JPS5825525A - Electronically controlled fuel injection method - Google Patents

Electronically controlled fuel injection method

Info

Publication number
JPS5825525A
JPS5825525A JP12310181A JP12310181A JPS5825525A JP S5825525 A JPS5825525 A JP S5825525A JP 12310181 A JP12310181 A JP 12310181A JP 12310181 A JP12310181 A JP 12310181A JP S5825525 A JPS5825525 A JP S5825525A
Authority
JP
Japan
Prior art keywords
fuel injection
fuel
injection valve
valve
starting
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
JP12310181A
Other languages
Japanese (ja)
Inventor
Kazuyoshi Mizuno
水野 和好
Koichi Osawa
幸一 大澤
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 JP12310181A priority Critical patent/JPS5825525A/en
Publication of JPS5825525A publication Critical patent/JPS5825525A/en
Pending 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
    • F02D41/06Introducing corrections for particular operating conditions for engine starting or warming up
    • F02D41/062Introducing corrections for particular operating conditions for engine starting or warming up for starting

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

PURPOSE:To ensure a prescribed feed quantity of fuel at a high load and the like, by injecting the fuel from a main fuel injection valve and starting fuel injection valve when a flow of fuel injection after starting exceeds a maximum flow of fuel injection of the main fuel injection valve. CONSTITUTION:A pump 42 feeds fuel from a fuel tank 43 to a main fuel injection valve 41 througi a fuel passage 44. A starting fuel injection valve 46, injecting excess fuel at a cold temperature start, is provided to a surge tank 4 and connected to the fuel passage 44. An electronic control unit 40 controls the main fuel injection valve 41, starting fuel injection valve 46, bypass flow control valve 22, exhaust gas recirculation (EGR) control valve 24, ignition coil 45, etc. When a flow of fuel injection after starting exceeds a maximum flow of fuel injection of the main fuel injection valve 41, fuel is injected from the both fuel injection valves 41, 46.

Description

【発明の詳細な説明】 本発明は、燃料噴射流量の範囲を拡大することができる
機関の電子制御燃料噴射方法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an electronically controlled fuel injection method for an engine that can expand the range of fuel injection flow rates.

電子制御燃料噴射機関では、各気筒ごとに主燃料噴射弁
が設けられ、CPU(中央処理装置)からの電圧信号に
より燃料噴射弁が操作され、所定の空燃比制御が行なわ
れている。第1図は燃料噴射弁の噴射時間の限界を示し
ている。
In an electronically controlled fuel injection engine, a main fuel injection valve is provided for each cylinder, and the fuel injection valve is operated by a voltage signal from a CPU (central processing unit) to perform predetermined air-fuel ratio control. FIG. 1 shows the limits of the injection time of the fuel injection valve.

Slはクランク軸が360°回転するごとにクランク角
センサが発生する同期信号であり、S2は燃料噴射弁へ
送られる噴射信号である。噴射信号S2が低レベルにあ
る期間では燃料噴射弁が開かれて燃料が吸気系へ噴射さ
れ、噴射信号S2が高レベルにある期間では燃料噴射弁
が閉じられて吸気系への燃料噴射が中止され、クランク
角に同期して燃料が噴射されている。このような燃料噴
射弁では、最小噴射時間τminが燃料噴射弁の弁体の
機械的運動のために制限され、最小噴射時間τmin以
下の噴射時間では燃料噴射が不整となって計量が不可能
となり、また、最大噴射時間τmaxは、燃料噴射時間
の間に所定の休止時間τS(τSは機関回転速度に関係
なく一定である。)が設けられかつ噴射信号S1の間隔
が、機関回転速度の増大に連れて減少するために制限さ
れるので、燃料噴射流量の制御範囲に制限が生じている
。第2図は燃料噴射弁A、Bの噴射1回当たりの燃料噴
射量の最大値Qmax a 、 Qmaxb、最小値Q
mina 、 Qminbを示しティる。
Sl is a synchronization signal generated by the crank angle sensor every time the crankshaft rotates 360 degrees, and S2 is an injection signal sent to the fuel injection valve. During the period when the injection signal S2 is at a low level, the fuel injection valve is opened and fuel is injected into the intake system, and during the period when the injection signal S2 is at a high level, the fuel injection valve is closed and fuel injection to the intake system is stopped. The fuel is injected in synchronization with the crank angle. In such a fuel injection valve, the minimum injection time τmin is limited due to the mechanical movement of the valve body of the fuel injection valve, and if the injection time is less than the minimum injection time τmin, fuel injection becomes irregular and metering becomes impossible. , and the maximum injection time τmax is such that a predetermined rest time τS (τS is constant regardless of the engine rotation speed) is provided between the fuel injection times, and the interval of the injection signal S1 is set as the engine rotation speed increases. Therefore, there is a limit to the control range of the fuel injection flow rate. Figure 2 shows the maximum values Qmax a, Qmaxb, and minimum value Q of the fuel injection amount per injection of fuel injection valves A and B.
Indicates mina and Qminb.

燃料噴射弁Bのノズル径は燃料噴射弁Aのノズル径より
大きく、ノズル径を変更したとしても、燃料噴射量の最
大値Qmax a 、 Qmax b′、および最小値
Qmin a 、 Qminbは噴射時間rmax 、
 tminによって大幅に制限される。第3図は噴射時
間τmax 、1m i nによる空燃比制御範囲を示
し、横軸は機関回転速度、縦軸は燃焼室における空気の
充てん効率であり、空燃比A/Fをパラメータとして制
御限界を図示している。例えば1m i nによる制御
限界に関してA/F=14.7の最小光てん効率は機関
回転速度に関係なく約12%であり、最小燃料噴射時間
τm i nのために燃料噴射量を減少することができ
ず、充てん効率12%以下でA/F=14.7以上を維
持することが不可能であることが分かる。また、τma
xによる制御限界に関して例えばA/F = 10の最
大光てん効率−曲線が示されており、最大燃料噴射時間
τmaxのために他科噴射量を増大することができず、
その曲線より上の範囲ではA/F=10以下を維持する
ことが不可能である。
The nozzle diameter of fuel injection valve B is larger than the nozzle diameter of fuel injection valve A, and even if the nozzle diameter is changed, the maximum values Qmax a, Qmax b' and the minimum values Qmin a, Qminb of the fuel injection amount are the injection time rmax ,
Significantly limited by tmin. Figure 3 shows the air-fuel ratio control range according to the injection time τmax and 1 min, the horizontal axis is the engine rotation speed, the vertical axis is the air filling efficiency in the combustion chamber, and the control limit is determined using the air-fuel ratio A/F as a parameter. Illustrated. For example, with respect to the control limit by 1min, the minimum fuel efficiency for A/F=14.7 is about 12% regardless of the engine speed, and the fuel injection amount must be reduced due to the minimum fuel injection time τmin. It can be seen that it is impossible to maintain A/F=14.7 or more with a filling efficiency of 12% or less. Also, τma
For example, the maximum photonic efficiency curve for A/F = 10 is shown for the control limit due to x, and it is not possible to increase the injection amount due to the maximum fuel injection time τmax,
In the range above the curve, it is impossible to maintain A/F=10 or less.

本発明の目的は、主燃料噴射弁の最大および最小噴射時
間の制限にもかかわらず、燃料噴射流量の制限範囲を拡
大して、空燃比の制御範囲を拡大することができる電子
制御燃料噴射方法を提供することである。
An object of the present invention is to provide an electronically controlled fuel injection method that can expand the restricted range of fuel injection flow rate and expand the control range of air-fuel ratio despite the limitations on the maximum and minimum injection times of the main fuel injection valve. The goal is to provide the following.

この目的を達成するために本発明の電子制御燃料噴射方
法によれば、従来、主燃料噴射弁とは別個に、専ら低温
始動時に増量分の燃料を噴射するために設けられている
始動用燃料噴射弁に着目し、始動後の燃料噴射流量が主
燃料噴射弁の最大燃料噴射流量を越えている場合には主
燃料噴射弁と始動用燃料噴射弁とから燃料を噴射する。
In order to achieve this object, according to the electronically controlled fuel injection method of the present invention, starting fuel is conventionally provided separately from the main fuel injection valve, exclusively for injecting an increased amount of fuel at the time of cold starting. Focusing on the injection valves, if the fuel injection flow rate after startup exceeds the maximum fuel injection flow rate of the main fuel injection valve, fuel is injected from the main fuel injection valve and the starting fuel injection valve.

第4図以降を参照して本発明の詳細な説明する。The present invention will be described in detail with reference to FIG. 4 and subsequent figures.

エアクリーナ1から吸入された空気はエアフローメータ
2、絞り弁3、サージタンク4、吸気ボート5、および
吸気弁6を含む吸気通路12を介して機関4体7の燃焼
室8へ送られる。絞り弁6は運転室の加速ペダル13に
連動する。燃焼室8はシリンダヘッド9、シリンダブロ
ック10、およびピストン11によって区画され、混合
気の燃焼によって形成された排気ガスは排気弁15、排
気ボー) 16、排気多岐管17、および排気管18を
介して大気へ放出される。バイパス通路21はle リ
弁3の上流とサージタンク4とを接続し、バイパス流量
制御弁22はパルスモータ、電磁作動弁等の電気制御弁
によって操作されてバイパス通路21の流通断面積を制
御する。排気ガス再循環(EGR)通路23は排気多岐
管17とサージタンク4とを接続し、オンオフ弁形式の
排気ガス再循環(BGR)制御弁24は電気パルスに応
動してEGR通路23を開閉する。吸気温上ンサ28は
エアフローメータ2内に設けられて吸気温を検出し、ス
ロットル位置センサ29は、絞り弁3がアイドリング開
度にあるか否かを検出する。
Air taken in from the air cleaner 1 is sent to the combustion chamber 8 of the engine 7 through an intake passage 12 that includes an air flow meter 2, a throttle valve 3, a surge tank 4, an intake boat 5, and an intake valve 6. The throttle valve 6 is linked to an accelerator pedal 13 in the driver's cab. The combustion chamber 8 is divided by a cylinder head 9, a cylinder block 10, and a piston 11, and the exhaust gases formed by the combustion of the mixture are passed through an exhaust valve 15, an exhaust bow 16, an exhaust manifold 17, and an exhaust pipe 18. released into the atmosphere. The bypass passage 21 connects the upstream of the re-valve 3 and the surge tank 4, and the bypass flow control valve 22 is operated by an electric control valve such as a pulse motor or an electromagnetic valve to control the flow cross-sectional area of the bypass passage 21. . An exhaust gas recirculation (EGR) passage 23 connects the exhaust manifold 17 and the surge tank 4, and an on-off valve type exhaust gas recirculation (BGR) control valve 24 opens and closes the EGR passage 23 in response to electrical pulses. . The intake air temperature riser 28 is provided in the air flow meter 2 to detect the intake air temperature, and the throttle position sensor 29 detects whether or not the throttle valve 3 is at an idling opening.

水温センサ30はシリンダブロック10に取付けられて
冷却水温度、すなわち機関温度を検出し、酸素濃度セン
サとして周知の空燃比センサ31は排気多岐管17の集
合部分に取付けられて集合部分における酸素濃度を検出
し、クランク角センサ32は、機関本体7のクランク軸
(図示騒ず)に結合する配電器33の軸34の回転から
クランク軸のクランク角を検出し、車速センサ35は変
速機36の出力軸の回転速度を検出する。これらのセン
サ2 、28 、29 、30 、31 、32 、3
5の出力、および蓄電池37の電圧は電子制御部40へ
送ら、れる。
The water temperature sensor 30 is attached to the cylinder block 10 to detect the cooling water temperature, that is, the engine temperature, and the air-fuel ratio sensor 31, known as an oxygen concentration sensor, is attached to the collecting part of the exhaust manifold 17 to detect the oxygen concentration in the collecting part. The crank angle sensor 32 detects the crank angle of the crankshaft from the rotation of the shaft 34 of the power distributor 33 coupled to the crankshaft (not shown) of the engine body 7, and the vehicle speed sensor 35 detects the crank angle of the crankshaft from the rotation of the shaft 34 of the power distributor 33 coupled to the crankshaft (not shown) of the engine body 7. Detects the rotation speed of the shaft. These sensors 2 , 28 , 29 , 30 , 31 , 32 , 3
5 and the voltage of the storage battery 37 are sent to the electronic control section 40.

主燃料噴射弁41は気筒に対応して吸気ボート5の近傍
に設けられ、ポンプ42は燃料タンク43からの燃料を
、燃料通路44を介して主燃料噴射弁41へ送る。さら
に低温始動時に増量分の燃料を噴射する始動用燃料噴射
弁46が、サージタンク4に設けられ、燃料通路44へ
接続されている。
The main fuel injection valve 41 is provided near the intake boat 5 in correspondence with the cylinder, and the pump 42 sends fuel from the fuel tank 43 to the main fuel injection valve 41 through a fuel passage 44. Furthermore, a starting fuel injection valve 46 that injects an increased amount of fuel during cold starting is provided in the surge tank 4 and connected to the fuel passage 44 .

電子制御部40は各センサからの入力信号をパラメータ
として燃料噴射量を計算し、計算した燃料噴射量に対応
したパルス幅の電気パルスを主燃料噴射弁41へ送る。
The electronic control unit 40 calculates the fuel injection amount using input signals from each sensor as parameters, and sends an electric pulse having a pulse width corresponding to the calculated fuel injection amount to the main fuel injection valve 41.

電子制御部40はまた、バイパス流量制御弁22、EG
R制御弁24、自動変速機の油圧制御回路のソレノイド
弁47(第5図)、点火コイル45、および始動用燃料
噴射弁46を制御する。点火コイル45の二次側は配電
器33へ接続されている。
The electronic control unit 40 also controls the bypass flow control valve 22, EG
It controls the R control valve 24, the solenoid valve 47 (FIG. 5) of the hydraulic control circuit of the automatic transmission, the ignition coil 45, and the starting fuel injection valve 46. The secondary side of the ignition coil 45 is connected to the power distributor 33.

第5図は電子制御部40の詳細を示している。FIG. 5 shows details of the electronic control section 40.

マイクロプロセッサからなるCPU(中央処理装置)4
8、ROM(リードオンリメモリ)49、RAM(ラン
ダムアクセスメモリ)50、機関停止時にも補助電源か
ら給電されて記憶を保持できる別のRAM 51、マル
チプレクサ付きA/D Cアナログ/デジタル)変換器
52、バッファ付きIlo (入力/出力)器53はバ
ス54を介して互いに接続されている。RAM 51は
不揮発性メモリであってもよい。エアフローメータ2、
吸気温センサ28、水温センーサ30、空燃比センサ3
1、および蓄電池37の出力はA/Dコンバータ52へ
送られる。また、スロットル位置センf29およびクラ
ンク角センサ32の出力はI10器53へ送られ、バイ
パス流量制御弁22、EGR制御弁24、主燃料噴射弁
41、点火コイル45、始動用燃料噴射弁46、および
ソレノイド弁47はI10器53を介してCPU48か
ら入力を受ける。
CPU (Central Processing Unit) 4 consisting of a microprocessor
8. ROM (read only memory) 49, RAM (random access memory) 50, another RAM that can be supplied with power from the auxiliary power supply and retain memory even when the engine is stopped 51, A/DC (analog/digital) converter with multiplexer 52 , buffered Ilo (input/output) devices 53 are connected to each other via a bus 54. RAM 51 may be non-volatile memory. air flow meter 2,
Intake temperature sensor 28, water temperature sensor 30, air-fuel ratio sensor 3
1 and the output of the storage battery 37 are sent to the A/D converter 52. Further, the outputs of the throttle position sensor f29 and the crank angle sensor 32 are sent to the I10 device 53, and are sent to the bypass flow control valve 22, EGR control valve 24, main fuel injection valve 41, ignition coil 45, starting fuel injection valve 46, and The solenoid valve 47 receives input from the CPU 48 via the I10 device 53.

第6図は実五例のフローチャートである。ステップ61
では実効噴射時間τeを計算する。
FIG. 6 is a flowchart of five actual examples. Step 61
Now, calculate the effective injection time τe.

τe=K・〜−−=〜  ・・・・・・・・・・・(1
)Ne−U ただしKは定数、Neは機関回転速度、Uはエアフロー
メータ2の出力電圧である。吸入空気流量が大きいとき
程、Uは小さい。ステップ62では実際の噴射時間τi
を計算する。
τe=K・〜−−=〜・・・・・・・・・・・・(1
) Ne-U where K is a constant, Ne is the engine rotation speed, and U is the output voltage of the air flow meter 2. The larger the intake air flow rate is, the smaller U is. In step 62, the actual injection time τi
Calculate.

τi =τex α十τ■    ・・・・1・・Φ拳
−(2)ただしαは、空燃比帰還信号、冷却水温度等に
関係する補正係数、τVは無効噴射時間であり、無効噴
射時間における燃料噴射量は零とみなすことができる。
τi = τex α×τ■ ...1...Φken-(2) However, α is a correction coefficient related to the air-fuel ratio feedback signal, cooling water temperature, etc., and τV is the invalid injection time. The fuel injection amount at can be considered to be zero.

ステップ63ではτmaxを計算する。In step 63, τmax is calculated.

60000      ・・・・・(3)Ne τSは第1図で定義した休止時間であり、Neの単位ハ
r、 p、m、テあるので、分子は60 X 1000
となっている。ステップ64ではτi〉τmaxか否か
を判別し、判別結果が正であればステップ65へ、否で
あればステップ67へ進む。τi〉τmaxということ
は始8動後の燃料噴射流量が主燃料噴射弁41の燃料噴
射流量を越えていることを意味する。
60000 (3) Ne τS is the pause time defined in Figure 1, and the units of Ne are r, p, m, and te, so the molecule is 60 x 1000
It becomes. In step 64, it is determined whether τi>τmax, and if the determination result is positive, the process proceeds to step 65, and if not, the process proceeds to step 67. τi>τmax means that the fuel injection flow rate after the initial operation exceeds the fuel injection flow rate of the main fuel injection valve 41.

ステップ65では始動用燃料噴射弁46を通電状態にし
、始動用燃料噴射弁46から燃料を噴射する。
In step 65, the starting fuel injection valve 46 is energized, and fuel is injected from the starting fuel injection valve 46.

実施例の始動用燃料噴射弁46では噴射ごとに休止時間
が設けられることはなく、主燃料噴射弁41における次
の燃料噴射においてもτi〉τmaxの条件が成立すれ
ば、始動用燃料の噴射弁46は連続して通電状態を維持
され、断続することなく燃料を噴射する。ステップ66
では、次の(4)式から主燃料噴射弁41の燃料噴射時
間τiを改めて計算する。改めて計算されるτiは、(
4)式から示されるように、始動用燃料噴射弁46がら
噴射された撚料量に相当する時間を、ステップ62で計
算したτiから引いたものである。
In the starting fuel injection valve 46 of the embodiment, there is no downtime for each injection, and if the condition τi>τmax is satisfied in the next fuel injection in the main fuel injection valve 41, the starting fuel injection valve 46 is kept energized continuously and injects fuel without interruption. Step 66
Now, the fuel injection time τi of the main fuel injection valve 41 is calculated again from the following equation (4). The recalculated τi is (
4) As shown in the equation, the time corresponding to the amount of twisting material injected from the starting fuel injection valve 46 is subtracted from τi calculated in step 62.

r i−、、m−−−r にn/Ne−、、、、、、、
(4)ただしmは主燃料噴射弁41の流量係数、nは始
動用燃料噴射弁46の流量係数であり、n/Neはクラ
ンク軸1回転当たりの始動用燃料噴射弁46からの燃料
噴射量に等しい。ステップ67では始動用燃料噴射弁4
6を閉状態に維持する。したがってτi≦τmaxの場
合には始動用燃料噴射弁46からの燃料噴射は行なわれ
ない。ステップ68では、主燃料噴射弁41ヘパルス信
号を送り、主燃料噴射弁41を噴射時間τiだけ開かせ
る。主燃料噴射弁41の燃料噴射時間は、燃料噴射流量
が主燃料噴射弁41の最大燃料噴射流量以下である場合
には(2)式により決められる燃料噴射時間τiとなり
、燃料噴射流量が主燃料噴射弁41の最大燃料噴射流量
を越えている場合には(4)式により決められる燃料噴
射時間τIとなる。τi≦τmaxの場合には主燃料噴
射弁41のみから燃料が噴射される。
r i-,, m---r to n/Ne-, ,,,,,,
(4) where m is the flow coefficient of the main fuel injection valve 41, n is the flow coefficient of the starting fuel injection valve 46, and n/Ne is the amount of fuel injected from the starting fuel injection valve 46 per crankshaft rotation. be equivalent to. In step 67, the starting fuel injection valve 4
6 is kept closed. Therefore, when τi≦τmax, fuel injection from the starting fuel injection valve 46 is not performed. In step 68, a pulse signal is sent to the main fuel injection valve 41 to open the main fuel injection valve 41 for an injection time τi. The fuel injection time of the main fuel injection valve 41 is the fuel injection time τi determined by equation (2) when the fuel injection flow rate is less than or equal to the maximum fuel injection flow rate of the main fuel injection valve 41, and the fuel injection flow rate is the main fuel injection flow rate. If the maximum fuel injection flow rate of the injection valve 41 is exceeded, the fuel injection time τI is determined by equation (4). When τi≦τmax, fuel is injected only from the main fuel injection valve 41.

このように本発明によれば、燃料噴射流量が主燃料噴射
弁の最大燃料噴射流量を越えている場合には主燃料噴射
弁と始動用燃料噴射弁とから燃料が噴射されるので、吸
気系における燃料供給流量の最大値を増大させることが
でき、高回転、高負荷時にも所定の燃料供給流量を確保
することができ、出力増加、および触媒過熱時の濃混合
気化による排気ガス温の低下を図ることができる。さら
に、主燃料噴射弁と始動用燃料噴射弁とを併用する結果
、ノズル径の小さい、すなわち最小燃料噴射量が小さい
主燃料噴射弁を採用することができ、吸気系における燃
料供給流量の最小値を減少させることができ、低負荷お
よびアイドリンク時の燃費改善、および有害成分の放出
抑制等を図ることができる。
As described above, according to the present invention, when the fuel injection flow rate exceeds the maximum fuel injection flow rate of the main fuel injection valve, fuel is injected from the main fuel injection valve and the starting fuel injection valve, so that the intake system It is possible to increase the maximum value of the fuel supply flow rate at high speeds and high loads, and it is possible to secure the specified fuel supply flow rate even at high speeds and high loads, increasing output and reducing exhaust gas temperature due to rich mixture vaporization when the catalyst is overheated. can be achieved. Furthermore, as a result of using the main fuel injection valve and the starting fuel injection valve together, it is possible to use the main fuel injection valve with a small nozzle diameter, that is, a small minimum fuel injection amount, and the minimum value of the fuel supply flow rate in the intake system. This makes it possible to improve fuel efficiency under low load and idling conditions, and to suppress the release of harmful components.

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

第1図は主燃料噴射弁の噴射時間の限界を示す説明図、
第2図は主燃料噴射弁の燃料噴射量の限界を示すグラフ
、第3図は充てん効率に関する空燃比の制御限界を示す
グラフ、第4図は本発明が適用される電子制御燃料噴射
機関の概略図、第5図は第4図の電子制御部内のブロッ
ク図、第6図は本発明の実施例のフロニチャートである
。 8・・・燃焼室、40・・・電子制御部、41・・・主
燃料噴射弁、46・・・始動用燃料噴射弁。
Fig. 1 is an explanatory diagram showing the limit of the injection time of the main fuel injection valve;
FIG. 2 is a graph showing the limit of the fuel injection amount of the main fuel injection valve, FIG. 3 is a graph showing the control limit of the air-fuel ratio related to charging efficiency, and FIG. 5 is a block diagram of the electronic control section in FIG. 4, and FIG. 6 is a flow chart of an embodiment of the present invention. 8... Combustion chamber, 40... Electronic control unit, 41... Main fuel injection valve, 46... Starting fuel injection valve.

Claims (1)

【特許請求の範囲】[Claims] 各気筒に対応して設けられて燃料を噴射する主燃料噴射
弁と低温始動時に増量分の燃料を噴射する始動用燃料噴
射弁とを吸気系にもつ機関の電子制御燃料噴射方法にお
いて、始動後の燃料噴射流量が主燃料噴射弁の最大燃料
噴射流量を越えている場合には主燃料噴射弁と始動用燃
料噴射弁とから燃料を噴射することを特徴とする、電子
制御燃料噴射方法。
In an electronically controlled fuel injection method for an engine whose intake system includes a main fuel injection valve that injects fuel corresponding to each cylinder and a starting fuel injection valve that injects an increased amount of fuel when starting at a low temperature, An electronically controlled fuel injection method, characterized in that when the fuel injection flow rate exceeds the maximum fuel injection flow rate of the main fuel injection valve, fuel is injected from the main fuel injection valve and the starting fuel injection valve.
JP12310181A 1981-08-07 1981-08-07 Electronically controlled fuel injection method Pending JPS5825525A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12310181A JPS5825525A (en) 1981-08-07 1981-08-07 Electronically controlled fuel injection method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12310181A JPS5825525A (en) 1981-08-07 1981-08-07 Electronically controlled fuel injection method

Publications (1)

Publication Number Publication Date
JPS5825525A true JPS5825525A (en) 1983-02-15

Family

ID=14852215

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12310181A Pending JPS5825525A (en) 1981-08-07 1981-08-07 Electronically controlled fuel injection method

Country Status (1)

Country Link
JP (1) JPS5825525A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0243946A2 (en) * 1986-04-29 1987-11-04 Mitsubishi Denki Kabushiki Kaisha Fuel control device for internal combustion engine
JPH0579494U (en) * 1992-03-27 1993-10-29 リズム時計工業株式会社 Beat clock

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0243946A2 (en) * 1986-04-29 1987-11-04 Mitsubishi Denki Kabushiki Kaisha Fuel control device for internal combustion engine
JPH0579494U (en) * 1992-03-27 1993-10-29 リズム時計工業株式会社 Beat clock

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