JPH0249940A - Internal combustion engine fuel supply control device - Google Patents

Internal combustion engine fuel supply control device

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Publication number
JPH0249940A
JPH0249940A JP19888088A JP19888088A JPH0249940A JP H0249940 A JPH0249940 A JP H0249940A JP 19888088 A JP19888088 A JP 19888088A JP 19888088 A JP19888088 A JP 19888088A JP H0249940 A JPH0249940 A JP H0249940A
Authority
JP
Japan
Prior art keywords
rate
injection
fuel injection
injection valve
fuel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP19888088A
Other languages
Japanese (ja)
Inventor
Masamichi Imamura
政道 今村
Hiroki Sunou
宏紀 数納
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Japan Electronic Control Systems Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Japan Electronic Control Systems Co Ltd filed Critical Japan Electronic Control Systems Co Ltd
Priority to JP19888088A priority Critical patent/JPH0249940A/en
Publication of JPH0249940A publication Critical patent/JPH0249940A/en
Pending legal-status Critical Current

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

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は、予混合気形成用の予備噴射を行う内燃機関の
燃料供給制御装置に関する。
DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to a fuel supply control device for an internal combustion engine that performs preliminary injection for forming a premixture.

〈従来の技術) 気筒毎に主燃料噴射弁を備える一方、吸気通路の上流部
で補助燃料噴射弁を設けて予備噴射を行い予混合気を形
成して気化熱による冷却作用で充填効率を高めたり、燃
焼性向上を図るようにしたものがある。
<Prior art> While each cylinder is equipped with a main fuel injection valve, an auxiliary fuel injection valve is provided upstream of the intake passage to perform preliminary injection, form a premixture, and increase charging efficiency through the cooling effect of vaporization heat. There are also some that are designed to improve flammability.

尚、この種の予混合気形成を行うものでは、補助噴射弁
の下流側に超音波微粒化装置を設け、補助燃料噴射弁か
ら噴射された燃料を超音波装置の振動子に付着させて微
粒化を促進するようにしたものが一般化している(実開
昭62−200157号公報等参照)。
In addition, in a device that performs this type of premixture formation, an ultrasonic atomization device is installed downstream of the auxiliary fuel injection valve, and the fuel injected from the auxiliary fuel injection valve is made to adhere to the vibrator of the ultrasonic device and become atomized. A device designed to promote the change in speed has become common (see Japanese Utility Model Application Publication No. 62-200157, etc.).

〈発明が解決しようとする課題〉 ところで、従来のこの種の装置にあっては、主燃料噴射
弁と補助燃料噴射弁との総噴射量に対する噴射量割合(
以下噴射率という)は予め設定された値に固定されてい
るが、過渡運転時においては、補助燃料噴射弁による噴
射率、即ち予混合率が高いと補助燃料噴射弁は上流側に
設けられているため、予備噴射された燃料の吸気通路壁
面への付着による燃焼室への供給遅れが大きくなり、空
燃比が加速時にはリーン、減速時にはリッチとなってし
まい過渡運転性能を損ねてしまうことがあった。
<Problems to be Solved by the Invention> By the way, in conventional devices of this type, the injection amount ratio (
The injection rate (hereinafter referred to as injection rate) is fixed to a preset value, but during transient operation, if the injection rate by the auxiliary fuel injection valve, that is, the premixing rate is high, the auxiliary fuel injection valve is installed on the upstream side. This increases the delay in the supply of pre-injected fuel to the combustion chamber due to adhesion to the intake passage wall, causing the air-fuel ratio to become lean during acceleration and rich during deceleration, impairing transient driving performance. Ta.

本発明は、このような従来の問題点に鑑みなされたもの
で、過渡運転時には運転状態に応じた減少率で補助燃料
噴射弁の噴射率を減少させることにより空燃比の変化を
抑制して過渡運転性能の向上を図ることを目的とする。
The present invention was developed in view of these conventional problems. During transient operation, the injection rate of the auxiliary fuel injector is reduced at a reduction rate according to the operating condition, thereby suppressing changes in the air-fuel ratio and reducing transient operation. The purpose is to improve driving performance.

また、このようにして過渡運転時に噴射率を変化させた
後、定常運転に移行する際には、前噴射弁の噴射率を同
時に変化させると燃料供給遅れの差により空燃比が変動
してしまう。
In addition, after changing the injection rate during transient operation in this way, when transitioning to steady operation, if the injection rate of the front injector is changed at the same time, the air-fuel ratio will fluctuate due to the difference in fuel supply delay. .

そこで、この場合は主燃料噴射弁の噴射率の変化を遅ら
せることにより、空燃比の変動を抑制することを第2の
目的とする。
Therefore, in this case, the second objective is to suppress fluctuations in the air-fuel ratio by delaying changes in the injection rate of the main fuel injector.

〈課題を解決するための手段〉 このため本発明は第1図に示すように、気筒毎に燃料噴
射する主燃料噴射弁を備えると共に、吸気通路の上流部
に全気筒に対して燃料噴射する予混合気形成用の補助燃
料噴射弁を備えてなる内燃機関の燃料供給制御装置にお
いて、機関の絞り弁開度の変化率を検出する絞り弁開度
変化率検出手段と、機関の冷却水温度を検出する水温検
出手段と、前記主燃料噴射弁及び補助燃料噴射弁からの
総噴射量に対する補助燃料噴射弁からの噴射量割合であ
る噴射率を、過渡運転時に絞り弁開度の変化率と冷却水
温度との検出値に基づいて減少させる予混合率制御手段
と、を含んで構成する。
<Means for Solving the Problems> Therefore, as shown in FIG. 1, the present invention includes a main fuel injection valve that injects fuel to each cylinder, and also injects fuel to all cylinders in the upstream portion of the intake passage. In a fuel supply control device for an internal combustion engine that includes an auxiliary fuel injection valve for forming a premixture, a throttle valve opening rate change detection means for detecting a rate of change in a throttle valve opening degree of the engine; and an injection rate, which is a ratio of the injection amount from the auxiliary fuel injection valve to the total injection amount from the main fuel injection valve and the auxiliary fuel injection valve, as a rate of change in the throttle valve opening during transient operation. The premixing ratio control means is configured to reduce the premixing ratio based on the detected value of the cooling water temperature.

また、前記第2の目的達成のため、前記主燃料噴射弁及
び補助燃料噴射弁からの総噴射量に対する補助燃料噴射
弁からの噴射量割合である噴射率を、過渡運転時に減少
させる第1予混合率制御手段と、過渡運転から定常運転
に移行する際に、前記補助燃料噴射弁の噴射率を定常運
転時の噴射率に戻す変化速度に対して、主燃料噴射弁の
噴射率を定常運転時の噴射率に戻す変化速度に遅れを持
たせて制御する第2予混合率制御手段と、を含んで構成
する。
In addition, in order to achieve the second objective, a first prediction is made to reduce the injection rate, which is the ratio of the injection amount from the auxiliary fuel injection valve to the total injection amount from the main fuel injection valve and the auxiliary fuel injection valve, during transient operation. a mixture ratio control means; when transitioning from transient operation to steady operation, the injection rate of the main fuel injector is adjusted to the steady state operation with respect to the rate of change in which the injection rate of the auxiliary fuel injector returns to the injection rate during steady operation; and second premixing ratio control means for controlling the rate of change to return to the original injection rate with a delay.

く作用〉 過渡運転時には、予混合率制御手段により、補助燃料噴
射弁の噴射率が絞り弁開度の変化率及び冷却水温度の検
出値に基づいて制御される。
Effect> During transient operation, the injection rate of the auxiliary fuel injection valve is controlled by the premix ratio control means based on the rate of change of the throttle valve opening and the detected value of the cooling water temperature.

ここで、絞り弁開度の変化率及び冷却水温度に基づいて
過渡の程度に応じた予備噴射燃料の吸気通路壁面への付
着量を推定することができる。したがって、該付着量に
対する供給遅れに見合って補助燃料噴射弁の噴射率を減
少させることにより空燃比の変化が効果的に抑制される
Here, it is possible to estimate the amount of pre-injected fuel adhering to the intake passage wall surface in accordance with the degree of transient based on the rate of change of the throttle valve opening degree and the cooling water temperature. Therefore, by reducing the injection rate of the auxiliary fuel injection valve in proportion to the supply delay with respect to the deposited amount, changes in the air-fuel ratio can be effectively suppressed.

また、第1予混合制御手段により、上記等の方法によっ
て過渡運転時に補助燃料噴射弁の噴射率を減少させた後
、定常運転に移行する際に第2予混合率制御手段は、補
助燃料噴射弁の噴射率の変化率に対して、主燃料噴射弁
の噴射率の変化率に遅れを持たせて制御するため、この
間の空燃比の変動も抑制される。
Further, after the first premixing control means reduces the injection rate of the auxiliary fuel injection valve during transient operation by the method described above, the second premixing ratio control means decreases the injection rate of the auxiliary fuel injection valve when transitioning to steady operation. Since the rate of change in the injection rate of the main fuel injection valve is controlled with a delay with respect to the rate of change in the injection rate of the valve, fluctuations in the air-fuel ratio during this time are also suppressed.

〈実施例〉 以下に、本発明の実施例を図面に基づいて説明する。<Example> Embodiments of the present invention will be described below based on the drawings.

一実施例の構成を示す第2図において、内燃機関1には
、吸気マニホールド2の各気筒の吸気ポート毎に所定の
タイミングで燃料噴射する主燃料噴射弁3が装着される
と共に、絞り弁4の上流側(若しくは下流側)近傍の吸
気通路上流部に全気筒に対して燃料噴射する補助燃料噴
射弁5が装着されている。
In FIG. 2 showing the configuration of one embodiment, an internal combustion engine 1 is equipped with a main fuel injection valve 3 that injects fuel at a predetermined timing for each intake port of each cylinder of an intake manifold 2, and a throttle valve 4. An auxiliary fuel injection valve 5 that injects fuel to all cylinders is installed at the upstream side of the intake passage near the upstream side (or downstream side) of the engine.

前記絞り弁4の下流側近傍には超音波微粒化装置6の振
動子6Aが設けられ、補助燃料噴射弁から噴射された燃
料を付着させて超音波振動により微粒化させる。
A vibrator 6A of an ultrasonic atomization device 6 is provided near the downstream side of the throttle valve 4, and the fuel injected from the auxiliary fuel injection valve is attached thereto and atomized by ultrasonic vibration.

前記絞り弁4には、該絞り弁4の開度を検出するスロッ
トルセンサ7が連結され、吸気マニホールド2の絞り弁
4より上流部には吸入空気流量Qを検出するエアフロー
メータ8が設けられる。この他、機関回転速度N検出用
のクランク角センサ9、冷却水温度検出手段としての水
温センサ10゜空燃比フィードバック制御用の空燃比検
出のため排気中の酸素濃度を検出する0□センサ11等
からの各信号がコントロールユニット12に入力され、
コントロールユニット12はこれら各信号に基づいて、
運転状態に応じた主燃料噴射弁3と補助燃料噴射弁5か
らの各燃料噴射量及び噴射時期を設定するようになって
いる。
A throttle sensor 7 that detects the opening degree of the throttle valve 4 is connected to the throttle valve 4, and an air flow meter 8 that detects the intake air flow rate Q is provided upstream of the throttle valve 4 of the intake manifold 2. In addition, there is a crank angle sensor 9 for detecting the engine rotation speed N, a water temperature sensor 10 as a cooling water temperature detecting means, a 0□ sensor 11 for detecting the oxygen concentration in exhaust gas to detect the air-fuel ratio for air-fuel ratio feedback control, etc. Each signal from is input to the control unit 12,
Based on these signals, the control unit 12
The fuel injection amount and injection timing from the main fuel injection valve 3 and the auxiliary fuel injection valve 5 are set according to the operating state.

次に、前記コントロールユニット12による燃料噴射制
御を第3図に示したフローチャートに従って説明する。
Next, fuel injection control by the control unit 12 will be explained according to the flowchart shown in FIG.

ステップ(図ではSと記す)1では、各種センサ類から
の信号を読み込む。
In step 1 (denoted as S in the figure), signals from various sensors are read.

ステップ2では、機関回転1回転当たりの気筒毎の燃料
噴射量を主燃料噴射弁3のみで得る場合の基本噴射パル
ス幅MT、を次式により演算する。
In step 2, the basic injection pulse width MT when the fuel injection amount for each cylinder per engine rotation is obtained only by the main fuel injection valve 3 is calculated using the following equation.

M T F ”” K ’ Q / Nステップ3では
、機関回転速度Nと前記MT。
M T F ""K' Q/N In step 3, the engine rotation speed N and the MT.

とに基づいてROMに記憶されたマツプから定常運転状
態に対応する予混合率KRBINJを検索する。
Based on this, the premix ratio KRBINJ corresponding to the steady operating state is searched from the map stored in the ROM.

ステップ4では、スロットルセンサ7からの検出された
絞り弁4開度θの今回値と前回値との差即ち絞り弁開度
の変化率Δθを演算する。したがって、スロットルセン
サ7と、このステップ4の機能とで絞り弁開度変化率検
出手段が構成される。
In step 4, the difference between the current value and the previous value of the throttle valve 4 opening degree θ detected from the throttle sensor 7, that is, the rate of change Δθ of the throttle valve opening degree is calculated. Therefore, the throttle sensor 7 and the function of step 4 constitute a throttle valve opening change rate detection means.

ステップ5では、前記絞り弁開度変化率Δθが0か否か
を判定する。
In step 5, it is determined whether the throttle valve opening degree change rate Δθ is 0 or not.

0でない過渡運転状態と判定されたときは、ステップ6
へ進み、前記絞り弁開度変化率Δθに基づいてROMに
記憶されたマツプから基本予混台率減少割合TDAPR
[!を検索する。
If it is determined that the transient operating state is not 0, step 6
, and calculates the basic premixing rate reduction rate TDAPR from the map stored in the ROM based on the throttle valve opening change rate Δθ.
[! Search for.

ここで、TDAPREは、Δθの絶対値が大である程大
に設定されているが、減速時(Δθく0)は減速前の燃
料壁流が流入することによるリッチ化の影響が大きいた
め、加速時(Δθ>O)より大きく設定されている(第
5図(A)参照)。
Here, TDAPRE is set to be large as the absolute value of Δθ is large, but during deceleration (Δθ 0), the effect of enrichment due to the inflow of the fuel wall flow before deceleration is large; It is set larger than during acceleration (Δθ>O) (see FIG. 5(A)).

次いでステップ7へ進み、水温センサ10により検出さ
れた冷却水温度(以下水温という)TI−に基づいてR
OMに記憶されたマツプから予混台率減少割合水温補正
率TTPREを検索する。ここで、TTPRII!は水
温T、4が低温である程気化されないまま壁流となって
付着する量が多いので、太き(設定されている(第5図
(B)参照)。
Next, the process proceeds to step 7, where R is determined based on the cooling water temperature (hereinafter referred to as water temperature) TI- detected by the water temperature sensor 10.
The pre-mixing vehicle rate reduction rate water temperature correction factor TTPRE is searched from the map stored in the OM. Here, TTPRII! is set to be thicker (see FIG. 5(B)) because the lower the water temperature T and 4, the greater the amount of water that adheres as a wall flow without being vaporized (see FIG. 5(B)).

ステップ8では、前記検索された基本予混合率KRB 
INJと、前記基本予混台率減少割合TDAPRE及び
予混台率減少割合水温補正率TTPRHとに基づいて次
式により予混合率RBINJを演算する。
In step 8, the retrieved basic premix ratio KRB
The premixing rate RBINJ is calculated by the following formula based on INJ, the basic premixing unit rate reduction rate TDAPRE, and the premixing unit rate decrease rate water temperature correction factor TTPRH.

RBINJ −KRBINJ−TDAPREXTTPR
Eこの予混合率RBINJは主燃料噴射弁3と補助燃料
噴射弁5からの総噴射量に対する補助燃料噴射弁5の噴
射量割合である噴射率に相当する値であり、したがって
前記各マツプとステップ6.7゜8の機能とが予混合率
制御手段(第1予混合率制御手段)に相当する。
RBINJ-KRBINJ-TDAPREXTTPR
EThis premix ratio RBINJ is a value corresponding to the injection rate, which is the ratio of the injection amount of the auxiliary fuel injection valve 5 to the total injection amount from the main fuel injection valve 3 and the auxiliary fuel injection valve 5, and therefore, each of the above maps and steps The function of 6.7°8 corresponds to the premixing ratio control means (first premixing ratio control means).

一方、ステップ5での判定で絞り弁開度変化率Δθが0
.即ち定常運転状態と判定されたときはステップ9に進
み、前回設定された補正予混合率RBINJ −+と基
本予混合率にRBINJとの差が0か否かを判定する。
On the other hand, in the judgment in step 5, the throttle valve opening degree change rate Δθ is 0.
.. That is, when it is determined that the operating state is steady, the process proceeds to step 9, where it is determined whether the difference between the previously set corrected premixing ratio RBINJ -+ and the basic premixing ratio RBINJ is 0.

ΔθがOでないとき、つまり過渡運転から定常運転に移
行した際は、ステップlOに進み、予混合変化率TBI
NJを次式により演算する。
When Δθ is not O, that is, when transition is made from transient operation to steady operation, the process proceeds to step lO, and the premixing change rate TBI
NJ is calculated using the following formula.

T81NJ=T、。、 XKPRED ここで、Tい、fはクランク角センサ9から気筒間の回
転角位相差(4気筒では180°)毎に出力される基準
信号の入力周期、 KPREDは予混合率の変化割合を
示す。
T81NJ=T. . .

次いでステップ1工に進み、主燃料噴射弁3の噴射率の
変化速度を補助燃料噴射弁5の噴射率の変化速度に対し
て遅らせるための予混合変化率補正値KBINJを次式
により演算する。
Next, proceeding to step 1, a premixing change rate correction value KBINJ for delaying the change rate of the injection rate of the main fuel injection valve 3 with respect to the change rate of the injection rate of the auxiliary fuel injection valve 5 is calculated using the following equation.

KBINJ =にINJN XKINJTWXKTNJ
TVOXKINJSBここでにINJNは機関回転速度
N、KINJTWは水温TWIにINJTVOは絞り弁
開度θ、KINJSBは補助燃料噴射弁5の噴射パルス
幅STiに対して夫々第6図に示すように設定された係
数である。
KBINJ = INJN XKINJTWXKTNJ
TVOXKINJSB Here, INJN is the engine rotation speed N, KINJTW is the water temperature TWI, INJTVO is the throttle valve opening θ, and KINJSB is the injection pulse width STi of the auxiliary fuel injection valve 5, respectively, as shown in FIG. It is a coefficient.

次いで、ステップ12へ進み、前回の補正予混合率RB
INJ −+に前記演算された予混合変化率TBINJ
を加算することにより新たな補正予混合率RBINJを
設定する。
Next, the process proceeds to step 12, where the previous corrected premixing ratio RB
The calculated premixing change rate TBINJ is added to INJ −+.
A new corrected premixing ratio RBINJ is set by adding .

ステップ13では、主燃料噴射弁3の噴射率設定用の係
数MRBINJを次式により演算する。
In step 13, a coefficient MRBINJ for setting the injection rate of the main fuel injection valve 3 is calculated using the following equation.

MRBINJ =RBINj −++TBINJ XK
BINJステップ14では予混合率RBINJと基本予
混合率KRBINJとを比較し、IIBINJ≦KII
BINJのときはステップ15に進んで、基本予混合率
KRBINJを最新の予混合率RBINJ及び係数MR
BINJとして更新するが、RBINJ >にRBIN
Jのときは、予混合率は既に定常時の設定値である基本
予混合率KRBINJに達しているので、このルーチン
を終了する。
MRBINJ =RBINj −++TBINJ XK
In the BINJ step 14, the premix ratio RBINJ and the basic premix ratio KRBINJ are compared, and IIBINJ≦KII
If BINJ, proceed to step 15 and convert the basic premixing ratio KRBINJ to the latest premixing ratio RBINJ and coefficient MR.
Update as BINJ, but RBINJ > RBIN
In the case of J, the premixing ratio has already reached the basic premixing ratio KRBINJ, which is the set value during steady state, so this routine ends.

尚、ステップ9の判定が0であるときも、ステップ15
に進む。
Note that even when the determination in step 9 is 0, step 15
Proceed to.

次に、かかる予混合率RBINJ、係数MRBINJを
用いて主燃料噴射弁3と補助燃料噴射弁5からの燃料噴
射量MTi とSTIとを演算するルーチンを第4図に
従って説明する。
Next, a routine for calculating the fuel injection amount MTi and STI from the main fuel injection valve 3 and the auxiliary fuel injection valve 5 using the premix ratio RBINJ and the coefficient MRBINJ will be explained with reference to FIG.

ステップ21では、主燃料噴射弁3の有効噴射ノぐルス
幅MT、を次式により演算する。
In step 21, the effective injection noggle width MT of the main fuel injection valve 3 is calculated using the following equation.

MT、−MT、  ・α・K、・C0EF・ (1−M
RBINJ) ここで、αは0.センサ11からの信号に基づいて比例
積分制御等により設定される空燃比フィードバック制御
用のフィードバック補正係数、K。
MT, -MT, ・α・K, ・C0EF・ (1-M
RBINJ) Here, α is 0. A feedback correction coefficient K for air-fuel ratio feedback control that is set by proportional-integral control or the like based on a signal from the sensor 11.

はフィードバック補正係数αを基準値に近づけて過渡運
転時の応答性向上を図るための学習補正係数、C0EF
は水温Tい等に基づいて設定される各種補正係数を示す
C0EF is a learning correction coefficient for improving responsiveness during transient operation by bringing the feedback correction coefficient α closer to the reference value.
indicates various correction coefficients set based on water temperature, etc.

ステップ22では、機関の1/2回転毎に行われる主燃
料噴射弁5の最終的な燃料噴射パルス幅MT。
In step 22, the final fuel injection pulse width MT of the main fuel injection valve 5 is determined every 1/2 revolution of the engine.

を次式により演算する。is calculated using the following formula.

MT、=2XMT、+MTs 但し、MT、はバッテリ電圧に基づく主燃料噴射弁3の
無効噴射パルス幅である。
MT, = 2XMT, +MTs where MT is the invalid injection pulse width of the main fuel injection valve 3 based on the battery voltage.

゛ステップ23では、前記MT、相当の噴射量を気筒数
分の主燃料噴射弁3で噴射した場合の機関1回転当たり
の総噴射量を1個の補助燃料噴射弁5で得る場合の基本
噴射パルス幅S T Fを次式により演算する。
゛In step 23, the MT performs basic injection when one auxiliary fuel injection valve 5 obtains the total injection amount per engine revolution when a corresponding injection amount is injected by the main fuel injection valves 3 for the number of cylinders. The pulse width S TF is calculated using the following equation.

STP =MT、  ・K。STP = MT, ・K.

但し、K5は同一流量に対する補助燃料噴射弁5と主燃
料噴射弁3の噴射パルス幅の比率を示し、この値は燃料
噴射弁の本数と流量特性の相違によって決定される。
However, K5 indicates the ratio of the injection pulse widths of the auxiliary fuel injection valve 5 and the main fuel injection valve 3 for the same flow rate, and this value is determined depending on the number of fuel injection valves and the difference in flow rate characteristics.

ステップ24では、補助燃料噴射弁5の有効噴射パルス
幅ST、を次式により演算する。
In step 24, the effective injection pulse width ST of the auxiliary fuel injection valve 5 is calculated using the following equation.

ST、=ST、  ・α・C0EF−RBINJステッ
プ25では、補助燃料噴射弁5からの最終的な燃料噴射
パルス幅STiを次式により演算する。
ST, =ST, .alpha..C0EF-RBINJ In step 25, the final fuel injection pulse width STi from the auxiliary fuel injection valve 5 is calculated using the following equation.

ST 五 =1/2XST、  +STs但し、1/2
なる係数は、補助燃料噴射弁5が機関の1回転当たり2
回噴射を行うためであり、S T sはバッテリ電圧に
基づ(補助燃料噴射弁5の無効噴射パルス幅である。
ST 5 = 1/2XST, +STs However, 1/2
The coefficient is 2 per revolution of the engine when the auxiliary fuel injector 5
This is to perform multiple injections, and S T s is based on the battery voltage (ineffective injection pulse width of the auxiliary fuel injection valve 5).

以上のようにして設定されたパルス幅STtを持つ噴射
パルスをクランク角センサ8からの基準クランク角信号
入力毎に補助燃料噴射弁5に出力して予備噴射させる。
An injection pulse having the pulse width STt set as described above is output to the auxiliary fuel injection valve 5 for preliminary injection every time the reference crank angle signal is input from the crank angle sensor 8.

尚、気筒毎の主燃料噴射弁3からの燃料噴射も同一周期
で行われる。
Note that fuel injection from the main fuel injection valve 3 for each cylinder is also performed at the same cycle.

かかる制御を行えば、過渡運転時は、絞り弁開度の変化
率Δθによって求まる加減速の程度と、水温T’wとに
基づいて予混合率RBINJを減少補正するため、補助
燃料噴射弁5から噴射されて壁流となる燃料による空燃
比の変動を効果的に抑制できる(第7図(A)実線参照
:点線は予混合率RBINJを減少させないとき)。
If such control is performed, during transient operation, the auxiliary fuel injection valve 5 is corrected to reduce the premix ratio RBINJ based on the degree of acceleration/deceleration determined by the rate of change Δθ of the throttle valve opening and the water temperature T'w. It is possible to effectively suppress fluctuations in the air-fuel ratio due to fuel injected into a wall flow (see the solid line in FIG. 7(A); the dotted line indicates when the premix ratio RBINJ is not reduced).

また、過渡運転から定常運転に移行する際には補助燃料
噴射弁5からの噴射燃料による空燃比変化に対して主燃
料噴射弁3からの噴射燃料による空燃比変化の応答性が
早いため、補助燃料噴射弁5の噴射率を定常時の噴射率
に戻す変化速度と、主燃料噴射弁3の噴射率を定常時の
噴射率に戻す変化速度とを同一とした場合には、空燃比
が大きく変化するが(第7図(B)の点線参照)、第2
発明を含む本実施例では前者の変化速度を後者の変化速
度に対してを遅らせる構成としたため、空燃比の変化を
抑制できる(第7図(B)の実線参照)。
In addition, when transitioning from transient operation to steady operation, the response of the air-fuel ratio change due to the fuel injected from the main fuel injection valve 3 to the change in air-fuel ratio due to the fuel injected from the auxiliary fuel injection valve 5 is quick, so the auxiliary If the rate of change in the injection rate of the fuel injector 5 to return to the steady state injection rate is the same as the rate of change to return the injection rate of the main fuel injector 3 to the steady state injection rate, the air-fuel ratio will increase. Although it changes (see the dotted line in Figure 7 (B)), the second
In this embodiment including the invention, since the former rate of change is delayed from the latter rate of change, changes in the air-fuel ratio can be suppressed (see the solid line in FIG. 7(B)).

〈発明の効果〉 以上説明したように本発明によれば、過渡運転時、及び
過渡運転から定常運転への移行時に主燃料噴射弁と補助
燃料噴射弁との噴射率及び噴射率の変化速度を適正に制
御することにより、空燃比の変動を可及的に抑制でき、
運転性、排気エミッション特性を改善できる。
<Effects of the Invention> As explained above, according to the present invention, the injection rate and the rate of change in the injection rate of the main fuel injector and the auxiliary fuel injector are controlled during transient operation and during transition from transient operation to steady operation. Through proper control, fluctuations in the air-fuel ratio can be suppressed as much as possible.
Drivability and exhaust emission characteristics can be improved.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は、本発明の構成を示すブロック図、第2図は、
本発明の一実施例の構成を示す図、第3図は、同上実施
例の予混台率設定ルーチンを示すフローチャート、第4
図は、同上実施例の燃料噴射量設定ルーチンを示すフロ
ーチャート、第5図(A)は同上実施例の絞り弁開度変
化率に対する予混合率の補正係数の関係を示す線図、同
図(B)は同じく水温に対する予混合率の補正係数の関
係を示す線図、第6図(A)は同上実施例の予混合変化
率補正値KBINJの機関回転速度Nに対する係数、同
図(B)は同じく水?IA’r、に対する係数。 同図(C)は同じく絞り弁開度に対する係数、同種状態
量を示す線図、同図(B)は同上実施例の過渡運転から
定常運転へ移行する際の各種状態量を示す線図である。 1・・・機関  3・・・主燃料噴射弁  5・・・補
助燃料噴射弁  7・・・スロットルセンサ  8・・
・エアフローメータ  9・・・クランク角センサ  
10・・・水温センサ  12・・・コントロールユニ
ット第2111 第4 図 #f5図 (A) (B)
FIG. 1 is a block diagram showing the configuration of the present invention, and FIG. 2 is a block diagram showing the configuration of the present invention.
FIG. 3 is a diagram showing the configuration of an embodiment of the present invention, and FIG.
5(A) is a flowchart showing the fuel injection amount setting routine of the above embodiment; FIG. B) is a diagram showing the relationship between the correction coefficient of the premixing ratio and the water temperature, and FIG. Is it also water? Coefficient for IA'r. The same figure (C) is a diagram showing coefficients and similar state quantities for the throttle valve opening, and the same figure (B) is a diagram showing various state quantities when transitioning from transient operation to steady operation in the same example. be. 1... Engine 3... Main fuel injection valve 5... Auxiliary fuel injection valve 7... Throttle sensor 8...
・Air flow meter 9...Crank angle sensor
10...Water temperature sensor 12...Control unit No. 2111 Fig. 4 Fig. #f5 (A) (B)

Claims (2)

【特許請求の範囲】[Claims] (1)気筒毎に燃料噴射する主燃料噴射弁を備えると共
に、吸気通路の上流部に全気筒に対して燃料噴射する予
混合気形成用の補助燃料噴射弁を備えてなる内燃機関の
燃料供給制御装置において、機関の絞り弁開度の変化率
を検出する絞り弁開度変化率検出手段と、機関の冷却水
温度を検出する冷却水温度検出手段と、前記主燃料噴射
弁及び補助燃料噴射弁からの総噴射量に対する補助燃料
噴射弁からの噴射量割合である噴射率を、過渡運転時に
絞り弁開度の変化率と冷却水温度との検出値に基づいて
減少させる予混合率制御手段と、を含んで構成したこと
を特徴とする内燃機関の燃料供給制御装置。
(1) Fuel supply for an internal combustion engine that is equipped with a main fuel injection valve that injects fuel into each cylinder and an auxiliary fuel injection valve that injects fuel into all cylinders upstream of the intake passage for forming a premixture. In the control device, a throttle valve opening change rate detection means for detecting a change rate of a throttle valve opening of the engine, a cooling water temperature detection means for detecting a cooling water temperature of the engine, and the main fuel injection valve and the auxiliary fuel injection Premixing ratio control means that reduces the injection rate, which is the ratio of the amount of injection from the auxiliary fuel injection valve to the total amount of injection from the valve, based on the detected value of the rate of change in the opening of the throttle valve and the temperature of the cooling water during transient operation. A fuel supply control device for an internal combustion engine, comprising:
(2)気筒毎に燃料噴射する主燃料噴射弁を備えると共
に、吸気通路の上流部に全気筒に対して燃料噴射する予
混合気形成用の補助燃料噴射弁を備えてなる内燃機関の
燃料供給制御装置において、前記主燃料噴射弁及び補助
燃料噴射弁からの総噴射量に対する補助燃料噴射弁から
の噴射量割合である噴射率を、過渡運転時に減少させる
第1予混合率制御手段と、過渡運転から定常運転に移行
する際に、前記補助燃料噴射弁の噴射率を定常運転時の
噴射率に戻す変化速度に対して、主燃料噴射弁の噴射率
を定常運転時の噴射率に戻す変化速度に遅れを持たせて
制御する第2予混合率制御手段と、を含んで構成したこ
とを特徴とする内燃機関の燃料供給制御装置。
(2) Fuel supply for an internal combustion engine that is equipped with a main fuel injection valve that injects fuel into each cylinder and an auxiliary fuel injection valve that injects fuel into all cylinders upstream of the intake passage for forming a premixed mixture. In the control device, a first premixing ratio control means for reducing an injection rate, which is a ratio of the injection amount from the auxiliary fuel injection valve to the total injection amount from the main fuel injection valve and the auxiliary fuel injection valve, during a transient operation; When transitioning from operation to steady operation, the injection rate of the main fuel injector is changed to return to the injection rate during steady operation relative to the rate of change in which the injection rate of the auxiliary fuel injector is returned to the injection rate during steady operation. 1. A fuel supply control device for an internal combustion engine, comprising: second premix ratio control means for controlling the speed with a delay.
JP19888088A 1988-08-11 1988-08-11 Internal combustion engine fuel supply control device Pending JPH0249940A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19888088A JPH0249940A (en) 1988-08-11 1988-08-11 Internal combustion engine fuel supply control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19888088A JPH0249940A (en) 1988-08-11 1988-08-11 Internal combustion engine fuel supply control device

Publications (1)

Publication Number Publication Date
JPH0249940A true JPH0249940A (en) 1990-02-20

Family

ID=16398458

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19888088A Pending JPH0249940A (en) 1988-08-11 1988-08-11 Internal combustion engine fuel supply control device

Country Status (1)

Country Link
JP (1) JPH0249940A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1398480A3 (en) * 2002-09-11 2006-06-28 Honda Giken Kogyo Kabushiki Kaisha Fuel injection control system for internal combustion engine
JP2012225224A (en) * 2011-04-18 2012-11-15 Kawasaki Heavy Ind Ltd Fuel injection control device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6217329A (en) * 1985-07-16 1987-01-26 Nissan Motor Co Ltd Fuel supply device for internal-combustion engine
JPS62288336A (en) * 1986-06-04 1987-12-15 Nissan Motor Co Ltd Fuel supply device for internal combustion engine
JPS63147952A (en) * 1986-12-10 1988-06-20 Honda Motor Co Ltd Fuel supply control method for internal combustion engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6217329A (en) * 1985-07-16 1987-01-26 Nissan Motor Co Ltd Fuel supply device for internal-combustion engine
JPS62288336A (en) * 1986-06-04 1987-12-15 Nissan Motor Co Ltd Fuel supply device for internal combustion engine
JPS63147952A (en) * 1986-12-10 1988-06-20 Honda Motor Co Ltd Fuel supply control method for internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1398480A3 (en) * 2002-09-11 2006-06-28 Honda Giken Kogyo Kabushiki Kaisha Fuel injection control system for internal combustion engine
JP2012225224A (en) * 2011-04-18 2012-11-15 Kawasaki Heavy Ind Ltd Fuel injection control device

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