの設定空燃比の変化幅ΔA
/Fを求める。
On the other hand, when it is determined in step 4 that the switching of the rich / lean air-fuel ratio is in the initial stage, the process proceeds to step 5 and it is determined whether or not it is the first switching. When it is the rich / lean switching for the first time, the routine proceeds to step 6, where the set air-fuel ratio MA / F obtained by searching from the other map this time from the set air-fuel ratio A / F before switching.
To obtain the step difference of the set air-fuel ratio to be changed,
Further, by dividing the step (A / F-MA / F) of the set air-fuel ratio by the number of injections n, it is necessary to change from the air-fuel ratio before switching to the air-fuel ratio after switching at the number of injections n. Variation of set air-fuel ratio per single injection ΔA
/ F is calculated.

【0022】即ち、本実施例では、設定空燃比がリッチ
・リーン切り換えされるときに、切り換え前の空燃比か
ら切り換え後の空燃比にまで噴射回数n回のうちに段階
的に変化するようにするものである(図4参照)。ステ
ップ6で1回噴射毎に変化させる設定空燃比の幅ΔA/
Fを求めると、次のステップ7では、前回の設定空燃比
切り換え時に変化幅ΔA/Fに基づいて設定空燃比を段
階的に変化させた最初の気筒と、今回の本プログラム実
行によって噴射されようとしている気筒とが同一である
か否かを判別する。
That is, in this embodiment, when the set air-fuel ratio is switched to rich / lean, the air-fuel ratio before switching is changed to the air-fuel ratio after switching stepwise within n injections. This is done (see FIG. 4). The width of the set air-fuel ratio that is changed for each injection in step 6 ΔA /
When F is obtained, in the next step 7, the first cylinder in which the set air-fuel ratio is changed stepwise based on the change width ΔA / F at the time of the previous change of the set air-fuel ratio, and the injection by this program execution will be performed. It is determined whether or not the same cylinder is used.

【0023】そして、前回切り換え時と同じ気筒から変
化幅ΔA/Fに基づく設定空燃比制御が行われようとし
ている場合には、ステップ8へ進み、次回切り換え時の
判別のために、次回の噴射気筒を切り換え制御初回の気
筒として記憶させてから、ステップ12へ進む。従って、
この場合、マップから今回検索して求めた設定空燃比M
A/Fを、燃料噴射量Tiの演算に用いる設定空燃比A
/Fとするステップ11での処理を行わないことになり、
切り換え前の設定空燃比A/Fを継続して用いて燃料噴
射量Tiを演算させる。
Then, when the set air-fuel ratio control based on the change width ΔA / F is about to be performed from the same cylinder as at the time of the previous switching, the routine proceeds to step 8, and the next injection is performed for the determination at the next switching. Switching control is performed after storing the cylinder as the first cylinder. Therefore,
In this case, the set air-fuel ratio M obtained by searching this time from the map
A / F is the set air-fuel ratio A used to calculate the fuel injection amount Ti
/ F will not be processed in step 11,
The fuel injection amount Ti is calculated by continuously using the set air-fuel ratio A / F before switching.

【0024】一方、ステップ7で、前回の切り換え初回
の気筒と今回の噴射気筒とが異なると判別されたときに
は、ステップ9へ進み、今回の噴射気筒を設定空燃比切
り換え初回の気筒として記憶させ、次にステップ10へ進
む。ステップ9からステップ10へ進んだ切り換え初回に
おいては、切り換え前の設定空燃比A/Fに前記ステッ
プ6で演算した変化幅ΔA/Fを加算して設定空燃比を
段階的に変化させる処理を行い、ステップ12へ進む。
On the other hand, if it is determined in step 7 that the cylinder for the first switching last time and the cylinder for the current injection are different, the process proceeds to step 9, where the current injection cylinder is stored as the cylinder for the first time the set air-fuel ratio is switched, Then proceed to step 10. In the first switching that proceeds from step 9 to step 10, a process for changing the set air-fuel ratio stepwise by adding the change width ΔA / F calculated in step 6 to the set air-fuel ratio A / F before switching is performed. , Go to step 12.

【0025】一方、ステップ5で初回でないと判別され
た場合にはステップ10へジャンプして進み、前回の設定
空燃比A/Fに更に変化幅ΔA/Fを加算した結果を新
たに設定空燃比A/Fとする処理を行うので、マップ切
り換えの初回から噴射n回に亘って切り換え前の設定空
燃比A/Fから切り換え後の設定空燃比A/Fに段階的
に近づくことになる(図4参照)。
On the other hand, if it is determined in step 5 that it is not the first time, the routine jumps to step 10 and the result obtained by further adding the change width ΔA / F to the previously set air-fuel ratio A / F is newly set. Since the processing for A / F is performed, the set air-fuel ratio A / F before switching is gradually approached to the set air-fuel ratio A / F after switching from the initial map switching to the injection n times (FIG. 4).

【0026】即ち、ステップ10における設定空燃比A/
Fの段階的な変化は、各気筒への噴射毎に行われること
になり、換言すれば、各気筒の吸気行程毎に設定空燃比
が段階的に切り換えられることになるから、図4に一点
鎖線で示したように設定空燃比をオン・オフ的に急激に
変化させた場合のような大きなトルク段差が発生するこ
とがなく、特に、リーン設定空燃比からリッチ設定空燃
比への切り換え時には、加速性の急激な変化を抑止でき
ることになる。
That is, the set air-fuel ratio A / in step 10
The stepwise change of F is performed for each injection into each cylinder. In other words, the set air-fuel ratio is switched stepwise for each intake stroke of each cylinder. As shown by the chain line, there is no large torque step like when the set air-fuel ratio is rapidly changed on and off, especially when switching from the lean set air-fuel ratio to the rich set air-fuel ratio. This will prevent sudden changes in acceleration.

【0027】また、前回切り換え時の初回気筒と同じ気
筒が噴射気筒であって、ステップ7からステップ8へ進
んだ場合には、図4の設定空燃比の減少変化時に示すよ
うに、噴射1回だけ段階的な設定空燃比A/Fの変化を
遅らせて、異なるの気筒から設定空燃比A/Fの段階的
な変化を開始させるから、設定空燃比を段階的に変化さ
せるときの気筒順が一定してしまうことを回避でき、以
て、特定気筒にのみ設定空燃比変化による大きな負担が
偏って加わってしまうことを回避できる。
Further, if the same cylinder as the first cylinder at the time of the previous switching is the injection cylinder and the process proceeds from step 7 to step 8, once the injection is performed as shown when the set air-fuel ratio decreases in FIG. Since the stepwise change of the set air-fuel ratio A / F is delayed and the stepwise change of the set air-fuel ratio A / F is started from different cylinders, the order of cylinders when the set air-fuel ratio is changed stepwise is It can be avoided that the value becomes constant, and thus a large load due to the change in the set air-fuel ratio can be prevented from being unevenly applied only to the specific cylinder.

【0028】即ち、図4に示す例の場合、リッチ空燃比
からリーン空燃比への段階的な切り換えは4気筒の中の
#1気筒を最初として、吸気行程順に#1→#3→#4
→#2→#1と順番に行われるが、次にリーン空燃比か
らリッチ空燃比への切り換え運転条件が判別されたとき
に同じ#1気筒の噴射タイミングであった場合には、段
階的な設定空燃比の切り換えを1回遅らせて、次の#3
気筒から設定空燃比を段階的に減少させる制御を行わ
せ、同じ#1気筒から設定空燃比の段階的移行が行われ
ないようにする。
That is, in the case of the example shown in FIG. 4, the stepwise switching from the rich air-fuel ratio to the lean air-fuel ratio is performed with the # 1 cylinder out of the four cylinders being the first, and the intake strokes in the order of # 1 → # 3 → # 4.
→ # 2 → # 1 are performed in order, but if the injection timing of the # 1 cylinder is the same when the operating condition for switching from the lean air-fuel ratio to the rich air-fuel ratio is next determined, it is stepwise. After switching the set air-fuel ratio once,
The control for gradually reducing the set air-fuel ratio from the cylinders is performed so that the set air-fuel ratio is not gradually changed from the same # 1 cylinder.

【0029】上記のようにして変化幅ΔA/Fに基づく
設定空燃比A/Fの段階的な変化をn回繰り返して、切
り換え後の設定空燃比にまで変化すると、ステップ4か
らステップ11を介してステップ12へ進み、継続して同じ
マップを参照して設定空燃比A/Fを設定し、かかる設
定空燃比A/Fに基づいて燃料噴射量Tiを演算させ
る。
When the stepwise change of the set air-fuel ratio A / F based on the change width ΔA / F as described above is repeated n times to reach the set air-fuel ratio after the switching, steps 4 to 11 are executed. In step 12, the set air-fuel ratio A / F is continuously set with reference to the same map, and the fuel injection amount Ti is calculated based on the set air-fuel ratio A / F.

【0030】尚、上記噴射回数のnは、設定空燃比の切
り換え速度を決定するパラメータであるから、設定空燃
比のリッチ・リーン変化方向によって異ならせても良い
し、また、機関の加減速度合いなどに基づいて変化させ
るようにしても良い。また、本実施例では、リッチ空燃
比とリーン空燃比との切り換え時に、段階的に設定空燃
比を変化させるよう構成したが、同じリッチ空燃比又は
リーン空燃比であっても大きな段差を有して変化させる
必要がある場合に、本実施例と同様にして段階的に変化
させるよう構成しても良い。
Since the number of injections n is a parameter that determines the switching speed of the set air-fuel ratio, it may be changed depending on the rich / lean change direction of the set air-fuel ratio, or the acceleration / deceleration degree of the engine. It may be changed based on the above. Further, in the present embodiment, when the rich air-fuel ratio and the lean air-fuel ratio are switched, the set air-fuel ratio is changed stepwise, but even if the same rich air-fuel ratio or lean air-fuel ratio, there is a large step. When it is necessary to change it in a stepwise manner, it may be configured to change stepwise as in the present embodiment.

【0031】[0031]

【発明の効果】以上説明したように本発明によると、空
燃比設定を切り換えるときに、各気筒の吸気行程毎に切
り換え前の空燃比から切り換え後の空燃比にまで段階的
に変化するよう構成したので、設定空燃比の急激な変化
によって大きなトルク段差が発生することを抑止でき、
特に、加速途中に設定空燃比が切り換えられる場合の加
速性の急激な変化を回避して運転性を円滑にできるとい
う効果がある。
As described above, according to the present invention, when the air-fuel ratio setting is switched, the air-fuel ratio before switching is gradually changed to the air-fuel ratio after switching for each intake stroke of each cylinder. Therefore, it is possible to prevent a large torque step from occurring due to a sudden change in the set air-fuel ratio,
In particular, there is an effect that the drivability can be smoothed by avoiding a rapid change in the acceleration performance when the set air-fuel ratio is switched during acceleration.

【0032】また、上記のように設定空燃比を各気筒の
吸気行程毎に段階的に変化させるときの最初の気筒が、
設定空燃比の切り換え毎に異なるようにしたので、設定
空燃比の段階的な変化による負担が特定気筒に偏ること
を回避できるという効果がある。
The first cylinder when the set air-fuel ratio is changed stepwise for each intake stroke of each cylinder as described above,
Since the setting is made different every time the set air-fuel ratio is switched, there is an effect that the load due to the stepwise change of the set air-fuel ratio can be prevented from being biased to a specific cylinder.

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

【図1】本発明の構成を示すブロック図。FIG. 1 is a block diagram showing a configuration of the present invention.

【図2】本発明の一実施例を示すシステム概略図。FIG. 2 is a system schematic diagram showing an embodiment of the present invention.

【図3】同上実施例における空燃比制御を示すフローチ
ャート。
FIG. 3 is a flowchart showing air-fuel ratio control in the embodiment.

【図4】同上実施例における設定空燃比の特性を示すタ
イムチャート。
FIG. 4 is a time chart showing the characteristics of the set air-fuel ratio in the above embodiment.

【図5】設定空燃比の切り換えによるトルク段差の発生
を説明するための線図。
FIG. 5 is a diagram for explaining the occurrence of a torque step due to switching of the set air-fuel ratio.

【符号の説明】[Explanation of symbols]

1 機関 6 燃料噴射弁 12 コントロールユニット 13 エアフローメータ 14 クランク角センサ 15 水温センサ 1 Engine 6 Fuel injection valve 12 Control unit 13 Air flow meter 14 Crank angle sensor 15 Water temperature sensor

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】機関の吸入空気量に関与するパラメータを
少なくとも含む機関運転条件を検出する運転条件検出手
段と、 該運転条件検出手段で検出された機関運転条件に基づい
て機関吸入混合気の空燃比が所定値となるように燃料供
給量を演算する燃料供給量演算手段と、 該燃料供給量演算手段で演算された燃料供給量に基づい
て各気筒毎に設けられた燃料供給手段を個別に制御する
燃料供給制御手段と、 機関吸入混合気の空燃比設定を切り換える機関運転条件
を判別する空燃比切り換え判別手段と、 該空燃比切り換え設定手段により空燃比設定を切り換え
る機関運転条件が判別されたときに、各気筒の吸気行程
毎に切り換え前の空燃比から切り換え後の空燃比にまで
段階的に変化するように前記燃料供給量演算手段におけ
る空燃比の所定値を段階的に変化させる空燃比切り換え
制御手段と、 を含んで構成されたことを特徴とする内燃機関の燃料供
給制御装置。
1. An operating condition detecting means for detecting an engine operating condition including at least a parameter relating to an intake air amount of the engine, and an empty engine intake air-fuel mixture based on the engine operating condition detected by the operating condition detecting means. Fuel supply amount calculation means for calculating the fuel supply amount so that the fuel ratio becomes a predetermined value, and fuel supply means provided for each cylinder individually based on the fuel supply amount calculated by the fuel supply amount calculation means The fuel supply control means for controlling, the air-fuel ratio switching determining means for determining the engine operating condition for switching the air-fuel ratio setting of the engine intake air-fuel mixture, and the engine operating condition for switching the air-fuel ratio setting by the air-fuel ratio switching setting means At each time, the predetermined value of the air-fuel ratio in the fuel supply amount calculation means is changed so as to change stepwise from the air-fuel ratio before switching to the air-fuel ratio after switching for each intake stroke of each cylinder. And a fuel supply control device for an internal combustion engine, comprising:
【請求項2】前記空燃比切り換え制御手段により空燃比
を段階的に変化させる最初の気筒が、前記空燃比切り換
え判別手段による判別毎に異なるように制御する切り換
え開始気筒制御手段を設けたことを特徴とする請求項1
記載の内燃機関の燃料供給制御装置。
2. A switching start cylinder control means is provided for controlling so that the first cylinder whose air-fuel ratio is changed stepwise by the air-fuel ratio switching control means is different for each judgment by the air-fuel ratio switching judgment means. Claim 1 characterized by
A fuel supply control device for an internal combustion engine as described above.
JP3233132A 1991-09-12 1991-09-12 Fuel supply control device for internal combustion engine Expired - Fee Related JP2696444B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3233132A JP2696444B2 (en) 1991-09-12 1991-09-12 Fuel supply control device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3233132A JP2696444B2 (en) 1991-09-12 1991-09-12 Fuel supply control device for internal combustion engine

Publications (2)

Publication Number Publication Date
JPH0571381A true JPH0571381A (en) 1993-03-23
JP2696444B2 JP2696444B2 (en) 1998-01-14

Family

ID=16950245

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3233132A Expired - Fee Related JP2696444B2 (en) 1991-09-12 1991-09-12 Fuel supply control device for internal combustion engine

Country Status (1)

Country Link
JP (1) JP2696444B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5640939A (en) * 1994-10-18 1997-06-24 Hitachi, Ltd. Engine control apparatus
EP0882879A3 (en) * 1997-06-03 2000-04-19 Nissan Motor Company, Limited Engine with torque control
US6089206A (en) * 1997-07-08 2000-07-18 Nissan Motor Co., Ltd. Ignition and combustion control in internal combustion engine

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6217340A (en) * 1985-07-15 1987-01-26 Toyota Motor Corp Air fuel ratio controller

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6217340A (en) * 1985-07-15 1987-01-26 Toyota Motor Corp Air fuel ratio controller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5640939A (en) * 1994-10-18 1997-06-24 Hitachi, Ltd. Engine control apparatus
EP0882879A3 (en) * 1997-06-03 2000-04-19 Nissan Motor Company, Limited Engine with torque control
US6089206A (en) * 1997-07-08 2000-07-18 Nissan Motor Co., Ltd. Ignition and combustion control in internal combustion engine

Also Published As

Publication number Publication date
JP2696444B2 (en) 1998-01-14

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