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JPH0610441B2 - Electronically controlled fuel injection device - Google Patents
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JPH0610441B2 - Electronically controlled fuel injection device - Google Patents

Electronically controlled fuel injection device

Info

Publication number
JPH0610441B2
JPH0610441B2 JP58031859A JP3185983A JPH0610441B2 JP H0610441 B2 JPH0610441 B2 JP H0610441B2 JP 58031859 A JP58031859 A JP 58031859A JP 3185983 A JP3185983 A JP 3185983A JP H0610441 B2 JPH0610441 B2 JP H0610441B2
Authority
JP
Japan
Prior art keywords
fuel injection
synchronous
amount
throttle opening
intake
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 - Lifetime
Application number
JP58031859A
Other languages
Japanese (ja)
Other versions
JPS59158341A (en
Inventor
鈴木  誠
憲一 野村
隆雄 館
衛 吉岡
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP58031859A priority Critical patent/JPH0610441B2/en
Publication of JPS59158341A publication Critical patent/JPS59158341A/en
Publication of JPH0610441B2 publication Critical patent/JPH0610441B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/02Circuit arrangements for generating control signals
    • F02D41/04Introducing corrections for particular operating conditions
    • F02D41/10Introducing corrections for particular operating conditions for acceleration
    • F02D41/105Introducing corrections for particular operating conditions for acceleration using asynchronous injection

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】 本発明は、複数吸気弁式、すなわち各気筒の燃焼室が複
数の吸気弁を有する電子制御機関の燃料噴射装置に係
り、特に燃料噴射時期を改善された燃料噴射装置に関す
る。
The present invention relates to a fuel injection device for an electronically controlled engine having a plurality of intake valve types, that is, a combustion chamber of each cylinder having a plurality of intake valves, and more particularly to a fuel injection device with improved fuel injection timing. Regarding

2吸気弁式内燃料機関は、(a)吸気弁開口の総面積が大
きいこと、(b)高出力を目指すために吸気弁と閉じる時
期が吸気行程下死点より遅れることに因り、吸気行程後
半における燃焼室から吸気通路への吸入空気の吹返しが
大きくなつている。同期燃料噴射は機関回転すなわちク
ランク角あるいは点火信号に同期して行なわれている
が、従来の電子制御燃料噴射装置のように燃料噴射弁か
らの同期燃料噴射が1回転に1回全気筒同期に行なわれ
る場合にはいずれかの気筒における燃料噴射時期が吸入
空気の吹返し期間になり、燃料が吹返されて燃料室へ入
らないという現象が起きている。また、2吸気弁式電子
制御機関の高吸気効率のためにスロットル開度の変化に
対する吸入空気流量の変化が大きくなり、加速時では燃
料噴射量の追従遅れが顕著となる。このような吹返しと
追従遅れのため加速時では燃焼室内の混合気が希薄にな
り、加速性能が悪化し易いという問題が生じ易い。
The two-intake-valve internal-fuel engine has (a) a large total area of the intake valve opening, and (b) the intake valve is closed at a time later than the bottom dead center of the intake stroke in order to achieve high output. In the latter half, the blowback of intake air from the combustion chamber to the intake passage is increasing. Synchronous fuel injection is performed in synchronism with the engine rotation, that is, the crank angle or the ignition signal, but the synchronous fuel injection from the fuel injection valve is performed once per revolution in all cylinders as in the conventional electronically controlled fuel injection device. When this is done, the fuel injection timing in any of the cylinders becomes the blowback period of the intake air, and the phenomenon occurs in which the fuel is blown back and does not enter the fuel chamber. Further, due to the high intake efficiency of the dual intake valve type electronically controlled engine, the change in the intake air flow rate with respect to the change in the throttle opening becomes large, and the delay in following the fuel injection amount becomes noticeable during acceleration. Due to such blow-back and follow-up delay, the air-fuel mixture in the combustion chamber becomes lean at the time of acceleration, and the problem that acceleration performance is likely to deteriorate easily occurs.

本発明の目的は、燃料の吹返しを回避することができか
つ加速時の燃料噴射量の追従性を改善することができる
複数吸気弁式電子制御機関の燃料噴射装置を提供するこ
とである。
An object of the present invention is to provide a fuel injection device for a multiple intake valve type electronically controlled engine that can avoid backflow of fuel and improve followability of the fuel injection amount during acceleration.

この目的を達成するために本発明は、各気筒に複数の吸
気弁を有する内燃機関で、同期燃料噴射が吸気吹き返し
の時期を外した噴射タイミングで行われる電子制御燃料
噴射装置であって、 前記同期噴射タイミングよりも短い等時間間隔毎に、単
位時間当たりのスロットル開度変化量を検出する検出手
段と、 前記スロットル開度変化量の検出時点で許容される燃料
噴射量の最大値と、前記スロットル開度変化量の検出時
点の直前の同期噴射による同期噴射量との差を求め、前
記差に応じた量の燃料を前記検出手段により検出された
スロットル開度変化量が小さい程小さくする補正を加え
た非同期燃料噴射量を演算する演算手段と、 前記検出手段により検出されたスロットル開度変化量が
所定値以上のスロットル開度変化量であるとき前記演算
手段により演算された非同期燃料噴射量に基づき非同期
燃料噴射を実行する制御手段とを有する。
In order to achieve this object, the present invention is an internal combustion engine having a plurality of intake valves in each cylinder, an electronically controlled fuel injection device in which synchronous fuel injection is performed at an injection timing other than the intake blowback timing, Detection means for detecting a throttle opening change amount per unit time at equal time intervals shorter than the synchronous injection timing; a maximum value of the fuel injection amount allowed at the time of detecting the throttle opening change amount; Correction for obtaining a difference from the synchronous injection amount by the synchronous injection immediately before the detection time of the throttle opening change amount, and reducing the amount of fuel corresponding to the difference as the throttle opening change amount detected by the detection means is smaller. Calculating means for calculating the asynchronous fuel injection amount, and the calculating means when the throttle opening change amount detected by the detecting means is a throttle opening change amount of a predetermined value or more. And a control means for performing an asynchronous fuel injection based on the asynchronous fuel injection amount calculated by the step.

このような同期燃料噴射時期の設定により燃料の吹返し
が回避され、燃料が燃焼室へ円滑に導入され、また、加
速時では同期燃料噴射の噴射量の不足分に関係して非同
期燃料噴射が行なわれるので、加速時の燃料噴射量を追
従性が改善される。
By setting the synchronous fuel injection timing in this way, the blowback of the fuel is avoided, the fuel is smoothly introduced into the combustion chamber, and during the acceleration, the asynchronous fuel injection is performed due to the shortage of the injection amount of the synchronous fuel injection. Therefore, the followability of the fuel injection amount during acceleration is improved.

図面を参照して本発明の実施例を説明する。Embodiments of the present invention will be described with reference to the drawings.

第1図において電子制御機関の吸気通路1には上流から
順番にエアクリーナ2、吸気温センサ3、エアフローメ
ータ4、吸気ホース5、スロットル弁6、サージタンク
7、および吸気管8が設けられ、バイパス通路9はスロ
ットル弁6に対して並列に設けられている。燃焼室10は
機関本体11に設けられ、シリンダヘッド12、シリンダブ
ロック13、およびピストン14により画定されている。燃
料は、吸気ポート近傍に取付けられた燃料噴射弁15から
噴射され、2つの吸気弁16a,16b(第2図)を経て燃焼
室10へ入り、燃焼後は排気ガスとなつて2つの排気弁17
a,17b(第2図)を経て排気通路18へ排出される。排気
通路18には上流から順番に排気分岐管19、排気管20、お
よび触媒コンバータ21が設けられる。水温センサ25はシ
リンダブロツク13に取付けられて期間冷却水温度を検出
し、スロツトルセンサ26はスロツトル弁6の開度を検出
し、O2センサ27は排気分岐管19の集合部分に設けられ
て排気中の酸素濃度を検出し、クランク角センサ30は配
電器31の軸の回転からクランク角を検出する。電子制御
装置32は蓄電池33から電力と電圧信号とを受け、各セン
サ3,4,25,26,27,30から入力を受け、これらの入
力データに基づいて燃料噴射弁15からの噴射燃料の量を
計算する。
In FIG. 1, the intake passage 1 of the electronic control engine is provided with an air cleaner 2, an intake air temperature sensor 3, an air flow meter 4, an intake hose 5, a throttle valve 6, a surge tank 7 and an intake pipe 8 in order from the upstream side. The passage 9 is provided in parallel with the throttle valve 6. The combustion chamber 10 is provided in the engine body 11 and is defined by the cylinder head 12, the cylinder block 13, and the piston 14. Fuel is injected from a fuel injection valve 15 installed near the intake port, enters the combustion chamber 10 through two intake valves 16a and 16b (Fig. 2), and after combustion, becomes exhaust gas and two exhaust valves. 17
It is discharged to the exhaust passage 18 via a and 17b (Fig. 2). The exhaust passage 18 is provided with an exhaust branch pipe 19, an exhaust pipe 20, and a catalytic converter 21 in order from the upstream. The water temperature sensor 25 is attached to the cylinder block 13 to detect the temperature of the cooling water for a certain period, the throttle sensor 26 detects the opening degree of the throttle valve 6, and the O 2 sensor 27 is provided at the collecting portion of the exhaust branch pipe 19. The crank angle sensor 30 detects the oxygen concentration in the exhaust gas and detects the crank angle from the rotation of the shaft of the distributor 31. The electronic control unit 32 receives power and voltage signals from the storage battery 33, receives inputs from the sensors 3, 4, 25, 26, 27, 30 and, based on these input data, injects fuel injected from the fuel injection valve 15. Calculate the amount.

第2図は吸気ポート近傍を示している。燃焼室10は2つ
の吸気弁16a,16bおよび2つの排気弁17a,17bを有し、
かつ頂部に点火プラグ36を有している。吸気管8および
吸気ポート内は各吸気弁16a,16bに対応して仕切壁37,
38により仕切られており、燃料噴射弁15からの噴射燃料
は各吸気弁16a,16bへ分配される。
FIG. 2 shows the vicinity of the intake port. The combustion chamber 10 has two intake valves 16a, 16b and two exhaust valves 17a, 17b,
It also has a spark plug 36 on the top. The intake pipe 8 and the inside of the intake port correspond to the intake valves 16a, 16b by a partition wall 37,
It is partitioned by 38, and the fuel injected from the fuel injection valve 15 is distributed to the intake valves 16a and 16b.

第3図は電子制御装置32を詳細に示している。CPU4
1、A/D(アナログ/デジタル)変換器42、出力イン
タフエース回路43、ROM44、およびRAM45はバス46
を介して相互に接続されている。クランク角センサ30は
180゜CA(CA:クランク角)変化ごとにパルスを生
じる180゜クランク角信号46と、クランク角の720゜ごと
にパルスを生じる720゜クランク角信号47とを発生し、1
80゜クランク角信号46は波形成形回路48を経てCPU41
の割込み入力端子およびTp1パルス成形用アナログ演
算回路49へ送られ、720゜クランク角信号47は波形整形
回路48を経てCPU41の割込み入力端子へ送られる。Tp
パルス成形用アナログ演算回路49は、コンデンサの充
電、放電を利用して、エアフローメータ4からの吸入空
気流量Qのデータと180゜クランク角信号の機関回転速
度Nのデータとから、パルス幅Tp1(Tp1は基本燃料
噴射時間Tp2の1/2である。)がQ/Nに比例し周期が
クランク角で360゜のTp1パルス信号50を発生する。A
/D変換器42は吸気温センサ3、水温センサ25、スロツ
トルセンサ26、O2センサ27、および蓄電池38から入力
信号を受け、これらの入力信号を選択的にA/D変換す
る。出力インタフエース43は燃料噴射弁15のグループご
とに変量噴射パルスを送る。実施例では電子制御機関を
4気筒機関とし、また機関本体11の一方の端から順番に
第1気筒、第2気筒、第3気筒、第4気筒と定義して点
火順序を第1気筒、第3気筒、第4気筒、第2気筒と
し、第1気筒と第2気筒とをグループA、第3気筒と第
4気筒とをグループBに分類する。
FIG. 3 shows the electronic control unit 32 in detail. CPU4
1, A / D (analog / digital) converter 42, output interface circuit 43, ROM 44, and RAM 45 are bus 46
Are connected to each other via. The crank angle sensor 30
A 180 ° crank angle signal 46 that generates a pulse for each 180 ° CA (CA: crank angle) change and a 720 ° crank angle signal 47 that generates a pulse for each 720 ° crank angle are generated.
The 80 ° crank angle signal 46 is sent to the CPU 41 via the waveform shaping circuit 48.
To the analog input circuit 49 for T p 1 pulse shaping, and the 720 ° crank angle signal 47 is sent to the interrupt input terminal of the CPU 41 via the waveform shaping circuit 48. T p 1
The pulse shaping analog calculation circuit 49 utilizes the charge and discharge of the capacitor to extract the pulse width T p from the data of the intake air flow rate Q from the air flow meter 4 and the data of the engine speed N of the 180 ° crank angle signal. 1 (T p 1 is one half of the basic fuel injection time T p 2) is proportional to Q / N and generates a T p 1 pulse signal 50 having a cycle of 360 ° in crank angle. A
The / D converter 42 receives input signals from the intake air temperature sensor 3, the water temperature sensor 25, the throttle sensor 26, the O 2 sensor 27, and the storage battery 38, and selectively A / D converts these input signals. The output interface 43 sends a variable injection pulse for each group of fuel injectors 15. In the embodiment, the electronically controlled engine is a 4-cylinder engine, and the first cylinder, the second cylinder, the third cylinder, and the fourth cylinder are defined in order from one end of the engine body 11, and the ignition order is the first cylinder, the first cylinder, and the second cylinder. There are three cylinders, a fourth cylinder, and a second cylinder. The first cylinder and the second cylinder are classified into a group A, and the third cylinder and the fourth cylinder are classified into a group B.

第4図は同期燃料噴射ルーチンのフローチヤートであ
る。最終燃料噴射時間Tauを計算するとともに、720゜
CA信号の有無に関係してAグループの燃料噴射弁15お
よびBグループの燃料噴射弁15を選択して駆動する。ス
テツプ54ではTp1パルス信号50からパルス幅Tp1を検
出する。Tp1パルス成形用アナログ回路49は機関1サ
イクルにつき同期燃料噴射が2回行なわれる。すなわち
クランク角360゜の変化ごとに同期燃料噴射が1回行な
われる1吸気弁式(各燃焼室が唯一の吸気弁を有す
る。)電子制御機関用に設計されており、Tp1は1回
の同期燃料噴射の基本燃料噴射時間Tp2の1/2である。
直接基本燃料噴射時間Tp2を計算しない理由は、基本
燃料噴射時間Tp2の検出に要する時間を短縮するため
である。ステツプ56では燃料カツト条件が成立している
か否かを判定し、燃料カツト条件が成立していれば以下
のステツプの実行を省略し、不成立であればステツプ58
へ進む。燃料カツト条件とは例えば機関回転速度が所定
値以上である減速期間であることである。ステツプ58で
は燃料噴射時間Tau1に2・Tp1・K1を代入する。
au1は各燃料噴射弁からの同期燃料噴射が機関1サイ
クルにつき2回行なわれる場合の最終燃料噴射時間であ
る。Tp1に2を掛けることにより基本燃料噴射時間Tp
2を得、さらに2・Tp1にK1を掛けることにより基本
燃料噴射時間を補正する。K1は吸気温度、機関冷却水温
度等により決まる補正係数である。ステップ60ではグル
ープ別噴射実行条件が成立しているか否かを判定し、条
件が成立していればステツプ64へ進み、不成立であれば
ステツプ62へ進む。グループ別噴射条件成立とは例えば
始動期間等の低機関回転速度期間のように期間回転速度
が変動し、180゜クランク角信号がばらつく場合であ
る。この場合にグループ別同期燃料噴射を行なうと、同
期燃料噴射の間隔が乱れ、期間運転上、好ましくない。
ステツプ62では同期燃料噴射が全気筒同時に行なわれ
る。ステツプ64では最終燃料噴射時間Tau2・Tau1を
代入する。Tau1に2を掛けた理由はグループ別燃料噴
射では各燃料噴射弁15からの同期燃料噴射が1サイクル
当たり2回ではなく1回となるからである。ステツプ66
では720゜クランク角信号があるか否かを判定し、有れ
ばステップ68へ進み、無ければステツプ70へ進む。720
゜クランク角信号は第1気筒の爆発行程上死点において
生じる。ステツプ68ではグループAの燃料噴射弁15を駆
動し、ステツプ70ではグループBの燃料噴射弁15を駆動
する。したがつて各燃料噴射弁からの同期燃料噴射が、
その燃料噴射弁の対応気筒の吸気行程後半、および圧縮
行程前半、すなわち吸入空気の吹返し期間を回避して行
なわれる。
FIG. 4 is a flow chart of the synchronous fuel injection routine. The final fuel injection time T au is calculated, and the fuel injection valve 15 of the A group and the fuel injection valve 15 of the B group are selected and driven depending on the presence or absence of the 720 ° CA signal. In step 54, the pulse width T p 1 is detected from the T p 1 pulse signal 50. In the T p 1 pulse shaping analog circuit 49, synchronous fuel injection is performed twice per cycle of the engine. That is, it is designed for one intake valve type (each combustion chamber has only one intake valve) electronically controlled engine in which synchronous fuel injection is performed once for each crank angle change of 360 °, and T p 1 is once Is 1/2 of the basic fuel injection time T p 2 of the synchronous fuel injection.
Reasons for not calculating the direct basic fuel injection time T p 2 is to reduce the time required for detection of the basic fuel injection time T p 2. In step 56, it is judged whether or not the fuel cut condition is satisfied, and if the fuel cut condition is satisfied, the execution of the following steps is omitted, and if not satisfied, step 58 is executed.
Go to. The fuel cut condition is, for example, a deceleration period in which the engine speed is equal to or higher than a predetermined value. At step 58, 2 · T p 1 · K1 is substituted for the fuel injection time T au 1.
T au 1 is the final fuel injection time when the synchronous fuel injection from each fuel injection valve is performed twice per engine cycle. By multiplying T p 1 by 2, the basic fuel injection time T p
2 is obtained, and the basic fuel injection time is corrected by further multiplying 2 · T p 1 by K1. K1 is a correction coefficient determined by the intake air temperature, engine cooling water temperature, etc. In step 60, it is determined whether or not the group-by-group injection execution condition is satisfied. If the condition is satisfied, the process proceeds to step 64, and if not, the process proceeds to step 62. Satisfying the injection conditions for each group means that the period rotation speed fluctuates and the 180 ° crank angle signal fluctuates, for example, during a low engine rotation speed period such as a starting period. In this case, if the group-by-group synchronous fuel injection is performed, the intervals of the synchronous fuel injection are disturbed, which is not preferable for the period operation.
In step 62, synchronous fuel injection is performed simultaneously for all cylinders. At step 64, the final fuel injection time T au 2 · T au 1 is substituted. The reason why T au 1 is multiplied by 2 is that in the fuel injection by group, the synchronous fuel injection from each fuel injection valve 15 is once instead of twice per cycle. Step 66
Then, it is determined whether or not there is a 720 ° crank angle signal, and if there is, the process proceeds to step 68, and if there is not, the process proceeds to step 70. 720
The ° crank angle signal occurs at the top dead center of the first cylinder's power stroke. In step 68, the group A fuel injection valve 15 is driven, and in step 70, the group B fuel injection valve 15 is driven. Therefore, synchronous fuel injection from each fuel injection valve
The latter half of the intake stroke and the first half of the compression stroke of the corresponding cylinder of the fuel injection valve, that is, the blowback period of the intake air is avoided.

第5図は非同期燃料噴射ルーチンのフローチヤートであ
る。このルーチンは16msecごとに行なわれる時間割込み
ルーチンである。スロツトル開度Thの変化量ΔThが所定
値以上であり、したがつて要求されている加速程度が大
きく、かつ最大燃料噴射時間Tpmaxと最後に行なわれた
同期燃料噴射に対応するTp1との差ΔTpが正である場
合にΔThとΔTpとに関係した燃料噴射時間だけ非同期
燃料噴射が行なわれる。ステツプ76ではスロツトル開度
Thを検出する。ステツプ78ではスロツトル開度の変化量
ΔThにTh−Th′を代入する。Th′は前回に、すなわち16
msec前に検出したスロツトル開度である。ステツプ80で
は変化量ΔThの上限ΔThaおよび下限ΔThbを制限する。
ステツプ82ではΔThΔTh1か否かを判定し、ΔThTh1
であればステツプ84へ進み、ΔTh<ΔTh1であれば以下
のステツプの実行を省略する。こうしてスロツトル開度
Thの変化量ΔThがΔTh1より大きい場合のみ、非同期燃
料噴射が行なわれる。ステツプ84では、ΔThからその関
数としての補正係数K2を計算する。第6図はΔThとK
2との関係を示している。急激な加速状態程、K2は増
大する。ステツプ86では現在の機関回転速度におけるス
ロツル弁全開時の基本燃料噴射時間として定義されてい
る最大値Tpmaxを取込む。Tpmaxは機関回転速度に関係
して定められる。ステツプ88ではTpmax−Tp1をΔTp
に代入する。ステツプ88におけるTp1は最後に行なわ
れた同期燃料噴射の噴射量の基礎となつたTp1であ
る。ステツプ90ではΔTp>0か否かを判定し、ΔTp
0であればステツプ92へ進み、ΔTp0であれば以下
のステツプの実行を終了する。こうして最後の同期燃料
噴射の量が要求燃料噴射量に対して不足している場合の
み、非同期燃料噴射が行なわれる。ステツプ92では非同
期燃料噴射時間TasにK2・ΔTpを代入する。ステツ
プ94では非同期燃料噴射を実行する。非同期燃料噴射は
全気筒同時に行なう。
FIG. 5 is a flow chart of the asynchronous fuel injection routine. This routine is a time interrupt routine executed every 16 msec. The change amount ΔTh of the throttle opening Th is equal to or larger than a predetermined value, and therefore the required degree of acceleration is large, and the maximum fuel injection time T pmax and T p 1 corresponding to the last synchronous fuel injection are set. If the difference ΔT p of ΔT p is positive, asynchronous fuel injection is performed for the fuel injection time related to ΔT h and ΔT p . At step 76, the throttle opening
Detect Th. At step 78, Th-Th 'is substituted for the change amount ΔTh of the throttle opening. Th ′ was the last time, ie 16
It is the throttle opening detected msec before. In step 80, the upper limit ΔTha and the lower limit ΔThb of the change amount ΔTh are limited.
In step 82, it is judged whether or not ΔThΔTh1, and ΔThTh1
If so, the process proceeds to step 84, and if ΔTh <ΔTh1, the execution of the following steps is omitted. Thus the throttle opening
The asynchronous fuel injection is performed only when the change amount ΔTh of Th is larger than ΔTh1. In step 84, the correction coefficient K2 as its function is calculated from ΔTh. Figure 6 shows ΔTh and K
The relationship with 2 is shown. K2 increases in a rapid acceleration state. At step 86, the maximum value Tpmax defined as the basic fuel injection time when the throttle valve is fully opened at the present engine speed is taken in. Tpmax is determined in relation to the engine speed. In step 88, T pmax -T p 1 is changed to ΔT p
To. T p 1 in the step 88 is T p 1 becomes such basic injection quantity of the last performed synchronization fuel injection. At step 90, it is determined whether or not ΔT p > 0, and ΔT p >
If it is 0, the process proceeds to step 92, and if ΔT p 0, the execution of the following steps is ended. Thus, the asynchronous fuel injection is performed only when the final synchronous fuel injection amount is insufficient with respect to the required fuel injection amount. At step 92, K2 · ΔT p is substituted for the asynchronous fuel injection time T as . At step 94, asynchronous fuel injection is performed. Asynchronous fuel injection is performed simultaneously for all cylinders.

第7図は機関回転速度1000rpmにおいてスロツトル開度T
hが0゜から全開までに急激に開かれた場合の同期燃料噴
射Isおよび非同期燃料噴射Iaのタイミングチヤートで
ある。第7図においては各気筒吸気行程を示す。同期燃
料噴射Isは、燃料噴射弁15のグループ別に行なわれ、
吸入空気の吹返しが生じる吸気行程下死点を含む所定の
クランク角範囲を外されて行なわれる。180゜クランク
角信号は各気筒の上死点よりクランク各10゜だけ前に発
生している。非同期燃料噴射Iaは要求燃料噴射時間が
最後の同期燃料噴射時間より大きい場合において第5図
の時間割込みルーチンの実行ごとに行なわれる。
Figure 7 shows the throttle opening T at an engine speed of 1000 rpm.
3 is a timing chart of the synchronous fuel injection I s and the asynchronous fuel injection I a when h is suddenly opened from 0 ° to full opening. FIG. 7 shows the intake stroke of each cylinder. The synchronous fuel injection I s is performed for each group of fuel injection valves 15,
The operation is performed outside the predetermined crank angle range including the bottom dead center of the intake stroke at which the intake air is blown back. The 180 ° crank angle signal occurs 10 ° before the top dead center of each cylinder. The asynchronous fuel injection I a is performed each time the time interrupt routine of FIG. 5 is executed when the required fuel injection time is longer than the last synchronous fuel injection time.

第8図は本発明の機能ブロツク図である。同期燃料噴射
計算手段100はクランク角センサ30、およびTp1パルス
成形用アナログ演算回路49からの入力信号に基づいて同
期燃料噴射の噴射量および噴射時期を計算する。要求燃
料噴射量計算手段101は現在の機関回転速度におけるス
ロツトル弁全開時の基本燃料噴射量Tpmaxを計算する。
非同期燃料噴射計算手段102はTp1パルス成形用アナロ
グ演算回路49からのTp1、要求燃料噴射量計算手段101
からのPpmax、およびスロツトルセンサ26からのスロツ
トル開度Thのデータに基づいて非同期燃料噴射の噴射量
および噴射時期を計算する。駆動手段103は同期燃料噴
射計算手段100の出力をクランク角センサ30の720゜クラ
ンク角信号に基づいてグループA燃料噴射弁15あるいは
グループB燃料噴射弁15へ送り、非同期燃料噴射計算手
段102の出力をグループAおよびグループB燃料噴射弁1
5へ送る。
FIG. 8 is a functional block diagram of the present invention. The synchronous fuel injection calculation means 100 calculates the injection amount and injection timing of the synchronous fuel injection based on the input signals from the crank angle sensor 30 and the T p 1 pulse shaping analog calculation circuit 49. The required fuel injection amount calculation means 101 calculates the basic fuel injection amount T pmax when the throttle valve is fully opened at the present engine speed.
Asynchronous fuel injection calculation means 102 T p 1 from T p 1 pulse shaping analog arithmetic circuit 49, the required fuel injection amount calculating means 101
And the injection amount and injection timing of the asynchronous fuel injection are calculated based on the data of P pmax from the throttle sensor 26 and the data of the throttle opening Th from the throttle sensor 26. The drive means 103 sends the output of the synchronous fuel injection calculation means 100 to the group A fuel injection valve 15 or the group B fuel injection valve 15 based on the 720 ° crank angle signal of the crank angle sensor 30, and the output of the asynchronous fuel injection calculation means 102. Group A and Group B fuel injection valve 1
Send to 5.

【図面の簡単な説明】[Brief description of drawings]

第1図は本発明が適用される電子制御機関の概略図、第
2図は2吸気弁に電子制御機関の吸気ポート近傍の詳細
図、第3図は第1図の電子制御装置の詳細なブロツク
図、第4図は同期燃料噴射ルーチンのフローチヤート、
第5図は非同期燃料噴射ルーチンのフローチヤート、第
6図はスロツトル開度の変化量と非同期燃料噴射補正係
数との関係を示すグラフ、第7図はスロツトル開度を0
゜から全開へ変化した場合の同期燃料噴射および非同期
燃料噴射等のタイミングチヤート、第8図は本発明の機
能ブロツク図である。 10…燃焼室、15…燃料噴射弁、16a,16b…吸気弁、30…
クランク角センサ、100…同期燃料噴射計算手段、101…
燃料噴射量計算手段、102…非同期燃料噴射計算手段。
FIG. 1 is a schematic view of an electronic control engine to which the present invention is applied, FIG. 2 is a detailed view of the two intake valves in the vicinity of an intake port of the electronic control engine, and FIG. 3 is a detailed view of the electronic control device of FIG. Block diagram, Fig. 4 shows the flow chart of the synchronous fuel injection routine,
FIG. 5 is a flow chart of the asynchronous fuel injection routine, FIG. 6 is a graph showing the relationship between the change amount of the throttle opening and the asynchronous fuel injection correction coefficient, and FIG. 7 is the throttle opening 0.
FIG. 8 is a functional block diagram of the present invention, which is a timing chart for synchronous fuel injection, asynchronous fuel injection, and the like when the angle changes from .degree. 10 ... Combustion chamber, 15 ... Fuel injection valve, 16a, 16b ... Intake valve, 30 ...
Crank angle sensor, 100 ... Synchronous fuel injection calculation means, 101 ...
Fuel injection amount calculation means 102 ... Asynchronous fuel injection calculation means.

フロントページの続き (72)発明者 吉岡 衛 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内 (56)参考文献 特開 昭56−54929(JP,A) 特開 昭56−124637(JP,A) 特開 昭56−148633(JP,A) 特開 昭55−131541(JP,A) 特開 昭58−28541(JP,A) 特公 昭47−41288(JP,B1)Front Page Continuation (72) Inventor Mamoru Yoshioka 1 Toyota Town, Toyota City, Aichi Prefecture Toyota Motor Corporation (56) References JP-A-56-54929 (JP, A) JP-A-56-124637 (JP, A) JP-A-56-148633 (JP, A) JP-A-55-131541 (JP, A) JP-A-58-28541 (JP, A) JP-B-47-41288 (JP, B1)

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】各気筒に複数の吸気弁を有する内燃機関
で、同期燃料噴射が吸気吹き返しの時期を外した噴射タ
イミングで行われる電子制御燃料噴射装置であって、 前記同期噴射タイミングよりも短い等時間間隔毎に、単
位時間当たりのスロットル開度変化量を検出する検出手
段と、 前記スロットル開度変化量の検出時点で許容される燃料
噴射量の最大値と、前記スロットル開度変化量の検出時
点の直前の同期噴射による同期噴射量との差を求め、前
記差に応じた量の燃料を前記検出手段により検出された
スロットル開度変化量が小さい程小さくする補正を加え
た非同期燃料噴射量を演算する演算手段と、 前記検出手段により検出されたスロットル開度変化量が
所定値以上のスロットル開度変化量であるとき前記演算
手段により演算された非同期燃料噴射量に基づき非同期
燃料噴射を実行する制御手段とを有することを特徴とす
る電子制御燃料噴射装置。
1. An electronically controlled fuel injection device, comprising: an internal combustion engine having a plurality of intake valves in each cylinder, wherein synchronous fuel injection is performed at an injection timing that deviates from a timing of intake blowback, and is shorter than the synchronous injection timing. Detection means for detecting the throttle opening change amount per unit time at equal time intervals, the maximum value of the fuel injection amount allowed at the time of detecting the throttle opening change amount, and the throttle opening change amount Asynchronous fuel injection in which a difference from the synchronous injection amount by the synchronous injection immediately before the detection time point is obtained, and the amount of fuel corresponding to the difference is reduced as the throttle opening change amount detected by the detection means is smaller. Calculation means for calculating the amount, and a non-calculated value calculated by the calculation means when the throttle opening change amount detected by the detection means is equal to or larger than a predetermined value. Electronically controlled fuel injection apparatus characterized by a control means for performing an asynchronous fuel injection on the basis of the period the fuel injection amount.
JP58031859A 1983-03-01 1983-03-01 Electronically controlled fuel injection device Expired - Lifetime JPH0610441B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58031859A JPH0610441B2 (en) 1983-03-01 1983-03-01 Electronically controlled fuel injection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58031859A JPH0610441B2 (en) 1983-03-01 1983-03-01 Electronically controlled fuel injection device

Publications (2)

Publication Number Publication Date
JPS59158341A JPS59158341A (en) 1984-09-07
JPH0610441B2 true JPH0610441B2 (en) 1994-02-09

Family

ID=12342769

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58031859A Expired - Lifetime JPH0610441B2 (en) 1983-03-01 1983-03-01 Electronically controlled fuel injection device

Country Status (1)

Country Link
JP (1) JPH0610441B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0617663B2 (en) * 1984-10-30 1994-03-09 マツダ株式会社 Fuel injection timing control device

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5654929A (en) * 1979-10-12 1981-05-15 Nissan Motor Co Ltd Fuel injection timing controller for internal combustion engine
JPS56124637A (en) * 1980-03-07 1981-09-30 Hitachi Ltd Method of controlling acceleration of engine

Also Published As

Publication number Publication date
JPS59158341A (en) 1984-09-07

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