JPH01123141A - Air-fuel-ratio control apparatus for internal combustion engine - Google Patents

Air-fuel-ratio control apparatus for internal combustion engine

Info

Publication number
JPH01123141A
JPH01123141A JP62281731A JP28173187A JPH01123141A JP H01123141 A JPH01123141 A JP H01123141A JP 62281731 A JP62281731 A JP 62281731A JP 28173187 A JP28173187 A JP 28173187A JP H01123141 A JPH01123141 A JP H01123141A
Authority
JP
Japan
Prior art keywords
fuel ratio
oxygen
battery cell
air
output
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.)
Pending
Application number
JP62281731A
Other languages
Japanese (ja)
Inventor
Ryoji Nishiyama
亮治 西山
Hitoshi Inoue
仁志 井上
Masanobu Uchinami
打浪 正信
Masaya Kominami
小南 正哉
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP62281731A priority Critical patent/JPH01123141A/en
Publication of JPH01123141A publication Critical patent/JPH01123141A/en
Pending legal-status Critical Current

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  • Measuring Oxygen Concentration In Cells (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

PURPOSE:To make it possible to perform accurate control, by detecting the output voltage of the oxygen battery cell of a broad range air fuel ratio sensor with a detecting circuit of the electromotive force of the oxygen battery, judging the active state of the broad range air fuel ratio sensor based on the output signal from the detecting circuit, and controlling the current for an oxygen pump. CONSTITUTION:A detecting circuit 82a for the electromotive force of an oxygen battery cell, which detects the output voltage of the oxygen battery cell 82, is added to the constitution of a conventional broad range air fuel ratio sensor 8. The output signal Vs is inputted into a control device 9. The current for an oxygen pump is controlled with a pump-current driving output circuit 97 by using a microprocessor 93. When the output voltage Vs of the cell 82 is less than a specified value not only when an engine is started but also when the engine is operating, it is judged that the sensor 8 is abnormal. The current for the oxygen pump is stopped. This state is maintained until the specified value is exceeded. Therefore, the measuring accuracy of the air fuel ratio with the sensor 8 is improved, and stable feedback fuel control based on the air fuel ratio can be performed.

Description

【発明の詳細な説明】 〔産業上の利用分舒〕 この発明は、リーンからリッチまで空燃比検出可能な広
域空燃比センサを用いて内燃機関の空燃比フィードバッ
ク制御を行う場合に、特に機関始動時、急加減速時と低
温時における空燃比センサ検出精度を向上させ、機関の
空燃比制御性能の向上を図った内燃機関の空燃比制御装
置に関するものである。
Detailed Description of the Invention [Industrial Applications] This invention is particularly useful when performing air-fuel ratio feedback control of an internal combustion engine using a wide-range air-fuel ratio sensor capable of detecting air-fuel ratios from lean to rich. The present invention relates to an air-fuel ratio control device for an internal combustion engine, which improves the detection accuracy of an air-fuel ratio sensor during sudden acceleration and deceleration, and at low temperatures, and improves the air-fuel ratio control performance of the engine.

〔従来の技術〕[Conventional technology]

第7図は例えば特開昭J31−204559号公報に示
された従来の内燃機関の空燃比制御装置の構成図であり
、図において、1は内燃機関、2はこの内燃機関1に接
続された吸気管、3はこの吸気v2内に設けられた絞り
弁である。
FIG. 7 is a configuration diagram of a conventional air-fuel ratio control device for an internal combustion engine disclosed in, for example, Japanese Unexamined Patent Publication No. Sho J31-204559. Intake pipe 3 is a throttle valve provided in this intake v2.

この吸気管2内の圧力は圧力センサ4で検出し、その検
出出力はADコンバータ91に送出するようになってい
る。
The pressure within this intake pipe 2 is detected by a pressure sensor 4, and its detection output is sent to an AD converter 91.

また、内燃機関1の回転をパルスとして回転センサ5で
検出するようにしており、この回転センサ5の出力は入
出力回路92に送出するようになっている。
Further, the rotation of the internal combustion engine 1 is detected as a pulse by the rotation sensor 5, and the output of the rotation sensor 5 is sent to the input/output circuit 92.

さらに、1fifi管2ヘインジ工クタ6により燃料を
噴射するようになっており、このインジェクタ6は出力
回路96の出力で駆動されるようになっている。
Further, fuel is injected by a 1fifi pipe 2 hinge injector 6, and this injector 6 is driven by the output of an output circuit 96.

また、内燃機関1に排気管7が接続されてお9、この排
気II!!ニア内の排気ガス成分がら空燃比に対応した
出力が広域空燃比センサ8からADコンバータ91に送
出するようにしている。
Further, an exhaust pipe 7 is connected to the internal combustion engine 1, and this exhaust pipe II! ! An output corresponding to the air-fuel ratio of the exhaust gas components in the near area is sent from the wide-range air-fuel ratio sensor 8 to the AD converter 91.

一方、9は圧力センサ4と回転センサ5と広域空燃比セ
ンサ8と冷却水温センサ1oなどの情報から所要燃料量
を演算し、インジェクタ6の駆動パルス幅を発生する制
御装置である。
On the other hand, 9 is a control device that calculates the required amount of fuel from information such as the pressure sensor 4, rotation sensor 5, wide range air-fuel ratio sensor 8, and cooling water temperature sensor 1o, and generates a drive pulse width for the injector 6.

この制御装置9におけるADコンバータ91は広域空燃
比センサ8および圧力センサ4などのアナログ信号をデ
ジタル値に変換してマイクロプロセッサ93に送出する
ようになっている。
The AD converter 91 in the control device 9 converts analog signals from the wide range air-fuel ratio sensor 8, pressure sensor 4, etc. into digital values and sends them to the microprocessor 93.

また、入力回路92は回転センサ5のパルス入力信号を
レベル変換するための入力回路で、その出力もマイクロ
プロセッサ93に送出するようになっている。
Further, the input circuit 92 is an input circuit for converting the level of the pulse input signal of the rotation sensor 5, and its output is also sent to the microprocessor 93.

このマイクロプロセッサ93はADコンバータ91およ
び入力回路92から得られたデジタルおよびパルス信号
に基づいて内燃機関1へ供給すべき燃料量を演算し、そ
の結果にしたがってインジェクタ6の駆動パルス幅を変
える駆動パルスを出力するものである。
This microprocessor 93 calculates the amount of fuel to be supplied to the internal combustion engine 1 based on the digital and pulse signals obtained from the AD converter 91 and the input circuit 92, and changes the drive pulse width of the injector 6 according to the result. This outputs the following.

このマイク彎プロセッ2す93の制御手順やデータを予
めROM94で記憶しており、またRAM95で演算過
程におけるデータを一時的に格納するようにしている。
Control procedures and data for the microphone processor 293 are stored in advance in a ROM 94, and data in the calculation process is temporarily stored in a RAM 95.

そして、マイクロプロセッサ93の出力信号にしたがっ
てインジェクタ駆動出力口゛路96でインジェクタ6を
駆動するようにしている。
The injector 6 is driven by an injector drive output port 96 in accordance with an output signal from the microprocessor 93.

上記第7図中の広域空燃比センサ8は第8図に示すよう
に構成されており、81は固体電解質酸素ポンプセル(
以下酸素ポンプセルという)、82は固体電解質酸素電
池セル(以下酸素電池セルという)、83m、83bお
よび83eは多孔質でできた電極、84は拡散室、85
は基準電圧源、86は基準電圧源85の基準電圧と酸素
電池セル82の電圧とを比較する比較増幅器、87はポ
ンプ駆動回路、88は酸素ポンプ電流(以下ポンプ電流
という)を検出するための抵抗、89はセンサを活性化
温度に保つため、のヒータ、90はk −夕制御回路で
ある。
The wide range air-fuel ratio sensor 8 in FIG. 7 above is constructed as shown in FIG. 8, and 81 is a solid electrolyte oxygen pump cell (
82 is a solid electrolyte oxygen battery cell (hereinafter referred to as an oxygen battery cell), 83m, 83b and 83e are porous electrodes, 84 is a diffusion chamber, 85
is a reference voltage source, 86 is a comparison amplifier that compares the reference voltage of the reference voltage source 85 and the voltage of the oxygen battery cell 82, 87 is a pump drive circuit, and 88 is for detecting the oxygen pump current (hereinafter referred to as pump current). A resistor, 89 is a heater for keeping the sensor at the activation temperature, and 90 is a control circuit.

この広域空燃比センサ8の構成は既に公知(例えば特開
昭60−128349号公報、特開昭59−67455
号)のものであり、機関始動の後第7図中制御装置9の
ヒータ制御駆動出力回路98より出された信号Shがオ
ンされるとヒータに通電され広域空燃比センサ8を所定
温度に保たれ、さらにポンプ電流駆動出力回路97の出
力信号ScがオンされるとポンプIB!勅回路87が動
作を開始し、基準電圧源85の電圧(約0.4V)と酸
素電池セル82の電圧とを比較増幅器86で比較する。
The configuration of this wide range air-fuel ratio sensor 8 is already known (for example, Japanese Patent Laid-Open No. 60-128349, Japanese Patent Laid-Open No. 59-67455).
When the signal Sh output from the heater control drive output circuit 98 of the control device 9 in FIG. 7 is turned on after the engine is started, the heater is energized and the wide range air-fuel ratio sensor 8 is maintained at a predetermined temperature. When the output signal Sc of the pump current drive output circuit 97 is further turned on, the pump IB! The output circuit 87 starts operating, and the comparator amplifier 86 compares the voltage of the reference voltage source 85 (approximately 0.4 V) and the voltage of the oxygen battery cell 82 .

この結果に基づき、その偏差が零になるようにポンプ駆
動回路87を介して酸素ポンプセル81に電流を流し込
むことによって、拡散室84内の排気ガスが理論空燃比
相当となるように作用させるものである。
Based on this result, a current is applied to the oxygen pump cell 81 via the pump drive circuit 87 so that the deviation becomes zero, so that the exhaust gas in the diffusion chamber 84 becomes equivalent to the stoichiometric air-fuel ratio. be.

このような原理を用いて理論空燃比よりもリーン、リッ
チ側ともに検出可能であり、その測定結果は抵抗88の
両端の電圧−として取り出すことができ、第3図に示す
ように広い空燃比の範囲に対して線形な出力電圧を得る
ことができる。そしてこの出力電圧ηに基づいて制御装
置9によって所望の空燃比になるように燃料噴射量がフ
ィードバック制御される。
Using this principle, it is possible to detect both leaner and richer sides than the stoichiometric air-fuel ratio, and the measurement results can be extracted as the voltage across the resistor 88. An output voltage that is linear over the range can be obtained. Based on this output voltage η, the fuel injection amount is feedback-controlled by the control device 9 so as to achieve a desired air-fuel ratio.

次に動作について第9図、第10図にしたがって説明す
る。この第9図、第10図はROM94に書き込まれて
いる広域空燃比センサ制御のプログラムの実行フローチ
ャートであり1ltlJtl装置9の制御手順をフロー
チャートで表わしたものである。
Next, the operation will be explained according to FIGS. 9 and 10. 9 and 10 are execution flowcharts of the program for wide range air-fuel ratio sensor control written in the ROM 94, and represent the control procedure of the 1ltlJtl device 9 in the form of a flowchart.

第9図は検知開始タイミング算出手順を示しており、割
込み処理の合間を縫って不定期に繰り返し実行される。
FIG. 9 shows a detection start timing calculation procedure, which is repeatedly executed at irregular intervals between interrupt processing.

まず、ステップ201で回転数Nが内燃機関始動判定回
転数(例えば400rpm)を超えているか否かを判定
し、N440 Orpmの場合は未だ始動完了せずと判
断してステップ2o2,203でそれぞれヒータ制御回
路駆動信号Sh、ポンプ駆動開始信号Scの出力を停止
して(既に停止されていれば停止を維持する)、リター
ンする。
First, in step 201, it is determined whether or not the rotational speed N exceeds the internal combustion engine starting determination rotational speed (for example, 400 rpm), and in the case of N440 orpm, it is determined that starting has not yet been completed, and the heater is turned off in steps 2o2 and 203, respectively. The output of the control circuit drive signal Sh and pump drive start signal Sc is stopped (if already stopped, the stops are maintained), and the process returns.

一方、N>40Orpmのときは始動完了と判断してス
テップ204に進む。
On the other hand, if N>40 Orpm, it is determined that the start is complete and the process proceeds to step 204.

ステップ204において、ヒータ制御回路駆動信号Sh
の出力の有無を判定する。ヒータ制御回路駆動信号Sh
が出力されていなければ、まずステップ205でヒータ
制御回路駆動信号Shの出力を開始し、ステップ206
でそのときの冷却水温−を読み込み、さらにステップ2
07でこの冷却水温尤に基づいてポンプ駆動開始信号S
、、の出力開始タイミングTf、Tをテーブルルックア
ップする。
In step 204, the heater control circuit drive signal Sh
Determine whether there is an output. Heater control circuit drive signal Sh
If not, output of the heater control circuit drive signal Sh is first started in step 205, and then in step 206.
Read the cooling water temperature at that time, and then proceed to step 2.
At step 07, a pump drive start signal S is generated based on the cooling water temperature.
The output start timings Tf and T of , , are looked up in a table.

この出力開始タイミングTITは広域空燃比センサ8が
排気中空燃比の検出を開始するタイミングであり、ヒー
タ制御回路駆動信号Shの出力開始時点からの経過時間
という形で設定される。
This output start timing TIT is the timing at which the wide range air-fuel ratio sensor 8 starts detecting the exhaust air-fuel ratio, and is set in the form of an elapsed time from the time when the output of the heater control circuit drive signal Sh starts.

次いで、ステップ208で回転数Nと燃料噴射量T2を
読み込む。燃料噴射l−は図示しない他のルーチンによ
って次式に従って演算される。
Next, in step 208, the rotational speed N and fuel injection amount T2 are read. Fuel injection l- is calculated by another routine (not shown) according to the following equation.

T、=に−Pb−+7、 ただしKは定数、1.は吸気圧力Pbと回転数Nに対応
して予め定められた充てん効率である。
T, = -Pb-+7, where K is a constant, 1. is a predetermined filling efficiency corresponding to the intake pressure Pb and the rotational speed N.

ステップ209で上記回転数Nと燃料噴射量T2に基づ
いて一定時間毎に上記出力開始タイミングT、から減算
する際に使用する減算値T1.、。をテーブルルックア
ップする。この出力開始タイミングT、Tおよび減算値
Tiubは後述するプログラムで使用されるものである
In step 209, the subtraction value T1. is used to subtract from the output start timing T at regular intervals based on the rotation speed N and the fuel injection amount T2. ,. table lookup. The output start timings T and T and the subtraction value Tiub are used in a program described later.

また、上記ステップ204でヒータ制御回路駆動信号S
hが既に出力されていると判断した場合は、ステップ2
08に進み運転状態すなわち回転数Nと燃料噴射量T1
に応じて減算値T、。ゎをテーブルルックアップする。
Further, in step 204 above, the heater control circuit drive signal S
If it is determined that h has already been output, step 2
Proceed to 08 to check the operating state, that is, the rotation speed N and the fuel injection amount T1
Subtract value T, depending on. Table lookup for ゎ.

第10図は検知開始タイミング実行プログラムを示して
おり、このプログラムは前記第9図の検知開始タイミン
グ算出の結果に基づき、所定時間毎に一度実行される。
FIG. 10 shows a detection start timing execution program, and this program is executed once every predetermined time based on the result of the detection start timing calculation shown in FIG. 9.

ステップ\115でポンプ駆動開始信号S0が出力され
ているか否かを判定し、出力されていなければステップ
116でポンプ駆動開始信号Sc%出力開始タイミング
Ts□を次式にしたがって演算する。
In step \115, it is determined whether or not the pump drive start signal S0 is being output. If not, in step 116, the pump drive start signal Sc% output start timing Ts□ is calculated according to the following equation.

T=T   −T ただし、TS7:今回の処理ルーチンのポンプ駆動開始
信号S00出力開始タイミング値、 T 、T1:  前回の処理ルーチンのポンプ駆動開始
信号S、の出力開始タイミング 値、 次いで、ステップ117でT6ア≦0になったか否かを
判別し、T、1≦0場合は検知タイミングであると判定
してステップ118でポンプ駆動開始信号Sを出力する
T=T −T However, TS7: Output start timing value of the pump drive start signal S00 of the current processing routine, T, T1: Output start timing value of the pump drive start signal S of the previous processing routine, Next, in step 117 It is determined whether or not T6a≦0, and if T,1≦0, it is determined that the detection timing has come, and a pump drive start signal S is output in step 118.

これにより、広域空燃比センサ8の酸素ポンプ電流IP
の供給が開始されて排気中空燃比の検出が。
As a result, the oxygen pump current IP of the wide range air-fuel ratio sensor 8
supply is started and the exhaust air fuel ratio is detected.

開始され、空燃比のフィードバック制御が開始される。air-fuel ratio feedback control is started.

また、ステップ117でT、□〉0と判定されたときは
、ステップ11Bをバイパスしてリターンする。
Further, when it is determined in step 117 that T, □>0, step 11B is bypassed and the process returns.

一方、上記ステップ115でポンプ駆動開始信号Scが
既に出力されていれば、ステップ116〜118を経る
ことなくこの処理を終了する。
On the other hand, if the pump drive start signal Sc has already been output in step 115, this process ends without going through steps 116 to 118.

このように、始動時にまず冷却水温−によって出力開始
タイミングT、工を設定した後、始動後におけるエンジ
ン運転状態より広域空燃比センサ8が空燃比検出可能な
状態に活性化する時期を予想して酸素ポンプ電流I2の
供給が開始され、空燃比フィードバックIIIIJ御が
開始され、空燃比が所望の値に制御される。
In this way, at the time of starting, the output start timing T and T are first set based on the cooling water temperature, and then the time when the wide range air-fuel ratio sensor 8 will be activated to a state where the air-fuel ratio can be detected is predicted based on the engine operating condition after starting. Supply of the oxygen pump current I2 is started, air-fuel ratio feedback IIIJ control is started, and the air-fuel ratio is controlled to a desired value.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

従来の内燃機関の空燃比制御装置は以上のように構成さ
れているので、機関始動完了時期のみを基準としていた
ため、外気温が低温時や高温時における様々な始動条件
に適応した酸素ポンプ電流!、を流し始める時期の適格
な制御が困難であった。
Conventional air-fuel ratio control devices for internal combustion engines are configured as described above, and are based only on the engine start completion time, so the oxygen pump current is adjusted to suit various starting conditions when the outside temperature is low or high. ! It has been difficult to properly control when the water begins to flow.

また、酸素ポンプ電流IPより排気中空燃比を検出する
際基準となる酸素電池セルの出力V、が以下に示すよう
な条件下で正常な値を示さないときにも一定手順で酸素
ポンプ電流を流し始める時期を決定するため、空燃比を
正確に検出できず空燃比フィードバック制御によってオ
ーバリッチになりエンジンストツ6ブしたり、酸素ポン
プ電流IPの流し過ぎにより広域空燃比センサ8が破損
することがあった。
In addition, even when the output V of the oxygen battery cell, which is the standard when detecting the exhaust gas air-fuel ratio from the oxygen pump current IP, does not show a normal value under the conditions shown below, the oxygen pump current is applied in a fixed procedure. In order to determine when to start, the air-fuel ratio cannot be accurately detected and the air-fuel ratio feedback control may cause the engine to stall due to over-rich conditions, or the wide-range air-fuel ratio sensor 8 may be damaged due to excessive flow of oxygen pump current IP. Ta.

このようなり6値の異常は、インジェクタ6からの吐出
燃料量が実効的に過度に大きくなる−10〜−30℃の
低温始動時および機関の急加減速時に、広域空燃比セン
サ8の拡散室内に高濃度の未燃ガスが浸入し酸素ポンプ
セル81の大気側電極83c付近にこの未燃ガスが多層
構造のセンサ各部接合部からもれて酸素ポンプセル81
の排気側と大気側電極とが同一未燃ガスでおおわれ、酸
素濃度が減少しv6出力が低下する場合に発生する。
Such a six-value abnormality occurs in the diffusion chamber of the wide-range air-fuel ratio sensor 8 when starting at a low temperature of -10 to -30°C, when the amount of fuel discharged from the injector 6 becomes excessively large, or when the engine suddenly accelerates or decelerates. A high concentration of unburned gas enters the oxygen pump cell 81 near the atmosphere-side electrode 83c.
This occurs when the exhaust side and the atmosphere side electrode are covered with the same unburned gas, the oxygen concentration decreases and the V6 output decreases.

また機関が停止しない限し酸素ポンプ電流1pを止める
乙とができず、機関運転中の異常に対応した酸素ポンプ
電流制御ができなかった。
Furthermore, it was not possible to stop the oxygen pump current 1p unless the engine stopped, and it was not possible to control the oxygen pump current in response to abnormalities during engine operation.

したがって酸素ポンプセル出力■、をプログラム上検知
せずに酸素ポンプ電流を流し始める従来の内燃機関の空
燃比制御装置では、正確な酸素ポンプ電流制御が難しく
、空燃比検出精度が低下し内燃機関の空燃比を精密にフ
ィードバック制御できず運転性能が低下する問題点があ
った。
Therefore, with conventional air-fuel ratio control devices for internal combustion engines that start flowing oxygen pump current without detecting the oxygen pump cell output in the program, it is difficult to accurately control the oxygen pump current, and the accuracy of air-fuel ratio detection decreases. There was a problem in that the fuel ratio could not be precisely controlled through feedback, resulting in poor driving performance.

この発明はかかる問題点を解決するためになされたもの
で、極低温時始動のみならず、始動完了後酸素ポンプ電
流が一度流れ始めた後、センサの異常が発生しても常に
最適な酸素ポンプ電流駆動禁止および開始制御を可能に
し、常に正確な空燃比を検出して安価な空燃比フィード
バック制御を実現することのできる内燃機関の空燃比制
御装置を得ることを目的とする。
This invention has been made to solve these problems, and is designed to provide an oxygen pump that is optimal not only for starting at extremely low temperatures, but also even when a sensor abnormality occurs after the oxygen pump current has started flowing once the starting has been completed. An object of the present invention is to provide an air-fuel ratio control device for an internal combustion engine that can perform current drive prohibition and start control, constantly detect accurate air-fuel ratios, and realize inexpensive air-fuel ratio feedback control.

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係る内燃機関の空燃比f!1lJil!l装
置は、広域空燃比センサの酸素電池セルの起電力を検出
する酸素電池セル起電力検出回路と、この酸素電池セル
起電力検出回路で検出された起電力の値に基づいて酸素
ポンプセルの酸素ポンプ電流を制御する制御装置とを設
けたものである。
The air-fuel ratio f! of the internal combustion engine according to this invention! 1l Jil! The device includes an oxygen battery cell electromotive force detection circuit that detects the electromotive force of the oxygen battery cell of the wide range air-fuel ratio sensor, and an oxygen battery cell electromotive force detection circuit that detects the electromotive force of the oxygen pump cell based on the value of the electromotive force detected by the oxygen battery cell electromotive force detection circuit. A control device for controlling the pump current is provided.

〔作 用〕[For production]

この発明においては、機関始動時に酸素電池セルの起電
力を酸素電池セル起電力検出回路で検出し、その検出し
た酸素電池セルの出力電圧Vの値に応じて酸素ポンプ電
流を流し始める時期を制御装置により決定し、機関運転
中においても、酸素電池セルの出力電圧V値が所定値以
下であれば広域空燃比センサが異常であると判定し酸素
ポンプ電流を停止し、再度酸素電池セルの出力電圧Vが
所定値を越えるまで酸素ポンプ電流停止の状態を維持す
るように制御する。
In this invention, the electromotive force of the oxygen battery cell is detected by the oxygen battery cell electromotive force detection circuit when the engine is started, and the timing at which the oxygen pump current starts to flow is controlled according to the detected value of the output voltage V of the oxygen battery cell. Determined by the device, even during engine operation, if the output voltage V value of the oxygen battery cell is below a predetermined value, the wide range air-fuel ratio sensor is determined to be abnormal, the oxygen pump current is stopped, and the output of the oxygen battery cell is restarted. The oxygen pump current is controlled to be stopped until the voltage V exceeds a predetermined value.

〔実施例〕〔Example〕

以下に、この発明の内燃機関の空燃比制御装置の実施例
について図面に基づき説明する。この発明の構成は、広
域空燃比センサ8の酸素電池セルの起電力を検出する酸
素電池セル起電力検出回路を除き、第7図に示す従来の
装置の構成と全く同一であるが、制御装置9内のマイク
四プロセッサ93を中心とする演算処理やデータ設定方
法が従来と異なる。
Embodiments of the air-fuel ratio control device for an internal combustion engine according to the present invention will be described below with reference to the drawings. The configuration of the present invention is completely the same as the configuration of the conventional device shown in FIG. 7, except for the oxygen battery cell electromotive force detection circuit that detects the electromotive force of the oxygen battery cell of the wide range air-fuel ratio sensor 8. The arithmetic processing mainly performed by the four microphone processors 93 and the data setting method are different from the conventional method.

第1図はこの発明の一実施例の構成を示し、第2図はこ
の発明の広域空燃比センサ8の構成を示している。第2
図において、この発明では従来の広域空燃比センサ8の
構成に加え酸素電池セルの出力電圧Vを検出する酸素電
池セル起電力検出回路82aが付加され、この出力信号
v5が第1図に示す制御装置9のADコンバータ91に
入力され、マイクロプロセッサ93によってポンプ電流
駆動出力回路97で酸素ポンプ電流を流し始めるかを制
御するようにしている。その他の構成は従来と同様であ
る。
FIG. 1 shows the configuration of an embodiment of the present invention, and FIG. 2 shows the configuration of a wide range air-fuel ratio sensor 8 of the present invention. Second
In the figure, in addition to the configuration of the conventional wide-range air-fuel ratio sensor 8, an oxygen battery cell electromotive force detection circuit 82a for detecting the output voltage V of the oxygen battery cell is added, and this output signal v5 is controlled by the control shown in FIG. The signal is input to the AD converter 91 of the device 9, and the microprocessor 93 controls whether or not to start flowing the oxygen pump current in the pump current drive output circuit 97. Other configurations are the same as before.

次に動作について説明する。第4図はこの発明の一実施
例の制御手順を示すフローチャートである。°この第4
図において、ステップ101〜103までは従来例の制
御手順を示した第9図のフローチャートのステップ20
1〜203までと同様なので説明を省略する。
Next, the operation will be explained. FIG. 4 is a flowchart showing the control procedure of an embodiment of the present invention. °this fourth
In the figure, steps 101 to 103 are step 20 of the flowchart of FIG. 9 showing the conventional control procedure.
Since it is the same as 1 to 203, the explanation will be omitted.

ステップ101で回転数N)400rpmと判定される
と、ステップ105に進み、と−夕制御回路駆動信号S
l、の出力の有無を判定し、ヒータ胴細回路駆動信号S
hが出力されていればステップ107に進み、ヒータ制
御回路駆動信号Shが出力されていなければステップ1
06に進み、ヒータ制御回路駆動信号Shの出力を開始
し、ステップ107に進む。
If it is determined in step 101 that the rotational speed N) is 400 rpm, the process proceeds to step 105, and the control circuit drive signal S
The presence or absence of the output of the heater body narrow circuit drive signal S is determined.
If h is output, the process proceeds to step 107, and if the heater control circuit drive signal Sh is not output, the process proceeds to step 1.
The process proceeds to step 06, where output of the heater control circuit drive signal Sh is started, and the process proceeds to step 107.

ステップ107において広域空燃比センサ8の酸素電池
セル82の出力電圧Vを検出する酸素電池セル起電力検
出回路82mの出方信号v6を読み込み、ステップ10
8で酸素電池セル起電力検出回路82aの出力電圧v3
が所定値V、。(例えば0.3V)以上かどうかを判定
し、鴇≧汽。の場合は酸素電池セル82が活性化し正常
となったと判断してステップ109に進む。
In step 107, the output signal v6 of the oxygen battery cell electromotive force detection circuit 82m that detects the output voltage V of the oxygen battery cell 82 of the wide range air-fuel ratio sensor 8 is read, and in step 10
8, the output voltage v3 of the oxygen battery cell electromotive force detection circuit 82a
is a predetermined value V. (for example, 0.3V) or higher, and determine whether the voltage is greater than or equal to 0.3V. In this case, it is determined that the oxygen battery cell 82 is activated and normal, and the process proceeds to step 109.

また、ステップ108でV、<V、。と判定された場合
は広域空燃比センサ8が不活性または異常であると判断
してステップ103に進み、ポンプ駆動開始信号S0の
出力を停止して(既に停止されていれば停止を維持する
)ステップ104に進み、後で詳しく説明するポンプ駆
動開始信号S0の出力開始タイミング時間T、Tを零に
リセットしてリターンする。
Also, in step 108, V,<V,. If it is determined that the wide range air-fuel ratio sensor 8 is inactive or abnormal, the process proceeds to step 103, and the output of the pump drive start signal S0 is stopped (if it has already been stopped, it is maintained stopped). Proceeding to step 104, the output start timing times T and T of the pump drive start signal S0, which will be explained in detail later, are reset to zero, and the process returns.

この動作によって機関の始動が完了し、以下に述べる手
順でポンプ駆動開始信号S。が出力された後でも、常に
酸素電池セル起電力検出回路82mの出力信号入を監視
することによって広域空燃比センサ8の異常、不活性状
態を検出し、酸素ポンプ電流■2を停止し、誤ったポン
プ電流の流し過ぎによる広域空燃比センサ8の破壊およ
び広域空燃比センサ8の異常出力値に基づく過大な燃料
噴射量フィードバック制御を防止することができる。
This operation completes engine starting, and the pump drive start signal S is generated by the procedure described below. Even after the output of Destruction of the wide-range air-fuel ratio sensor 8 due to excessive pump current flow and excessive fuel injection amount feedback control based on an abnormal output value of the wide-range air-fuel ratio sensor 8 can be prevented.

一方、ステップ109に進んだ場合、酸素電池セル82
が正常に活性化したと考えて、酸素電池セル起電力検出
回路82aの出力信号V、が所定値v、。以上となった
時期t0から所定の出力開始タイミング時間T8T後に
酸素ポンプ電流lpを流し始めるために、この出力開始
タイミング時間T8.が既に設定されている(すなわち
T、7\O)かどうかを判定しT、□−〇の場合は、ス
テップ110で冷却水温−を読み込んだ後ステップ11
1で出力開始タイミング時間TSTを冷却水温度孔の値
に基づき一テーブルルックアップしてステップ112に
進む。
On the other hand, if the process proceeds to step 109, the oxygen battery cell 82
Considering that has been activated normally, the output signal V, of the oxygen battery cell electromotive force detection circuit 82a is a predetermined value v,. In order to start flowing the oxygen pump current lp after a predetermined output start timing time T8T from the above timing t0, this output start timing time T8. It is determined whether T, 7\O has already been set (that is, T, 7\O), and if T, □-〇, the cooling water temperature - is read in step 110, and then step 11
1, the output start timing time TST is looked up in a table based on the value of the cooling water temperature hole, and the process proceeds to step 112.

また、ステップ109で出力開始タイミング時間T、□
が零でないと判断された場合は、−度設定された出力開
始タイミング時間T、Tの値を誤って再び設定すること
のないようにステップ110,111をジャンプしてス
テップ112に進む。
Also, in step 109, the output start timing time T, □
If it is determined that is not zero, steps 110 and 111 are skipped and the process proceeds to step 112 so that the output start timing times T and T, which have been set by − degrees, are not erroneously set again.

ステップ112で機関の回転数Nと燃料噴射量;を読み
込みステップ113に進み、上記出力開始タイミング時
間TS□から減算処理をし、ポンプ駆動開始信号S0の
出力開始時期を決める時間Tauゎをこの回転数Nと燃
料噴射量Tpに基づいてテーブルルックアップした後、
この処理を終了する。
In step 112, the engine speed N and fuel injection amount are read, and the process proceeds to step 113, where subtraction processing is performed from the output start timing time TS□, and the time Tau which determines the output start timing of the pump drive start signal S0 is determined by this rotation. After looking up the table based on the number N and the fuel injection amount Tp,
This process ends.

ただし、出力開始タイミング時間T9□の設定法が従来
と異るから上記時間Taubのテーブルルックアップを
するためのROMに予め記録された値は、従来値と異る
のは言うまでもない。
However, since the method for setting the output start timing time T9□ is different from the conventional one, it goes without saying that the value previously recorded in the ROM for performing the table lookup of the above-mentioned time Taub is different from the conventional value.

次に以上の処理を必ず終了した後に第10図のフローチ
ャートのステップ115〜118に基づいてポンプ駆動
開始信号S。の出力開始の制御を行う。この処理は従来
のものと全く同一であるので説明を省略する。
Next, after the above-mentioned processing is completed, the pump drive start signal S is generated based on steps 115 to 118 of the flowchart of FIG. Controls the start of output. This process is completely the same as the conventional process, so the explanation will be omitted.

以上の処理は従来例と大きく異り、機関の外界条件(例
えば外気温)によって実効ヒータ能力が変化し広域空燃
比センサ8の活性化時期が様々に変化するにもかかわら
ず従来例がポンプ駆動開始信号S0出力開始時期の基準
をヒータのオンした時点(すなわちヒータ制御回路駆動
信号Sh出力時点)としているのに比べ、この発明では
広域空燃比センサ8自身がヒータによって活性化温度に
達し酸素電池セル82の出力電圧Vが正常な値を出力し
始めた時点をヒータ制御回路駆動信号Scの出力開始の
基準としている。
The above processing is significantly different from the conventional example, and although the effective heater capacity changes depending on the external conditions of the engine (for example, outside temperature) and the activation timing of the wide range air-fuel ratio sensor 8 varies, the conventional example drives the pump. Compared to the standard for the output start timing of the start signal S0, which is the time when the heater is turned on (that is, the time when the heater control circuit drive signal Sh is output), in this invention, the wide range air-fuel ratio sensor 8 itself reaches the activation temperature by the heater, and the oxygen battery The point in time when the output voltage V of the cell 82 starts to output a normal value is used as a reference for starting to output the heater control circuit drive signal Sc.

また、従来例が始動時のみのヒータ制御回路駆動信号S
。の出力開始割部しかできなかったのに比べ、この発明
では常にヒータ制御回路駆動信号Vを検出することによ
って酸素電池セルの出力電圧の異常を検出して広域空燃
比センサ8の破壊および過度の誤った燃料フィードバッ
ク制御をさけることができる。
In addition, in the conventional example, the heater control circuit drive signal S is used only at the time of starting.
. In contrast, in the present invention, by constantly detecting the heater control circuit drive signal V, an abnormality in the output voltage of the oxygen battery cell can be detected to prevent damage to the wide range air-fuel ratio sensor 8 and excessive Erroneous fuel feedback control can be avoided.

第5図はこの発明の横開始動時におけるポンプ電流を流
し始める時期t、と酸素電池セル82の出力電圧を酸素
電池セル起電力検出回路82aで検出した出力信号v6
が所定値V、、11上となる時間t0と前期第4図を用
いて示した手順で設定した七−夕割部回路駆動信号Sc
の出力開始、タイミング時間T、との関係を示している
FIG. 5 shows the timing t at which the pump current begins to flow during the horizontal start operation of the present invention, and the output signal v6 detected by the oxygen battery cell electromotive force detection circuit 82a, and the output voltage of the oxygen battery cell 82.
is above the predetermined value V, .
The relationship between the start of output and the timing time T is shown.

この出力開始タイミング時間T、□が第10図に示した
手順で順次時間’r、、、bずつ減算され零以下になっ
た時点、すなわち、酸素ポンプ電流オン時点tで酸素ポ
ンプ電流■2が流れ始める。
The output start timing time T, □ is sequentially subtracted by time 'r, , b by the procedure shown in Fig. 10, and when it becomes less than zero, that is, at the time t when the oxygen pump current is turned on, the oxygen pump current ■2 becomes It starts to flow.

また、第6図(b)は第6図(a)に示すようにすでに
酸素ポンプ電流が流れ排気中空燃比の計測が実施されて
いるときに、第6図(b)に示すように高濃度の未燃燃
料ガスが広域空燃比センサに侵入し、酸素電池セル出力
82の出力電圧を酸素電池セル起電力検出回路82aで
検出した出方信号V、が正常な値からずれたとき、この
出力信号v8を検出し第4図に示した手順で酸素ポンプ
電流が停止され、その後高濃度ガスが消え再び出力信号
鴇が所定値v8゜以上となり酸素ポンプ電流が流れ排気
中空燃比の測定が開始される例を示している。
In addition, Fig. 6(b) shows that when the oxygen pump current is already flowing and the exhaust air fuel ratio is being measured as shown in Fig. 6(a), a high concentration is detected as shown in Fig. 6(b). When unburned fuel gas enters the wide range air-fuel ratio sensor and the output signal V, which is the output voltage of the oxygen battery cell output 82 detected by the oxygen battery cell electromotive force detection circuit 82a, deviates from the normal value, this output Signal v8 is detected and the oxygen pump current is stopped according to the procedure shown in Fig. 4, and then the high concentration gas disappears and the output signal becomes equal to or higher than the predetermined value v8° again, and the oxygen pump current flows and measurement of the exhaust air fuel ratio is started. An example is shown below.

なお、上記実施例では、燃料噴射システムとしてスピー
ドデンシティ方式の燃料噴射装置の具体例としたが、エ
アフローセンサを用いた燃料噴射装置や電子制御気化蕾
に適用できるのは言うまでもない。
In the above embodiment, a speed density type fuel injection device is used as a specific example of the fuel injection system, but it goes without saying that the present invention can also be applied to a fuel injection device using an air flow sensor or an electronically controlled vaporizer.

〔発明の効果〕〔Effect of the invention〕

この発明は重上説明したとおり、広域空燃比センサの酸
素電池セル出力電圧を酸素電池起電力検出回路で検出し
て、この出力信号に基づき広域空燃比センサの活性状態
を判定し酸素ポンプ電流を流すように制御したので、精
度の高い活性化判定および酸素ポンプ電流制御が可能と
なり、横開始動時のみならず運転中で排気中空燃比測定
中においても酸素ポンプ電流出力停止および開始が可能
となり、広域空燃比センサの空燃比計測精度が向上し信
頼性が増し、安定した空燃比フィードバック燃料制御が
行え、運転フィーリングが向上する効果がある。
As explained above, this invention detects the oxygen battery cell output voltage of the wide-range air-fuel ratio sensor using the oxygen battery electromotive force detection circuit, determines the activation state of the wide-range air-fuel ratio sensor based on this output signal, and determines the oxygen pump current. Since the flow is controlled to flow, highly accurate activation judgment and oxygen pump current control are possible, and oxygen pump current output can be stopped and started not only during side start operation but also during operation and while measuring the exhaust air-fuel ratio. This has the effect of improving the air-fuel ratio measurement accuracy of the wide-range air-fuel ratio sensor, increasing reliability, enabling stable air-fuel ratio feedback fuel control, and improving driving feeling.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図はこの発明の内燃機関の空燃比制御装置の一実施
例の構成図、第2図は同上実施例における広域空燃比セ
ンサの構成図、第3図はこの発明および従来の内燃機関
の空燃比制御装置における広域空燃比センサの特性図、
第4図は同上実施例における制御装置の動作を示すフロ
ーチャート、第5図は同上実施例における制御方法を説
明するための動作説明図、第6図(a)は同上実施例を
説明するための時間対酸素ポンプ電流の関係を示す説明
図、第6図(b)は第6図(a)の酸素ポンプ電流に対
する排気ガス中の空燃比の測定開始時間との関係を示す
説明図、第7図は従来の内燃機関の空燃比制御装置の構
成図、第8図は従来の内燃機関の空燃比制御装置におけ
る広域空燃比センサの構成図、第9図は従来の内燃機関
の空燃比制御装置の動作を表わすフローチャート、第1
0図はこの発明の一実施例および従来の内燃機関の空燃
比制御装置の動作を表わすフローチャートである。 1・・・内燃機関、2・・・吸気管、3・・・絞り弁、
4・・・圧力センサ、5・・・回転センサ、6・・・イ
ンジェクタ、7・・・排気管、8・・・広域空燃比セン
サ、9・・・制御装置、10・・・冷却水温センサ、8
1・・・酸素ポンプセンサ、82・・・酸素電池セル、
82 a−酸素電池セル起電力検出回路、84・・・拡
散室、85・・・基準電圧源、86・・・比較増幅器、
96・・・インジェクタ駆動出力回路、97・・・ポン
プ電流駆動出力回路、98・・・ヒータ制御駆動出力回
路、 なお、図中、同一符号は同一、又は相当部分を示す。
FIG. 1 is a block diagram of an embodiment of an air-fuel ratio control device for an internal combustion engine according to the present invention, FIG. 2 is a block diagram of a wide-range air-fuel ratio sensor in the same embodiment, and FIG. Characteristic diagram of wide range air-fuel ratio sensor in air-fuel ratio control device,
FIG. 4 is a flowchart showing the operation of the control device in the above embodiment, FIG. 5 is an operation explanatory diagram for explaining the control method in the above embodiment, and FIG. 6(a) is a flow chart for explaining the control method in the above embodiment. FIG. 6(b) is an explanatory diagram showing the relationship between time and oxygen pump current. FIG. 6(b) is an explanatory diagram showing the relationship between the oxygen pump current in FIG. Figure 8 is a configuration diagram of a conventional air-fuel ratio control device for an internal combustion engine, Figure 8 is a configuration diagram of a wide range air-fuel ratio sensor in a conventional air-fuel ratio control device for an internal combustion engine, and Figure 9 is a configuration diagram of a conventional air-fuel ratio control device for an internal combustion engine. Flowchart showing the operation of
FIG. 0 is a flowchart showing the operation of an embodiment of the present invention and a conventional air-fuel ratio control device for an internal combustion engine. 1... Internal combustion engine, 2... Intake pipe, 3... Throttle valve,
4... Pressure sensor, 5... Rotation sensor, 6... Injector, 7... Exhaust pipe, 8... Wide range air-fuel ratio sensor, 9... Control device, 10... Cooling water temperature sensor , 8
1... Oxygen pump sensor, 82... Oxygen battery cell,
82 a-oxygen battery cell electromotive force detection circuit, 84... diffusion chamber, 85... reference voltage source, 86... comparison amplifier,
96... Injector drive output circuit, 97... Pump current drive output circuit, 98... Heater control drive output circuit. In the drawings, the same reference numerals indicate the same or equivalent parts.

Claims (2)

【特許請求の範囲】[Claims] (1)内燃機関の排気ガスを導入する間隙部とこの間隙
部内の酸素分圧を制御する固体電解質酸素ポンプセルと
前記間隙部分の酸素分圧と大気中の酸素分圧に対応した
起電力を発生する固体電解質酸素電池セルと上記固体電
解質酸素ポンプセルを加熱するヒータとを備えた広域空
燃比センサと、開始信号が入力されると前記固体電解質
酸素電池セルの起電力を所定値に保つように酸素ポンプ
電流を供給するポンプ電流供給手段と、前記固体電解質
酸素ポンプセルの温度を所定値となるように前記ヒータ
に電力を供給するヒータ電力供給手段と、前記固体電解
質酸素電池セルの起電力を検出する酸素電池セル起電力
検出手段と、前記酸素ポンプ電流を検出するための酸素
ポンプ電流検出手段と、前記内燃機関の運転状態を検出
する運転状態検出手段と、前記内燃機関が始動完了とと
もに前記ヒータに電力を供給するとともに前記固体電解
質酸素電池セルの起電力が所定値を越えると、始動時の
運転状態に応じた所定時間後に前記開始信号を出力する
制御装置とを備えた内燃機関の空燃比制御装置。
(1) A gap section into which the exhaust gas of the internal combustion engine is introduced, a solid electrolyte oxygen pump cell that controls the oxygen partial pressure in this gap section, and an electromotive force that generates an electromotive force corresponding to the oxygen partial pressure in the gap section and the oxygen partial pressure in the atmosphere. a wide range air-fuel ratio sensor including a solid electrolyte oxygen battery cell to heat the solid electrolyte oxygen battery cell and a heater to heat the solid electrolyte oxygen pump cell; a pump current supply means for supplying a pump current; a heater power supply means for supplying power to the heater so that the temperature of the solid electrolyte oxygen pump cell becomes a predetermined value; and detecting an electromotive force of the solid electrolyte oxygen battery cell. an oxygen battery cell electromotive force detection means; an oxygen pump current detection means for detecting the oxygen pump current; an operating state detection means for detecting the operating state of the internal combustion engine; Air-fuel ratio control for an internal combustion engine, comprising: a control device that supplies power and outputs the start signal after a predetermined time depending on the operating state at startup when the electromotive force of the solid electrolyte oxygen battery cell exceeds a predetermined value. Device.
(2)制御装置は機関の始動が完了し前記酸素ポンプ電
流が流れた後において、前記固体電解質酸素電池セルの
起電力が所定値以下の場合、前記酸素ポンプ電流を停止
し、前記固体電解質酸素電池セルの起電力が所定値を越
えるまでポンプ電流停止状態を維持するように制御する
ことを特徴とする特許請求の範囲第1項記載の内燃機関
の空燃比制御装置。
(2) After the starting of the engine is completed and the oxygen pump current flows, if the electromotive force of the solid electrolyte oxygen battery cell is less than a predetermined value, the control device stops the oxygen pump current and 2. The air-fuel ratio control device for an internal combustion engine according to claim 1, wherein control is performed to maintain the pump current stopped state until the electromotive force of the battery cell exceeds a predetermined value.
JP62281731A 1987-11-07 1987-11-07 Air-fuel-ratio control apparatus for internal combustion engine Pending JPH01123141A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62281731A JPH01123141A (en) 1987-11-07 1987-11-07 Air-fuel-ratio control apparatus for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62281731A JPH01123141A (en) 1987-11-07 1987-11-07 Air-fuel-ratio control apparatus for internal combustion engine

Publications (1)

Publication Number Publication Date
JPH01123141A true JPH01123141A (en) 1989-05-16

Family

ID=17643196

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62281731A Pending JPH01123141A (en) 1987-11-07 1987-11-07 Air-fuel-ratio control apparatus for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH01123141A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5970967A (en) * 1996-12-11 1999-10-26 Unisia Jecs Corporation Method and apparatus for diagnosing an abnormality in a wide range air-fuel ratio sensor
US6161376A (en) * 1997-03-04 2000-12-19 Unisia Jecs Corporation Method and apparatus for controlling air-fuel ratio of internal combustion engine
JP2017207444A (en) * 2016-05-20 2017-11-24 日本特殊陶業株式会社 Sensor controller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5970967A (en) * 1996-12-11 1999-10-26 Unisia Jecs Corporation Method and apparatus for diagnosing an abnormality in a wide range air-fuel ratio sensor
US6161376A (en) * 1997-03-04 2000-12-19 Unisia Jecs Corporation Method and apparatus for controlling air-fuel ratio of internal combustion engine
JP2017207444A (en) * 2016-05-20 2017-11-24 日本特殊陶業株式会社 Sensor controller

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