JPH045819B2 - - Google Patents
Info
- Publication number
- JPH045819B2 JPH045819B2 JP7930583A JP7930583A JPH045819B2 JP H045819 B2 JPH045819 B2 JP H045819B2 JP 7930583 A JP7930583 A JP 7930583A JP 7930583 A JP7930583 A JP 7930583A JP H045819 B2 JPH045819 B2 JP H045819B2
- Authority
- JP
- Japan
- Prior art keywords
- air
- fuel ratio
- cylinder
- fuel
- fuel injection
- 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
Links
- 239000000446 fuel Substances 0.000 claims description 143
- 238000002347 injection Methods 0.000 claims description 58
- 239000007924 injection Substances 0.000 claims description 58
- 238000002485 combustion reaction Methods 0.000 claims description 22
- 238000000034 method Methods 0.000 claims description 22
- 239000001301 oxygen Substances 0.000 description 11
- 229910052760 oxygen Inorganic materials 0.000 description 11
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 10
- 239000007789 gas Substances 0.000 description 6
- 235000017284 Pometia pinnata Nutrition 0.000 description 5
- 240000009305 Pometia pinnata Species 0.000 description 5
- 238000001514 detection method Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 239000000872 buffer Substances 0.000 description 2
- 239000000498 cooling water Substances 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000004043 responsiveness Effects 0.000 description 2
- 238000012935 Averaging Methods 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 150000002926 oxygen Chemical class 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000007142 ring opening reaction Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000001052 transient effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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
- F02D41/1486—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor with correction for particular operating conditions
- F02D41/1488—Inhibiting the regulation
- F02D41/1491—Replacing of the control value by a mean value
-
- 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
- F02D41/1497—With detection of the mechanical response of the engine
- F02D41/1498—With detection of the mechanical response of the engine measuring engine roughness
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/10—Parameters related to the engine output, e.g. engine torque or engine speed
- F02D2200/1015—Engines misfires
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)
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、電子制御内燃機関の燃料噴射制御方
法に係り、特に多気筒電子制御内燃機関の各気筒
の空燃比制御精度を改善する燃料噴射制御方法に
関する。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a fuel injection control method for an electronically controlled internal combustion engine, and particularly to a fuel injection method for improving the air-fuel ratio control accuracy of each cylinder of a multi-cylinder electronically controlled internal combustion engine. Regarding control method.
従来より、多気筒電子制御内燃機関では、燃料
噴射弁は各気筒ごとに対応して設けられている
が、空燃比センサとしての酸素(O22)センサは
全気筒共通に設けられ、この酸素センサからのフ
イードバツク信号に基づいて計算されたフイード
バツク係数い基づいて全気筒の燃料噴射量が計算
されている。各燃料噴射弁の流量にはばらつきが
生じるので、従来の多気筒電子制御内燃機関にお
いて各燃料噴射弁の流量ばらつきを吸収して各気
筒の空燃比を目標値に制御する場合にはフイード
バツク係数の計算の定数としてのスキツプ量(酸
素センサの出力レベルの反転時に応答性の改善す
るためにフイードバツク係数を不連続に増減する
際のその不連続量)あるいは傾き(酸素センサの
出力レベルが同一に維持されている期間のフイー
ドバツク係数の増減量)を大きく、すなわちフイ
ードバツク係数の振幅を大きくするしかないが、
これは空燃比の変動を増大させ、運転性能(ドア
リブアピリテイ)の悪化、触媒の浄化能力の低下
等の不具合を伴う。特に酸素センサが排気系の比
較的下流に設けられている多気筒電子制御内燃機
関では、酸素センサへの排気ガスの到達遅れがあ
るので、燃料噴射弁の流量のばらつきを吸収して
各気筒の空燃比の制御精度を改善するためには、
スキツプ量および傾きを増大してフイードバツク
周波数を大きくする必要があるが、前述の不具愛
のためにスキツプ量および傾きの増大には所定の
制限がある。このような問題を解決する装置の一
つとして、特開昭57−122144号公報に記載された
技術が知られており、この方法によれば各気筒毎
の空燃比のバラツキにより排気の悪化防止のため
に、各気筒毎の空燃比を独立して制御可能として
いる。さらに、この方法によれば、
(A) 排気管の集合部に設置された空燃比センサの
出力信号の変動の大きさが小さくなるように、
順次ある気筒の空燃比を他の気筒の空燃比と異
ならせる。
Conventionally, in multi-cylinder electronically controlled internal combustion engines, fuel injection valves have been provided for each cylinder, but an oxygen (O2 2 ) sensor serving as an air-fuel ratio sensor is provided commonly for all cylinders, and this oxygen sensor The fuel injection amount for all cylinders is calculated based on the feedback coefficient calculated based on the feedback signal from the cylinder. Since variations occur in the flow rate of each fuel injector, when controlling the air-fuel ratio of each cylinder to the target value by absorbing the variation in the flow rate of each fuel injector in a conventional multi-cylinder electronically controlled internal combustion engine, it is necessary to adjust the feedback coefficient. The amount of skip (the amount of discontinuity when the feedback coefficient is increased or decreased discontinuously to improve the response when the output level of the oxygen sensor is reversed) or the slope (the output level of the oxygen sensor remains the same) as a constant in the calculation. The only option is to increase the increase/decrease in the feedback coefficient (increase/decrease in the feedback coefficient during the period in which the
This increases fluctuations in the air-fuel ratio, leading to problems such as deterioration in driving performance (door liveability) and a decrease in the purification ability of the catalyst. In particular, in multi-cylinder electronically controlled internal combustion engines where the oxygen sensor is installed relatively downstream in the exhaust system, there is a delay in the arrival of exhaust gas to the oxygen sensor. In order to improve the control accuracy of the air-fuel ratio,
Although it is necessary to increase the skip amount and slope to increase the feedback frequency, there are certain limits to increasing the skip amount and slope due to the above-mentioned disadvantages. As one of the devices to solve such problems, the technique described in Japanese Patent Application Laid-open No. 122144/1983 is known. According to this method, the deterioration of exhaust gas is prevented by the variation in the air-fuel ratio of each cylinder. Therefore, the air-fuel ratio of each cylinder can be controlled independently. Furthermore, according to this method, (A) so that the magnitude of fluctuation in the output signal of the air-fuel ratio sensor installed at the collecting part of the exhaust pipe is reduced;
The air-fuel ratio of a certain cylinder is made to be different from the air-fuel ratio of other cylinders in sequence.
(B) 排気管の集合部に設置された空燃比センサの
出力信号を、気筒判別信号に同期して読み込ん
で、空燃比検出センサの出力信号がどの気筒の
空燃比を検出しているかを判別し、どの気筒の
空燃比がバラツイているかを検出して、それに
基づき各気筒の空燃比を制御する。(B) Read the output signal of the air-fuel ratio sensor installed at the collecting part of the exhaust pipe in synchronization with the cylinder discrimination signal, and determine which cylinder's air-fuel ratio is detected by the output signal of the air-fuel ratio detection sensor. Then, it detects which cylinder's air-fuel ratio varies, and controls the air-fuel ratio of each cylinder based on that.
しかしながら、上述(A)の方法は、空燃比のバラ
ツキが、どの気筒から発生しているか判別しない
まま、ある気筒の空燃比をずらしてやり、そお制
御結果である空燃比検出センサの出力信号が以前
の出力信号に較べ、変動の大きさが隙なくなつた
か否かを検知しているので、場合によつては空燃
比変動を助長することもありえ、また制御の応答
性も好ましくない。さらに、空燃比の変動を検出
するには、空燃比検出センサの出力信号すべて
を、読み込む必要があり、本来、空燃比がリツチ
がリーンかだけを判断して、その判断結果のみを
コンピユータが読み取るような形式の性御装置で
は、採用が困難との問題がある。
However, in method (A) above, the air-fuel ratio of a certain cylinder is shifted without determining in which cylinder the air-fuel ratio variation is occurring, and the output signal of the air-fuel ratio detection sensor, which is the control result, is Since it is detected whether or not the magnitude of fluctuation has become uniform compared to the output signal of , this may encourage air-fuel ratio fluctuation in some cases, and the responsiveness of the control may also be unfavorable. Furthermore, in order to detect fluctuations in the air-fuel ratio, it is necessary to read all output signals from the air-fuel ratio detection sensor. Originally, the computer would only judge whether the air-fuel ratio is rich or lean, and only read the results of that judgment. This type of sex control device has the problem of being difficult to employ.
また、上述(B)の方法では、一般に、燃焼された
ガスが、排気管集合部に設置された空燃比検出セ
ンサに到達するまでには、時間遅れがあり、また
その時間遅れ分も、機関の運転状態により大きく
変動すること、及び、特に空気流量の大きい運転
状態や機関回転数が高い運転状態では、燃焼され
た各気筒のガスが排気管集合部に到達する以前に
混合されることになり、従つて、空燃比検出セン
サが、どの気筒の空燃比を検出しているのかを精
度良く判断することは困難との問題がある。 In addition, in the method (B) above, there is generally a time delay before the combusted gas reaches the air-fuel ratio detection sensor installed at the exhaust pipe collection part, and the time delay also affects the engine. In particular, in operating conditions where the air flow rate is large or the engine speed is high, the combusted gases from each cylinder may be mixed together before reaching the exhaust pipe collecting section. Therefore, there is a problem in that it is difficult to accurately determine which cylinder's air-fuel ratio is detected by the air-fuel ratio detection sensor.
そこで、本発明の目的は、上記問題を解決しつ
つ、精度良く各気筒の燃料噴射弁における流量の
ばらつきを補償して各気筒の空燃比制御精度を改
善できる多気筒電子制御内燃機関の燃料噴射制御
方法を提供することである。 SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide a fuel injection system for a multi-cylinder electronically controlled internal combustion engine that can solve the above problems and improve the air-fuel ratio control accuracy of each cylinder by accurately compensating for variations in flow rate in the fuel injection valves of each cylinder. The object of the present invention is to provide a control method.
本発明は上記目的を達成するために、燃料噴射
弁が内燃機関の各気筒ごとに対応して設けられ、
空燃比センサが複数気筒共通に設けられ、該空燃
比センサの出力信号に応じて前記内燃機関の複数
気筒に対する空燃比フイードバツク係数を求め、
該係数の基づき補正された燃料噴射料が前記各気
筒の燃料噴射弁より噴射されるフイードバツク制
御方法により空燃比制御される電子制御内燃機関
の燃料噴射制御方法であつて、前記複数気筒の燃
料噴射弁より噴射される燃料噴射量を、前記フイ
ードバツク制御方法により制御した期間の空燃比
フイードバツク係数Faと、前記複数気筒の内の
特定気筒nの燃料噴射量については、前記空燃比
センサの出力信号に無関係に制御し、残りの気筒
の燃料噴射量については、前記フイードバツク制
御方法により制御した期間の空燃比フイードバツ
ク係数Fbとに基づき、前記特定気筒nについて
のみの補正値Knを求め、前記フイードバツク係
数Faと前記特定気筒nについてのみの補正値Kn
とに基づき、該気筒nについての燃料噴射量を制
御することを特徴としている。
In order to achieve the above object, the present invention provides a fuel injection valve corresponding to each cylinder of an internal combustion engine,
an air-fuel ratio sensor is provided commonly to a plurality of cylinders, and an air-fuel ratio feedback coefficient for the plurality of cylinders of the internal combustion engine is determined according to an output signal of the air-fuel ratio sensor;
A fuel injection control method for an electronically controlled internal combustion engine in which the air-fuel ratio is controlled by a feedback control method in which a fuel injection corrected based on the coefficient is injected from the fuel injection valve of each of the cylinders, the fuel injection control method comprising: The air-fuel ratio feedback coefficient Fa during the period in which the amount of fuel injected from the valve is controlled by the feedback control method and the amount of fuel injected into a specific cylinder n among the plurality of cylinders are determined by the output signal of the air-fuel ratio sensor. Regarding the fuel injection amount of the remaining cylinders, the correction value Kn only for the specific cylinder n is determined based on the air-fuel ratio feedback coefficient Fb during the period controlled by the feedback control method, and the correction value Kn is calculated based on the feedback coefficient Fa. and the correction value Kn only for the specific cylinder n.
The present invention is characterized in that the fuel injection amount for the cylinder n is controlled based on the above.
本発明は、以下のように作用する。尚、ここで
は理解し易いよう、必須とは限らない用件も追加
し4気筒内燃機関として説明する。
The invention works as follows. In order to make it easier to understand, the description will be made here assuming that the engine is a four-cylinder internal combustion engine, with additional requirements that are not necessarily essential.
() 複数気筒からの排気が接触する位置に設け
られた空燃比センサの出力に基づき、第n気筒
の燃料噴射弁の噴射量Taunは、
Taun=Kn・Fa・Fe・Tp+Tv
にて求められ、第n気筒の噴射弁より、噴射さ
れる。() Based on the output of the air-fuel ratio sensor installed at the position where the exhaust gases from multiple cylinders come into contact, the injection amount Taun of the fuel injection valve of the nth cylinder is calculated as Taun=Kn・Fa・Fe・Tp+Tv, It is injected from the injection valve of the n-th cylinder.
ここで、 Kn:気筒nについてのみ補償値。 here, Kn: Compensation value only for cylinder n.
Fa:上式に求めらる燃料量を噴射した場合に、
空燃比センサの出力に基づいてフイードバツ
ク制御された結果の、複数気筒共通のフイー
ドバツク係数。 Fa: When the amount of fuel determined by the above formula is injected,
Feedback coefficient common to multiple cylinders as a result of feedback control based on the output of the air-fuel ratio sensor.
Fe:空燃比センサ出力以外の、機関運転パラ
メータにより求められる補正係数。 Fe: Correction coefficient determined by engine operating parameters other than the air-fuel ratio sensor output.
Tp:機関の吸入吸気量を主パラメータとして
求められる基本燃料噴射時間。 Tp: Basic fuel injection time determined using the intake air amount of the engine as the main parameter.
Tv:燃料噴射弁の無効噴射時間 これを、所定時間実施する。 Tv: Invalid injection time of fuel injector This is carried out for a predetermined period of time.
() 次に例えば、気筒1について、所定の期間
次の式に噴射量を与える。() Next, for example, for cylinder 1, the injection amount is given to the following equation for a predetermined period.
Tau1=K1・Fe・Tp+Tv
同時に、気筒1以外の残りの気筒について
は、上述した式とは同様な以下の式、
Tau2=K2・Fe・Tp+Tv
Tau3=K3・Fe・Tp+Tv
Tau4=K4・Fe・Tp+Tv
ここで、
Fb:上式にて求められる燃料量Tau1、Tau2、
Tau3、Tau4をそれぞれの噴射弁から噴射し
た場合に、空燃比センサの出力に基づいて、
フイードバツク制御された結果の、フイード
バツク係数。 Tau1=K1・Fe・Tp+Tv At the same time, for the remaining cylinders other than cylinder 1, the following formula is similar to the above formula: Tau2=K2・Fe・Tp+Tv Tau3=K3・Fe・Tp+Tv Tau4=K4・Fe・Tp+Tv Where, Fb: Fuel amount Tau1, Tau2, determined by the above formula
When Tau3 and Tau4 are injected from each injection valve, based on the output of the air-fuel ratio sensor,
Feedback coefficient as a result of feedback control.
にて求まる噴射量を与える。Give the injection amount determined by .
() 上式()、()で求めた、Fa及びFbに
基づき、気筒1についての補正値であるK1を
求める。() Based on Fa and Fb found using the above formulas () and (), find K1, which is the correction value for cylinder 1.
() 次は、気筒2について同様な制御を実施
し、K2を求めるとともに、順次気筒3、気筒
4についても同様な制御を実施する。() Next, similar control is performed for cylinder 2 to obtain K2, and similar control is performed for cylinders 3 and 4 in turn.
以下、実施例を説明する。 Examples will be described below.
まず、本実施例の概要を説明すれば、燃料噴射
弁が各気筒ごとに対応して設けられ、空燃比セン
サが全気筒に共通して設けられ、燃料噴射弁にお
ける燃料噴射量が、空燃比センサからのフイード
バツク信号に基づいて計算されたフイードバツク
係数に関係して補正される電子制御内燃機関の燃
料噴射制御方法において、全気筒の空燃比をフイ
ードバツク制御している期間のフイードバツク係
数の平均値Faを求め、特定の1つの気筒nの空
燃比はオープンループ制御して残りの全気筒の空
燃比はフイードバツク制御している期間のフイー
ドバツク係数の平均値Fbを求め、補正値Knを次
式から計算し、
Kn=1−Fb/C・(1−Fb/Fa)……(1)
ただしCは気筒の総数
特定の1つの気筒6の燃料噴射量をKnに基づ
いて計算する。 First, to explain the outline of this embodiment, a fuel injection valve is provided corresponding to each cylinder, an air-fuel ratio sensor is provided in common to all cylinders, and the fuel injection amount at the fuel injection valve is determined by the air-fuel ratio. In a fuel injection control method for an electronically controlled internal combustion engine that is corrected in relation to a feedback coefficient calculated based on a feedback signal from a sensor, the average value Fa of the feedback coefficient during the period when the air-fuel ratio of all cylinders is feedback-controlled. Find the average value Fb of the feedback coefficient during the period when the air-fuel ratio of one specific cylinder n is under open-loop control and the air-fuel ratio of all remaining cylinders is under feedback control, and calculate the correction value Kn from the following formula. Then, Kn=1-Fb/C (1-Fb/Fa) (1) where C is the total number of cylinders.The fuel injection amount for a specific cylinder 6 is calculated based on Kn.
例えば4気筒電子制御内燃機関における第1気
筒から第4気筒までの各気筒のオープンループ制
御の空燃比をA/F1、A/F2、A/F3、A/F4
と定義する。各気筒の吸入空気量Qは等しいの
で、全空燃比の空燃比がフイードバツク制御され
ている期間では、すなわち各燃料噴射弁における
燃料噴射量をフイードバツク係数で補正している
期間では、1サイクルにおける全気筒の燃料噴射
量の合計は
Fa・Q(1/A/F1+1/A/F2+1/A/F3+
1/A/A/F4) …(2)
となる。 For example, the open-loop control air-fuel ratio of each cylinder from the first cylinder to the fourth cylinder in a four-cylinder electronically controlled internal combustion engine is A/F1, A/F2, A/F3, A/F4.
It is defined as Since the intake air amount Q of each cylinder is the same, during the period when the air-fuel ratio of the total air-fuel ratio is under feedback control, that is, during the period when the fuel injection amount at each fuel injection valve is corrected by the feedback coefficient, the total air-fuel ratio in one cycle is The total amount of fuel injected into the cylinders is Fa·Q (1/A/F1+1/A/F2+1/A/F3+1/A/A/F4)...(2).
燃料噴射量の合計を吸入空気量の合計4Qで割
れば目標空燃比(例えば理論空燃比)の逆数にな
るはずであるので、次式が成立する。 Dividing the total fuel injection amount by the total intake air amount 4Q should yield the reciprocal of the target air-fuel ratio (for example, the stoichiometric air-fuel ratio), so the following equation holds true.
Fa・Q(1/A/F1+1/A/F2+1/A/F3+
1/A/A/F4)=4/14.7 ……(3)
ただし14.7は理論空燃比
さらに特定の1つの気筒n、例えば第1気筒の
空燃比はオープンループ制御して残りの3つの全
気筒の空燃比はフイードバツク制御している期
間、すなわち第1気筒の燃料噴射弁における燃料
噴射量はフイードバツク係数による補正を行なわ
ずに、残りの3つの全気筒の燃料噴射弁における
燃料噴射量はフイードバツク係数による補正を行
なつている期間では1サイクルにおける全気筒の
燃料噴射量の合計は
Q・1/A/F1+Fb・Q
(1/A/F2+1/A/F3+1/A/A/F4) …(4)
となる。Fa・Q(1/A/F1+1/A/F2+1/A/F3+ 1/A/A/F4)=4/14.7...(3) However, 14.7 is the stoichiometric air-fuel ratio. During the period in which the air-fuel ratio of one cylinder is under open-loop control and the air-fuel ratios of all remaining three cylinders are under feedback control, that is, the fuel injection amount at the fuel injection valve of the first cylinder is not corrected by the feedback coefficient. During the period in which the fuel injection amount of the fuel injection valves of the remaining three cylinders is corrected using the feedback coefficient, the total fuel injection amount of all cylinders in one cycle is Q・1/A/F1+Fb・Q (1/ A/F2+1/A/F3+1/A/A/F4) ...(4).
(4)市を4Qで割つた値は理論空燃比の逆数にな
らなければならないから次式をが成立する。 (4) The value obtained by dividing city by 4Q must be the reciprocal of the stoichiometric air-fuel ratio, so the following equation holds true.
1/A/F1+Fb(1/A/F2+1/A/F3
+1/A/A/F4=1/14.7 …(5)
A/F1〜A/F4は(3)式および(5)市から
(1/A/F2+1/A/F3+1/A/A/F4を消去する
と
次式が成立する。1/A/F1+Fb (1/A/F2+1/A/F3 +1/A/A/F4=1/14.7...(5) A/F1 to A/F4 are calculated from equation (3) and (5) by (1 When /A/F2+1/A/F3+1/A/A/F4 is eliminated, the following equation holds true.
1/A/F1=4/14.7・(1−Fb/Fa/1−Fb …(6)
一方、Knを、導入する前お最後燃料噴射時
Tauは例えば次式から定義される。 1/A/F1=4/14.7・(1-Fb/Fa/1-Fb...(6) On the other hand, at the last fuel injection before introducing Kn
Tau is defined, for example, from the following equation.
Tau=Fa・Fe・Tp+Tv …(7)
ただし、
Fe:機関冷却水温度等の機関の他の運転パラ
メータにより計算される補正係数
Ta:(吸入空気流量/機関回転速度)から計算
される基本燃料噴射時間
Tv:燃料噴射弁の無効噴射時間
したがつてA/F1を理論空燃比14.7にするため
にはK1を次式から定義し、
K1=A/F1/14.7 …(8)
第1気筒の最終燃料噴射時間Tau1を次式から
計算すればよい。 Tau=Fa・Fe・Tp+Tv…(7) However, Fe: Correction coefficient calculated from other operating parameters of the engine such as engine cooling water temperature Ta: Basic fuel calculated from (intake air flow rate/engine speed) Injection time Tv: Ineffective injection time of the fuel injector Therefore, in order to make A/F1 the stoichiometric air-fuel ratio of 14.7, K1 is defined from the following formula, K1=A/F1/14.7...(8) The final fuel injection time Tau1 can be calculated from the following formula.
Tau1=K1・Fa・Fe・Tp+Tv …(9) (6)および(8)式からK1は次式から定義される。 Tau1=K1・Fa・Fe・Tp+Tv…(9) From equations (6) and (8), K1 is defined from the following equation.
K1=1−Fb/4・(1−Fb/Fa)……(10)
K2〜K4についても同様に定義される。したが
つて気筒の総数がCである内燃機関のn番目の気
筒の補正値Knは(1)式のように定義できる。 K1=1−Fb/4·(1−Fb/Fa) (10) K2 to K4 are defined in the same way. Therefore, the correction value Kn for the n-th cylinder of an internal combustion engine whose total number of cylinders is C can be defined as in equation (1).
なおn番目の気筒についての最終燃料噴射時間
Taunを定義すると、次式のようになる。 Furthermore, the final fuel injection time for the nth cylinder
When Taun is defined, it becomes as follows.
Taun=Kn・Fa・Fe・Tp+Tv …(11)
このように本発明の実施例ではフイードバツク
係数の定義としてのスキツプ量および傾きを増大
することなく、前述のように定義される補正値
Knを導入することにより各燃料噴射弁の流量の
ばらつきを補償し、空燃比制御制度を改善するこ
ともがきる。 Taun=Kn・Fa・Fe・Tp+Tv (11) In this way, in the embodiment of the present invention, the correction value defined as described above is obtained without increasing the skip amount and slope as the definition of the feedback coefficient.
By introducing Kn, it is possible to compensate for variations in the flow rate of each fuel injector and improve the air-fuel ratio control system.
図面を参照して説明する。 This will be explained with reference to the drawings.
第1図はは4気筒電子制御内燃機関の概略図で
ある。吸気通路1には上流から順番にエアフロー
メーター2、吸気温センサ3、絞り弁4、サージ
タンク5、吸気管6が設けられている。燃料噴射
弁7は各気筒に対応して吸気管6に取付けられ、
吸気系へ燃料を噴射する。燃焼室11は、点火プ
ラグ12を備え、シリンダヘツド13、シリンダ
ブロツク14、およびピストン15により固定さ
れ、吸気弁16を経て混合気を供給される。燃焼
室11で燃焼した混合気は排気弁19を経て排気
管20へ排出される。酸素センサ21は排気中の
酸素濃度を検出し、水温センサ22はシリンダブ
ロツク14に取付けられて冷却水温度を検出す
る。気筒判別センサ25および回転角センサ26
は配電器27の軸28の回転からクランク角を検
出する。気筒判別センサ25および回転角センサ
26はクランク角がそれぞれ720°および30°変化
するごとにパルス発生する。アイドルスイツチ2
9は絞り弁4がアイドルリング開度にあるか否か
を検出する。電子制御装置31は、各種センサか
ら入力信号を受け、燃料噴射弁7および点火装置
32へ出力信号を送る。点火装置32の二次点火
電流は配電器27を経て点火プラグ12へ送られ
る。 FIG. 1 is a schematic diagram of a four-cylinder electronically controlled internal combustion engine. An air flow meter 2, an intake temperature sensor 3, a throttle valve 4, a surge tank 5, and an intake pipe 6 are provided in the intake passage 1 in this order from upstream. A fuel injection valve 7 is attached to the intake pipe 6 corresponding to each cylinder,
Inject fuel into the intake system. The combustion chamber 11 includes a spark plug 12, is fixed by a cylinder head 13, a cylinder block 14, and a piston 15, and is supplied with an air-fuel mixture through an intake valve 16. The air-fuel mixture combusted in the combustion chamber 11 is discharged to the exhaust pipe 20 via the exhaust valve 19. An oxygen sensor 21 detects the oxygen concentration in exhaust gas, and a water temperature sensor 22 is attached to the cylinder block 14 to detect the temperature of cooling water. Cylinder discrimination sensor 25 and rotation angle sensor 26
detects the crank angle from the rotation of the shaft 28 of the power distributor 27. The cylinder discrimination sensor 25 and the rotation angle sensor 26 generate pulses every time the crank angle changes by 720° and 30°, respectively. idle switch 2
9 detects whether or not the throttle valve 4 is at the idle ring opening degree. The electronic control device 31 receives input signals from various sensors and sends output signals to the fuel injection valve 7 and the ignition device 32. The secondary ignition current of the ignition device 32 is sent to the spark plug 12 via the power distributor 27.
第2図は電子制御装置31の内部のブロツク図
である。RAM35、ROM36、CPU37、入
出力ポート38,39、出力ポート40a〜40
d,41はバス42を介して互いに接続されてい
る。CLOCK43はCPU37へクロツクパルスを
送る。エアフローメーター2および吸気温センサ
3のアナログ出力はバツフア45,46を経てマ
ルチプレクサ47へ送られる。マルチプレクサ4
7は入力信号を選択し、選択された入力信号は
A/D(アナログ/デジタル)変換器48におい
てA/D変換されてから入出力ポート38へ送ら
れる。酸素センサ21の出力はバツフア50およ
びコンパレータ51を経て入出力ポート39へ送
られ、気筒判別センサ25および回転角センサ2
6の出力は整形回路53を経て入出力ポート39
へ送られ、アイドルスイツチ29の出力は直接入
出力ポート39へ送られる。各燃料噴射弁7a〜
7dは出力ポート40a〜40dから駆動回路5
5a〜55dを経て入力信号を受け、点火装置3
2は出力ポート41から駆動回路56を経手て入
力信号を受ける。 FIG. 2 is a block diagram of the inside of the electronic control unit 31. RAM35, ROM36, CPU37, input/output ports 38, 39, output ports 40a to 40
d and 41 are connected to each other via a bus 42. CLOCK43 sends a clock pulse to CPU37. The analog outputs of the air flow meter 2 and the intake air temperature sensor 3 are sent to a multiplexer 47 via buffers 45 and 46. multiplexer 4
7 selects an input signal, and the selected input signal is A/D converted by an A/D (analog/digital) converter 48 and then sent to the input/output port 38. The output of the oxygen sensor 21 is sent to the input/output port 39 via the buffer 50 and the comparator 51, and is sent to the cylinder discrimination sensor 25 and the rotation angle sensor 2.
The output of 6 passes through the shaping circuit 53 to the input/output port 39.
The output of the idle switch 29 is sent directly to the input/output port 39. Each fuel injection valve 7a~
7d is the drive circuit 5 from the output ports 40a to 40d.
The ignition device 3 receives an input signal via 5a to 55d.
2 receives an input signal from the output port 41 via the drive circuit 56.
第3図は燃料噴射弁7a〜7dの流量のばらつ
きを補償するための補正値Knの計算ルーチンの
フローチヤートである。全気筒の空燃比をフイー
ドバツク制御している期間のフイードバツク係数
Faを求め、特定の1つの気筒nの空燃比はオー
プンループ制御して残りの全気筒の空燃比はフイ
ードバツク制御している期間のフイードバツク係
数の平均値Fbを求め、Fa、Fbから前述の(1)式に
基づいてKnが計算される。Knは前述の(11)式
で示した通り、最終燃料噴射時間Taunの計算の
際に乗算項として用いられ、この結果、各燃料噴
射弁7a〜7dの流量のばらつきにもかかわら
ず、各気筒の空燃比は目標空燃比として理論空燃
比に制御される。各ステツプを詳述するとステツ
プ62では補正値Knの計算条件が成立しているか
否かを判定し、判定が正であればステツプ64以降
へ進む。計算条件としては、暖機がすでに終了し
ていること、空燃比のフイードバツク条件が成立
していること、および定常状態(非過度時の例え
ば40Km/h走行時)であることが挙げられる。ス
テツプ64ではnに初期値としての1を代入する。
nは補正値Knを計算する気筒番号である。ステ
ツプ66では全気筒の空燃比をフイードバツク制御
し、この期間のフイードバツク係数の平均値Fa
を取込む。フイードバツク係数は、酸素センサ2
1が濃(リツチ)信号あるいは薄(リーン)信号
を維持している期間では減少あるいは増大し、濃
信号から薄信号へあるいはその逆へ変化した時に
は応答性改善のためにスキツプを付与される。平
均値はスキツプ値前のフイードバツク係数を複数
個取込み、平均化して求めてもよい。ステツプ68
ではn番目の気筒の空燃比のみをオープンループ
制御し(フイードバツク制御の中止)、すなわち
フイードバツク係数により燃料噴射量を補正せ
ず、n番目の気筒以外の他の残りの気筒の燃料噴
射量はフイードバツク制御し、この期間のフイー
ドバツク係数の平均値Fbを取込む。ステツプ70
では仮のKnを前述の(1)式に従つて計算する。ス
テツプ72ではステツプ70の仮のKnを真のKnに代
入する。ステツプ70の仮のKnの真のKnに直接代
入しないで、今までの真のKnとステツプ70の仮
のKnとの平均値を真のKnに代入してもよい。な
お真のKnの初期値は1.0に設定されている。ステ
ツプ74ではn+1をnに代入する。ステツプ76で
はn>4か否かを判定し、判定が否であれはステ
ツプ66へ戻り、判定が正であればこのルーチンを
終了する。こうしてK1〜K4が計算される。 FIG. 3 is a flowchart of a calculation routine for a correction value Kn for compensating for variations in the flow rates of the fuel injection valves 7a to 7d. Feedback coefficient during feedback control of air-fuel ratio of all cylinders
Find Fa, then find the average value Fb of the feedback coefficient during the period when the air-fuel ratio of one specific cylinder n is under open-loop control and the air-fuel ratio of all remaining cylinders is under feedback control, and from Fa and Fb, calculate the above-mentioned ( 1) Kn is calculated based on the formula. As shown in equation (11) above, Kn is used as a multiplication term when calculating the final fuel injection time Taun, and as a result, despite the variation in the flow rate of each fuel injection valve 7a to 7d, The air-fuel ratio is controlled to the stoichiometric air-fuel ratio as the target air-fuel ratio. To explain each step in detail, in step 62, it is determined whether the calculation conditions for the correction value Kn are satisfied, and if the determination is positive, the process proceeds to step 64 and subsequent steps. The calculation conditions include that warm-up has already been completed, that air-fuel ratio feedback conditions are met, and that the vehicle is in a steady state (for example, when traveling at 40 km/h in a non-transient state). In step 64, 1 is assigned to n as an initial value.
n is the cylinder number for calculating the correction value Kn. In step 66, the air-fuel ratio of all cylinders is feedback-controlled, and the average value Fa of the feedback coefficient during this period is
take in. The feedback coefficient is oxygen sensor 2
1 decreases or increases while maintaining a rich signal or a lean signal, and when the signal changes from a rich signal to a thin signal or vice versa, a skip is given to improve responsiveness. The average value may be obtained by taking in a plurality of feedback coefficients before the skip value and averaging them. step 68
In this case, only the air-fuel ratio of the n-th cylinder is controlled in open loop (feedback control is stopped), that is, the fuel injection amount is not corrected by the feedback coefficient, and the fuel injection amount of the remaining cylinders other than the n-th cylinder is controlled by the feedback control. control and take in the average value Fb of the feedback coefficient during this period. step 70
Now, calculate the temporary Kn according to equation (1) above. In step 72, the temporary Kn in step 70 is substituted for the true Kn. Instead of directly assigning the temporary Kn of step 70 to the true Kn, the average value of the true Kn up to now and the temporary Kn of step 70 may be substituted to the true Kn. Note that the initial value of true Kn is set to 1.0. At step 74, n+1 is assigned to n. In step 76, it is determined whether n>4, and if the determination is negative, the process returns to step 66, and if the determination is positive, this routine is ended. In this way, K1 to K4 are calculated.
以上述べたように、本発明によれば、各気筒の
空燃比を、燃料噴射弁の流量ばらつきによらず、
精度良く制御することができ、また、空燃比セン
サの出力すべてを読み込んでいない制御装置へも
適用でき、さらに、空燃比センサが、どの気筒の
空燃比を検出しているかの、困難な判断も必要な
いので、正確な空燃比制御が達成される。
As described above, according to the present invention, the air-fuel ratio of each cylinder can be adjusted without depending on the flow rate variations of the fuel injection valves.
It can be controlled with high accuracy, and can be applied to control devices that do not read all the outputs of the air-fuel ratio sensor, and can also be used to make difficult decisions about which cylinder's air-fuel ratio is being detected by the air-fuel ratio sensor. Accurate air/fuel ratio control is achieved since no need exists.
第1図は本発明が適用される電子制御内燃機関
の概略図、第2図は第1図の電子制御装置のブロ
ツク図、第3図は各燃料噴射弁の流量のばらつき
を補償するための補正値の計算ルーチンのフロー
チヤートである。
7,7a〜7d……燃料噴射弁、11……燃焼
室、21……酸素センサ、31……電子制御装
置。
FIG. 1 is a schematic diagram of an electronically controlled internal combustion engine to which the present invention is applied, FIG. 2 is a block diagram of the electronic control device of FIG. 7 is a flowchart of a correction value calculation routine. 7,7a-7d...Fuel injection valve, 11...Combustion chamber, 21...Oxygen sensor, 31...Electronic control device.
Claims (1)
て設けられ、空燃比センサが複数気筒共通に設け
られ、該空燃比センサの出力信号に応じて前記内
燃機関の複数気筒に対する空燃比フイードバツク
係数を求め、該係数の基づき補正された燃料噴射
料が前記各気筒の燃料噴射弁より噴射されるフイ
ードバツク制御方法により所定空燃比に制御され
る電子制御内燃機関の燃料噴射制御方法であつ
て、 前記複数気筒の燃料噴射弁より噴射される燃料
噴射量を、前記フイードバツク制御方法により制
御した期間の空燃比フイードバツク係数Faと、 前記複数気筒の内の特定気筒nの燃料噴射量に
ついては、前記空燃比センサの出力信号に無関係
に制御し、同時に残りの気筒の燃料噴射量につい
ては、前記フイードバツク制御方法により制御し
た期間の空燃比フイードバツク係数Fbとに基づ
き、前記特定気筒nについてのみ補正値Knを求
め、 前記空燃比フイードバツク係数Faと前記特定
気筒nについてのみ補正値Knとに基づき、該気
筒nについてほ燃料噴射量を制御する電子制御内
燃機関の燃料噴射制御方法。[Scope of Claims] 1. A fuel injection valve is provided correspondingly to each cylinder of the internal combustion engine, an air-fuel ratio sensor is provided in common to the plurality of cylinders, and an air-fuel ratio sensor is provided in common to the plurality of cylinders of the internal combustion engine according to an output signal of the air-fuel ratio Fuel injection control of an electronically controlled internal combustion engine in which the air-fuel ratio is controlled to a predetermined air-fuel ratio by a feedback control method in which an air-fuel ratio feedback coefficient for a cylinder is determined and fuel injection corrected based on the coefficient is injected from a fuel injection valve of each cylinder. The method comprises: an air-fuel ratio feedback coefficient Fa during a period in which the amount of fuel injected from the fuel injection valves of the plurality of cylinders is controlled by the feedback control method; and an amount of fuel injection for a specific cylinder n among the plurality of cylinders. is controlled regardless of the output signal of the air-fuel ratio sensor, and at the same time, the fuel injection amount of the remaining cylinders is controlled for the specific cylinder n based on the air-fuel ratio feedback coefficient Fb of the period controlled by the feedback control method. A fuel injection control method for an electronically controlled internal combustion engine, wherein a correction value Kn is determined only for the specific cylinder n, and a fuel injection amount is controlled for the specific cylinder n based on the air-fuel ratio feedback coefficient Fa and the correction value Kn only for the specific cylinder n.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7930583A JPS59206619A (en) | 1983-05-09 | 1983-05-09 | Method of controlling fuel injection amount in electronically controlled internal-combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7930583A JPS59206619A (en) | 1983-05-09 | 1983-05-09 | Method of controlling fuel injection amount in electronically controlled internal-combustion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59206619A JPS59206619A (en) | 1984-11-22 |
| JPH045819B2 true JPH045819B2 (en) | 1992-02-03 |
Family
ID=13686128
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7930583A Granted JPS59206619A (en) | 1983-05-09 | 1983-05-09 | Method of controlling fuel injection amount in electronically controlled internal-combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59206619A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0949451A (en) * | 1995-08-08 | 1997-02-18 | Hitachi Ltd | Engine controller |
-
1983
- 1983-05-09 JP JP7930583A patent/JPS59206619A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59206619A (en) | 1984-11-22 |
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