JPS62247148A - Abnormality detector for air-fuel ratio sensor - Google Patents
Abnormality detector for air-fuel ratio sensorInfo
- Publication number
- JPS62247148A JPS62247148A JP9092386A JP9092386A JPS62247148A JP S62247148 A JPS62247148 A JP S62247148A JP 9092386 A JP9092386 A JP 9092386A JP 9092386 A JP9092386 A JP 9092386A JP S62247148 A JPS62247148 A JP S62247148A
- Authority
- JP
- Japan
- Prior art keywords
- fuel ratio
- air
- sensor
- ratio sensor
- fuel
- 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
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 69
- 230000005856 abnormality Effects 0.000 title claims description 11
- 238000001514 detection method Methods 0.000 claims abstract description 14
- 230000002159 abnormal effect Effects 0.000 claims abstract description 6
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 238000002347 injection Methods 0.000 abstract description 10
- 239000007924 injection Substances 0.000 abstract description 10
- 238000004364 calculation method Methods 0.000 abstract description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 6
- 230000006866 deterioration Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 3
- 230000004043 responsiveness Effects 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
Landscapes
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
この発明は空燃比センサの応答性劣化などの異常を検知
する空燃比センナの異常検知装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to an abnormality detection device for an air-fuel ratio sensor that detects abnormalities such as deterioration in responsiveness of the air-fuel ratio sensor.
第1図は一般的な内燃機関の制御装置の構成を示す図で
ある。この第1因において、1はエンジン、2および3
はエンジン1に混合気を導入する吸気管、4は吸気管2
に配設され燃料の供給を行うインジェクタ、5は吸気管
2および30間に位置し、運転者の意志によって開閉さ
れる絞り弁、6はこの絞り弁5下流の吸気管3内圧力を
検出する圧力センサ%7はエンジン1の回転に比例して
パルスを発生する回転センサ、8はエンジン1の冷却水
温Kt検出する水温センサ、9はエンジン1の排気管1
0に配設され、排出ガス成分がら空燃比を検出する空燃
比センサとしての02センサ、11は上記各センサの出
力に基づいて演算処理を行いインジェクタ4t−制御す
る制御装置である。FIG. 1 is a diagram showing the configuration of a general control device for an internal combustion engine. In this first factor, 1 is the engine, 2 and 3
4 is the intake pipe that introduces the air-fuel mixture into the engine 1, and 4 is the intake pipe 2.
5 is located between the intake pipes 2 and 30 and is opened or closed according to the will of the driver; 6 detects the pressure inside the intake pipe 3 downstream of the throttle valve 5; Pressure sensor %7 is a rotation sensor that generates a pulse in proportion to the rotation of the engine 1, 8 is a water temperature sensor that detects the cooling water temperature Kt of the engine 1, and 9 is the exhaust pipe 1 of the engine 1.
A 02 sensor is disposed at 0 and serves as an air-fuel ratio sensor for detecting the air-fuel ratio from exhaust gas components, and 11 is a control device that performs arithmetic processing based on the outputs of the above-mentioned sensors and controls the injector 4t.
t*111idA/Dコンバータで、圧力センサ6の検
出出力および水温センサ8の検出出力を入力してアナロ
グ信号をディジタル値に変換した後、マイクロプロセッ
サ113に送出するようになっている。112は回転セ
ンサ7のオン/オフ信号および02センサ9の検出信号
を入力する入力回路で、これら信号をマイクロプロセッ
サ113に送出するようになっている。マイクロプロセ
ッサ113はA/Dコンバータ111および入力回路1
12から入力された情報をもとにして、インジェクタ4
の駆動周期や駆動ノ々ルス幅を演算するもので、このマ
イクロプロセッサ113には、演算処理の手順やデータ
(設定値)を記憶しているROMI 15と、演算処理
中のデータを一時的に記憶するRAMI 16とが接続
されている。そしてマイクロプロセッサ113の出力は
出力回路114に送出されてインジェクタ4′ft駆動
するようになっている。The t*111id A/D converter inputs the detection output of the pressure sensor 6 and the detection output of the water temperature sensor 8, converts the analog signal into a digital value, and then sends it to the microprocessor 113. Reference numeral 112 denotes an input circuit that receives the on/off signal of the rotation sensor 7 and the detection signal of the 02 sensor 9, and sends these signals to the microprocessor 113. Microprocessor 113 includes A/D converter 111 and input circuit 1
Based on the information input from 12, injector 4
The microprocessor 113 has a ROMI 15 that stores the calculation processing procedures and data (setting values), and a ROMI 15 that temporarily stores the data during calculation processing. It is connected to RAMI 16 for storage. The output of the microprocessor 113 is sent to an output circuit 114 to drive the injector 4'ft.
このように構成された内燃機関の制御装置は、先ず圧力
センサ61回転センサ7および水温センサ8等の検出信
号すなわちエンジン1の作動パラメータをマイクロプロ
セッサ113が読込み基本燃料噴射漬の演算を行う。そ
して更にOXセンサ9の出力に基づいて演算結果が補正
されて燃料噴射量の演算が行われ、求められた駆動パル
ス幅でインジェクタ4が駆動されエンジン1に対して所
定量の燃料が供給される。In the internal combustion engine control device configured as described above, first, the microprocessor 113 reads the detection signals of the pressure sensor 61, rotation sensor 7, water temperature sensor 8, etc., that is, the operating parameters of the engine 1, and performs a basic fuel injection calculation. Then, the calculation result is further corrected based on the output of the OX sensor 9 to calculate the fuel injection amount, and the injector 4 is driven with the determined drive pulse width to supply a predetermined amount of fuel to the engine 1. .
第2図は上記02センサ9の出力とエンジン1の実際の
空燃比との空燃比フィードバック制御を示す図である。FIG. 2 is a diagram showing air-fuel ratio feedback control between the output of the 02 sensor 9 and the actual air-fuel ratio of the engine 1.
すなわち、0冨センサの出力aがリッチからり一ンに変
化すると補正値Cはこれに対応して増量積分補正が行わ
れ、ま−ttV−ンからリッチに変化すると減量積分補
正が行われて実際の空燃比すは理論空燃比を中心とした
±1〜2%の範囲内で変動し略理論空燃比に近い制御が
行われる。That is, when the output a of the 0-ttV sensor changes from rich to 1, the correction value C is subjected to a corresponding increase integral correction, and when it changes from full to rich, a decrease integral correction is performed. The actual air-fuel ratio varies within a range of ±1 to 2% around the stoichiometric air-fuel ratio, and control is performed close to the stoichiometric air-fuel ratio.
彦お、t4は実空燃比が理論空燃比を横切ってから02
センサ9の出力が反転するまでの時間で、これはエンジ
ン1から排出されたガスがOzセンサ9まで到達する時
間や0冨センサ9の応答時間などによって生じるもので
ある。Hikoo, t4 is 02 after the actual air-fuel ratio crosses the stoichiometric air-fuel ratio.
This is the time it takes for the output of the sensor 9 to reverse, and this is caused by the time it takes for the gas exhausted from the engine 1 to reach the Oz sensor 9, the response time of the zero-limit sensor 9, and the like.
従来の空燃比制御装置は以上のように構成されているが
、長期間の使用によって生じる排ガス中のカーゼンなど
による目づまシや粗悪ガソリンの使用による異物の付着
等で02センサ9の応答性が悪化する問題がある。この
ような場合の空燃比フィードバック制御の様子を示した
のが第3図の波形図である。すなわち、実際の空燃比が
理論空燃比を横切ってがら空燃比センサの出力が反転す
るまでの時間tdが正常時より長くなると、補正値Cの
波形の傾きは制御上で決っており正常時と同じであるた
めその振幅が大きくなる。従って実際の空燃比すは補正
値Cの振幅に応じて大きく変動してしまう。このため三
元触媒の浄化効率が悪くなり排ガスが悪化してしまう等
の問題点があった。Although the conventional air-fuel ratio control device is constructed as described above, the responsiveness of the 02 sensor 9 may deteriorate due to clogging caused by carbon in the exhaust gas caused by long-term use or adhesion of foreign matter due to the use of poor quality gasoline. There is a problem that is getting worse. The waveform diagram in FIG. 3 shows the air-fuel ratio feedback control in such a case. In other words, if the time td until the output of the air-fuel ratio sensor is reversed while the actual air-fuel ratio crosses the stoichiometric air-fuel ratio is longer than normal, the slope of the waveform of the correction value C is determined by control and will be different from normal. Since they are the same, their amplitude increases. Therefore, the actual air-fuel ratio varies greatly depending on the amplitude of the correction value C. For this reason, there were problems such as the purification efficiency of the three-way catalyst deteriorated and the exhaust gas deteriorated.
この発明は上記の問題点を解決するためになされたもの
で、排ガスの悪化を抑制できる空燃比センサの異常検知
装fit−得ることを目的とする。The present invention was made to solve the above problems, and an object of the present invention is to provide an abnormality detection device for an air-fuel ratio sensor that can suppress deterioration of exhaust gas.
この発明に係る空燃比センサの異常検知装置は、内燃機
関の排出ガス成分がら空燃比を検出する空燃比センサと
、この空燃比センサの出力に応じて供給燃料量を補正す
るとともに、この補正値の変動幅が所定値以上かつ所定
時間以上である場合は空燃比センサが異常であると判断
する制御装置とを備えたものである。An abnormality detection device for an air-fuel ratio sensor according to the present invention includes an air-fuel ratio sensor that detects an air-fuel ratio from exhaust gas components of an internal combustion engine, and corrects the amount of supplied fuel according to the output of the air-fuel ratio sensor, and corrects the amount of fuel supplied according to the output of the air-fuel ratio sensor. A control device that determines that the air-fuel ratio sensor is abnormal if the fluctuation range is greater than a predetermined value and for a predetermined time.
この発明においては、空燃比フィードバック制御の補正
値の振幅が所定値を超えてこれが所定時間以上続くと制
御装置は空燃比センサが異常であると判断し、空燃比セ
ンサの交換を促すことができる。In this invention, if the amplitude of the correction value of the air-fuel ratio feedback control exceeds a predetermined value and this continues for a predetermined time or more, the control device can determine that the air-fuel ratio sensor is abnormal and prompt the air-fuel ratio sensor to be replaced. .
〔実施例〕 以下、この発明の一実施例を図面を参照して説明する。〔Example〕 An embodiment of the present invention will be described below with reference to the drawings.
この発明の図面上の構成は第1図に示す装置と同様であ
り、異なるのは制御装置11の制御の内容である、
第4図はこの制御手順金示すフローチャートであり、先
ずステップ201で、圧力センサ61回転センサ7お工
び水温センサ8などの検出出力から、吸気管内圧力1機
関回転数および水温などエンジンの作動パラメータを読
込む。次にステップ202で基本燃料噴射量の演算が行
われる。すなわち回転センサ7から得られるクランク角
信号に同期してインジェクタ4が駆動される回転同期噴
射ノぞルス幅τ1が求められる。そして次にステップ2
03で空燃比センサの出力判別が行われ、ここで出力が
リッチであると燃料減量積分補正CFBIが行われ(ス
テップ204)、出力がリーンであると燃料増i積分補
正CFB2が行われる(ステップ205)。更にステッ
プ206で出力がリッチからり一ンに変化しtか否かを
判別し、変化しt場合はステップ207で補正値Crn
zt記憶してステップ210に進み、変化していない場
合はステップ208に進む。ステップ208では出力が
I)−ンからリッチに変化したか否かを判別し、変化し
た場合はステップ209で補正値Crnxk記憶してス
テップ210に進む。ステップ210では補正値の変動
幅CFB2− CFBIが第3図(c)に示すように所
定値α1例えば理論空燃比に対して±3%以上でかつこ
れが所定時間以上継続しているか否かを判別し、所定値
を超えている場合はステップ211で故障判別結果を記
憶し、更にステップ212で空燃比センサの異常を報知
する警報信号を発生させ、ステップ213で基本燃料噴
射量演算結果を補正値CFBで補正し燃料噴射量すなわ
ち噴射パルス幅τ2の演算を行う。またステップ208
で出力がリーンからリッチに変化しない場合およびステ
ップ210で補正値の変動幅が所定値を超えない場合は
ステップ213に進み燃料噴射量の演算を行う。なお、
Cr2− CFBI >αが所定時間以上継続した場合
に故障判別するようにしたのは、加減速時など変動幅が
過渡的に大きくなることは有り得るので%時限を設けて
誤動作を防止するためである。The configuration of this invention in the drawings is the same as the device shown in FIG. 1, and the difference is the content of control by the control device 11. FIG. 4 is a flowchart showing this control procedure. First, in step 201, Engine operating parameters such as intake pipe internal pressure, engine speed, and water temperature are read from the detection outputs of the pressure sensor 61, rotation sensor 7, and water temperature sensor 8. Next, in step 202, a basic fuel injection amount is calculated. That is, the rotation-synchronized injection nozzle width τ1 in which the injector 4 is driven in synchronization with the crank angle signal obtained from the rotation sensor 7 is determined. And then step 2
In step 03, the output of the air-fuel ratio sensor is determined, and if the output is rich, a fuel decrease integral correction CFBI is performed (step 204), and if the output is lean, a fuel increase i integral correction CFB2 is performed (step 204). 205). Further, in step 206, it is determined whether the output changes from rich to rich to t, and if the output changes to t, then in step 207, the correction value Crn is set.
zt is stored and the process proceeds to step 210, and if it has not changed, the process proceeds to step 208. In step 208, it is determined whether or not the output has changed from I) to rich. If it has changed, the correction value Crnxk is stored in step 209, and the process proceeds to step 210. In step 210, it is determined whether the variation range CFB2-CFBI of the correction value is greater than or equal to a predetermined value α1, for example, ±3% of the stoichiometric air-fuel ratio, as shown in FIG. 3(c), and whether this continues for a predetermined time or longer. However, if it exceeds a predetermined value, the failure determination result is stored in step 211, an alarm signal is generated to notify an abnormality of the air-fuel ratio sensor in step 212, and the basic fuel injection amount calculation result is converted to a correction value in step 213. The fuel injection amount, that is, the injection pulse width τ2 is calculated by correcting it using CFB. Also step 208
If the output does not change from lean to rich in step 210, and if the fluctuation range of the correction value does not exceed a predetermined value in step 210, the process proceeds to step 213, where the fuel injection amount is calculated. In addition,
The reason why a failure is determined when Cr2-CFBI > α continues for a predetermined period of time is to prevent malfunction by setting a % time limit, since it is possible that the fluctuation range becomes large transiently, such as during acceleration/deceleration. .
また、上記実施例では空燃比センサの異常検知装置とし
て空燃比フィードバック制御燃料噴射装置を例にとって
説明したが、これに限定されるものではなくフィードバ
ック制御気化器を用いたものであっても上記実施例と同
様の効果を奏する。Further, in the above embodiment, the air-fuel ratio feedback control fuel injection device was explained as an example of the abnormality detection device of the air-fuel ratio sensor, but the above embodiment is not limited to this, and even if a feedback control carburetor is used. It has the same effect as the example.
以上のようにこの発明によれば、空燃比フィードバック
制御の補正値の変動幅が所定値を超えかつ所定時間以上
継続すると空燃比センサが異常であると判別するよう構
成したので、空燃比センサの交換を促すことができ、従
って排ガスの悪化を抑制することができる効果がある。As described above, according to the present invention, the air-fuel ratio sensor is determined to be abnormal if the fluctuation range of the correction value of the air-fuel ratio feedback control exceeds a predetermined value and continues for a predetermined time or more. This has the effect of encouraging replacement and therefore suppressing deterioration of exhaust gas.
fa1図はこの発明に係る内燃機関の制御装置の構成図
、第2図は正常時の空燃比フィードバック制御を示す動
作波形図、第3図は空燃比センサの応答性が悪化した場
合の空燃比フィードバック制御を示す動作波形図、第4
図はこの発明の一実施例による空燃比センサの異常検知
装置の動作を示すフローチャートである。
1・・・エンジン、9・・・空燃比センサ、11・・・
制御装置。Fig. fa1 is a configuration diagram of the control device for an internal combustion engine according to the present invention, Fig. 2 is an operation waveform diagram showing air-fuel ratio feedback control under normal conditions, and Fig. 3 shows the air-fuel ratio when the responsiveness of the air-fuel ratio sensor deteriorates. Operation waveform diagram showing feedback control, 4th
The figure is a flowchart showing the operation of an abnormality detection device for an air-fuel ratio sensor according to an embodiment of the present invention. 1... Engine, 9... Air-fuel ratio sensor, 11...
Control device.
Claims (3)
ッチに応じた出力を発生する空燃比センサと、この空燃
比センサの出力に応じて前記内燃機関への供給燃料量を
補正し理論空燃比にフィードバック制御するとともに、
前記補正値の変動幅が予め設定した所定値を超えかつこ
れが所定時間以上である場合は前記空燃比センサが異常
であると判断する制御装置とを備えたことを特徴とする
空燃比センサの異常検知装置。(1) An air-fuel ratio sensor that generates an output according to lean or rich air-fuel ratio from the exhaust gas components of the internal combustion engine, and an air-fuel ratio sensor that corrects the amount of fuel supplied to the internal combustion engine according to the output of this air-fuel ratio sensor, and In addition to feedback control of the fuel ratio,
and a control device that determines that the air-fuel ratio sensor is abnormal if the fluctuation range of the correction value exceeds a predetermined value and exceeds a predetermined time. Detection device.
を発生させることを特徴とする特許請求の範囲第1項記
載の空燃比センサの異常検知装置。(2) The abnormality detection device for an air-fuel ratio sensor according to claim 1, wherein the control device generates an alarm signal when determining an abnormality in the air-fuel ratio sensor.
であることを特徴とする特許請求の範囲第1項または第
2項に記載の空燃比センサの異常検知装置。(3) The preset value is ±3% of the stoichiometric air-fuel ratio.
An abnormality detection device for an air-fuel ratio sensor according to claim 1 or 2, characterized in that:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9092386A JPS62247148A (en) | 1986-04-18 | 1986-04-18 | Abnormality detector for air-fuel ratio sensor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9092386A JPS62247148A (en) | 1986-04-18 | 1986-04-18 | Abnormality detector for air-fuel ratio sensor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS62247148A true JPS62247148A (en) | 1987-10-28 |
Family
ID=14011947
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9092386A Pending JPS62247148A (en) | 1986-04-18 | 1986-04-18 | Abnormality detector for air-fuel ratio sensor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS62247148A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4947818A (en) * | 1988-04-28 | 1990-08-14 | Toyota Jidosha Kabushiki Kaisha | Internal combustion engine with device for warning of malfunction in an air-fuel ratio control system |
US5901691A (en) * | 1996-08-09 | 1999-05-11 | Toyota Jidosha Kabushiki Kaisha | Device for determining deterioration of air-fuel ratio sensor |
-
1986
- 1986-04-18 JP JP9092386A patent/JPS62247148A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4947818A (en) * | 1988-04-28 | 1990-08-14 | Toyota Jidosha Kabushiki Kaisha | Internal combustion engine with device for warning of malfunction in an air-fuel ratio control system |
US5901691A (en) * | 1996-08-09 | 1999-05-11 | Toyota Jidosha Kabushiki Kaisha | Device for determining deterioration of air-fuel ratio sensor |
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