JPS6338535B2 - - Google Patents
Info
- Publication number
- JPS6338535B2 JPS6338535B2 JP56195148A JP19514881A JPS6338535B2 JP S6338535 B2 JPS6338535 B2 JP S6338535B2 JP 56195148 A JP56195148 A JP 56195148A JP 19514881 A JP19514881 A JP 19514881A JP S6338535 B2 JPS6338535 B2 JP S6338535B2
- Authority
- JP
- Japan
- Prior art keywords
- pulse width
- pulse
- basic
- fuel injection
- engine
- 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 29
- 238000002347 injection Methods 0.000 claims description 27
- 239000007924 injection Substances 0.000 claims description 27
- 238000000034 method Methods 0.000 claims description 11
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 238000010586 diagram Methods 0.000 description 6
- 238000007493 shaping process Methods 0.000 description 4
- 230000001133 acceleration Effects 0.000 description 3
- 239000000498 cooling water Substances 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 238000003079 width control Methods 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
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/10—Introducing corrections for particular operating conditions for acceleration
Description
【発明の詳細な説明】
本発明は内燃機関の電子制御燃料噴射装置の制
御方法に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method of controlling an electronically controlled fuel injection system for an internal combustion engine.
内燃機関の電子制御燃料噴射装置は、機関が常
に適正な燃焼を行なうように各種エンジンパラメ
ータに基づいたパルス幅の燃料噴射パルスを算出
し、その燃料噴射パルスによつて電磁噴射弁を駆
動して機関へ間欠的に燃料を供給するものであ
る。 An electronically controlled fuel injection system for an internal combustion engine calculates a fuel injection pulse with a pulse width based on various engine parameters so that the engine always performs proper combustion, and uses the fuel injection pulse to drive an electromagnetic injection valve. It supplies fuel to the engine intermittently.
かかる電子制御燃料噴射装置の従来例を第1図
を参照して説明する。 A conventional example of such an electronically controlled fuel injection device will be explained with reference to FIG.
第1図において、1は波形整形回路であり、イ
グニシヨンコイル(図示せず)の1次側より得ら
れる振動波形のイグニシヨン信号を波形整形して
方形波の回転パルスを発生する。波形整形回路1
の出力端には基本パルス発生回路2が接続されて
おり、基本パルス発生回路2には吸気管(図示せ
ず)に設けられたエアフローメータ3の出力端が
別に接続されている。基本パルス発生回路2の出
力端には基本パルスの最大パルス幅を制限するパ
ルス幅制御回路4を介して増量補正回路5が接続
されている。増量補正回路5には基本パルスのパ
ルス幅の補正を指令するように機関の運転状態を
検出するスロツトル開度センサ(図示せず)、冷
却水温センサ(図示せず)等の各種のセンサが接
続されている。増量補正回路5の出力端には駆動
回路6が接続され、駆動回路6は気筒毎に設けら
れた電磁噴射弁7を駆動する。 In FIG. 1, reference numeral 1 denotes a waveform shaping circuit which shapes an ignition signal in a vibration waveform obtained from the primary side of an ignition coil (not shown) to generate a square wave rotation pulse. Waveform shaping circuit 1
A basic pulse generating circuit 2 is connected to the output end of the basic pulse generating circuit 2, and an output end of an air flow meter 3 provided in an intake pipe (not shown) is separately connected to the basic pulse generating circuit 2. An increase correction circuit 5 is connected to the output end of the basic pulse generation circuit 2 via a pulse width control circuit 4 that limits the maximum pulse width of the basic pulse. The increase correction circuit 5 is connected to various sensors such as a throttle opening sensor (not shown), a cooling water temperature sensor (not shown), etc., which detect the operating state of the engine so as to command correction of the pulse width of the basic pulse. has been done. A drive circuit 6 is connected to the output end of the increase correction circuit 5, and the drive circuit 6 drives an electromagnetic injection valve 7 provided for each cylinder.
上記構成の電子制御燃料噴射装置においては、
波形整形回路1の出力端から機関の点火すなわち
クランクシヤフトの回転に同期した回転パルスが
基本パルス発生回路2に供給される。一方、エア
フローメータ3は機関の吸入空気量に応じた電圧
を発生する。このエアフローメータ3の出力電圧
と回転パルスとに応じて基本パルス発生回路2が
基本噴射量に対応する基本パルスを発生する。基
本パルスのパルス幅が所定幅より大の場合にはパ
ルス幅制限回路4が基本パルスのパルス幅を所定
幅に制限する。そして基本パルスは増量補正回路
5において各種センサの出力信号に応じてそのパ
ルス幅が補正されて燃料噴射パルスとなる。こう
して発生した燃料噴射パルスのパルス幅に応じて
駆動回路6が電磁噴射弁7を駆動して燃料が機関
に供給されるのである。 In the electronically controlled fuel injection device with the above configuration,
A rotational pulse synchronized with the ignition of the engine, that is, the rotation of the crankshaft, is supplied from the output end of the waveform shaping circuit 1 to the basic pulse generation circuit 2. On the other hand, the air flow meter 3 generates a voltage according to the intake air amount of the engine. In response to the output voltage of the air flow meter 3 and the rotation pulse, the basic pulse generation circuit 2 generates a basic pulse corresponding to the basic injection amount. When the pulse width of the basic pulse is larger than the predetermined width, the pulse width limiting circuit 4 limits the pulse width of the basic pulse to the predetermined width. The pulse width of the basic pulse is corrected in the increase correction circuit 5 according to the output signals of various sensors, and becomes a fuel injection pulse. The drive circuit 6 drives the electromagnetic injection valve 7 in accordance with the pulse width of the fuel injection pulse thus generated, and fuel is supplied to the engine.
ところで、内燃機関において、吸入空気は第2
図のように矢印Zの方向にエアフイルター8を通
過して吸気管9内に設けられた上記エアフローメ
ータ3のフラツプ3a、スロツトル弁10、そし
てサージタンク室11を経て機関12へ供給され
る。エアフローメータ3は、フラツプ3aの回転
に連動するポテンシヨメータ(図示せず)を有
し、吸入空気量に応じてフラツプ3aが回転し、
そのプラツプ3aの回転角度に応じた出力電圧が
ポテンシヨメータより発生するようになつてい
る。例えば、機関回転数が低回転数にあるときに
スロツトル弁10を急開弁した場合、エアフロー
メータ3の出力電圧VOUTは第3図のように変化
する。第3図において時間topはスロツトル開弁
時、期間Aはフラツプ3の慣性による動作遅れの
部分、期間Bはサージタンク室11を満たすため
に急に流入する空気量によりフラツプ3aが余分
に回転してオーバシユートを生ずる部分、期間C
は定常状態になつた部分である。なお、サージタ
ンク室11は機関のサイクル動作による吸入空気
の脈動を緩和するために形成されている。 By the way, in an internal combustion engine, intake air is
As shown in the figure, the air passes through the air filter 8 in the direction of arrow Z and is supplied to the engine 12 via the flap 3a of the air flow meter 3 provided in the intake pipe 9, the throttle valve 10, and the surge tank chamber 11. The air flow meter 3 has a potentiometer (not shown) that is linked to the rotation of the flap 3a, and the flap 3a rotates according to the amount of intake air.
An output voltage corresponding to the rotation angle of the plug 3a is generated by the potentiometer. For example, if the throttle valve 10 is suddenly opened when the engine speed is low, the output voltage V OUT of the air flow meter 3 changes as shown in FIG. In Fig. 3, time top is when the throttle valve is opened, period A is a delay in operation due to the inertia of flap 3, and period B is when flap 3a rotates extra due to the amount of air suddenly flowing in to fill surge tank chamber 11. The part where overshoot occurs, period C
is the part that has reached a steady state. Incidentally, the surge tank chamber 11 is formed to alleviate the pulsation of intake air caused by the cycle operation of the engine.
しかしながら、従来の電子制御燃料噴射装置に
おいては、機関の高負荷、高回転での運転状態を
考慮してパルス幅制限回路4による基本パルスの
パルス幅の制限幅が比較的大きく設定されてい
る。このため、上記のように機関回転数が低回転
数にあるときにスロツトル弁10を急開弁した場
合、第3図の期間Bではオーバシユートにより基
本パルスのパルス幅は低回数からの加速時にして
は大となるが、パルス幅制限回路4によりパルス
幅が制限されるほど大でもないため空燃比がオー
バリツチになるという問題点があつた。 However, in the conventional electronically controlled fuel injection system, the pulse width limitation of the basic pulse by the pulse width limiting circuit 4 is set relatively large in consideration of the high load and high rotational engine operating conditions. Therefore, if the throttle valve 10 is suddenly opened when the engine speed is low as described above, the pulse width of the basic pulse will change during acceleration from a low number of times due to overshoot in period B in Fig. 3. Although the pulse width is large, it is not so large that the pulse width is limited by the pulse width limiting circuit 4, so there is a problem that the air-fuel ratio becomes overbalanced.
そこで、本発明の目的は、機関の低回転からの
加速時の空燃比の悪化を防止し得る電子制御燃料
噴射装置の制御方法を提供することである。 SUMMARY OF THE INVENTION Accordingly, an object of the present invention is to provide a control method for an electronically controlled fuel injection device that can prevent deterioration of the air-fuel ratio during acceleration of an engine from low rotation speeds.
本発明による電子制御燃料噴射装置の制御方法
は、吸入空気量及び機関回転数に応じて基本噴射
量に対応するパルス幅の基本パルスを発生し、基
本パルスのパルス幅を基準最大パルス幅以下に制
限し、その制限した基本パルスを各種のエンジン
パラメータに応じて補正して燃料噴射パルスを発
生し、該燃料噴射パルスのパルス幅だけ燃料噴射
する制御方法であり、機関回転数が低いほど基準
最大パルス幅を小さくしたことを特徴としてい
る。 A control method for an electronically controlled fuel injection device according to the present invention generates a basic pulse with a pulse width corresponding to a basic injection amount according to an intake air amount and an engine speed, and sets the pulse width of the basic pulse to a reference maximum pulse width or less. This control method generates fuel injection pulses by correcting the limited basic pulses according to various engine parameters, and injects fuel by the pulse width of the fuel injection pulses.The lower the engine speed, the higher the reference maximum. It is characterized by a small pulse width.
以下、本発明の実施例を第4図を参照して説明
する。 Embodiments of the present invention will be described below with reference to FIG.
第4図において、第1図と同等部分は同一符号
で示されており、パルス幅制限回路4には、基本
パルスが供給されると共に波形整形回路1から回
転パルスも供給されるようになつている。本発明
の制御方法を適用した電子制御燃料噴射装置のそ
の他の構成は第1図に示した従来例と同様であ
る。 In FIG. 4, parts equivalent to those in FIG. There is. The rest of the configuration of the electronically controlled fuel injection system to which the control method of the present invention is applied is the same as that of the conventional example shown in FIG.
上記構成において、パルス幅制限回路4は回転
パルスの発生、すなわち機関回転数に応じて基本
パルスのパルス幅の制限幅を設定し、第5図のよ
うに機関回転数Nが大きくなるほど基本パルスの
最大パルス幅TPMAXも大きくなるように制限す
る。 In the above configuration, the pulse width limiting circuit 4 sets the pulse width limit width of the basic pulse according to the generation of rotational pulses, that is, the engine rotational speed, and as shown in FIG. The maximum pulse width T PMAX is also limited to be large.
この結果、機関回転数が低回転数にあるときに
スロツトル弁10を急開弁した場合に、第3図の
ようにエアフローメータ3の出力電圧波形にオー
バシユートが生じて基本パルス発生回路2の出力
端に発生する基本パルスのパルス幅が機関の低回
転数からの加速にしては大となつても、その基本
パルスのパルス幅はパルス幅制限回路4により機
関回転数に応じたパルス幅に制限させるのであ
る。 As a result, when the throttle valve 10 is suddenly opened when the engine speed is low, an overshoot occurs in the output voltage waveform of the air flow meter 3 as shown in FIG. Even if the pulse width of the basic pulse generated at the end is large for acceleration from a low engine speed, the pulse width of the basic pulse is limited by the pulse width limiting circuit 4 to a pulse width corresponding to the engine speed. Let it happen.
このように、本発明による電子制御燃料噴射装
置の制御方法によれば、基本パルスが基準最大パ
ルス幅以下に制限され、機関回転数が低くなるほ
ど基準最大パルス幅が小さく設定される。よつ
て、機関の低回転からの加速時の空燃比の悪化を
防止することができるため、運転性能、燃費、そ
して排ガス浄化の向上が図れるのである。 As described above, according to the control method for an electronically controlled fuel injection device according to the present invention, the basic pulse is limited to the reference maximum pulse width or less, and the lower the engine speed, the smaller the reference maximum pulse width is set. Therefore, it is possible to prevent the air-fuel ratio from deteriorating when the engine accelerates from low rotation speeds, thereby improving driving performance, fuel efficiency, and exhaust gas purification.
なお、上記した本発明の制御方法を適用した電
子制御燃料噴射装置においては、第4図の破線で
囲まれた部分をマイクロコンピユータに置換えて
プログラムに応じて上記同様の動作を処理するよ
うにしても良いのである。例えば、第5図に示し
た機関回転数―最大パルス幅特性がROMにデー
タテーブルとして予め書き込まれ、検出された機
関回転数に応じた最大パルス幅をデータテーブル
から読み出し、吸入空気量及び機関回転数に応じ
て設定された基本パルス幅が読み出した最大パル
ス幅より大なるときには基本パルス幅をその最大
パルス幅に等しくする動作がプログラムに従つて
行なわれる。 In the electronically controlled fuel injection system to which the control method of the present invention described above is applied, the part surrounded by the broken line in FIG. 4 is replaced with a microcomputer to process the same operations as described above according to a program. It's also good. For example, the engine speed vs. maximum pulse width characteristic shown in Figure 5 is written in advance as a data table in the ROM, and the maximum pulse width corresponding to the detected engine speed is read from the data table, and the intake air amount and engine speed are When the basic pulse width set according to the number is larger than the read maximum pulse width, an operation is performed according to the program to make the basic pulse width equal to the maximum pulse width.
第1図は電子制御燃料噴射装置の従来例を示す
ブロツク図、第2図は内燃機関の吸気系を示す概
略図、第3図はエアフローメータの出力電圧波形
図、第4図は本発明の制御方法を適用した電子制
御燃料噴射装置を示すブロツク図、第5図は基本
パルスの最大パルス幅特性図である。
主要部分の符号の説明、1…波形整形回路、2
…基本パルス発生回路、3…エアフローメータ、
4…パルス幅制限回路、10…スロツトル弁、1
1…サージタンク室。
Fig. 1 is a block diagram showing a conventional example of an electronically controlled fuel injection device, Fig. 2 is a schematic diagram showing an intake system of an internal combustion engine, Fig. 3 is an output voltage waveform diagram of an air flow meter, and Fig. 4 is a diagram of the present invention. A block diagram showing an electronically controlled fuel injection system to which the control method is applied, FIG. 5 is a maximum pulse width characteristic diagram of the basic pulse. Explanation of symbols of main parts, 1...Waveform shaping circuit, 2
...Basic pulse generation circuit, 3...Air flow meter,
4... Pulse width limiting circuit, 10... Throttle valve, 1
1...Surge tank room.
Claims (1)
て基本噴射量に対応するパルス幅の基本パルスを
発生し、前記基本パルスのパルス幅を基準最大パ
ルス幅以下に制限し、その制限した基本パルスを
各種のエンジンパラメータに応じて補正して燃料
噴射パルスを発生し、該燃料噴射パルスのパルス
幅だけ燃料噴射する電子制御燃料噴射装置の制御
方法であつて、前記機関回転数が低いほど前記基
準最大パルス幅を小さくしたことを特徴とする制
御方法。1 Generate a basic pulse with a pulse width corresponding to the basic injection amount according to the intake air amount and engine speed of the internal combustion engine, limit the pulse width of the basic pulse to a reference maximum pulse width or less, and generate the limited basic pulse. A control method for an electronically controlled fuel injection device that generates a fuel injection pulse by correcting it according to various engine parameters, and injects fuel by the pulse width of the fuel injection pulse, wherein the lower the engine speed, the lower the reference value. A control method characterized by reducing the maximum pulse width.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19514881A JPS5896132A (en) | 1981-12-04 | 1981-12-04 | Electronic control fuel injection device of internal-combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19514881A JPS5896132A (en) | 1981-12-04 | 1981-12-04 | Electronic control fuel injection device of internal-combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5896132A JPS5896132A (en) | 1983-06-08 |
JPS6338535B2 true JPS6338535B2 (en) | 1988-08-01 |
Family
ID=16336229
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP19514881A Granted JPS5896132A (en) | 1981-12-04 | 1981-12-04 | Electronic control fuel injection device of internal-combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5896132A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH063613Y2 (en) * | 1989-11-08 | 1994-02-02 | 株式会社八光電機製作所 | Implantable reservoir |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6050245A (en) * | 1983-08-29 | 1985-03-19 | Nissan Motor Co Ltd | Fuel injection device in internal-combustion engine |
JPS61241431A (en) * | 1985-04-16 | 1986-10-27 | Nippon Denso Co Ltd | Fuel injection controlling method |
JPH0663470A (en) * | 1991-10-30 | 1994-03-08 | Nippon Kansen Kogyo Kk | Mist recovery device and outward air curtain device of automatic painting machine |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5428936A (en) * | 1977-08-06 | 1979-03-03 | Bosch Gmbh Robert | Method for deciding injection time of internal combustion engine and its device |
JPS5598624A (en) * | 1979-01-24 | 1980-07-26 | Nippon Denso Co Ltd | Fuel injection controlling method |
JPS57212336A (en) * | 1981-06-24 | 1982-12-27 | Nippon Denso Co Ltd | Electronic controlled fuel injection system |
JPS5828552A (en) * | 1981-07-27 | 1983-02-19 | Toyota Motor Corp | Method and device for electronically controlled fuel injection to internal combustion engine |
-
1981
- 1981-12-04 JP JP19514881A patent/JPS5896132A/en active Granted
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5428936A (en) * | 1977-08-06 | 1979-03-03 | Bosch Gmbh Robert | Method for deciding injection time of internal combustion engine and its device |
JPS5598624A (en) * | 1979-01-24 | 1980-07-26 | Nippon Denso Co Ltd | Fuel injection controlling method |
JPS57212336A (en) * | 1981-06-24 | 1982-12-27 | Nippon Denso Co Ltd | Electronic controlled fuel injection system |
JPS5828552A (en) * | 1981-07-27 | 1983-02-19 | Toyota Motor Corp | Method and device for electronically controlled fuel injection to internal combustion engine |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH063613Y2 (en) * | 1989-11-08 | 1994-02-02 | 株式会社八光電機製作所 | Implantable reservoir |
Also Published As
Publication number | Publication date |
---|---|
JPS5896132A (en) | 1983-06-08 |
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