JPH0733806B2 - Multi-cylinder engine controller - Google Patents

Multi-cylinder engine controller

Info

Publication number
JPH0733806B2
JPH0733806B2 JP59044400A JP4440084A JPH0733806B2 JP H0733806 B2 JPH0733806 B2 JP H0733806B2 JP 59044400 A JP59044400 A JP 59044400A JP 4440084 A JP4440084 A JP 4440084A JP H0733806 B2 JPH0733806 B2 JP H0733806B2
Authority
JP
Japan
Prior art keywords
cylinder
angular velocity
maximum angular
combustion state
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 - Lifetime
Application number
JP59044400A
Other languages
Japanese (ja)
Other versions
JPS60187739A (en
Inventor
昇 橋本
英樹 田中
操 藤本
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.)
Mazda Motor Corp
Original Assignee
Mazda 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 Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP59044400A priority Critical patent/JPH0733806B2/en
Publication of JPS60187739A publication Critical patent/JPS60187739A/en
Publication of JPH0733806B2 publication Critical patent/JPH0733806B2/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
    • F02D41/008Controlling each cylinder individually
    • F02D41/0085Balancing of cylinder outputs, e.g. speed, torque or air-fuel ratio
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P5/00Advancing or retarding ignition; Control therefor
    • F02P5/04Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
    • F02P5/145Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using electrical means
    • F02P5/1455Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using electrical means by using a second control of the closed loop type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D35/00Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
    • F02D35/02Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
    • F02D35/023Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions by determining the cylinder pressure
    • 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
    • F02D41/14Introducing closed-loop corrections
    • F02D41/1497With detection of the mechanical response of the engine
    • F02D41/1498With detection of the mechanical response of the engine measuring engine roughness
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

Landscapes

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

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、多気筒エンジンにおいて各気筒間の燃焼状態
のバラツキいわゆるラフネスをなくすように制御するラ
フネス制御装置の改良に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement in a roughness control device that controls a multi-cylinder engine so as to eliminate variations in the combustion state among the cylinders, so-called roughness.

(従来の技術) 従来より、多気筒エンジンにおいて、エンジンの振動の
原因となる各気筒相互間に生じる燃焼状態のバラツキを
なくすべくラフネス制御するものとして、例えば特公昭
56−33569号公報に示されるように、各気筒の燃焼状態
をエンジンの回転角速度や燃焼圧により検出し、それら
に基づいて角気筒への空燃比等を夫々一律に制御するこ
とにより、各気筒の燃焼状態のバラツキ(ラフネス)を
解消するようにしたものが知られている。
(Prior Art) Conventionally, in a multi-cylinder engine, for example, as a roughness control for eliminating the variation in the combustion state between the cylinders that causes the vibration of the engine, for example, Japanese Patent Publication No.
As shown in Japanese Patent Laid-Open No. 56-33569, the combustion state of each cylinder is detected by the rotational angular velocity and combustion pressure of the engine, and the air-fuel ratio and the like for each of the cylinders are uniformly controlled based on the detected combustion state. It is known to eliminate the variation (roughness) in the combustion state of.

(発明が解決しようとする課題) ところが、上記従来のラフネス制御装置では、各気筒の
燃焼状態の検出によるラフネスの発生時には全気筒の空
燃比等を一律に調整して、各気筒相互間に生じるラフネ
スを制御するものであるため、燃焼状態の良好な気筒に
他の気筒を揃える場合には問題はないが、燃焼状態の不
良な気筒に他の気筒を揃える場合には、それまで良好に
運転していた気筒迄が燃焼状態の不良な気筒に揃えられ
ることになり、かえってその気筒の燃焼状態を悪化させ
る場合がある。
(Problems to be Solved by the Invention) However, in the above-described conventional roughness control device, when the roughness occurs due to the detection of the combustion state of each cylinder, the air-fuel ratios of all the cylinders are uniformly adjusted to occur between the cylinders. Since it controls the roughness, there is no problem when aligning another cylinder with a cylinder in good combustion condition, but when aligning another cylinder with a cylinder in poor combustion condition, it runs well until then. The cylinders that were already in operation will be aligned with the cylinders in a poor combustion state, which may rather deteriorate the combustion state in that cylinder.

一方、特公昭56−50114号公報及び特開昭57−129260号
公報等には、各気筒毎にノッキングレベルを判定して、
各気筒毎に点火時期を最適に制御することが提案されて
いる。しかし、この場合には、各気筒個別のノッキング
抑制には有効であるが、各気筒の燃焼状態が一律に揃わ
ず、却ってラフネスの要因となることがある。
On the other hand, Japanese Examined Patent Publication No. 56-50114 and Japanese Unexamined Patent Publication No. 57-129260 disclose a knocking level for each cylinder,
It has been proposed to optimally control the ignition timing for each cylinder. However, in this case, although it is effective in suppressing knocking of each cylinder individually, the combustion state of each cylinder is not uniformly arranged, which may rather cause roughness.

本発明は、上記の点に鑑みてなされたものであり、その
目的とするところは、多気筒エンジンにおいて、各気筒
の回転角速度を検出し、その最大角速度が各気筒でその
ときのエンジン回転数と吸気負圧で決まる最適な値にな
るように各気筒毎に制御を行うことにより、各気筒相互
間に生じる燃焼状態のバラツキがつまりラフネスをなく
すとともに、各気筒の燃焼状態を最良のものにして効率
のよいラフネス制御を行うことである。
The present invention has been made in view of the above points, and an object thereof is to detect the rotational angular velocity of each cylinder in a multi-cylinder engine and to determine the maximum angular velocity of each cylinder in each cylinder. By controlling each cylinder so that it becomes an optimum value determined by the intake negative pressure, variation in the combustion state that occurs between the cylinders is eliminated, and roughness is eliminated, and the combustion state of each cylinder is optimized. And efficient roughness control.

(課題を解決するための手段) 上記目的を達成するために、本発明の解決手段は、第1
図に示すように、各気筒の回転角速度を検出する角速度
検出手段と、各気筒の燃焼状態を支配する各種制御手段
と、上記角速度検出手段の出力を受け、各気筒の最大角
速度をそのときの各気筒についてのエンジン回転数と吸
気負圧によって決まる最適な基準最大角速度の値に一致
させるように上記各種制御手段を調整する燃焼調整手段
とを備えたものとする。
(Means for Solving the Problems) In order to achieve the above object, the solving means of the present invention is
As shown in the figure, the angular velocity detecting means for detecting the rotational angular velocity of each cylinder, various control means for controlling the combustion state of each cylinder, and the output of the angular velocity detecting means, and the maximum angular velocity of each cylinder at that time Combustion adjusting means is provided for adjusting the various control means so as to match the optimum reference maximum angular velocity value determined by the engine speed and the intake negative pressure for each cylinder.

(作用) このことにより、各気筒の最大角速度が、各気筒毎の最
適燃焼状態を示す基準最大角速度値と比較されて、該基
準最大角速度値に一致するように燃焼噴射弁からの燃料
噴射量や点火時期等、燃焼状態を支配する各種要素が調
整される。
(Operation) As a result, the maximum angular velocity of each cylinder is compared with the reference maximum angular velocity value indicating the optimum combustion state for each cylinder, and the fuel injection amount from the combustion injector is adjusted so as to match the reference maximum angular velocity value. Various factors that govern the combustion state, such as ignition timing and ignition timing, are adjusted.

(発明の効果) したがって、本発明に係る多気筒エンジンの制御装置に
よると、各気筒の回転角速度を検出して、各気筒の最大
角速度が各気筒毎の最適燃焼状態を示す基準最大各速度
値になるように燃焼状態を支配する各種要素を調整する
ようにしたものであるので、全気筒の燃焼状態を良好に
保持しながら、効率のよいラフネス制御を行うことがで
きるものである。
(Effects of the Invention) Therefore, according to the control device for a multi-cylinder engine according to the present invention, the reference maximum speed values indicating the optimum combustion state of each cylinder are detected by detecting the rotation angular speed of each cylinder. Since various elements that govern the combustion state are adjusted so that the combustion state of all cylinders is adjusted, efficient roughness control can be performed while maintaining good combustion states of all cylinders.

(実施例) 以下、本発明の実施例を図面に基づいて詳細に説明す
る。
(Example) Hereinafter, the Example of this invention is described in detail based on drawing.

第2図は本発明の実施例に係る全体概略構成を示すもの
である。同図において、1は第1〜第4の気筒1a〜1dを
有する4気筒エンジン、2はエンジン1に吸気を供給す
るための吸気通路である。該吸気通路2の下流側は第1
〜第4分岐通路2a〜2dに分岐されていて、それぞれ対応
する気筒1a〜1dに連通されている。該各分岐通路2a〜2d
には夫々、各気筒1a〜1dの燃焼状態を支配する制御手段
としての燃料噴射弁3a〜3dが配設されている。また、上
記第1〜第4分岐通路2a〜2dの集合部上流の吸気通路2
には、吸入空気量を制御するスロットル弁4が設けられ
ているとともに、該スロットル弁4上流の吸気通路2に
は吸入空気量を検出するエアフローメータ5が設けられ
ている。また、6は各気筒1a〜1dの点火プラグ(図示せ
ず)を作動制御するイグナイタである。
FIG. 2 shows an overall schematic configuration according to an embodiment of the present invention. In the figure, 1 is a four-cylinder engine having first to fourth cylinders 1a to 1d, and 2 is an intake passage for supplying intake air to the engine 1. The downstream side of the intake passage 2 is the first
~ It branches into the 4th branch passages 2a-2d, and is open for free passage to the corresponding cylinders 1a-1d, respectively. Each of the branch passages 2a to 2d
Fuel injection valves 3a to 3d as control means for controlling the combustion state of the cylinders 1a to 1d are arranged in the respective cylinders. Further, the intake passage 2 upstream of the collecting portion of the first to fourth branch passages 2a to 2d.
Is provided with a throttle valve 4 for controlling the intake air amount, and an air flow meter 5 for detecting the intake air amount is provided in the intake passage 2 upstream of the throttle valve 4. An igniter 6 controls the operation of spark plugs (not shown) of the cylinders 1a to 1d.

また、上記エンジン1のクランク軸7の軸端には、クラ
ンク角検出用の円板8が一体に取り付けられ、該円板8
に対向して、円板8の回転角によりクランク角、エンジ
ン回転数およびその回転角速度を検出するクランク角セ
ンサ9が設けられている。該クランク角センサ9によ
り、各気筒1a〜1dの回転角速度を検出する角速度検出手
段を構成している。上記クランク角センサ9の出力信号
は、イグナイタ6の点火プラグへの点火パルス信号、エ
ンジンの冷却水温を検出する水温センサ10の出力信号お
よび吸気通路2のスロットル弁4下流の吸気負圧を検出
する負圧センサ11の出力信号と共に、マイクロコンピュ
ータよりなる制御回路12に入力されており、該制御回路
12により上記各燃料噴射弁3a〜3dがその燃料噴射量を調
整するように制御される。
Further, a disc 8 for detecting a crank angle is integrally attached to the shaft end of the crank shaft 7 of the engine 1.
A crank angle sensor 9 for detecting the crank angle, the engine rotation speed and the rotation angular velocity thereof by the rotation angle of the disc 8 is provided opposite to. The crank angle sensor 9 constitutes an angular velocity detecting means for detecting the rotational angular velocity of each cylinder 1a to 1d. The output signal of the crank angle sensor 9 detects the ignition pulse signal to the ignition plug of the igniter 6, the output signal of the water temperature sensor 10 that detects the cooling water temperature of the engine, and the intake negative pressure downstream of the throttle valve 4 in the intake passage 2. Along with the output signal of the negative pressure sensor 11, it is input to a control circuit 12 composed of a microcomputer.
The fuel injection valves 3a to 3d are controlled by 12 so as to adjust the fuel injection amount.

次に、上記制御回路12の作動について第3図〜第5図に
より説明するに、第3図はラフネスを制御するためのメ
インルーチンを示し、第4図および第5図はそのメイン
ルーチンの一部としてのサブルーチンを示す。第3図の
メインルーチンにおいて、スタート後、先ず、第1ステ
ップS1において、あるクランク角における点火パルス信
号を入力して、第2ステップS2でこの点火パルス信号時
期を予め求められた各気筒に対応する基準のパルス発生
時期と照合して気筒判別を行う。それにより、第3ステ
ップS3で上記判別した例えば第1気筒1aについてのエン
ジン回転数,吸気負圧および冷却水温の各信号を入力す
るとともに、第4ステップS4で第1気筒1aに対応する点
火パルス信号をトリガー回路を介してトリガー作用によ
り回転パルス信号として入力し、さらに第5ステップS5
でその入力した第1気筒1aに対応する回転パルス信号か
らその気筒に対応した角速度を計算し、その最大角速度
の値ωを求める。
Next, the operation of the control circuit 12 will be described with reference to FIGS. 3 to 5. FIG. 3 shows a main routine for controlling the roughness, and FIGS. 4 and 5 show one of the main routines. The subroutine as a part is shown. In the main routine of FIG. 3, after starting, first, in a first step S 1 , an ignition pulse signal at a certain crank angle is input, and in a second step S 2 , the ignition pulse signal timing is obtained in advance for each cylinder. Cylinder discrimination is performed by collating with the reference pulse generation timing corresponding to. Thereby, the third step S 3 in the engine rotational speed for the first cylinder 1a for example the above determination, inputs the respective signals of the intake negative pressure and the cooling water temperature, corresponding to the first cylinder 1a in the fourth step S 4 The ignition pulse signal is inputted as a rotation pulse signal by a trigger action through the trigger circuit, and further the fifth step S 5
Then, the angular velocity corresponding to the cylinder is calculated from the input rotation pulse signal corresponding to the first cylinder 1a, and the value ω of the maximum angular velocity is obtained.

次に、第6ステップS6で、上記の如く求めた最大角速度
ωが、予めエンジン回転数と吸気負圧によって実験的に
求められた最適な基準最大角速度ωよりも大きいか否
かを判別する。そして、最大角速度ωが基準最大角速度
ωより小さい場合、つまり第1気筒1aの最大角速度ω
が遅いNOの場合には、第7ステップS7つまり第1サブル
ーチンに進み、第4図に示すように燃料噴射弁3aの燃料
噴射量を増やして空燃比をリッチにしたり、あるいは点
火時期を進めたり、副次的には、EGR量を減らしたり、
スワールを強化したりすることにより、出力の向上を促
進させて第1気筒1aの最大角速度を、上記基準最大角速
度ωに一致させるようにする。一方、最大角速度ωが
基準最大角速度ωより大きい場合、つまり第1気筒1a
の最大角速度ωが速いYESの場合には、第8ステップS8
つまり第2サブルーチンに進み、第5図に示すように燃
料噴射弁3aの燃料噴射量を減らして空燃比をリーンにし
たり、あるいは点火時期を遅らせたりし、副次的には、
EGR量を増やしたり、スワールを弱めたりすることによ
り、出力の向上を抑制して第1気筒1aの最大角速度ωを
上記基準最大角速度ωに一致させるようにする。
Next, in a sixth step S 6 , it is determined whether or not the maximum angular velocity ω obtained as described above is larger than the optimum reference maximum angular velocity ω 0 which is experimentally obtained in advance by the engine speed and the intake negative pressure. To do. When the maximum angular velocity ω is smaller than the reference maximum angular velocity ω 0 , that is, the maximum angular velocity ω of the first cylinder 1a
If the slow NO, the process proceeds to a seventh step S 7, that the first sub-routine, or the air-fuel ratio to rich by increasing the fuel injection amount of the fuel injection valve 3a as shown in FIG. 4, or advances the ignition timing Or, secondarily, reduce the EGR amount,
By enhancing the swirl, the output is promoted so that the maximum angular velocity of the first cylinder 1a matches the reference maximum angular velocity ω 0 . On the other hand, when the maximum angular velocity ω is larger than the reference maximum angular velocity ω 0 , that is, the first cylinder 1a
If the maximum angular velocity ω of is YES, the eighth step S 8
That is, the routine proceeds to the second subroutine, and as shown in FIG. 5, the fuel injection amount of the fuel injection valve 3a is reduced to make the air-fuel ratio lean, or the ignition timing is delayed, and secondarily,
By increasing the EGR amount and weakening the swirl, the output improvement is suppressed and the maximum angular velocity ω of the first cylinder 1a is made to match the reference maximum angular velocity ω 0 .

その後、第9ステップS9で、今度は第3気筒1cについて
のエンジン回転数,吸気負圧および冷却水温の各信号を
入力し、第10ステップS10で点火パルス信号をトリガー
回路を介してトリガー作用により回転パルス信号として
入力して、上記第1気筒1aの場合と同様に第11ステップ
S11で上記点火パルス信号に対応した第3気筒1cの回転
角速度を計算してその最大角速度ωの値を求める。しか
る後、第12ステップS12で上記最大角速度ωと上記エン
ジン回転数と吸気負圧によって求められた基準最大角速
度ωとを比較判別し、最大角速度ωが基準最大角速度
ωよりも小さいNOの場合には、第13ステップS13つま
り第1サブルーチンに進み、最大角速度ωが基準最大角
速度ωよりも大きいYESの場合には、第14ステップS14
つまり第2サブルーチンに進んで、それぞれ燃焼状態を
支配する燃料噴射弁3c等の各種制御手段を調整し、第3
気筒1cの最大角速度ωを上記基準最大角速度ωに一致
させるようにする。
Then, in the ninth step S 9, this time the engine speed for the third cylinder 1c, enter the respective signals of the intake negative pressure and the cooling water temperature, via the trigger circuit of the ignition pulse signal in the tenth step S 10 triggers By inputting as a rotation pulse signal by the action, in the 11th step as in the case of the first cylinder 1a.
The rotation angular velocity of the third cylinder 1c corresponding to the ignition pulse signal calculated in S 11 and determines the value of the maximum angular velocity omega. Thereafter, 12th step and the reference maximum angular velocity omega 0 determined by the maximum angular velocity omega and the engine speed and the intake negative pressure compared to determine at S 12, the maximum angular velocity omega is smaller than the reference maximum angular velocity omega 0 NO In the case of, the process proceeds to the 13th step S 13, that is, the first subroutine, and in the case of YES where the maximum angular velocity ω is larger than the reference maximum angular velocity ω 0 , the 14th step S 14
In other words, the procedure proceeds to the second subroutine to adjust various control means such as the fuel injection valve 3c that respectively governs the combustion state,
The maximum angular velocity ω of the cylinder 1c is made to match the reference maximum angular velocity ω 0 .

以下、上記と同様の方法によって、順次、第4気筒1d,
第2気筒1bについて、第3ステップS3ないし第8ステッ
プS8と同様の処理を行い、しかる後、第3ステップに戻
って一連のラフネス制御を行う。よって、このような制
御により、各気筒1a〜1dの最大角速度ωが各気筒1a〜1d
についてのエンジン回転数と吸気負圧によって決まる最
適な基準最大角速度ωに一致させるように燃料噴射弁
3a〜3d等の各種制御手段を調整するようにした燃焼調整
手段を構成している。
Thereafter, in the same manner as above, the fourth cylinder 1d,
The second cylinder 1b, was treated in the same manner as the third step S 3 through the eighth step S 8, and thereafter, a series of roughness control returns to the third step. Therefore, by such control, the maximum angular velocity ω of each cylinder 1a to 1d is changed to each cylinder 1a to 1d.
Of the fuel injection valve to match the optimum reference maximum angular velocity ω 0 determined by the engine speed and the intake negative pressure.
Combustion adjusting means is arranged to adjust various control means such as 3a to 3d.

したがって、上記実施例によると、各気筒1a〜1dの最大
角速度ωが各気筒1a〜1dについてエンジン回転数と吸気
負圧によって実験的に求められた最適な基準最大角速度
ωの値になるように各気筒1a〜1d毎に燃料噴射弁3a〜
3d等の各種制御手段の調整を行うものであるので、従来
の全気筒を一律に制御する場合の如くそれまで良好であ
った気筒の運転状態が悪化するようなことがなく、全気
筒1a〜1dの良好な燃焼状態を確保しながら効率のよいラ
フネス制御を行うことができる。
Therefore, according to the above-described embodiment, the maximum angular velocity ω of each cylinder 1a to 1d becomes the value of the optimum reference maximum angular velocity ω 0 experimentally determined by the engine speed and the intake negative pressure for each cylinder 1a to 1d. Fuel injection valve 3a for each cylinder 1a-1d
Since it adjusts various control means such as 3d, it does not deteriorate the operating condition of the cylinder which was good until then as in the case of uniformly controlling all the conventional cylinders. It is possible to perform efficient roughness control while ensuring a good combustion state of 1d.

尚、本発明は上記実施例の如き4気筒エンジンに限らず
その多の多気筒エンジンに対しても適用できるのは勿論
である。
Of course, the present invention can be applied not only to the four-cylinder engine as in the above-described embodiment but also to many multi-cylinder engines.

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

第1図は本発明の構成を示すブロック図である。第2〜
第5図は本発明の一実施例を示し、第2図は全体概略構
成図、第3図は制御回路のメインルーチンを示すフロー
チャート図、第4図および第5図はそれぞれ制御回路の
第1および第2サブルーチンを示すフローチャート図で
ある。 1……エンジン、1a〜1d……第1〜第4気筒、3a〜3d…
…燃料噴射弁、6……イグナイタ、9……クランク角セ
ンサ、10……水温センサ、11……負圧センサ、12……制
御回路。
FIG. 1 is a block diagram showing the configuration of the present invention. 2nd
FIG. 5 shows an embodiment of the present invention, FIG. 2 is an overall schematic configuration diagram, FIG. 3 is a flow chart diagram showing a main routine of a control circuit, and FIGS. 4 and 5 are respectively first control circuit. It is a flowchart figure which shows and a 2nd subroutine. 1 ... Engine, 1a-1d ... 1st-4th cylinder, 3a-3d ...
... Fuel injection valve, 6 ... Igniter, 9 ... Crank angle sensor, 10 ... Water temperature sensor, 11 ... Negative pressure sensor, 12 ... Control circuit.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】各気筒の回転角速度を検出する角速度検出
手段と、各気筒の燃焼状態を支配する各種制御手段と、
上記角速度検出手段の出力を受け、各気筒の最大角速度
をそのときの各気筒についてのエンジン回転数と吸気負
圧によって決まる最適な基準最大角速度の値に一致させ
るように上記各種制御手段を調整する燃焼調整手段とを
備えたことを特徴とする多気筒エンジンの制御装置。
1. An angular velocity detecting means for detecting a rotational angular velocity of each cylinder, and various control means for controlling a combustion state of each cylinder,
Receiving the output of the angular velocity detection means, the various control means are adjusted so that the maximum angular velocity of each cylinder matches the optimum reference maximum angular velocity value determined by the engine speed and the intake negative pressure for each cylinder at that time. A control device for a multi-cylinder engine, comprising: a combustion adjusting means.
JP59044400A 1984-03-07 1984-03-07 Multi-cylinder engine controller Expired - Lifetime JPH0733806B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59044400A JPH0733806B2 (en) 1984-03-07 1984-03-07 Multi-cylinder engine controller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59044400A JPH0733806B2 (en) 1984-03-07 1984-03-07 Multi-cylinder engine controller

Publications (2)

Publication Number Publication Date
JPS60187739A JPS60187739A (en) 1985-09-25
JPH0733806B2 true JPH0733806B2 (en) 1995-04-12

Family

ID=12690457

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59044400A Expired - Lifetime JPH0733806B2 (en) 1984-03-07 1984-03-07 Multi-cylinder engine controller

Country Status (1)

Country Link
JP (1) JPH0733806B2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62132252U (en) * 1986-02-17 1987-08-20
DE3923757A1 (en) * 1988-07-20 1990-01-25 Mitsubishi Electric Corp FUEL REGULATOR FOR INTERNAL COMBUSTION ENGINES
JP2835672B2 (en) * 1993-01-28 1998-12-14 株式会社ユニシアジェックス Surge and torque detector for internal combustion engine
DE19741965C1 (en) * 1997-09-23 1999-01-21 Siemens Ag Procedure for smooth running control

Also Published As

Publication number Publication date
JPS60187739A (en) 1985-09-25

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