JPH089975B2 - Air-fuel ratio control device for internal combustion engine - Google Patents

Air-fuel ratio control device for internal combustion engine

Info

Publication number
JPH089975B2
JPH089975B2 JP61240697A JP24069786A JPH089975B2 JP H089975 B2 JPH089975 B2 JP H089975B2 JP 61240697 A JP61240697 A JP 61240697A JP 24069786 A JP24069786 A JP 24069786A JP H089975 B2 JPH089975 B2 JP H089975B2
Authority
JP
Japan
Prior art keywords
fuel ratio
air
internal combustion
combustion engine
correction coefficient
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.)
Expired - Lifetime
Application number
JP61240697A
Other languages
Japanese (ja)
Other versions
JPS6394050A (en
Inventor
亮治 西山
翔一 鷲野
晴司 綿谷
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 JP61240697A priority Critical patent/JPH089975B2/en
Publication of JPS6394050A publication Critical patent/JPS6394050A/en
Publication of JPH089975B2 publication Critical patent/JPH089975B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、リーンからリッチまで検出可能な空燃比
センサを用いて空燃比のフイードバツク制御を行うよう
にした内燃機関の空燃比制御装置に関し、特に絞り弁全
開近くの機関パワーゾーンにおける空燃比制御の安定限
界を拡大し、機関を安定に運転できるようにしたもので
ある。
Description: TECHNICAL FIELD The present invention relates to an air-fuel ratio control device for an internal combustion engine, which uses an air-fuel ratio sensor capable of detecting from lean to rich to perform air-fuel ratio feedback control. In particular, the stability limit of air-fuel ratio control in the engine power zone near the full opening of the throttle valve is expanded to enable stable engine operation.

〔従来の技術〕[Conventional technology]

第1図は従来および後述するこの発明の内燃機関の空
燃比制御装置の構成を示すものであり、従来の内燃機関
の空燃比制御装置の説明に際し、この第1図を援用して
説明する。
FIG. 1 shows a configuration of an air-fuel ratio control system for an internal combustion engine according to a conventional and later-described invention, which will be described with reference to FIG. 1 when describing a conventional air-fuel ratio control system for an internal combustion engine.

この第1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はこの吸気管2内に設けら
れた絞り弁である。
In FIG. 1, reference numeral 1 is an internal combustion engine, 2 is an intake pipe connected to the internal combustion engine 1, and 3 is a throttle valve provided in the intake pipe 2.

この吸気管2内の圧力は圧力センサ4で検出し、その
検出圧力はADコンバータ91に送出するようになつてい
る。
The pressure in the intake pipe 2 is detected by the pressure sensor 4, and the detected pressure is sent to the 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つている。
The rotation sensor 5 uses the rotation of the internal combustion engine 1 as a pulse.
The output of the rotation sensor 5 is sent to the input / output circuit 92.

さらに、吸気管2へインジエクタ6により燃料を噴射
するようになつており、このインジエクタ6は出力回路
96の出力で駆動されるようになつている。
Further, fuel is injected into the intake pipe 2 by an injector 6, which is an output circuit.
It is designed to be driven by 96 outputs.

また、内燃機関1に排気管7が接続されており、この
排気管7内の排ガス成分から空燃比に対応した出力が空
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 an exhaust gas component in the exhaust pipe 7 outputs an output corresponding to the air-fuel ratio from the 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と空燃比セン
サ8などの情報から所要燃料量を演算し、インジエクタ
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 fuel amount from the information of the pressure sensor 4, the rotation sensor 5, the air-fuel ratio sensor 8 and the like, and generates the drive pulse width of the injector 6.

この制御装置9におけるADコンバータ91は空燃比セン
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ツサ93に出力するようにな
つている。
The AD converter 91 in the control device 9 is adapted to convert analog signals from the air-fuel ratio sensor 8 and the pressure sensor 4 into digital values and output 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
プロセツサ93に送出するようになつている。
Further, the input circuit 92 is an input circuit for converting the level of the pulse input signal of the rotation sensor 5, and the output thereof is also sent to the microprocessor 93.

このマイクロプロセツサ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
にしたがつてインジエクタ6の駆動パルス幅を出力する
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 according to the result, the drive pulse width of the injector 6 is calculated. It is what is output.

このマイクロプロセツサ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。そして、マ
イクロプロセツサ93の出力信号にしたがつて出力回路96
でインジエクタ6を駆動するようにしている。
Pre-set the control procedure and data of this microprocessor 93.
It is stored in the ROM 94, and the data in the calculation process is temporarily stored in the RAM 95. Then, according to the output signal of the microprocessor 93, the output circuit 96
It is designed to drive the Injector 6.

上記第1図中の空燃比センサ8は第4図に示すように
構成されており、81は酸素ポンプセル、82は酸素電池セ
ル、83aおよび83bは多孔質でできた電極、84は拡散室、
85は基準電圧源、86は比較増幅器、87はポンプ駆動回
路、88はポンプの電流を検出するための抵抗である。こ
の空燃比センサ8の構成は既に公知(特開昭59−190646
号公報および特開昭60−128349号公報)のものであり、
基準電圧源85を約0.4Vに設定し、この電圧と酸素電池セ
ル82の電圧を比較増幅器86にて比較し、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つて、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。
The air-fuel ratio sensor 8 in FIG. 1 is configured as shown in FIG. 4, 81 is an oxygen pump cell, 82 is an oxygen battery cell, 83a and 83b are electrodes made of a porous material, 84 is a diffusion chamber,
Reference numeral 85 is a reference voltage source, 86 is a comparison amplifier, 87 is a pump drive circuit, and 88 is a resistor for detecting the current of the pump. The construction of the air-fuel ratio sensor 8 is already known (Japanese Patent Laid-Open No. 59-190646).
And Japanese Patent Laid-Open No. 60-128349).
The reference voltage source 85 is set to about 0.4 V, this voltage is compared with the voltage of the oxygen battery cell 82 by the comparison amplifier 86, and the oxygen pump cell 81 is set via the pump drive circuit 87 so that the deviation becomes zero.
By flowing an electric current into the exhaust gas, the exhaust gas in the diffusion chamber 84 is caused to act so as to have a stoichiometric air-fuel ratio.

このような原理を用いて理論空燃比よりもリーン,リ
ツチ側とも検出可能であり、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5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。
Using such a principle, it is possible to detect both the lean side and the rich side of the theoretical air-fuel ratio, and the measurement results can be taken out as the voltage across the resistor 88. As shown in FIG. It is possible to obtain a linear output voltage with respect to.

次に、上記空燃比センサ8を用いた空燃比フイードバ
ツクの従来の制御方法について第6図にしたがつて説明
する。この第6図は第1図に示す制御装置9の制御手順
をフローチヤートで表わしたものである。
Next, a conventional method for controlling the air-fuel ratio feedback using the air-fuel ratio sensor 8 will be described with reference to FIG. FIG. 6 is a flow chart showing the control procedure of the controller 9 shown in FIG.

ステツプ100で回転センサ5から入力されるパルス信
号、すなわちエンジン回転数Neを読み込み、ステツプ10
1で圧力センサ4から得られた吸気管内圧力(絶体圧
力)の値Pbを読み込み、ステツプ102では、ステツプ100
および101で読み込まれた情報を基に空燃比オープンル
ープ制御の目標空燃比を定めるエンリツチ補正係数KER
を設定する。
In step 100, the pulse signal input from the rotation sensor 5, that is, the engine speed Ne is read, and in step 10
In step 1, the value Pb of the intake pipe internal pressure (absolute pressure) obtained from the pressure sensor 4 is read, and in step 102, step 100
Enrichment correction coefficient K ER that determines the target air-fuel ratio for air-fuel ratio open loop control based on the information read in
To set.

このエンリツチ補正係数KERは吸気圧力Pbとエンジン
回転数Neに対応して定められた、たとえば第7図のよう
な関係となるように設定される。
The entrainment correction coefficient K ER is set so as to have a relationship, for example, as shown in FIG.

ステツプ103では、ステツプ100、101および102で読込
みまたは設定した値を基にインジエクタ6の基本駆動パ
ルス幅τを演算する。
In step 103, the basic drive pulse width τ 0 of the injector 6 is calculated based on the value read or set in steps 100, 101 and 102.

演算式は、τ=K・KER・Pb・ηvで表わされ、K
は定数、ηvは吸気圧力Pbとエンジン回転数Neに対応し
て予め定められた充填効率である。
The arithmetic expression is represented by τ 0 = K · K ER · Pb · ηv, and K
Is a constant, and ηv is a charging efficiency predetermined in correspondence with the intake pressure Pb and the engine speed Ne.

次に、ステツプ104で目標空燃比(A/F)Sが設定され
る。この目標空燃比(A/F)Sはたとえば第8図に示す
ようにエンジン回転数Neと吸気圧力Pbに対応して最適な
動力性能と燃費を得るように予め設定されており、絞り
弁全開近くでは(A/F)S=13となつているが、さらに
エンジンの温度や加減速状態などによつて変化されても
よい。
Next, at step 104, the target air-fuel ratio (A / F) S is set. This target air-fuel ratio (A / F) S is preset so as to obtain optimum power performance and fuel efficiency corresponding to the engine speed Ne and the intake pressure Pb, as shown in FIG. In the vicinity, (A / F) S = 13, but it may be changed depending on the temperature of the engine and the acceleration / deceleration state.

ステツプ105では、空燃比センサ8の出力信号(A/F)
Rを読み込み、ステツプ106で空燃比の偏差eを、 e=(A/F)S−(A/F)R で求め、この値を適当なゲインKIを積分し、空燃比フイ
ードバツク補正係数CFBを算出する。
At step 105, the output signal (A / F) of the air-fuel ratio sensor 8
R is read and the deviation e of the air-fuel ratio is obtained by step 106, e = (A / F) S- (A / F) R, and this value is integrated with an appropriate gain K I to obtain the air-fuel ratio feedback correction coefficient C Calculate FB .

次に、ステツプ107で噴射パルス幅τをステツプ103で
先に求めた基本噴射パルス幅τに上記空燃比フイード
バツク補正係数CFBを乗算することにより求める。
Next, in step 107, the injection pulse width τ is obtained by multiplying the basic injection pulse width τ 0 previously obtained in step 103 by the air-fuel ratio feedback back correction coefficient C FB .

以上の動作が繰り返されて空燃比は目標値(A/F)S
になるようにフイードバツク制御される。
The above operation is repeated and the air-fuel ratio becomes the target value (A / F) S
Feedback control is performed so that.

〔発明が解決しようとする問題点〕[Problems to be solved by the invention]

上記のような従来の内燃機関の空燃比制御装置にあつ
ては、機関が絞り弁全開の運転領域において、空燃比フ
イードバツクを行つた場合、空燃比オープンループ制御
の目標空燃比の補正係数KERが、たとえば、1.3となり、
燃料増量の動作を行い、かつ空燃比フイードバツク制御
の目標空燃比がリツチ((A/F)S=13)であるので、
オープンおよびフイードバツク制御がともに燃料増量を
行い、特に機関全開加速時に空燃比がオーバリツチとな
り失火を発生し機関の不調を招来し、運転フイーリング
が悪化する問題があつた。
In the conventional air-fuel ratio control device for an internal combustion engine as described above, when the engine performs air-fuel ratio feedback in the operating region where the throttle valve is fully opened, the correction coefficient K ER for the target air-fuel ratio of the air-fuel ratio open loop control is set. Becomes 1.3,
Since the fuel increase operation is performed and the target air-fuel ratio of the air-fuel ratio feedback control is the latch ((A / F) S = 13),
Both open and feedback control increase the fuel amount, and especially when the engine is fully opened, the air-fuel ratio becomes over-lit and misfire occurs, which causes engine malfunction and deteriorates driving feeling.

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、機関全開状態においても、過度の燃料増量による
機関不調を回避し、いかなる運転条件においても所望の
空燃比を維持制御して常に良効な運転フイーリングを得
ることが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。
The present invention has been made to solve the above problems, and avoids engine malfunction due to excessive fuel increase even when the engine is fully open, and maintains a desired air-fuel ratio under any operating condition to always achieve good results. It is an object of the present invention to obtain an air-fuel ratio control device for an internal combustion engine, which can obtain various operating feelings.

〔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制御装置は、空燃比
フイードバツク制御を行う場合、エンリッチ補正係数を
1.0とし、目標空燃比と実空燃比との偏差に基づいてフ
イードバック補正係数を演算し、このエンリッチ補正係
数およびフイードバック補正係数を用いて噴射パルス幅
を演算して、空燃比オープンループ側の目標空燃比を理
論空燃比に制御する手段を設けたものである。
The air-fuel ratio control device for an internal combustion engine according to the present invention, when performing air-fuel ratio feedback control, sets the enrichment correction coefficient to
1.0, the feedback correction coefficient is calculated based on the deviation between the target air-fuel ratio and the actual air-fuel ratio, and the injection pulse width is calculated using this enrichment correction coefficient and the feedback correction coefficient to determine the target air-fuel ratio on the open-loop side. A means for controlling the fuel ratio to the stoichiometric air-fuel ratio is provided.

〔作 用〕[Work]

この発明においては、空燃比フイードバツク制御する
場合エンリツチ補正係数KERを1.0にして、機関の空燃比
を目標空燃比にフイードバツク制御する。
In the present invention, in the air-fuel ratio feedback control, the engine correction coefficient K ER is set to 1.0, and the air-fuel ratio of the engine is controlled to the target air-fuel ratio.

〔実施例〕〔Example〕

以下、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が、この発明の構成は前
述の第1図のものと全く同一であるが、制御装置9内の
マイクロプロセツサ93を中心とする演算部における演算
処理およびデータ設定の方法が従来装置とは異なり、そ
の演算手順は第2図のフローチヤートに示されている。
An embodiment of an air-fuel ratio control system for an internal combustion engine of the present invention will be described below with reference to the drawings. Although the configuration of the present invention is exactly the same as that of FIG. The calculation processing and data setting method in the calculation unit centering on 93 is different from the conventional apparatus, and the calculation procedure is shown in the flow chart of FIG.

この第2図のフローチヤートのステツプ200のエンジ
ン回転数Ne読込みからステツプ201の吸気圧力Pb読込み
までは従来例を示した第6図のフローチヤートのステツ
プ101から102までと同様なので説明を省略する。
The process from reading the engine speed Ne of the flow chart step 200 of FIG. 2 to reading of the intake pressure Pb of step 201 is the same as the flow chart steps 101 to 102 of FIG. .

ステツプ202において、空燃比フイードバツクするか
どうかを判定する。この判定基準は吸気圧力Pbとエンジ
ン回転数Neと機関冷却水温および機関始動後経過時間に
よつて予め定められている。
At step 202, it is judged whether or not the air-fuel ratio feedback is performed. This criterion is predetermined based on the intake pressure Pb, the engine speed Ne, the engine cooling water temperature, and the elapsed time after engine start.

ステツプ202で空燃比フイードバツクを行うと判定さ
れれば、ステツプ203へ進み、空燃比フイードバツクを
行わないと判定されれば、ステツプ207を実行する。
If it is determined in step 202 that the air-fuel ratio feedback is to be performed, the process proceeds to step 203, and if it is determined that the air-fuel ratio feedback is not to be performed, step 207 is executed.

空燃比フイードバツクを実行すると判定された場合は
ステツプ203において空燃比オープンループ側の目標空
燃比を設定するエンリツチ補正係数(KER)を例えば第
3図に示すような関係を満すように1.0一定にする。
If it is determined that the air-fuel ratio feedback is to be executed, in step 203 the enrichment correction coefficient (K ER ) that sets the target air-fuel ratio on the air-fuel ratio open loop side is set to 1.0 constant to satisfy the relationship shown in FIG. 3, for example. To

次に、ステツプ204で機関回転数Neと吸気圧力Pbに対
応して最適な動力性能と燃費を得るように予め設定され
た、たとえば第8図に示すような関係を満すように、目
標空燃比(A/F)Sの設定を行う。
Next, in step 204, the target air gap is set so as to satisfy the relationship preset in order to obtain the optimum power performance and fuel efficiency corresponding to the engine speed Ne and the intake pressure Pb, for example, as shown in FIG. Set the fuel ratio (A / F) S.

ステツプ205では空燃比センサ8の出力信号(A/F)R
を読み込み、ステツプ206で空燃比偏差e=(A/F)S−
(A/F)Rを求め、この値を適当なゲインで積分してフ
イードバツク係数CFBを算出する。
At step 205, the output signal (A / F) R of the air-fuel ratio sensor 8
Reading, and at step 206, the air-fuel ratio deviation e = (A / F) S-
(A / F) R is obtained, and this value is integrated with an appropriate gain to calculate the feed back coefficient C FB .

一方、ステツプ202で空燃比フイードバツクを実行し
ないと判定された場合は、ステツプ207においてエンリ
ツチ補正係数(KER)を機関回転数Neと吸気圧力Pbに対
応して、たとえば第7図のような関係となるように定め
る。次に、ステツプ208において、空燃比フイードバツ
ク係数CFBを1.0とする。
On the other hand, when it is determined in step 202 that the air-fuel ratio feedback is not executed, in step 207, the entrainment correction coefficient (K ER ) is set in correspondence with the engine speed Ne and the intake pressure Pb, for example, as shown in FIG. To be Next, at step 208, the air-fuel ratio feedback coefficient C FB is set to 1.0.

ステツプ203および206またはステツプ207および208で
定めたエンリツチ係数KERおよびフイードバツク補正係
数CFBを用いて噴射パルス幅τを演算する。この演算式
は、 τ=K×KER×CFB×Pb×ηv で表わされ、Kは定数、ηvは充填効率である。
The injection pulse width τ is calculated using the en-rich coefficient K ER and the feed back correction coefficient C FB determined in steps 203 and 206 or steps 207 and 208. This arithmetic expression is expressed by τ = K × K ER × C FB × Pb × ηv, where K is a constant and ηv is a packing efficiency.

以上の動作を繰り返すことによつて、空燃比偏差が零
になるように空燃比が制御される。
By repeating the above operation, the air-fuel ratio is controlled so that the air-fuel ratio deviation becomes zero.

また、上記実施例では、ステツプ206でフイードバツ
ク補正係数CFBを算出する際、CFBの値に制限を加えなか
つたが、たとえば、CFB1.3の関係を満すように上・
下限の制限を付加してもよい。
Further, in the above embodiment, when calculating the feedback back correction coefficient C FB in step 206, the value of C FB was not limited, but, for example, the upper limit should be set so that the relationship of C FB 1.3 is satisfied.
A lower limit may be added.

さらに、上記実施例の説明においては、燃料噴射シス
テムとしてスピードデンシテイ方式の燃料噴射装置の具
体例としたが、エアーフローセンサを用いた燃料噴射装
置や電子制御気化器にも適用できるのは云うまでもな
い。
Furthermore, in the description of the above embodiments, the fuel injection system is a specific example of a fuel injection device of the speed density type, but it can be said that the present invention is also applicable to a fuel injection device using an air flow sensor and an electronically controlled carburetor. There is no end.

〔発明の効果〕〔The invention's effect〕

この発明は以上説明したとおり、空燃比フイードバツ
ク制御を行う際にオープンループ制御の目標空燃比を理
論空燃比に制御するように空燃比制御装置を構成したの
で、機関全開加速時等において空燃比フイードバツク制
御と従来の空燃比オープンループ制御の干渉を無くすこ
とができ、空燃比がオーバリツチになり失火を招来せず
安価に良効な運転フイーリングを得ることができる。
As described above, according to the present invention, the air-fuel ratio control device is configured to control the target air-fuel ratio of the open-loop control to the stoichiometric air-fuel ratio when performing the air-fuel ratio feedback control. It is possible to eliminate the interference between the control and the conventional air-fuel ratio open loop control, and it is possible to obtain a good operating feeling at low cost without causing misfiring due to the air-fuel ratio becoming overlit.

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

第1図はこの発明および従来装置の内燃機関の空燃比制
御装置の構成を示す図、第2図はこの発明の内燃機関の
空燃比制御装置の動作を表わすフローチヤート、第3図
はこの発明の内燃機関の空燃比制御装置における空燃比
オープンループ制御のエンリツチ補正係数の特性図、第
4図はこの発明および従来の内燃機関の空燃比制御装置
における空燃比センサの構成を示す図、第5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空燃
比センサの特性図、第6図は従来の内燃機関の空燃比制
御装置の動作を表わしたフローチヤート、第7図および
第8図はそれぞれ従来およびこの発明の内燃機関の空燃
比制御装置におけるエンジン回転数対吸気圧力の関係を
示す図である。 1……内燃機関、2……吸気管、4……圧力センサ、5
……回転センサ、6……インジエクタ、8……空燃比セ
ンサ、9……制御装置、81……酸素ポンプセル、82……
酸素電池セル、93……マイクロプロセツサ、94……RO
M、95……RAM。
FIG. 1 is a diagram showing the construction of an air-fuel ratio control device for an internal combustion engine of the present invention and a conventional device, FIG. 2 is a flow chart showing the operation of the air-fuel ratio control device for an internal combustion engine of the present invention, and FIG. 3 is this invention. FIG. 4 is a characteristic diagram of an enrichment correction coefficient of air-fuel ratio open loop control in the air-fuel ratio control device for an internal combustion engine, FIG. 4 is a diagram showing a configuration of an air-fuel ratio sensor in the air-fuel ratio control device for an internal combustion engine according to the present invention, and FIG. FIG. 6 is a characteristic diagram of an air-fuel ratio sensor in an air-fuel ratio control system for an internal combustion engine according to the present invention. FIG. 6 is a flow chart showing the operation of an air-fuel ratio control system for a conventional internal combustion engine. FIG. 3 is a diagram showing a relationship between an engine speed and an intake pressure in an air-fuel ratio control device for an internal combustion engine according to the related art and the present invention, respectively. 1 ... Internal combustion engine, 2 ... Intake pipe, 4 ... Pressure sensor, 5
...... Rotation sensor, 6 …… Injector, 8 …… Air-fuel ratio sensor, 9 …… Control device, 81 …… Oxygen pump cell, 82 ……
Oxygen battery cell, 93 …… Microprocessor, 94 …… RO
M, 95 ... RAM.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 綿谷 晴司 兵庫県姫路市千代田町840番地 三菱電機 株式会社姫路製作所内 (56)参考文献 特開 昭62−182457(JP,A) ─────────────────────────────────────────────────── ─── Continuation of front page (72) Inventor Haruji Wataya 840 Chiyoda-cho, Himeji City, Hyogo Prefecture Mitsubishi Electric Co., Ltd. Himeji Works (56) References JP 62-182457 (JP, A)

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】内燃機関の排ガス成分からリッチ側および
リーン側の空燃比が検出可能な空燃比センサと、この空
燃比センサの出力信号と目標空燃比とが一致するように
空燃比をフイードバック制御する空燃比の制御手段とを
備えた内燃機関において、空燃比フイードバック制御を
行う場合、エンリッチ補正係数を1.0として定めた目標
空燃比と空燃比センサから得た実空燃比との偏差に基づ
いてフイードバック補正係数を演算し、このエンリッチ
補正係数およびフイードバック補正係数を用いて噴射パ
ルス幅を演算して、空燃比オープンループ側の目標空燃
比を理論空燃比とするように制御する手段を備えたこと
を特徴とする内燃機関の空燃比制御装置。
1. An air-fuel ratio sensor capable of detecting the rich-side and lean-side air-fuel ratios from an exhaust gas component of an internal combustion engine, and a feedback control of the air-fuel ratio so that an output signal of the air-fuel ratio sensor and a target air-fuel ratio match. When performing air-fuel ratio feedback control in an internal combustion engine equipped with an air-fuel ratio control means, the feedback based on the deviation between the target air-fuel ratio set as the enrichment correction coefficient of 1.0 and the actual air-fuel ratio obtained from the air-fuel ratio sensor. A means for calculating a correction coefficient, calculating an injection pulse width using the enrichment correction coefficient and the feedback correction coefficient, and controlling the target air-fuel ratio on the air-fuel ratio open loop side to be the theoretical air-fuel ratio is provided. An air-fuel ratio control device for an internal combustion engine, which is characterized.
JP61240697A 1986-10-08 1986-10-08 Air-fuel ratio control device for internal combustion engine Expired - Lifetime JPH089975B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61240697A JPH089975B2 (en) 1986-10-08 1986-10-08 Air-fuel ratio control device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61240697A JPH089975B2 (en) 1986-10-08 1986-10-08 Air-fuel ratio control device for internal combustion engine

Publications (2)

Publication Number Publication Date
JPS6394050A JPS6394050A (en) 1988-04-25
JPH089975B2 true JPH089975B2 (en) 1996-01-31

Family

ID=17063354

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61240697A Expired - Lifetime JPH089975B2 (en) 1986-10-08 1986-10-08 Air-fuel ratio control device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPH089975B2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0658080B2 (en) * 1986-02-04 1994-08-03 トヨタ自動車株式会社 Air-fuel ratio control method for internal combustion engine

Also Published As

Publication number Publication date
JPS6394050A (en) 1988-04-25

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