JPS5835246A - Air-fuel ratio controller of engine - Google Patents
Air-fuel ratio controller of engineInfo
- Publication number
- JPS5835246A JPS5835246A JP13448281A JP13448281A JPS5835246A JP S5835246 A JPS5835246 A JP S5835246A JP 13448281 A JP13448281 A JP 13448281A JP 13448281 A JP13448281 A JP 13448281A JP S5835246 A JPS5835246 A JP S5835246A
- Authority
- JP
- Japan
- Prior art keywords
- fuel ratio
- air
- control system
- engine
- control
- 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
-
- 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
- F02D41/1477—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the regulation circuit or part of it,(e.g. comparator, PI regulator, output)
- F02D41/1482—Integrator, i.e. variable slope
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (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】
本発明は、エンノンの空燃比制御装置に関し、更に拝細
には、エンノンの諸条件に応じ最も好捷しい空燃比でエ
ンジンの運転が行なわれるようにする使燃比制御装参に
関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an air-fuel ratio control device for an ennon, and more particularly, to a working fuel ratio control device that allows an engine to be operated at the most favorable air-fuel ratio according to various conditions of an ennon. Regarding loading.
排ガス対策のため排気系に触媒を備えたエンノンにおい
ては、触媒の浄化能力が吸入混合気の空燃比により変る
ところから、空燃比制御#e曾と耕ガス中の特定成分た
とえば酸素b!分の検出を行なう排ガス成分センサとを
設けて、伏出される排ガスbi分の一度に応じて空燃比
の制御を何ない、触媒の浄化Hヒカを最大限に発揮させ
るようにしたものが仙られている。エンノンがほぼ一定
速度および−だ負荷で運転されている定だ運転状70I
−qたはエンノン速贋お工び負荷の変動が比較的ゆるや
〃・な運転状憑では、このような空燃比制御で特1・て
1問題はないが、エンノンの始動および冷蘭蓮転時、ア
イドル運転時、加減速時などのような特定運転領域にお
いては、定常運転状態とは真なる窒比燃の混合気の供給
を必要とする。このため、従来の。In Ennon equipped with a catalyst in the exhaust system for exhaust gas control, the purification ability of the catalyst changes depending on the air-fuel ratio of the intake air-fuel mixture. There is a device equipped with an exhaust gas component sensor that detects the amount of exhaust gas bi, and does not control the air-fuel ratio depending on the amount of exhaust gas bi to maximize the purification H power of the catalyst. ing. Steady operation condition 70I where Ennon is operated at almost constant speed and - load
- In operating conditions where the load fluctuations are relatively slow, there is no particular problem with this type of air-fuel ratio control, but when starting the ennon and In certain operating ranges such as engine speed, idling, acceleration/deceleration, etc., steady operating conditions require the supply of an air-fuel mixture with a true nitrogen/fuel ratio. For this reason, conventional.
空燃比制御装置は、排ガス成分センサにより検出された
排ガスll+32分の濃度に応じて空燃比の制御を行な
゛う帰還制御のほかに、特定運転領域において、その運
転状態に応じた所定値に空燃比を設定するW定f!II
# e行ない、運転領域に応じて、帰還制御と固定制
御とを切り換えるように構成されている。In addition to feedback control that controls the air-fuel ratio according to the concentration of exhaust gas 1 + 32 minutes detected by the exhaust gas component sensor, the air-fuel ratio control device controls the air-fuel ratio to a predetermined value according to the operating state in a specific operating region. W constant f! that sets the air-fuel ratio. II
#e, and is configured to switch between feedback control and fixed control depending on the operating range.
ところが、こうした従来の空燃比制御装置は、−運転状
態が継続する場合には、満足な結果を与えることは考え
られるが、固定制御系から帰還制御系に切り換わったと
き、固定制御時の設定空燃比と帰還制御時の目標空燃比
の間には相当の差があること、また帰還制御系において
は通常積分制御動作によって制御を行なっているので、
帰還制御系によって空燃比を特定運転時の空燃比から通
常運転時の目標空燃比に設定するには相当の時間teし
、応答が遅いという欠点がある。However, such conventional air-fuel ratio control devices may give satisfactory results when the operating state continues, but when switching from a fixed control system to a feedback control system, the setting during fixed control There is a considerable difference between the air-fuel ratio and the target air-fuel ratio during feedback control, and the feedback control system normally performs control by integral control operation.
It takes a considerable amount of time to set the air-fuel ratio from the air-fuel ratio during specific operation to the target air-fuel ratio during normal operation using the feedback control system, and the response is slow.
この空燃比制御の応答性を向上させるため、特開昭S’
l−−’7023号公、報に記載された空燃比帰還式混
合気制御装置においては、特定運転のための固定制御系
から通常運転における帰還fftlJ御系へのリノ侯時
に、燃料噴射lit 1blI N信号をエンジンの運
転条件に応じて最終的に補正する補正回路において、こ
の制御信号を、特定運転時と通常運転時との適正空燃比
の差に基ついて11接補正し、この補正した制御信号に
よって燃料噴射装置を制御している。、
し〃・シながら、この空燃比帰還式混合気制御装置にお
いては、上述のように燃料噴射音制御信号を特定運転時
と通常運転時との適正空燃比の差に基ついて直接補正し
ているので、上記した帰還〜1」御および積分制御によ
る遅延はないが、制御系の17I侠え時すなわち運転状
態の切換え時に、仝・燃比があまりにも急減に変化する
ため、エンジンの運転状態vC債撃的な変動を生ずるお
それがある。In order to improve the responsiveness of this air-fuel ratio control,
In the air-fuel ratio feedback type mixture control device described in the '7023 publication, when the fixed control system for specific operation is changed to the feedback fftlJ control system for normal operation, the fuel injection lit 1blI In the correction circuit that finally corrects the N signal according to the engine operating conditions, this control signal is corrected based on the difference in the appropriate air-fuel ratio between specific operation and normal operation, and this corrected control The fuel injection device is controlled by the signal. However, in this air-fuel ratio feedback mixture control device, as mentioned above, the fuel injection sound control signal is directly corrected based on the difference in the appropriate air-fuel ratio between specific operation and normal operation. Therefore, there is no delay due to the above-mentioned feedback control and integral control, but when the control system reaches 17I, that is, when the operating state is switched, the fuel ratio decreases too rapidly, so the engine operating state vC There is a risk of a debt-like fluctuation.
そこで本発明は、・固定制御系から帰還制御光への切換
え時の空燃比制御における上記したようなhmのないエ
ンジンの空燃比制御製wを提供すること金目的とするも
のである。SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide an air-fuel ratio control method for an engine that does not have the above-mentioned hm in air-fuel ratio control when switching from a fixed control system to feedback control light.
本冗明によるエンジンの空燃比制御装置は、仝燃比亀1
1#糸が、特定運転時の固定制御系から通常運転時の帰
還制御系に切り換ったとき、この帰還制御系め制御利得
を一時的に高める補正手段を設けたことを特徴とする吃
のである。The engine air-fuel ratio control device according to the present invention has a fuel-fuel ratio of 1.
When the #1 yarn is switched from a fixed control system during a specific operation to a feedback control system during normal operation, a correction means is provided to temporarily increase the control gain of the feedback control system. It is.
制御利得を高める手段としては、帰還制御のための積分
係数を、固定制御から帰還制御への切シ換え後、一定時
間だけ高くすればよい。また、別の手段としては、制御
系の積分手段への入力信号値が反転するまでは尚い積分
係数で、反転後は低い積分係数で空燃比制御を行なうよ
うにしてもよい。As a means for increasing the control gain, the integral coefficient for feedback control may be increased for a certain period of time after switching from fixed control to feedback control. Alternatively, the air-fuel ratio may be controlled using an integral coefficient until the input signal value to the integrating means of the control system is reversed, and after the reverse is performed using a lower integral coefficient.
このような構成を備えた本発明のエンジンの空燃比制御
装置によれば、上記制御系の切換え時に爆速制御系の制
御利得を一時的に高めるようにしているので、この制御
系の切換え時に適正な状態で空燃比を変化させることか
でと、従ってエンノンの運転状態に衝撃的な変動を生ず
ることがない。According to the engine air-fuel ratio control device of the present invention having such a configuration, the control gain of the explosive speed control system is temporarily increased when switching the control system, so that the control gain of the explosion speed control system is temporarily increased when switching the control system. Therefore, by changing the air-fuel ratio under the same conditions, there will be no shocking changes in the operating conditions of the Ennon.
以下、添付□□□面を参照しつつ本発明の好ましい実施
例によるエンジンの空燃比制御装置について説明する。Hereinafter, an engine air-fuel ratio control device according to a preferred embodiment of the present invention will be described with reference to the attached page □□□.
第1図は、本発明のエンジン1の空燃比制御装置の全体
構成図である。FIG. 1 is an overall configuration diagram of an air-fuel ratio control device for an engine 1 according to the present invention.
エンジンlは、吸気通路2および排気通路8を有してい
る。この吸気通路2には吸気負圧センサ4が、排気通路
8には酸素濃度センサからなる排気センサ5が、それぞ
れ配設されている。液@管路2の吸気負圧センサ4の上
流側には、例えばエアプリーダを開閉する電磁弁からな
るアクチュエータ6會介して作動制御されて、雇会気の
空燃比を調整する例えば気化益のような燃料#A111
装置7が設けられている。この燃料−型装置7には、吸
気負圧センサ4の検出出力と排気センサ5の横出出力と
から混合気の空燃比を制御するための制仇回鮎8が接続
されている。このll+l制御回路8については、後に
詳細に説明する。この制御回路8には、排気センサ5の
濃度構出信号Slと設定電圧発生回路9からの目標空燃
比を示す設定電圧Vref とを比較し、そのVA差
を示す偏差信@S2・を発生する比軟回路IOが接続さ
れている。なお、図中、符号11はエアクリーナを、符
号12は排気通路8に介設された触りn!:装置をそれ
ぞれ示す。The engine 1 has an intake passage 2 and an exhaust passage 8. An intake negative pressure sensor 4 is disposed in the intake passage 2, and an exhaust sensor 5 consisting of an oxygen concentration sensor is disposed in the exhaust passage 8. On the upstream side of the intake negative pressure sensor 4 in the liquid @ pipe 2, the operation is controlled via an actuator 6 consisting of a solenoid valve that opens and closes an air leader, for example, to adjust the air-fuel ratio of the intake air, such as vaporization gain. Fuel #A111
A device 7 is provided. A control valve 8 is connected to the fuel type device 7 for controlling the air-fuel ratio of the air-fuel mixture based on the detection output of the intake negative pressure sensor 4 and the side output of the exhaust sensor 5. This ll+l control circuit 8 will be explained in detail later. This control circuit 8 compares the concentration configuration signal Sl of the exhaust sensor 5 with a set voltage Vref indicating the target air-fuel ratio from the set voltage generating circuit 9, and generates a deviation signal @S2 indicating the VA difference. A soft circuit IO is connected. In the figure, reference numeral 11 indicates an air cleaner, and reference numeral 12 indicates an air cleaner provided in the exhaust passage 8. : Indicates each device.
次に、第2図を参照しつつ、本発明のエンジンの空燃比
制御装置の制御回路8について絆細に説明する。Next, the control circuit 8 of the engine air-fuel ratio control device of the present invention will be explained in detail with reference to FIG.
制御回路8は、比較器IOに接続された積分演算器18
を備λており、この積分演算器18は・その積分係数が
、通常運転時用の積分係数に/。The control circuit 8 includes an integral calculator 18 connected to the comparator IO.
This integral calculator 18 is equipped with λ, whose integral coefficient is the integral coefficient for normal operation.
およびこの積分係数k ’/より大きな値の積分係数に
2のいずれかに選択的に設定されるようになっている。The integral coefficient k'/2 is selectively set to an integral coefficient larger than the integral coefficient k'/2.
積分演算器18は、通常運転時において比較器IOから
の偏差信号S2に基づき積分係数に/に従って積分演算
し、デユーティ比制御信号S3を出力するようになって
いる。この積分演算器18には、駆動回路14が接続さ
れており、この駆動回路14は、上記デユーティ比制御
信号S3に基づきアクチュエータ6t−駆動制御する。The integral calculator 18 performs an integral calculation in accordance with an integral coefficient based on the deviation signal S2 from the comparator IO during normal operation, and outputs a duty ratio control signal S3. A drive circuit 14 is connected to the integral calculator 18, and the drive circuit 14 controls the drive of the actuator 6t based on the duty ratio control signal S3.
制御回路8は、以上により通常運転4時の帰還制御系を
構成する。The control circuit 8 thus constitutes a feedback control system during normal operation 4.
一方、符号15は、エンジン1の特定運転状態の固定制
御系の固定制御信号出力回路を示し、この固定制御信号
出力回路15は、ゲート16を介して積分器算器1Bに
接続されている。積分演惇器18は、固定制御信号出力
回路15からの固定制H−Is ’jj S IIを受
けたとき、その積分作用を停止し、人力をそのままの状
態で出力するようになっている。f−)16は、運転状
態検出回路17に接続されており、この運転状態検出回
路l?は、負圧センサ4の検出出力に基づいてエンジン
の運転状態を検出し、このエンジン1の運転状態が一負
荷運転状態等の特定運転状態のときc−ト16を開くも
のである。On the other hand, reference numeral 15 indicates a fixed control signal output circuit of a fixed control system for a specific operating state of the engine 1, and this fixed control signal output circuit 15 is connected to the integrator 1B via a gate 16. When the integral compensator 18 receives the fixed control H-Is'jj S II from the fixed control signal output circuit 15, it stops its integral action and outputs the human power as it is. f-) 16 is connected to the operating state detection circuit 17, and this operating state detection circuit l? The system detects the operating state of the engine based on the detection output of the negative pressure sensor 4, and opens the door 16 when the operating state of the engine 1 is in a specific operating state such as a one-load operating state.
運転状態検出回路l?には、積分係数設定器I8が接続
されており、この積分係数設定器18は、璋転状態検出
回路17が、エンジンlが特定運転状態から通常運転状
態に切り換ったことを検出したとき、積分!613の積
分係数をkl力・らにコに切り換えるように指示するも
のである。この積分係数設定器18には、スイッチング
回路】9が反転器20を介して、あるいはこの反転器2
0を介さすに直接接続されている。反転器20は、槓4
r隊数kl、k、2を反転、すなわち−kl、−一コと
なす本のである。スイッチング回路19a、比較器IO
の出力である偏差信号s2に基つき積分器18の積分係
数をに/、k2、−に/、−に、lのいずれかに設定す
る本のである。図中、符号21はタイマであり、このタ
イマ21は、運転状態検出回路17が、特定運転状態か
ら通常運転状態Vc切シ換ったことを検出したとき始勲
し、所定時聞稜に上I−積分係数をに2からに/に切り
換えるものである。Operating state detection circuit l? An integral coefficient setter I8 is connected to the integral coefficient setter I8, and this integral coefficient setter 18 is connected to , integral! This command instructs to switch the integral coefficient of 613 to kl force/ra niko. This integral coefficient setter 18 is connected to a switching circuit 9 via an inverter 20 or
It is directly connected through 0. The inverter 20 is a ram 4
This is a book in which the number of r squads kl, k, and 2 are inverted, that is, -kl, -1. Switching circuit 19a, comparator IO
The integration coefficient of the integrator 18 is set to one of , k2, -, -, and l based on the deviation signal s2 which is the output of the integrator 18. In the figure, reference numeral 21 is a timer, and this timer 21 starts when the operating state detection circuit 17 detects that the normal operating state Vc has been switched from the specific operating state, and the timer 21 starts operating when the operating state is switched from the specific operating state to the normal operating state Vc. I - This is to switch the integral coefficient from 2 to /.
次・に、iJ、2図に示す構成をもっ電0@回路8の作
用を第3図および第9図を参照しながら説明する。Next, the operation of the circuit 8 having the configuration shown in FIG. 2 will be explained with reference to FIGS. 3 and 9.
例えば、エンジンlの通常運転時において、エンジン1
に供給される混合気の空燃比が第3図(Alのように変
動したとすると、これに応じて排気センサ5は、濃検出
信4gS/を出力する。比較器lυは、この濃度検出信
号S/と設定電圧発生回路9からの設定電圧Vrefと
を比較して第3図(81に示されているような偏差信号
s2を出力する。この偏差信号Sコは、濃度検出信号s
〕が設定電圧Vrefより大きいことを示す高レベル部
分すなわちり/qの部分と、濃度検出信号S/が設定電
圧Vrefよね小さいことを示す低レベル部分すなわち
θ“の部分とからなっている。積分器1i#器↓3は、
この−差ifI号S2に基づき積分係数kl、−に/で
積分演舞し、第3図(C)に示されているようなデユー
ディ比制御信号53を出力する。躯勧回w?!r11は
、このガニ−ティ比制御信号S−3に基づきアクチュエ
ータ6を駆動制御し、吸入混合気の空燃比が設定′¥坏
比に収束するように帰還空燃比II御を行なう。For example, during normal operation of engine 1, engine 1
Assuming that the air-fuel ratio of the mixture supplied to the air-fuel mixture fluctuates as shown in FIG. S/ is compared with the set voltage Vref from the set voltage generation circuit 9 to output a deviation signal s2 as shown in FIG.
] consists of a high level portion, ie, a portion RI/q, which indicates that the concentration detection signal S/ is larger than the set voltage Vref, and a low level portion, ie, a portion θ”, which indicates that the concentration detection signal S/ is smaller than the set voltage Vref. Vessel 1i# Vessel↓3 is
Based on this -difference ifI signal S2, the integral coefficient kl is integrated by -//, and a duty ratio control signal 53 as shown in FIG. 3(C) is output. Body solicitation lol? ! r11 drives and controls the actuator 6 based on this Gunnity ratio control signal S-3, and performs feedback air-fuel ratio II control so that the air-fuel ratio of the intake air-fuel mixture converges to the set `JPY ratio.
以上説明したような帰還空燃北側−を行なっているとき
、運転状態検出回路17が負圧センサ4の挽出出力によ
って通常運転状態がら時足導転状態、ν1jえば高負荷
運転状態に切り換わったことτ検出すると、この運転状
態検出回路17は、ダート16を−く。従って、固定制
御信号出力回路15からの固定制御信号Sダは、積分波
14.器18に供給され、檀分演′II4器18の作用
を停止トして、帰還制御系を停止する。この結果、固定
制御信号sgは、その贅まの状態で駆動回路14に出刃
される。When performing the return air-fuel north side operation as described above, the operating state detection circuit 17 switches from the normal operating state to the hourly conduction state and, if ν1j, to the high-load operating state based on the output of the negative pressure sensor 4. When detecting τ, the driving state detection circuit 17 detects the dirt 16. Therefore, the fixed control signal Sda from the fixed control signal output circuit 15 is an integral wave 14. The feedback control system is stopped by stopping the operation of the DAN-BUN'II4 device 18. As a result, the fixed control signal sg is delivered to the drive circuit 14 in its luxurious state.
かくして、駆動回路14は、固定制御信号S!に基づき
アクチュエータ6を澗1足制御して、吸入混合気の空燃
比が例えば一定のリッチな値となるように置市空燃比制
御を行なう。Thus, the drive circuit 14 receives the fixed control signal S! Based on this, the actuator 6 is controlled one step at a time, and air-fuel ratio control is performed so that the air-fuel ratio of the intake air-fuel mixture becomes, for example, a constant rich value.
一方、運転状態検出回&817が、特定運転状態から通
常運転状態Kf化したことを検出したとき、検分係数設
定618に、スイッチング回路19を介して積分演算器
18の積分係数をに2あるいは−に2VcgJシ換える
。積分器18は、積分係数に2または−に2によって比
較器10の偏差信号S2に基つき積分演算し、デユーテ
ィ比制御18号S3を出力する。この状態はタイマー2
11Cよって所定時ill T後に切り換えられ、積分
演算器18は再び積分係数に/、−に/に基づいてその
作用ケ行なう。この制御の結果による空燃比の変化を第
9図の曲l1lilRに示す。この撰び図から明らかな
ように、%足運転時の固定制御において空燃比がリッチ
な状態の一足II!R/にあったとすると、固定制御か
ら帰還制御に′gQり換わったとき、空燃比は積分係数
に2の作用により部分R2のように望ましい勾配で過渡
的に変化し、その後積分係数klの作用により部分R3
のように通常の帰還制御が行なわれる。なお、第9図に
おいて、紐解は補正中段なしに固定制御から帰還制御に
切り挾7)つた場合の空燃比の変化の状態を示し、破−
は#!j開昭5 ’7−’70.23号の璧慾比帰還式
混合気制御装置による上記と同様の場合・の空燃比の変
化の伏悲忙示す。On the other hand, when the operating state detection circuit &817 detects that the specific operating state has changed to the normal operating state Kf, the integral coefficient of the integral calculator 18 is set to 2 or - to the verification coefficient setting 618 via the switching circuit 19. Replace 2VcgJ. The integrator 18 performs an integral calculation based on the deviation signal S2 of the comparator 10 with an integral coefficient of 2 or -2, and outputs a duty ratio control signal S3. This state is timer 2
11C after a predetermined time ill T, and the integral calculator 18 again performs its operation based on the integral coefficients /, - and /. Changes in the air-fuel ratio as a result of this control are shown in curves l1lilR in FIG. As is clear from this diagram, the air-fuel ratio is rich in the fixed control during % foot driving! R/, when fixed control is switched to feedback control 'gQ, the air-fuel ratio changes transiently at a desired slope as in part R2 due to the effect of 2 on the integral coefficient, and then changes by the effect of integral coefficient kl. Due to part R3
Normal feedback control is performed as follows. In addition, in FIG. 9, the solution shows the state of change in the air-fuel ratio when switching from fixed control to feedback control without intermediate correction stage.
teeth#! This figure shows the changes in the air-fuel ratio in the same case as above using the ratio feedback type mixture control device of No. J Kaisho 5 '7-'70.23.
なお、この実施例においては、積分係数かに/からに、
2にf侯されfc後、褥びに、2〃・らに/に反転する
のにタイマ21を用い友が、第5図に示すように、積分
係数設足器18を比較器lOに長続し、この比較器】0
の出力である一走信号SコかりOqからq/ゲvC1あ
るいはI/ / L/から〃θηに切り候わっだときに
、積分係数をにノからにノに戻すようにしてもよい。ま
た、上記実施例においては、比較器10の一差イg号S
ノ會績分するのに積分演算器18すなt″′)ちコンピ
ュータを用いたが、この積分演算器18の代りに、コン
ピュ−タ)光、放電金利用する通常の積分器音用いるこ
とカーでき、この場合は反転器20を必埜としない。In addition, in this example, the integral coefficient is
After f is set to 2 and after fc, the timer 21 is used to invert to 2, and then the integral coefficient adder 18 is connected to the comparator lO as shown in FIG. And this comparator】0
The integral coefficient may be returned from 2 to 2 when the one-stroke signal S output from Oq to q/gevC1 or from I//L/ to θη. Further, in the above embodiment, one difference Ig signal S of the comparator 10
An integral calculator 18, i.e., a computer, was used to divide the number of minutes, but instead of this integral calculator 18, a normal integrator sound using light and discharge metal could be used. In this case, the inverter 20 is not required.
Alしくは、木竜明の1ンジンの堂1輸比匍制御湊噛゛
の全14−構成図、
第Ω図は、第7図に示されたエンジンの仝・黙北側坤装
首の制御回路の一例を示すグロック1図、第3図(Al
、(81、(C)は、それぞれ空験比、4度検出16鉤
、デユーティ比制御信号の変化を示す改酩図、
渠4図は、固定制御系から帰M制御系ヘゲ)切換え時(
fc 、本発明のエンジンの空炉比制御装首によって・
tI++御された空燃比の変化を示す彼肘し11.4J
、5図は、altII御回路の変形例を示すブロック図
である。
1・・・エンジン、4・・・負圧センサ、5・・・排気
センサ、<S・・・アクチュエータ、7・・・燃#12
脚悩装置、8・・・知」(財)回路、9・・・設′定電
圧発生回路、1 (1・・・比較回路、18・・・積分
演算器、15・・・bs+定制御信号出力回路、17・
・・運転状特検出益、■8・・・麺分係数設足旨。In other words, all 14 configuration diagrams of Ryumei Mok's 1-engine engine control port, and Figure Ω shows the control of the engine's silent north side mount shown in Figure 7. Glock 1 and 3 (Al
, (81, (C) are the revised diagrams showing the changes in the blank ratio, 4-degree detection 16 hooks, and duty ratio control signals, respectively. Figure 4 shows the change from the fixed control system to the return M control system). (
fc, by the air-to-furnace ratio control head of the engine of the present invention.
11.4J showing the change in air-fuel ratio controlled by tI++
, 5 is a block diagram showing a modification of the altII control circuit. 1... Engine, 4... Negative pressure sensor, 5... Exhaust sensor, <S... Actuator, 7... Fuel #12
Leg pain device, 8... Chi' (Incorporated Foundation) circuit, 9... Setting voltage generation circuit, 1 (1... Comparison circuit, 18... Integral calculator, 15... bs + constant control Signal output circuit, 17.
・・Driving letter special detection profit, ■ 8 ・・Establishment of noodle coefficient.
Claims (1)
度を検出することによって実際零燃比を検出し、この検
出した寮際空燃比と目標空燃比とを比較して雨空燃比の
差を検出し、この雨空燃比の差に基づいて、空燃比が前
記目標空燃比となるように制御する帰還制御系、および
エンジンの特定運転時に、その運転状wllK応じた望
ましい値に空燃比を固定維持する固定制御系からなり、
前記帰還制御系と固定制御系とが、エンジンの運転状態
に応じて切り換えられて作動す、るようになっている空
燃比制御装置において、制御系が、前記固定制御系から
帰還制御系に切り換ったとき、該帰還制御系の制御利得
を一時的に高める補正手段を設けたことを特徴とするエ
ンジンの空燃比制御装置。During normal engine operation, the actual zero-fuel ratio is detected by detecting the concentration of engine exhaust gas components, and the detected air-fuel ratio near the dormitory is compared with the target air-fuel ratio to detect the difference in the rain air-fuel ratio. a feedback control system that controls the air-fuel ratio to the target air-fuel ratio based on the difference in the air-fuel ratio; and a fixed control system that fixes and maintains the air-fuel ratio at a desired value according to the operating condition wllK during a specific operation of the engine. Consisting of
In the air-fuel ratio control device in which the feedback control system and the fixed control system are switched and operated according to the operating state of the engine, the control system is switched from the fixed control system to the feedback control system. 1. An air-fuel ratio control device for an engine, comprising a correction means for temporarily increasing a control gain of the feedback control system when the feedback control system is changed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13448281A JPS5835246A (en) | 1981-08-27 | 1981-08-27 | Air-fuel ratio controller of engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13448281A JPS5835246A (en) | 1981-08-27 | 1981-08-27 | Air-fuel ratio controller of engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5835246A true JPS5835246A (en) | 1983-03-01 |
| JPH0353459B2 JPH0353459B2 (en) | 1991-08-15 |
Family
ID=15129352
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13448281A Granted JPS5835246A (en) | 1981-08-27 | 1981-08-27 | Air-fuel ratio controller of engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5835246A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59201959A (en) * | 1983-04-28 | 1984-11-15 | Suzuki Motor Co Ltd | Control device of air-fuel ratio in engine |
| JPS60128954A (en) * | 1983-12-16 | 1985-07-10 | Mazda Motor Corp | Air-fuel ratio controller for engine |
| US4872117A (en) * | 1984-11-30 | 1989-10-03 | Suzuki Jidosha Kogyo Kabushiki Kaisha | Apparatus for controlling an air-fuel ratio in an internal combustion engine |
| US5394856A (en) * | 1992-08-17 | 1995-03-07 | Unisia Jecs Corporation | System for and method of controlling air-fuel ratio in internal combustion engine |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS52154929A (en) * | 1976-06-18 | 1977-12-23 | Nippon Denso Co Ltd | Air-fuel ratio feedback system mixed gas control apparatus |
| JPS547023A (en) * | 1977-06-17 | 1979-01-19 | Nippon Denso Co Ltd | Air-fuel-ratio feedback type mixture controller |
| JPS569634A (en) * | 1980-05-29 | 1981-01-31 | Nippon Denso Co Ltd | Feedback control of air-fuel ratio |
-
1981
- 1981-08-27 JP JP13448281A patent/JPS5835246A/en active Granted
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS52154929A (en) * | 1976-06-18 | 1977-12-23 | Nippon Denso Co Ltd | Air-fuel ratio feedback system mixed gas control apparatus |
| JPS547023A (en) * | 1977-06-17 | 1979-01-19 | Nippon Denso Co Ltd | Air-fuel-ratio feedback type mixture controller |
| JPS569634A (en) * | 1980-05-29 | 1981-01-31 | Nippon Denso Co Ltd | Feedback control of air-fuel ratio |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59201959A (en) * | 1983-04-28 | 1984-11-15 | Suzuki Motor Co Ltd | Control device of air-fuel ratio in engine |
| JPS60128954A (en) * | 1983-12-16 | 1985-07-10 | Mazda Motor Corp | Air-fuel ratio controller for engine |
| US4872117A (en) * | 1984-11-30 | 1989-10-03 | Suzuki Jidosha Kogyo Kabushiki Kaisha | Apparatus for controlling an air-fuel ratio in an internal combustion engine |
| US5394856A (en) * | 1992-08-17 | 1995-03-07 | Unisia Jecs Corporation | System for and method of controlling air-fuel ratio in internal combustion engine |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0353459B2 (en) | 1991-08-15 |
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