JPS6027754A - Air-fuel ratio controlling apparatus for engine - Google Patents
Air-fuel ratio controlling apparatus for engineInfo
- Publication number
- JPS6027754A JPS6027754A JP58137115A JP13711583A JPS6027754A JP S6027754 A JPS6027754 A JP S6027754A JP 58137115 A JP58137115 A JP 58137115A JP 13711583 A JP13711583 A JP 13711583A JP S6027754 A JPS6027754 A JP S6027754A
- Authority
- JP
- Japan
- Prior art keywords
- fuel ratio
- air
- engine
- sensor
- oxygen
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N27/00—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means
- G01N27/26—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating electrochemical variables; by using electrolysis or electrophoresis
- G01N27/416—Systems
- G01N27/417—Systems using cells, i.e. more than one cell and probes with solid electrolytes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1473—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the regulation method
- F02D41/1475—Regulating the air fuel ratio at a value other than stoichiometry
- F02D41/1476—Biasing of the sensor
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N27/00—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means
- G01N27/26—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating electrochemical variables; by using electrolysis or electrophoresis
- G01N27/403—Cells and electrode assemblies
- G01N27/406—Cells and probes with solid electrolytes
- G01N27/4065—Circuit arrangements specially adapted therefor
Landscapes
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Biochemistry (AREA)
- Immunology (AREA)
- Physics & Mathematics (AREA)
- Analytical Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Electrochemistry (AREA)
- Pathology (AREA)
- Molecular Biology (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
【発明の詳細な説明】
この発明は、内燃機関等の排気ガス中の酸素濃度を測定
して空燃比を制御する装置に関するものであシ、特にイ
オン伝導性固体電解質で構成された酸素ポンプ式の空燃
比センサを用いfc機関の空燃比制御装置に関するもの
である。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a device for controlling an air-fuel ratio by measuring the oxygen concentration in exhaust gas of an internal combustion engine, etc., and particularly relates to an oxygen pump type device made of an ion-conducting solid electrolyte. This invention relates to an air-fuel ratio control device for an FC engine using an air-fuel ratio sensor.
従来、イオン伝導性固体電解質(例えば安定化ジルコニ
ア〕で構成された酸素センナを用い、排気ガスの酸素分
圧と空気の酸素分圧との差によって生じる起電力の変化
によって理論空燃比での燃焼状態を検知することにより
、例えば自動車の機関を理論空燃比で運転するように制
御することは衆知の通りである。ところで、上記酸素セ
ンサは空気と燃料との重量比率である空燃比(A/F)
が理論空燃比(A/F )T = 14.7である時は
大き々変化出力が得られるが、他の運転空燃比域では出
力変化かはとんどなく、理論空燃比(v’) T以外の
空燃比で機関全運転する場合には、上記酸素センサの出
力を利用することが出来ない。Conventionally, an oxygen sensor composed of an ion-conducting solid electrolyte (e.g. stabilized zirconia) is used to achieve combustion at the stoichiometric air-fuel ratio by changing the electromotive force caused by the difference between the oxygen partial pressure of the exhaust gas and the oxygen partial pressure of the air. It is well known that, for example, an automobile engine is controlled to operate at a stoichiometric air-fuel ratio by detecting the state.By the way, the above-mentioned oxygen sensor detects the air-fuel ratio (A/ F)
When the stoichiometric air-fuel ratio (A/F) is T = 14.7, a large change in output can be obtained, but in other operating air-fuel ratio ranges, the output changes very little and the stoichiometric air-fuel ratio (v') When the engine is fully operated at an air-fuel ratio other than T, the output of the oxygen sensor cannot be used.
しかし、特開昭56−130649号で提案されている
ような固体電解質要素ポンプ式の酸素濃度測定装置?用
いることにより、理論空燃比(A/F )T以外の空燃
比(A/F) kも検知することが出来る空燃比センサ
が先に発明された。However, an oxygen concentration measuring device using a solid electrolyte element pump as proposed in JP-A-56-130649? An air-fuel ratio sensor was previously invented which can detect an air-fuel ratio (A/F)k other than the stoichiometric air-fuel ratio (A/F)T.
第1図はこの空燃比センサの一実施例金示す構成図であ
る。FIG. 1 is a block diagram showing one embodiment of this air-fuel ratio sensor.
図において、lは機関の排気管、2は上記排気管1内に
配設された空燃比センサである。空燃比センサ2は厚さ
が約0.5 vanの平板状のイオン伝導性固体電解質
(安定化ジルコニア)3の両側面にそれぞれ白金電極4
,5を設けて構成された固体電解質酸素ボンゾロと、こ
の酸素ポンプ6と同じように平板状のイオン伝導性固体
電解質7の両側面にそれぞれ白金電極8および9を設け
て構成された固体電解質酸素上ンサ10と、上記酸素ポ
ンゾロと上記酸素センサ10’i0.1m程度の微小間
隙d’t−介して対向配置するための支持台11で構成
されている。12は電子制御装置であり、上記酸素セン
サ10が電極8,9間に発生する起電力ef抵抗Rte
介して演算増幅器Aの反転入力端子(ハ)に印加し、一
方、その非反転入力端子(ト)に印加されている基準電
圧V1と上記起電力eの差異に比例した上記演算増幅器
Aの出力によりトランジスタTRを駆動して上記酸素ポ
ンゾロの電極4,5に流すポンプ電流Ipt−制御する
機能を備えている。In the figure, 1 is an exhaust pipe of the engine, and 2 is an air-fuel ratio sensor disposed within the exhaust pipe 1. The air-fuel ratio sensor 2 has platinum electrodes 4 on both sides of a flat ion-conductive solid electrolyte (stabilized zirconia) 3 with a thickness of about 0.5 van.
. It consists of an upper sensor 10, and a support stand 11 for disposing the oxygen sensor 10' and the oxygen sensor 10'i facing each other with a minute gap d't- of about 0.1 m interposed therebetween. Reference numeral 12 denotes an electronic control unit, which controls the electromotive force ef resistance Rte generated between the electrodes 8 and 9 by the oxygen sensor 10.
The output of the operational amplifier A is proportional to the difference between the electromotive force e and the reference voltage V1 applied to the inverting input terminal (c) of the operational amplifier A through the inverting input terminal (c), while being applied to the non-inverting input terminal (g) of the operational amplifier A. It has a function of driving the transistor TR to control the pump current Ipt flowing through the electrodes 4 and 5 of the oxygen pump.
すなわち、該電子制御装置12は上記起電力ef上記基
準電圧である所定値■工に保つのに必要な上記ポンプ電
流Ip’にその供給手段である直流電源Bから供給され
るように構成され、また該ボンデ電流IPに対応した出
力信号O8を出力端子01.02の間に得る為の抵抗塩
が備えられている。この抵抗ルは上記直流電源Bと対応
してよ記ヂンゾ電流IPが過大に流れないような所望の
抵抗値が選ばれている。Cはコンデンサ、Sは上記基準
電圧vl、v6金切り換えるための切換装置である。That is, the electronic control unit 12 is configured such that the pump current Ip' necessary to maintain the electromotive force ef at a predetermined value (1), which is the reference voltage, is supplied from the DC power supply B serving as its supply means; Further, a resistive salt is provided between the output terminals 01.02 to obtain an output signal O8 corresponding to the bond current IP. This resistor corresponds to the DC power source B, and has a desired resistance value selected so that the electric current IP does not flow excessively. C is a capacitor, and S is a switching device for switching the reference voltages vl and v6.
以上の構成において、空燃比センサ2の酸素センサ10
社電極8,9間に発生する起電力eを演算増幅器Aに入
力し、これにより上記起電力eと基準電圧vlとの差異
に比例した出力がトランジスターのペースに印加され、
酸素ボンデ6の電極4゜5間に流れるポンプ電流IPは
所定範囲値内に制御され、該ポンプ電流IPに対応した
出力信号O8が出力端子O1,0□より、出力されて後
述の如く1機関のインジェクターを制御して空燃比を変
える制御手段に入力される。In the above configuration, the oxygen sensor 10 of the air-fuel ratio sensor 2
The electromotive force e generated between the electrodes 8 and 9 is input to the operational amplifier A, whereby an output proportional to the difference between the electromotive force e and the reference voltage vl is applied to the transistor pace.
The pump current IP flowing between the electrodes 4° and 5 of the oxygen bonder 6 is controlled within a predetermined range, and an output signal O8 corresponding to the pump current IP is outputted from the output terminals O1 and 0□, and as described later, one engine It is input to a control means that controls the injectors of the air-fuel ratio and changes the air-fuel ratio.
第3図は、上記空燃比センサ2′t−国産乗用車用20
00 cc (Dガソリン機関に装着して試験した結果
を示す空燃比(A/F)とポンプ電流IP特性図である
。Figure 3 shows the air-fuel ratio sensor 2't - 20 for domestic passenger cars.
00 cc (D) This is an air-fuel ratio (A/F) and pump current IP characteristic diagram showing the results of a test installed on a gasoline engine.
すなわち、過大なポンプ電流IPが流れると上記酸素ポ
ンゾロが破壊するので、上記ポンプ電流IPは例えば1
00mA以上流れないように上記直流電源BKより制限
され、基準電圧Vtk 55 mVとした場合には、第
3図に示すグラフaの空燃比/ポンプ電流値性が、また
基準電圧■ik 200 mVとした場合には同図に示
すグラフbの空燃比/ボンデ電流特性がそれぞれ得られ
た。That is, if an excessive pump current IP flows, the oxygen pump will be destroyed, so the pump current IP may be reduced to 1, for example.
If the DC power supply BK is limited so that the flow does not exceed 00 mA, and the reference voltage Vtk is set to 55 mV, the air-fuel ratio/pump current value characteristic shown in graph a shown in Fig. In this case, the air-fuel ratio/Bonde current characteristics shown in graph b shown in the figure were obtained.
上記特性を利用して空燃比(A/F ) ’Ft: 1
2〜19の広い範囲で検知しようとすると+a)の特性
では同じポンプ電流値の空燃比点が2個所存在するので
、上記ポンプ電流値のみで検知することができない。Using the above characteristics, air-fuel ratio (A/F) 'Ft: 1
If an attempt is made to detect in a wide range from 2 to 19, in the characteristic +a) there are two air-fuel ratio points with the same pump current value, so detection cannot be made using only the pump current value.
他方(b)の特性では理論空燃比14.7以下の範囲で
はボンデ電流IPの変化がないのでこの範囲での空燃比
を検知することはできないという欠点があった。On the other hand, the characteristic (b) has a drawback in that the Bonde current IP does not change in the range of the stoichiometric air-fuel ratio of 14.7 or less, so the air-fuel ratio cannot be detected in this range.
この発明は上記の如き従来のものの欠点全除去するため
になされた〜もので、所定値Vl又は■2に維持された
酸素センサ起電力全機関の運転中に所定の周期で任意に
切換え変更し、この切換え前後のボンデ電流に対応した
出力信号によす空燃比を検出する手段を備えた構成によ
り、上記切換え時のボンデ電流の差から上記基準電圧V
lの空燃比/電流ボンデ特性が理論空燃比よジ濃い側に
あるのか。This invention was made in order to eliminate all the drawbacks of the conventional ones as described above, and the oxygen sensor electromotive force is maintained at a predetermined value Vl or (2) and is switched and changed arbitrarily at a predetermined period during the operation of the entire engine. , by means of detecting the air-fuel ratio based on an output signal corresponding to the Bonde current before and after the switching, the reference voltage V is determined from the difference in the Bonde current at the time of the switching.
Is the air-fuel ratio/current bond characteristic of l on the richer side than the stoichiometric air-fuel ratio?
或いは薄い側にあるのかを判定することで1機関の運転
状態に応じて予め設定された空燃比にフイ−ト°バック
制御することが出来る機関の空燃比制御装置を提供する
ことを目的としている。It is an object of the present invention to provide an air-fuel ratio control device for an engine that can perform footback control to a preset air-fuel ratio depending on the operating state of one engine by determining whether the air-fuel ratio is on the lean side or on the lean side. .
以下、この発明の一実施例を図面に従って説明する。An embodiment of the present invention will be described below with reference to the drawings.
第4図はこの発明の一実施例金示す構成図であり1図に
おいて、20は自動車に搭載される公知の4サイクル火
花点火式内燃機関で(以下機関という)、燃焼用空気を
エアクリーナζ2.吸気管21、スロットルバルブ23
を経て吸入、する。また、燃料は上記スロットルバルブ
23の上流側に設ケラれたインジェクター24により制
御され、図示しな(へ燃料系から該インジェクター24
へ燃料が供給される。また、上記スロットルバルブ23
の下流側には上記吸気管21圧力全検出し電圧に変換す
る圧力センサ25が接続されている。水温センサ26は
内燃機関1の冷却水温に対応して抵抗値が変化するサー
ミスタ如きものから成り1回転センサ27は機関20の
回転数に応じた周波数信号全出力する。機関20の排気
管1には前記空燃比センサ2が配設されている。制御装
置30は上記圧力センサ25.水温センサ262回転セ
ンサ27.空燃比センサ2の出力に基づき、インジェク
ター24の駆動時間を制御することにより機関20の空
燃比(A/F) t−制御可能に構成される。FIG. 4 is a block diagram showing one embodiment of the present invention. In FIG. 1, 20 is a known four-stroke spark ignition internal combustion engine (hereinafter referred to as engine) mounted on an automobile, and combustion air is supplied to an air cleaner ζ2. Intake pipe 21, throttle valve 23
After inhalation, do it. Further, the fuel is controlled by an injector 24 installed upstream of the throttle valve 23, and the fuel is supplied from the fuel system to the injector 24 (not shown).
Fuel is supplied to. In addition, the throttle valve 23
A pressure sensor 25 is connected to the downstream side of the intake pipe 21 to detect the entire pressure of the intake pipe 21 and convert it into a voltage. The water temperature sensor 26 is made of something like a thermistor whose resistance value changes in accordance with the temperature of the cooling water of the internal combustion engine 1, and the one revolution sensor 27 outputs a full frequency signal corresponding to the number of revolutions of the engine 20. The air-fuel ratio sensor 2 is disposed in the exhaust pipe 1 of the engine 20. The control device 30 includes the pressure sensor 25. Water temperature sensor 262 Rotation sensor 27. By controlling the drive time of the injector 24 based on the output of the air-fuel ratio sensor 2, the air-fuel ratio (A/F) of the engine 20 can be controlled.
前述した様に、第1図において基準電圧k Vs 。As mentioned above, in FIG. 1, the reference voltage k Vs.
V2とそれぞれに切り換えると、空燃比センサ2のポン
プ電流IPは第3図(a) 、 (b)の如くなり、従
ッて抵抗値鳥の両端の出力端子01,02に発生する出
力O8は第5図の(e) 、 (d)の如くになる。つ
まり、基準電圧’t’VxからV2に切換えた時の抵抗
itoの電圧の差Δ■は空燃比(4/F)が理論空燃比
(Mk’ )T より薄い側の値△■□の方が濃い側の
値△V2よりも数倍も大きい。基準電圧がVlの時の空
燃比(AA’ )に対する抵抗鳥の電圧をVSとし、理
論空燃比(A/F)T近傍で電圧vSがVCIの値にな
るとし、適当に設定するオフセット電圧’i VC2と
し、理論空燃比(八4゛)Tより濃い側では下記の(1
)式で、薄い側では(2)式で抵抗掲の補正電圧vso
’1計算すると、空燃比(A/F )に対する値は第5
図の破i%13i (elの如くなる4、V’80=’
VC2−(Vs−’VC1) ・・・(1)。When switched to V2 and V2 respectively, the pump current IP of the air-fuel ratio sensor 2 becomes as shown in FIG. It will look like (e) and (d) in Figure 5. In other words, the voltage difference Δ■ across the resistor ito when switching from the reference voltage 't'Vx to V2 is the value △■□ where the air-fuel ratio (4/F) is thinner than the stoichiometric air-fuel ratio (Mk')T. is several times larger than the value ΔV2 on the dark side. Let VS be the voltage across the resistor with respect to the air-fuel ratio (AA') when the reference voltage is Vl, and assume that the voltage VS becomes the value of VCI near the stoichiometric air-fuel ratio (A/F) T, and set the offset voltage' appropriately. i VC2, on the side richer than the stoichiometric air-fuel ratio (84゛) T, the following (1
), and on the thin side, the correction voltage vso of the resistance is expressed in equation (2).
'1 calculation, the value for the air-fuel ratio (A/F) is the 5th
Broken diagram i%13i (4 like el, V'80='
VC2-(Vs-'VC1)...(1).
VSO=VC2+(VS−Vel) ・・・(2)従っ
て、補正電圧V81 は制御装置30で計算され、空燃
比センサ2の検出した空燃比(A/F )に対し単調増
加の特性を得て空燃比(A/F)に対し1対1の対応と
なり1機関20の空燃比(A/I”)は所望の如く制御
される。VSO=VC2+(VS-Vel) (2) Therefore, the correction voltage V81 is calculated by the control device 30 and has a monotonically increasing characteristic with respect to the air-fuel ratio (A/F) detected by the air-fuel ratio sensor 2. There is a one-to-one correspondence with the air-fuel ratio (A/F), and the air-fuel ratio (A/I'') of one engine 20 is controlled as desired.
第6図は第5図に示す制御装置30の#g構成図あ91
図において、圧力センサ25はフィルター31で平滑さ
れ、水温センサ26はインタフェース32を介して出力
され、第1図に示す出力信号08は増幅器33で増幅さ
れ、上記各出力はAI)変換器34に入力されてディジ
タル数値に変換された後、これらのディジタルデータは
マイクロコンピュータ38に入力するように構成されて
いる。FIG. 6 is a #g configuration diagram of the control device 30 shown in FIG. 5.
In the figure, the pressure sensor 25 is smoothed by a filter 31, the water temperature sensor 26 is outputted via an interface 32, the output signal 08 shown in FIG. After being input and converted into digital values, these digital data are configured to be input to the microcomputer 38.
比較器35は回転センサ27の出力全波形整形し。The comparator 35 shapes the entire output waveform of the rotation sensor 27.
カウンター36は上記比較器35の出力の立上りから立
上Vまでの周期全計測し、その出力はマイクロコンピュ
ータ38の第1の割込端子ITIに入力するように構成
される。タイマー37は5m5ecの周期的な割込信号
音マイクロコンピュータ38の第2の割込端子IT、へ
出力するようになっている。上記マイクロコンピュータ
38は制御用のプログラムやデータを記憶するROM3
9と一時的にデータ會記憶するH、AM 40 ′t−
内蔵している。The counter 36 is configured to measure the entire period from the rise of the output of the comparator 35 to the rise V, and its output is input to the first interrupt terminal ITI of the microcomputer 38. The timer 37 outputs a periodic interrupt signal tone of 5 m5 ec to the second interrupt terminal IT of the microcomputer 38. The microcomputer 38 is a ROM 3 that stores control programs and data.
9 and temporarily store data H, AM 40't-
Built-in.
タイマー41はマイクロコンピュータ38の出力するト
リガ信号と設定値により発振器43の出力パルスをカウ
ントして、この設定値に対応したノ々ルス幅を出力し、
ドライノ々−42を介して上記インジェクター24を駆
動する。h” ライノf−44はマイクロコンピュータ
38の出力により切換装置8を制御し、基準電圧kVx
又はN2に切換える。The timer 41 counts the output pulses of the oscillator 43 according to the trigger signal output from the microcomputer 38 and the set value, and outputs the Norse width corresponding to the set value.
The injector 24 is driven through the dry nozzles 42. h” Rhino F-44 controls the switching device 8 by the output of the microcomputer 38, and sets the reference voltage kVx.
Or switch to N2.
上記構成に基づき1.この発明の一実施例による制御装
置30.特にマイクロコンピュータ38の制御動作2
H,OM 39に記憶された第7図の制御プログラムの
フローチャートと共に説明する。Based on the above configuration 1. A control device 30 according to an embodiment of the invention. In particular, the control operation 2 of the microcomputer 38
This will be explained with reference to the flowchart of the control program shown in FIG. 7 stored in the H,OM 39.
制御装置30に電源が投入されると、ステップ100よ
ジスタートする。ステップ100でマイクロコンピュー
タ38の出力及びRAM 40 ’e初期化する。When the power is turned on to the control device 30, the process starts from step 100. At step 100, the output of the microcomputer 38 and the RAM 40'e are initialized.
ステップ101で、第2の割込端子IT、に入力される
S m sec毎の割込信号を第2の割込処理プログラ
ムによりカウントされた経過に基づき1秒毎の判定を行
ない、1秒経過していればステップ102で切換装置S
を現在の状態とは反対側に制御して。In step 101, a determination is made every second based on the progress of counting the interrupt signal inputted to the second interrupt terminal IT every S m sec by the second interrupt processing program, and it is determined that one second has elapsed. If so, in step 102 the switching device S
to the opposite side of the current state.
基準電圧ヲ■lから■2又は■zから■!に切換えてス
テップ103に移り、1秒経過していなければ直接ステ
ップ103に進む。Reference voltage wo ■l to ■2 or ■z to ■! If one second has not elapsed, the process directly advances to step 103.
ステップ103では、フィルター31.インタフェース
32.増幅器33の出力をAD変換器34によジ順次デ
ィジタル数値に変換し、RAM40に記憶する。この各
データをそれぞれ圧力(FB)。In step 103, filter 31. Interface 32. The output of the amplifier 33 is sequentially converted into digital values by the AD converter 34 and stored in the RAM 40. Each of these data is expressed as pressure (FB).
水温(WT)及び空燃比データ(DSO)とする。Water temperature (WT) and air-fuel ratio data (DSO).
ステップ104で切換装置Sが基準電圧■!の方になっ
ていればステップ105へ進み、基準電圧V2の方にな
っていればステップ106の処理を行なめ。In step 104, the switching device S sets the reference voltage ■! If it is in the direction of the reference voltage V2, proceed to step 105, and if it is in the direction of the reference voltage V2, proceed to step 106.
ステップ107に移る。The process moves to step 107.
ステップ105では、空燃比f−タ(DSO)をデータ
(DSI)に記憶し、ステップ106では空燃比データ
(DSO)!cデータ(D82) ic記憶する。次イ
テ。In step 105, the air-fuel ratio data (DSO) is stored in data (DSI), and in step 106, the air-fuel ratio data (DSO)! c data (D82) IC storage. Next item.
ステラf107”C上記f’−タ(J)82)かう(D
SI)’(z減算し、その結果が所定値αより大きけれ
ばステップ108で下記の(3)式により演算し、小さ
ければステップ109で(4)式によシ演算してステッ
プ110に移る。Stella f107"C above f'-ta (J)82) Kai (D
SI)'(z is subtracted, and if the result is larger than a predetermined value α, it is calculated by the following equation (3) in step 108, and if it is smaller, it is calculated by the equation (4) in step 109, and the process moves to step 110.
(D83) = 02− ((DSI)−C1) ・・
・(3)(DS3) = C2+ ((DSL) −C
I) ・・・(4)ここで、データ(D83)は上記式
(IJ 、 (21の補正電圧VSOに対応する値であ
り、定数CI、C2はvcl。(D83) = 02- ((DSI)-C1)...
・(3)(DS3) = C2+ ((DSL) -C
I) ... (4) Here, the data (D83) is a value corresponding to the correction voltage VSO of the above formula (IJ, (21), and the constants CI and C2 are vcl.
VO2に対応する値である。つまり、(3)式は(1)
式に対応し、(4)式は(2)式にそれぞれ対応し、デ
ータ(DS3)は第5図の(eJと同様の特性となるシ
ステップ110では2.切換装置Sが基準電圧vI側で
あれば、処理はステップ111へ、 V’z’R1であ
ればステップ113へ移る。そして、ステップ111で
圧力(FB)と、カウンター36で測定した回転センサ
27の出力周期より計算した機関20の回転数(N)で
予めl(,0M39に記憶されている目標空燃比テーブ
ルF1からデータを選択し、)LAM40に目標空燃比
データ(D84)として記憶する。This value corresponds to VO2. In other words, equation (3) becomes (1)
The data (DS3) corresponds to the equation (4) and the equation (2) respectively, and the data (DS3) has the same characteristics as (eJ) in FIG. If so, the process moves to step 111, and if it is V'z'R1, the process moves to step 113.In step 111, the engine 20 is calculated from the pressure (FB) and the output cycle of the rotation sensor 27 measured by the counter 36. At the rotation speed (N), data is selected in advance from the target air-fuel ratio table F1 stored in 0M39 and stored in the LAM 40 as target air-fuel ratio data (D84).
ステップ112では、それまでの空燃比補正係数゛(I
)、上記データCD83) 、 (DS4)を用いて下
記の(5)式により演算し、その結果を新しい空燃比補
正係数(I)とする。In step 112, the air-fuel ratio correction coefficient ゛(I
), data CD83), and (DS4) are used to calculate the following equation (5), and the result is used as a new air-fuel ratio correction coefficient (I).
従って、切換装置Sが基準電圧Vl側であれば。Therefore, if the switching device S is on the reference voltage Vl side.
データ(D83)、(DS4)によジ空燃比補正係数C
I)’を徐々に更新するが、■2側であればこの更新を
停止する。Air-fuel ratio correction coefficient C according to data (D83) and (DS4)
I)' is gradually updated, but if it is on the ■2 side, this update is stopped.
ステップ113では、圧力(PB) 、回転数(N)で
予めROM39に記憶されている駆動時間テーブルF2
からデータ全選択し、インジェクター24の基本駆動時
間(TO)としてRAM 40 K−記憶する。In step 113, a drive time table F2 is stored in advance in the ROM 39 with pressure (PB) and rotation speed (N).
All data are selected from , and stored in the RAM 40K as the basic drive time (TO) of the injector 24.
次いで、ステップ″′114で上記基本駆動時間(TO
)に上記空燃比補正係数(I)’を乗じて補正し、駆動
時間(T1)としてRAM40に記憶し、ステップ10
1へ戻る。その結果、マイクロコンピュータ38の上記
第2の割込端子IT2に機関20の回転に同期して割込
信号が入ると、上記駆動時間(TI)’tタイマー41
に設定し、トリガ全かけるとこの駆動時間(T1)に対
応した時間、インジェクター24が駆動される。従って
、空燃比センサ2で検出された空燃比(八41)と上記
目標空燃比(A/F )Tデータが一致する様[、上記
空燃比補正係数CI)により上記基本駆動時間(TO)
がフィート°バック制御され1機関20の空燃比(A/
F )が所定の値に制御される。Next, in step ''114, the basic driving time (TO
) is corrected by multiplying it by the air-fuel ratio correction coefficient (I)', and the result is stored in the RAM 40 as the drive time (T1), and step 10
Return to 1. As a result, when an interrupt signal is input to the second interrupt terminal IT2 of the microcomputer 38 in synchronization with the rotation of the engine 20, the drive time (TI)'t timer 41
When the trigger is fully applied, the injector 24 is driven for a time corresponding to this drive time (T1). Therefore, the basic drive time (TO) is adjusted so that the air-fuel ratio (841) detected by the air-fuel ratio sensor 2 matches the target air-fuel ratio (A/F) T data [, the air-fuel ratio correction coefficient CI).
is foot-back controlled and the air-fuel ratio (A/
F ) is controlled to a predetermined value.
以上の如く1本実施例では基準電圧■lとv2の時の1
40の出力電圧の偏差から、空燃比(A/F)が理論空
燃比(A/F )Tよりも濃いか、薄いかを判定した゛
が、基準電圧がV2の時に所定値以上が以下かにより上
記判定を行って、も良い。As described above, in this embodiment, 1 when the reference voltages 1 and v2 are
Based on the deviation of the output voltage of 40, it was determined whether the air-fuel ratio (A/F) was richer or thinner than the stoichiometric air-fuel ratio (A/F)T. It is okay to make the above judgment.
また、上記空燃比補正係数(i) ′(il−上記(5
)式で更新したが、上記データ(1)83)、(1)8
4)の大。In addition, the above air-fuel ratio correction coefficient (i)'(il - the above (5
) formula, but the above data (1)83), (1)8
4) Large.
小により上記係数(I) ’e所定値ずつ増減ぜせても
良く、また上記データ(D83)、(D84)の偏差に
比例して上記駆動時間(TO)’に補正しても良い。The coefficient (I) may be increased or decreased by a predetermined value, or the driving time (TO) may be corrected in proportion to the deviation of the data (D83) and (D84).
更に、上記目標空燃比f−タ(DS4)k上記水温(W
T)や機関2oの加減速状態に対応して補正しても良い
。Further, the target air-fuel ratio f-ta (DS4) k the water temperature (W
T) or the acceleration/deceleration state of the engine 2o.
以上説明した通り、この発明によれば所定値■!又はV
2に維持された酸素センサ起電力を機関の運転中に所定
の周期で任意に切換え変更し、この切換え前後のポンプ
電流に対応した出力信号により空燃比を検出する手段を
備えた構成により、基準電圧を所定の時間間隔で切換え
、空燃比センサの出力が理論空燃比より濃いか薄いかを
判定することで、空燃比に対応した出力を演算すること
ができ、その結果機関のどのような運転状態においても
所定の空燃比になる様にフィードバック制御することが
出来るという大なる実用的効果を奏する。As explained above, according to the present invention, the predetermined value ■! or V
The oxygen sensor electromotive force maintained at By switching the voltage at predetermined time intervals and determining whether the output of the air-fuel ratio sensor is richer or thinner than the stoichiometric air-fuel ratio, it is possible to calculate the output corresponding to the air-fuel ratio, and as a result, it is possible to calculate the output that corresponds to the air-fuel ratio. This provides a great practical effect in that feedback control can be performed to maintain a predetermined air-fuel ratio even in the current state.
第1図はこの発明の一実施例で用いられた空燃比センサ
を示す構成図、第2図は第1図の■−■線横断面図、第
3図は第1図の空燃比センサを2000cc のガソリ
ン機関に装着して得られた試験結果を示す特性図、第4
図は、この発明の一実施例による機関の空燃比制御装置
全示す構成図。
第5図は第3図の特性音補正した特性図、第6図は第4
図に示す制御装置の部分拡大構成図、第7図はこの発明
の一実施例による制御装置の動作を示す制御プログラム
のフローチャートである。
1・・・排気管、2・・・空燃比センサ、6・・・固体
電解質酸素ポンプ、10・・・固体電解質酸素センサ、
12・・・電子制御装置、21・・・吸気管、24・・
・インジエII”−,25・・・圧力センサ、27・・
・回転センサ。
30・・・制御装置、31・・・フィルター、32・・
・インタフェース、34・・・ADコンバータ、3B・
・・マイクロコンピュータ、41・・・タイ−?−,4
2,44・・・ドライバー、8・・−切換装置。
なお1図中、同一符号は同一部分又は相当部分を示す。
代理人 大 岩 増 雄
第1図
第3図
鍮
空
危
t
(へ)。
第4図
第5図
第7図
手続補正書(自発)
特許庁長官殿
1、事件の表示 特願昭58−137115号2、発明
の名称
機関の空燃比制御装置
3、補正をする者
代表者片山仁へ部
5、 補正の対象
明細書の発明の詳細な説明の欄。
6、 補正の内容
明細書8頁17行「濃い側では下記の(1)式で。
薄い側」を「薄い側では下記の(1)式で、礎い側」と
訂正する。Fig. 1 is a configuration diagram showing an air-fuel ratio sensor used in an embodiment of the present invention, Fig. 2 is a cross-sectional view taken along the line ■-■ in Fig. 1, and Fig. 3 shows the air-fuel ratio sensor shown in Fig. 1. Characteristic diagram showing the test results obtained when installed on a 2000cc gasoline engine, No. 4
FIG. 1 is a diagram showing the entire configuration of an air-fuel ratio control device for an engine according to an embodiment of the present invention. Figure 5 is a characteristic diagram with corrected characteristic sound of Figure 3, Figure 6 is a characteristic diagram of Figure 4.
FIG. 7 is a partially enlarged configuration diagram of the control device shown in the figure, and FIG. 7 is a flowchart of a control program showing the operation of the control device according to an embodiment of the present invention. DESCRIPTION OF SYMBOLS 1... Exhaust pipe, 2... Air-fuel ratio sensor, 6... Solid electrolyte oxygen pump, 10... Solid electrolyte oxygen sensor,
12...Electronic control device, 21...Intake pipe, 24...
・Injie II"-, 25...Pressure sensor, 27...
・Rotation sensor. 30...Control device, 31...Filter, 32...
・Interface, 34...AD converter, 3B・
...Microcomputer, 41...Thailand? -, 4
2, 44...driver, 8...-switching device. In addition, in FIG. 1, the same reference numerals indicate the same or equivalent parts. Agent Masuo Oiwa Figure 1 Figure 3 Brass Vacancy (to). Figure 4 Figure 5 Figure 7 Procedural amendment (voluntary) Commissioner of the Japan Patent Office 1, Indication of the case, Japanese Patent Application No. 137115/1982 2, Name of the invention Air-fuel ratio control device for an engine 3, Representative of the person making the amendment Hitoshi Katayama Part 5: Detailed explanation of the invention in the specification subject to amendment. 6. In the detailed description of the amendment, page 8, line 17, "For the darker side, use the following formula (1). The thinner side" should be corrected to "For the thinner side, use the following formula (1) for the foundation side."
Claims (2)
の酸素分圧を制御する固体電解質酸素ポンプと上記間隙
部内の酸素分圧及び上記間隙部外の排気ガス中の酸素分
圧に対応した起電力全発生する固体電解質酸素センサと
金備え、該酸素センサが発生する起電力を所定値に保つ
のに必要な上記酸素ポンプのゾンデ電流に対応した出力
信号全上記機関の運転状態に応じて予め定められた値に
なるように上記機関の空燃比をフィードバック制御する
機関の空燃比制御装置において、上記所定値に保たれf
c、酸素センサ起電力を機関の運転中に所定の周期で任
意に切換え変更し、この切換え前後の上記出力信号によ
り、上記空燃比を検出する手段と上記機関の空燃比を補
正する手段とを備えたことを特徴とする機関の空燃比制
御装置。(1) A gap part that introduces engine exhaust gas, a solid electrolyte oxygen pump that controls the oxygen partial pressure in this gap, and a solid electrolyte oxygen pump that controls the oxygen partial pressure in the gap and the oxygen partial pressure in the exhaust gas outside the gap. An output signal corresponding to the sonde current of the oxygen pump necessary to maintain the electromotive force generated by the oxygen sensor at a predetermined value is generated depending on the operating state of the engine. In the engine air-fuel ratio control device, the air-fuel ratio of the engine is feedback-controlled so that the air-fuel ratio of the engine is maintained at the predetermined value.
c. means for arbitrarily switching and changing the oxygen sensor electromotive force at predetermined intervals during engine operation, and detecting the air-fuel ratio and correcting the air-fuel ratio of the engine based on the output signals before and after the switching; An air-fuel ratio control device for an engine, characterized by comprising:
新するものとし、上記所定値に保たれた酸素センサの起
電力を第1の電圧と第2の電圧の2つの値に所定の周期
で変更し、上記第2の電圧にある時は上記補正係数の更
新全停止するようにしたこと全特徴とする特許請求の範
囲第1項記載の機関の空燃比制御装置。(2) The means for correcting the air-fuel ratio of the engine shall update all correction coefficients, and the electromotive force of the oxygen sensor maintained at the predetermined value may be changed to two predetermined values, the first voltage and the second voltage. 2. The air-fuel ratio control device for an engine according to claim 1, wherein the air-fuel ratio control device changes the correction coefficient periodically, and completely stops updating the correction coefficient when the voltage is at the second voltage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58137115A JPS6027754A (en) | 1983-07-25 | 1983-07-25 | Air-fuel ratio controlling apparatus for engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58137115A JPS6027754A (en) | 1983-07-25 | 1983-07-25 | Air-fuel ratio controlling apparatus for engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6027754A true JPS6027754A (en) | 1985-02-12 |
| JPH0315979B2 JPH0315979B2 (en) | 1991-03-04 |
Family
ID=15191178
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58137115A Granted JPS6027754A (en) | 1983-07-25 | 1983-07-25 | Air-fuel ratio controlling apparatus for engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6027754A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005024561A (en) * | 2003-07-03 | 2005-01-27 | Sulzer Hexis Ag | Measuring device for monitoring residual oxygen in exhaust gas |
-
1983
- 1983-07-25 JP JP58137115A patent/JPS6027754A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005024561A (en) * | 2003-07-03 | 2005-01-27 | Sulzer Hexis Ag | Measuring device for monitoring residual oxygen in exhaust gas |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0315979B2 (en) | 1991-03-04 |
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