JPH0472436A - Fuel injector of engine - Google Patents

Fuel injector of engine

Info

Publication number
JPH0472436A
JPH0472436A JP18414990A JP18414990A JPH0472436A JP H0472436 A JPH0472436 A JP H0472436A JP 18414990 A JP18414990 A JP 18414990A JP 18414990 A JP18414990 A JP 18414990A JP H0472436 A JPH0472436 A JP H0472436A
Authority
JP
Japan
Prior art keywords
engine
pressure
injection
acceleration
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
JP18414990A
Other languages
Japanese (ja)
Inventor
Koji Nishimoto
西本 浩二
Koichi Yamane
山根 恒一
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP18414990A priority Critical patent/JPH0472436A/en
Publication of JPH0472436A publication Critical patent/JPH0472436A/en
Pending legal-status Critical Current

Links

Landscapes

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

Abstract

PURPOSE:To perform asynchronizing injection of a proper quantity by providing an asynchronizing injection forbidden time for a specified time, and not performing the asynchronzining injection even if an acceleration condition is detected during that time, after only using an intake pipe pressure sensor without using a throttle opening sensor, so as to detect acceleration condition followed by making asynchronizing injection. CONSTITUTION:A pressure detection means 3 which detects pressure in the intake pipe 2 of an engine 1 is provided, and a pressure average value is calculated by averaging output signals of the pressure detection means 3. When a deviation of a specified value or more from the calculated pressure average value is generated at the output signal of the pressure detection means, it is judged that an engine is under an acceleration condition, and fuel is injected asynchronizingly from an injector 4 by a first control means 6. Injection of asynchronous fuel is forbidden by the second control means 6 for a specified time of a specified stroke of the engine, after the asynchronous fuel is injected one. Consequently, the asynchronous injection of the optimum quantity can be performed in all acceleration conditions such as warming acceleration for which the acceleration time is long.

Description

【発明の詳細な説明】 [産業上の利用分野] この発明は、自動車等に用いられるエンジンの燃料噴射
装置に関し、特にエンジン加速時の燃料噴射手段に関す
るものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a fuel injection device for an engine used in an automobile or the like, and particularly to a fuel injection means during engine acceleration.

[従来の技術] 従来、自動車等のエンジンの燃料噴射では、エンジン燃
料室に吸入される空気量に見合った燃料を噴射するが、
加速時などの過渡状態では、空気量の検出遅れや吸気管
に噴射された燃料が燃焼室に吸入されるまでの搬送遅れ
などにより燃焼室への燃料供給が遅れるため、混合気の
空燃比を最適に保つことができない、そのため、加速状
態を検出した時に燃料増量を行なうが、逸速く加速状態
を検出するために、加速状態検出手段には一般にスロッ
トル開度センサを用い、一定時間間隔毎のセンサ出力の
変化量が所定値以上の時に加速状態を検出し、加速状態
が生じた時に非同期噴射を行なっていた。
[Prior Art] Conventionally, in fuel injection for engines such as automobiles, fuel is injected in an amount commensurate with the amount of air taken into the engine fuel chamber.
During transient conditions such as during acceleration, the air-fuel ratio of the mixture is Therefore, when an acceleration state is detected, the amount of fuel is increased. However, in order to quickly detect an acceleration state, a throttle opening sensor is generally used as the acceleration state detection means, and the amount of fuel is increased at regular intervals. An acceleration state is detected when the amount of change in the sensor output is equal to or greater than a predetermined value, and asynchronous injection is performed when the acceleration state occurs.

「発明が解決しようとする課題] 従来のエンジンの燃料噴射装置は上記のように精成され
ていたので、加速状態検出のためにスロットル開度セン
サが必要であり、コストが増大するという問題があった
。そこで、スロットル開度センサを用いずに逸速く加速
状態を検出し、非同期噴射により加速時の空燃比を最適
に保つことができるエンジンの燃料噴射装置を提案され
た。しかし、この装置は加速状態を検出する毎に非同期
燃料を噴射する装置であった為、例えば、加速時間の長
い緩加速時等において非同期燃料を複数回噴射すること
となり、その結果燃料が過剰となり排気ガスやドライバ
ビリティを悪化させるという問題点があった。
``Problem to be solved by the invention'' Since the fuel injection system for conventional engines was sophisticated as described above, a throttle opening sensor was required to detect the acceleration state, which caused the problem of increased cost. Therefore, an engine fuel injection device was proposed that could quickly detect the acceleration state without using a throttle opening sensor and maintain the optimal air-fuel ratio during acceleration using asynchronous injection.However, this device was a device that injected asynchronous fuel every time it detected an acceleration state, so for example, during slow acceleration with a long acceleration time, asynchronous fuel would be injected multiple times, resulting in excess fuel and exhaust gas and driver There was a problem in that it worsened the stability.

この発明は上記のような問題点を解決するためになされ
たもので、加速時間の長い緩加速時等あらゆる加速状態
において最適な量の非同期噴射を行うコストパフォーマ
ンスの優れたエンジンの燃料噴射装置を得ることを目的
とする。
This invention was made in order to solve the above-mentioned problems, and provides an engine fuel injection system with excellent cost performance that performs asynchronous injection of the optimum amount in all acceleration conditions, such as during slow acceleration with a long acceleration time. The purpose is to obtain.

[課題を解決するための手段] この発明に係るエンジンの燃料噴射装置は、エンジンの
吸気管内圧力を検出する圧力検出手段と、この圧力検出
手段の出力信号を平均化して圧力平均値を算出し、前記
圧力検出手段の出力信号値が前記算出した圧力平均値か
ら所定値以上の偏差を生じた時にエンジンが加速状態で
あると判定し、前記加速状態と判定した時に非同期に燃
料を噴射する第1の制御手段と、−度非同期燃料を噴射
した後に、所定時間またはエンジンの所定行程の間非同
期燃料を噴射することを禁止する第2の制御手段とを備
えたものである。
[Means for Solving the Problems] A fuel injection device for an engine according to the present invention includes a pressure detection means for detecting the pressure inside the intake pipe of the engine, and an output signal of the pressure detection means to calculate a pressure average value. , determining that the engine is in an acceleration state when the output signal value of the pressure detection means deviates from the calculated pressure average value by a predetermined value or more, and injecting fuel asynchronously when it is determined that the engine is in the acceleration state. The engine is equipped with a second control means that prohibits the injection of the asynchronous fuel for a predetermined period of time or a predetermined stroke of the engine after injecting the asynchronous fuel.

「作 用] この発明においては、吸気管圧力で加速状態を検出し、
加速状態を検出した時に非同期噴射を行ない、その後所
定時間またはエンジンの所定の行程の間加速状態を検出
しても非同期噴射を禁止する。
"Function" In this invention, the acceleration state is detected by the intake pipe pressure,
Asynchronous injection is performed when an acceleration state is detected, and asynchronous injection is then prohibited even if an acceleration state is detected for a predetermined time or a predetermined stroke of the engine.

[実施例コ 以下、この発明の一実施例を図について説明する。第1
図は、この発明によるエンジンの燃料噴射装置の一実施
例を示す精成図である。第1図において、(1)はエン
ジン、(2)はエンジン(1)に接続された吸気管、(
3)は吸気管(2)の内部の圧力を検出する圧力センサ
である。圧力センサ(3)の出力は制御部(6)のA/
Dコンバータ(61)に入力される。(4)は吸気管(
2)の各シリンダ吸気ホト近傍に設Wされたインジェク
タであり、インジェクタ(4)には圧力を一定に調整し
た燃料が圧送される。(5)はエンジン(1)の回転を
パルスとして検出するクランク角センサであり、クラン
ク角センサ(5)の出力は制御部(6)の入力回路(6
2)に入力される。制御部(6)は、圧力センサ(3)
やクランク角センサ(5)などの出力から所要噴射燃料
量を演算し、これに応じたパルス幅の駆動パルスをイン
ジェクタ(4)に対し発生する。制御部(6)において
は、A/Dコンバータ(61)が圧力センサ(3)のア
ナログ信号をデジタル値に変換し、マイクロプロセッサ
(63)に送出する。入力回路(62)は、クランク角
センサ(5)からのパルス入力信号をレベル変換し、そ
の出力をマイクロプロセッサ(63)に送出する。マイ
クロプロセッサ(63)は、A/Dコンバータ(61)
および入力回路(62)から得られたデジタル値および
パルス信号に基づいてエンジン(1)へ供給する燃料量
を演算し、その結果に応じたパルス幅の駆動パルスをイ
ンジェクタ(4)に対して出力する。マイクロプロセッ
サ(63)の制御手順やデータは予めROM(64)に
記憶され、またはRAM(65)は演i過程におけるデ
ータを一時的に格納する。出力回路(66)は、マイク
ロプロセッサ(63)の出力に応じてインジェクタ(4
)を駆動する。
[Example 1] An example of the present invention will be described below with reference to the drawings. 1st
FIG. 1 is a detailed diagram showing an embodiment of an engine fuel injection device according to the present invention. In Fig. 1, (1) is the engine, (2) is the intake pipe connected to the engine (1), and (2) is the intake pipe connected to the engine (1).
3) is a pressure sensor that detects the pressure inside the intake pipe (2). The output of the pressure sensor (3) is controlled by the A/
It is input to a D converter (61). (4) is the intake pipe (
2) is an injector W installed near each cylinder intake port, and fuel whose pressure is adjusted to a constant level is fed under pressure to the injector (4). (5) is a crank angle sensor that detects the rotation of the engine (1) as a pulse, and the output of the crank angle sensor (5) is the input circuit (6) of the control unit (6).
2). The control unit (6) includes a pressure sensor (3)
The required amount of fuel to be injected is calculated from the output of a crank angle sensor (5), etc., and a drive pulse having a pulse width corresponding to the calculated amount is generated to the injector (4). In the control section (6), an A/D converter (61) converts the analog signal of the pressure sensor (3) into a digital value and sends it to the microprocessor (63). The input circuit (62) converts the level of the pulse input signal from the crank angle sensor (5) and sends the output to the microprocessor (63). The microprocessor (63) is an A/D converter (61)
The amount of fuel to be supplied to the engine (1) is calculated based on the digital value and pulse signal obtained from the input circuit (62), and a drive pulse with a pulse width corresponding to the result is output to the injector (4). do. The control procedure and data of the microprocessor (63) are stored in advance in the ROM (64), or the RAM (65) temporarily stores data in the i-process. The output circuit (66) outputs the injector (4) according to the output of the microprocessor (63).
) to drive.

次に、4サイクル3気筒エンジンの全気筒同時噴射シス
テムの場合の動作について説明する。第2図〜第4図は
制御部(6)の動作を示すフローチャトで、第2図はプ
ログラムのメイン演算部を示し、ステップ(201)で
は、第4図のクランク角センサ(5)による一定クラン
ク角割込処理のステップ(401)で計測したクランク
角センサ信号周期T(第5図(a)参照)に基づき、エ
ンジン回転数Neを演算する。ステップ(202)では
、ステップ(201)で求めたエンジン回転数Neと第
3図のステップ(301)で求めた吸気管圧力pb、 
 (第5図(c)参照)の値とから、あらかじめROM
(64)に記憶させている体積効率η、の値を補間演算
し求める。
Next, the operation in the case of an all-cylinder simultaneous injection system of a four-stroke three-cylinder engine will be described. 2 to 4 are flowcharts showing the operation of the control section (6). FIG. 2 shows the main calculation section of the program. In step (201), the crank angle sensor (5) of FIG. The engine rotation speed Ne is calculated based on the crank angle sensor signal period T (see FIG. 5(a)) measured in step (401) of the crank angle interrupt processing. In step (202), the engine speed Ne obtained in step (201) and the intake pipe pressure pb obtained in step (301) in FIG.
(See Figure 5(c)).
The value of the volumetric efficiency η stored in (64) is determined by interpolation.

第3図はタイマーによる一定時間割込処理を示し、例え
ば5ミリ秒(+1lsec)毎にステップ(301>で
圧力センサ(3)の出力をA/D変換する。ステラフ責
302)では、第4図のステップ(403)で圧カセン
サA/D変換平均値pb、、、。(第5図(c)参照)
を算出するために、ステップ(302)でA/D変換し
た圧力センサA/D変換値Pboを積算する。ステップ
(303)でも、ステラフ責302)と同じく、第4図
のステップ(403)で圧カセンサA/D変換平均値P
b、、、、を算出するために、ステップ(301)のA
/D変換回数をカウントするカウンタの値Nをカウント
アツプする。ステップ(304)では、エンジンが加速
状態か否かを判定するため、ステップ(301)でA/
D変換した圧力センサA/D変換値Pboと、第4図の
ステップ(403)で算出した圧力センサA/D変換平
均値Pbm**aに所定値α(第5図(c)参照)を加
えた値とを比較し、ステップ(301)でA/D変換し
た圧力センサA/D変換値Pb、、が小さい場合は、第
5図(C)の期間T1で示すように、加速状態とは判定
せず、ステップ(305)で加速状態フラグをクリアし
、処理を終了する。
FIG. 3 shows a fixed time interrupt process by a timer, and for example, the output of the pressure sensor (3) is A/D converted in step (301>) every 5 milliseconds (+1 lsec). In step (403), the pressure sensor A/D conversion average value pb, . (See Figure 5(c))
In order to calculate , the pressure sensor A/D converted value Pbo that was A/D converted in step (302) is integrated. In step (303), as in the case of Stellaf Responsibility 302), in step (403) of FIG. 4, the pressure sensor A/D conversion average value P
In order to calculate b, , , A of step (301)
/Increments the value N of a counter that counts the number of D conversions. In step (304), in order to determine whether the engine is in an acceleration state, in step (301)
A predetermined value α (see FIG. 5(c)) is set for the D-converted pressure sensor A/D conversion value Pbo and the pressure sensor A/D conversion average value Pbm**a calculated in step (403) of FIG. If the pressure sensor A/D conversion value Pb, which was A/D converted in step (301), is small, the acceleration state is changed as shown by period T1 in FIG. is not determined, the acceleration state flag is cleared in step (305), and the process ends.

もし、第5図(c)の期間T2.T3およ−びT4で示
すように圧カセンサA/D変換値Pb7が圧カセンサA
/D平均値Pbmaanより大きい場合は、第5図(c
)の時刻tm+、tmzおよびtmzで加速状態と判定
し、ステップ(306)に進む、ステ・ンブ(306)
では前回加速状態であったか否かを判定し、前回も加速
状態であればステラフ責311)に進み、前回が加速状
態でなければステップ(307)に進む。
If period T2 in FIG. 5(c). As shown by T3 and T4, the pressure sensor A/D conversion value Pb7 is
/D is larger than the average value Pbmaan in Figure 5 (c
) is determined to be in an acceleration state at times tm+, tmz, and tmz, and proceeds to step (306).
Then, it is determined whether or not the vehicle was in an accelerated state last time, and if the previous time was also in an accelerated state, the process proceeds to Step 311), and if the previous time was not an accelerated state, the process proceeds to step (307).

ステップ(307)では、加速状態と判定した第5図(
c)の期間T2.T3およびT4において、非同期燃料
噴射後所定時間が経過したか否かを非同期禁止タイマに
て判定する。第5図(e)の期間T3で示すように非同
期禁止タイマが0でなければステップ(311)に進む
、第5図(c)の期間T2およびT4て示すように非同
期禁止タイマがOであればステップ(308)に進み、
非同期噴射のインジェクタ駆動パルス幅PW21 、P
W22(第5図(b)のパルスP3およびP5参照)を
演算し、ステップ(309)でインジェクタ(4)を駆
動し、燃料をエンジン(1)に供給する。インジェクタ
(4)の駆動後ステップ(310)で非同期禁止時間を
非同期禁止タイマにセットし、ステップ(311)で加
速状態フラグをセットする。その後ステップ(312)
で非同期禁止タイマが0か否かを判定し、0であればそ
のまま処理を終了し、Oでなければステップ(313)
で非同期禁止タイマを減算してから終了する。
In step (307), the acceleration state is determined as shown in FIG.
c) period T2. At T3 and T4, the asynchronous prohibition timer determines whether a predetermined time has elapsed after the asynchronous fuel injection. If the asynchronous prohibition timer is not 0, as shown in period T3 in FIG. 5(e), the process proceeds to step (311); if the asynchronous prohibition timer is O, as shown in periods T2 and T4 in FIG. 5(c), Then proceed to step (308).
Injector drive pulse width PW21 of asynchronous injection, P
W22 (see pulses P3 and P5 in FIG. 5(b)) is calculated, and in step (309) the injector (4) is driven to supply fuel to the engine (1). After driving the injector (4), an asynchronous prohibition time is set in the asynchronous prohibition timer in step (310), and an acceleration state flag is set in step (311). Then step (312)
Determine whether the asynchronous prohibition timer is 0 or not, and if it is 0, end the process as is, and if it is not 0, step (313)
decrements the asynchronous prohibition timer with , and then exits.

また、ステップ(312) 、 (313)の演算を第
4図に示すクランク角センサによる所定クランク角割込
の中で行えば、非同期燃料噴射後所定の行程の開弁同期
燃料噴射を行わないシステムとなる。
Furthermore, if the calculations in steps (312) and (313) are performed during a predetermined crank angle interruption by the crank angle sensor shown in FIG. Become.

なお、第5図(b)でPi 、P2.P4.P6は同期
噴射パルス、P3.P5は非同期噴射パルスであり、第
5図(e)で、(11) 〜(14)は圧力センサA/
D変換平均値算出タイミング、tl 、 t2〜を鴫+
 、 tJz 、 tm3〜tnは一定時間割込処理タ
イミングである。
In addition, in FIG. 5(b), Pi, P2. P4. P6 is a synchronous injection pulse, P3. P5 is an asynchronous injection pulse, and in FIG. 5(e), (11) to (14) are pressure sensors A/
D conversion average value calculation timing, tl, t2 ~ is +
, tJz, and tm3 to tn are interrupt processing timings for a certain period of time.

第4図のステップ(401)でクランク角センサ信号の
周期Tを計測し、第2図のステップ(201)で回転数
Neの演算に使用する。ステップ(402)では、今回
の一定クランク角割込処理が燃料噴射タイミングかどう
かを判別し、今回が噴射タイミングでなければ処理を終
了し、今回が噴射タイミングであれば次のステップ(4
03)に進む、ステップ(403)では、第3図のステ
ップ(302)で求めた圧力センサA/D変換値の積算
値pb、u、をステップ(303)で求めた圧カセンサ
A/D変換回数Nで割ることにより、圧カセンサA/D
変換平均値pb、、、。を算出する。今回の平均値演算
が終了したので、ステップ(404)でA/D変換積算
値pb、u、をクリアし、ステップ(405)で圧力セ
ンサA/D変換値積算回数カウンタの値Nをクリアする
。ステップ(406)では、第3図のステップ(301
)で求めた圧力センサA/D変換値pb、と、第2図の
ステップ(202)で求めた体積効率η9とから、同期
噴射インジェクタ駆動パルス幅PH1(第5図(b)参
照)を演算し、ステップ(407)でインジェクタ(4
)を駆動し、燃料をエンジン(1)に供給し、処理を終
了する。
The cycle T of the crank angle sensor signal is measured in step (401) in FIG. 4, and used to calculate the rotational speed Ne in step (201) in FIG. In step (402), it is determined whether the current constant crank angle interrupt processing is the fuel injection timing, and if this is not the injection timing, the processing is terminated, and if this is the injection timing, the next step (402) is performed.
In step (403), the integrated values pb, u of the pressure sensor A/D conversion values obtained in step (302) in FIG. By dividing by the number of times N, the pressure sensor A/D
Converted average value pb, . Calculate. Since the current average value calculation has been completed, the A/D conversion integrated values pb, u are cleared in step (404), and the value N of the pressure sensor A/D converted value integrated number counter is cleared in step (405). . In step (406), step (301
Calculate the synchronous injection injector drive pulse width PH1 (see Figure 5(b)) from the pressure sensor A/D conversion value pb determined in ) and the volumetric efficiency η9 determined in step (202) in Figure 2. Then, in step (407), the injector (4
) is driven, fuel is supplied to the engine (1), and the process is completed.

なお、上記実施例では、加速判定における所定値α(第
3図のステップ(304)参照)を一定値としたが、第
6図の所定値α1.α2で示すように吸気管圧力pbが
低い場合には所定値を小さく、吸気管圧力pbが高い場
合には所定値を大きくすれば、吸気管圧力のリップルが
小さい低圧力側でより速い加速検出が行なえ、吸気管圧
力のリップルの大きい高圧力側で加速誤検出の防止を行
なうことができる。第6図で、Pblは所定値切換判定
吸気管圧力である。さらに、第3図のステップ(304
)の所定値αを第7図のようにα−f (Pb)とすれ
ば、低圧力から高圧力まで吸気管圧力のリップルに応じ
た値を設定できるので、全運転域でより速く加速検出が
できる。
In the above embodiment, the predetermined value α (see step (304) in FIG. 3) in the acceleration determination was set to a constant value, but the predetermined value α1 in FIG. As shown by α2, if the predetermined value is made smaller when the intake pipe pressure pb is low, and if the predetermined value is made larger when the intake pipe pressure pb is high, acceleration can be detected faster on the low pressure side where the intake pipe pressure ripple is small. This makes it possible to prevent erroneous detection of acceleration on the high pressure side where the ripple of the intake pipe pressure is large. In FIG. 6, Pbl is the predetermined value switching determination intake pipe pressure. Furthermore, step (304) in FIG.
) as α-f (Pb) as shown in Figure 7, it is possible to set the value according to the ripple of the intake pipe pressure from low pressure to high pressure, which enables faster acceleration detection in the entire operating range. I can do it.

[発明の効果] 以上説明したようにこの発明は、スロットル開度センサ
を用いずに吸気管圧力センサのみを用いて加速状態を検
出し、加速状態を検出して非同期噴射をした後に、所定
時間(または所定の行程期間)の非同期噴射禁止時間を
設け、その間に加速状態を検出しても非同期噴射を行わ
ないようにしたので、加速時間の長い緩加速などあらゆ
る加速状態において最適な量の非同期噴射を行うコスト
パフォーマンスの優れたエンジンの燃料噴射装置を得る
ことができるという効果を奏する。
[Effects of the Invention] As explained above, the present invention detects the acceleration state using only the intake pipe pressure sensor without using the throttle opening sensor, and after detecting the acceleration state and performing asynchronous injection, (or a predetermined stroke period), and asynchronous injection is not performed even if an acceleration state is detected during that time, so the optimal amount of asynchronous injection can be achieved in any acceleration state, such as slow acceleration with a long acceleration time. It is possible to obtain a fuel injection device for an engine that performs injection and has excellent cost performance.

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

第1図はこの発明によるエンジンの燃料噴射装置の一実
施例を示す構成図、第2図〜第4図は第1図の装置の動
作を説明するためのフローチャj・、第5図は第1図の
装置の動作を説明するためのタイムチャート、第6図お
よび第7図は所定値設定の他の例を示す特性図である。 (1)   ・エンジン、(2)・・吸気管、(3)圧
力センサ、(4)・・インジェクタ、(5)・・クラン
ク角センサ、(6)・・制御部、(61)・・^/Dコ
ンバータ、(62)・・入力回路、(63)・・マイク
ロプロセッサ、(64) 、 、 ROM、(65)・
 RAM、(66)・・出力回路。 代理人     曾  我  道  照第1図 箒3叉 形20 第6図 o、pづ^y〒凱りじり(Pb)
FIG. 1 is a block diagram showing an embodiment of an engine fuel injection device according to the present invention, FIGS. 2 to 4 are flowcharts for explaining the operation of the device shown in FIG. 1, and FIG. A time chart for explaining the operation of the device shown in FIG. 1, and FIGS. 6 and 7 are characteristic diagrams showing other examples of predetermined value setting. (1) Engine, (2) Intake pipe, (3) Pressure sensor, (4) Injector, (5) Crank angle sensor, (6) Control unit, (61)...^ /D converter, (62)...input circuit, (63)...microprocessor, (64), , ROM, (65)...
RAM, (66)...output circuit. Agent Zeng Wa Do Teru Figure 1 Broom three prongs 20 Figure 6 o, pzu^y〒Kairijiri (Pb)

Claims (1)

【特許請求の範囲】 エンジンの吸気管圧力を検出して燃料噴射量を演算し、
所定クランク角毎または所定点火毎に発生する信号に同
期して燃料噴射を行なうエンジンの燃料噴射装置におい
て、 エンジンの吸気管内圧力を検出する圧力検出手段と、 この圧力検出手段の出力信号を平均化して圧力平均値を
算出し、前記圧力検出手段の出力信号値が前記算出した
圧力平均値から所定値以上の偏差を生じた時にエンジン
が加速状態であると判定し、前記加速状態と判定した時
に非同期に燃料を噴射する第1の制御手段と、 一度非同期燃料を噴射した後に、所定時間またはエンジ
ンの所定行程の間非同期燃料を噴射することを禁止する
第2の制御手段と を備えたことを特徴とするエンジンの燃料噴射装置。
[Claims] Detecting the intake pipe pressure of the engine and calculating the fuel injection amount,
A fuel injection device for an engine that performs fuel injection in synchronization with a signal generated at every predetermined crank angle or every predetermined ignition includes a pressure detection means for detecting the pressure inside the intake pipe of the engine, and an output signal of the pressure detection means that is averaged. calculates a pressure average value, and determines that the engine is in an acceleration state when the output signal value of the pressure detection means deviates from the calculated pressure average value by a predetermined value or more; and when it is determined that the engine is in the acceleration state. The first control means injects fuel asynchronously, and the second control means prohibits injecting the asynchronous fuel for a predetermined time or for a predetermined stroke of the engine once the asynchronous fuel is injected. Features the engine's fuel injection system.
JP18414990A 1990-07-13 1990-07-13 Fuel injector of engine Pending JPH0472436A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18414990A JPH0472436A (en) 1990-07-13 1990-07-13 Fuel injector of engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18414990A JPH0472436A (en) 1990-07-13 1990-07-13 Fuel injector of engine

Publications (1)

Publication Number Publication Date
JPH0472436A true JPH0472436A (en) 1992-03-06

Family

ID=16148227

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18414990A Pending JPH0472436A (en) 1990-07-13 1990-07-13 Fuel injector of engine

Country Status (1)

Country Link
JP (1) JPH0472436A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003038263A1 (en) * 2001-10-29 2003-05-08 Yamaha Hatsudoki Kabushiki Kaisha Engine control device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62189335A (en) * 1986-02-13 1987-08-19 Toyota Motor Corp Fuel injection method for internal combustion engine
JPS6473145A (en) * 1987-09-11 1989-03-17 Daihatsu Motor Co Ltd Fuel contorl method for electronic control type engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62189335A (en) * 1986-02-13 1987-08-19 Toyota Motor Corp Fuel injection method for internal combustion engine
JPS6473145A (en) * 1987-09-11 1989-03-17 Daihatsu Motor Co Ltd Fuel contorl method for electronic control type engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003038263A1 (en) * 2001-10-29 2003-05-08 Yamaha Hatsudoki Kabushiki Kaisha Engine control device
US6934623B2 (en) 2001-10-29 2005-08-23 Yamaha Hatsudoki Kabushiki Kaisha Engine control device
CN1324230C (en) * 2001-10-29 2007-07-04 雅马哈发动机株式会社 Engine control device

Similar Documents

Publication Publication Date Title
JPH1122512A (en) Control device for direct injection spark ignition internal combustion engine
EP0924420B1 (en) Torque controller for internal combustion engine
JPH0586953A (en) Crank angle and cylinder deciding method for internal combustion engine
US4977876A (en) Fuel injection control system for internal combustion engine with fuel cut-off control at high engine speed range suppressive of recovery shock upon fuels resumption
US4875452A (en) Fuel control apparatus for an internal combustion engine
KR0148387B1 (en) Engine control method and apparatus
JP2754513B2 (en) Engine fuel injection device
JPH0472436A (en) Fuel injector of engine
US5590633A (en) Fuel injection control system for engine
JP2634278B2 (en) Internal combustion engine fuel injection device
US4987889A (en) Method for controlling fuel at an acceleration time of an electronically-controlled fuel engine
JP2696444B2 (en) Fuel supply control device for internal combustion engine
JPH0325622B2 (en)
JP4006743B2 (en) Fuel injection control device for internal combustion engine
JP2518669B2 (en) Electronically controlled fuel injection device for internal combustion engine
JPH09133040A (en) Combustion control device classified by cylinder for engine
JP3726432B2 (en) Air quantity detection device for internal combustion engine
JPH0734193Y2 (en) Electronically controlled fuel injection device for internal combustion engine
JP2561248B2 (en) Fuel cut control device for internal combustion engine
JP3564923B2 (en) Engine air-fuel ratio control device
JP2523524Y2 (en) Engine fuel control device
JPH0263096B2 (en)
JPS61223243A (en) Surging controller for internal-combustion engine
JPH0727002A (en) Fuel controller of engine
JPH0598946A (en) Device for diagnosing deterioration of catalyst converter device of internal combusiton engine