JPS59206630A - Method of regulating asynchronous fuel injection in acceleration of electronically controlled fuel injection engine - Google Patents

Method of regulating asynchronous fuel injection in acceleration of electronically controlled fuel injection engine

Info

Publication number
JPS59206630A
JPS59206630A JP8129083A JP8129083A JPS59206630A JP S59206630 A JPS59206630 A JP S59206630A JP 8129083 A JP8129083 A JP 8129083A JP 8129083 A JP8129083 A JP 8129083A JP S59206630 A JPS59206630 A JP S59206630A
Authority
JP
Japan
Prior art keywords
engine
injection
asynchronous
fuel injection
acceleration
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.)
Granted
Application number
JP8129083A
Other languages
Japanese (ja)
Other versions
JPH0647957B2 (en
Inventor
Hiroshi Ito
博 伊藤
Tatsutake Nishimura
西村 達武
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 JP58081290A priority Critical patent/JPH0647957B2/en
Publication of JPS59206630A publication Critical patent/JPS59206630A/en
Publication of JPH0647957B2 publication Critical patent/JPH0647957B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

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

Landscapes

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

Abstract

PURPOSE:To prevent fuel from becoming overrich in the sharp acceleration of an engine in which asynchronous fuel injection is performed in the acceleration of the engine, by controlling the number of times of continual fuel injection depending on the rotational number of the engine. CONSTITUTION:In a step S1, it is judged from the change in the degree of opening of a throttle valve whether asynchronous fuel injection should be effected in the acceleration of an engine. If it is judged that the asynchronous fuel injection should be effected, the number of times of the asynchronous fuel injection to be continually effected depending on the rotational frequency of the engine is determined in a step S2. In a step S3, a series of asynchronous fuel injection within the determined number of times are effected. The fuel is thus prevented from becoming overrich in the sharp acceleration of the engine.

Description

【発明の詳細な説明】 4、発明は、電子制御燃料噴射式エンジンの加速時非同
期噴射制御方法に係り、特に、゛電子制御l焦:料噴用
装匝を備えた自動車用エンジンに用いるのに好適な、エ
ンジン回転と同期してだ期的に行われる同期噴射に加え
て、加速時は非同期噴射を行うようにした電子制御燃料
@例式1ンジンの加速時非同期噴用制御方法の改良に関
する。
[Detailed Description of the Invention] 4. The present invention relates to a method for controlling asynchronous injection during acceleration of an electronically controlled fuel injection engine, and in particular, to a method for controlling asynchronous injection during acceleration of an electronically controlled fuel injection engine, particularly for use in an automobile engine equipped with an electronically controlled fuel injection mount. Improvement of the control method for asynchronous injection during acceleration of an electronically controlled fuel@Example 1 engine, which performs asynchronous injection during acceleration in addition to synchronous injection that is performed periodically in synchronization with the engine rotation, which is suitable for Regarding.

自動車用エンジン等の内燃開開の燃焼至に所定空燃比の
混合気を供給づる方法の1″)に、電子制御燃料噴射装
置を用いるものがある。これは、エンジン内に燃料を噴
射づるためのインジエクタを、例えばエンジンの吸気ン
二ホルドに上ンシン気筒数個配設し、該インジエクタの
開弁時間をエンジンの運転状態、例えば吸気管圧力又は
吸入空気≠から検知される、rンジン負荷と土ンジン回
転速淑等に応じて制御づることにより、所定の空燃比の
混合気が」ンジン燃焼至に供給されるようにづるもので
ある。
One of the methods for supplying a mixture with a predetermined air-fuel ratio to the internal combustion engine of an automobile engine, etc. is to use an electronically controlled fuel injection device.This method is used to inject fuel into the engine. For example, an injector is installed in several upper cylinders in the intake manifold of the engine, and the valve opening time of the injector is adjusted to the engine load, which is detected from the engine operating condition, for example, the intake pipe pressure or the intake air≠. By controlling the air-fuel mixture according to the engine rotational speed, etc., a mixture having a predetermined air-fuel ratio is supplied to the engine combustion chamber.

このような電子制御燃料噴射装置を漏えた自動申開エン
ジンにおいては、通常、エンジン回転に同期して定期的
に行われる同期@射だ(プでは、加速時に燃料が不足し
、空燃比が一時的にオーバーリーンとなって、息付ぎや
もたつき等の加速不良が発生−4るため、例えばスロッ
トル弁開度の変化速度や、吸気面圧力又は吸入空気量の
変化速度が大であることから検知される加速時は、前記
同期噴射に加えt、エンジン回転角に拘わらず所定量の
燃料を噴射づる、所謂非同期噴射が行われている。
In automatic injection engines equipped with such electronically controlled fuel injection devices, synchronous injection is normally carried out periodically in synchronization with engine rotation (in automatic injection engines, fuel is insufficient during acceleration and the air-fuel ratio temporarily changes). This can be detected by, for example, the rate of change in the throttle valve opening, intake surface pressure, or intake air amount being large. During acceleration, so-called asynchronous injection is performed, in which a predetermined amount of fuel is injected regardless of the engine rotation angle, in addition to the synchronous injection.

しかしI−一から、加速時の要求噴射量は、エンジン運
転状態に応じC変化するため、例えばスロットル弁開瓜
の変化速度に一神に対応した非同期噴射量を設定づると
、エンジンの運転状態によっては、空燃比が必ずしも適
切とならない場合があり、例えば急加速時に空燃比がオ
ーバーリッチとなつ(、アフターバーン等を発生りる場
合があるといこのような問題点を解消するべく、各同期
噴射サイクル間に実行される非同期噴射の燃料量の合計
を、同期噴射量に応じて、例えば同期噴射量の所定倍で
制限することも考えられるが、同期噴射量に基づいて制
限値を決定づ“るのでは、非同期噴射処理が非常に′f
2雑になってしまうという問題がある。
However, from I-1, the required injection amount during acceleration changes C depending on the engine operating state. For example, if an asynchronous injection amount that corresponds to the rate of change in throttle valve opening is set, then the engine operating state Depending on the situation, the air-fuel ratio may not always be appropriate; for example, during sudden acceleration, the air-fuel ratio may become overrich (or afterburn may occur). It is conceivable to limit the total amount of fuel for asynchronous injections performed between injection cycles, depending on the synchronous injection amount, for example, by a predetermined multiple of the synchronous injection amount, but it is also possible to “In this case, the asynchronous injection process is very
There is a problem that it becomes cluttered.

本発明は、面記従来の問題点を解湘するべくなされたも
ので、加速時の非同期噴射1を、容易に、且つ確実に制
限づることかでき、従って、エンジン運転状態に応じた
適切な非同期噴射量を、容易に得ることができる電子制
御燃F3.@躬式エンジンの加速時非同期噴射制御方法
を提供りることを目的とづる。
The present invention has been made in order to solve the above-mentioned problems of the conventional art, and it is possible to easily and reliably limit the asynchronous injection 1 during acceleration. Electronically controlled fuel F3. can easily obtain asynchronous injection amount. The purpose of this paper is to provide a method for controlling asynchronous injection during acceleration of a @manufactured engine.

本発明は、エンジン回転と同期して定期的に行われる同
期噴射に加えて、加速時は非同期噴射を行うようにした
電子制御燃料噴射式二1ンジンの加速時非同期@剣制御
方法において、第1図にその要旨を示J如く、 エンジン運転状態が加速時の非IH]期噴しJを行うべ
き状態にのるか否かを判定づる手順と、算量!lJ噴口
J (r i’iうべき状態にある時は、少くとも[ン
ジン回転速磨に応じて、続けで行われる非M 1llJ
噴則回故の制限値を求める手順と、81′l記制限値の
範囲内で一連の算量1すj噴射を実行づる手順と、 を含むことにより、前記目的を達成したものである。
The present invention provides an asynchronous control method for an electronically controlled fuel injection type 21 engine during acceleration, in which in addition to synchronous injection performed periodically in synchronization with engine rotation, asynchronous injection is performed during acceleration. The gist is shown in Figure 1. The procedure and calculations for determining whether or not the engine operating state is in a state where non-IH injection during acceleration should be performed. lJ nozzle J
The above object has been achieved by including the following steps: a procedure for determining a limit value for jet irregularity; and a procedure for executing a series of calculated injections within the limit value described in 81'l.

又、前記非同期噴射回数の制限値を、エンジン1引転速
度、Lンジン温度、吸気室圧)〕又は吸入空気量等に応
じ(求めるようにしC1的確な制限値が14られるよう
にしたものである。
In addition, the limit value of the number of asynchronous injections can be determined according to the engine rotation speed, L engine temperature, intake chamber pressure) or the intake air amount, etc., so that an accurate limit value for C1 can be determined. be.

本発明にJ3い(は、少くともエンジン回転速度に応じ
で求められる、続けて行われる非同期噴射回数の制限値
の範囲内で、一連の非同期噴射を実行づるよづにし−(
、加速時の非同期噴射量を、エンジン運転状態に応じた
適切な量に制i1J’lるものである。
According to the present invention, a series of asynchronous injections are executed at least within the limit value of the number of consecutive asynchronous injections determined according to the engine speed.
, the amount of asynchronous injection during acceleration is controlled to an appropriate amount according to the engine operating state.

以下図面を参照しく、本発明に係る電子制御燃料噴射式
エンジンの加速時非同期@躬制御方法が採用されI;、
吸気巴圧力感知式の電子制御燃I3噴副装置を渦えた自
動車用エンジンの実施例を詳細に説明擾る。
Referring to the drawings below, the asynchronous control method during acceleration of an electronically controlled fuel injection engine according to the present invention is adopted.
An embodiment of an automobile engine equipped with an electronically controlled fuel I3 injection sub-device based on intake pressure sensing will be described in detail.

本実施例は、第2図に示す如く、 外部から吸入される吸入空気の湿aを検出づる]こめの
吸気温センサ12と、 スロットルボディ14に配設され、運転席に配設された
アクセルペダル〈図示省略〉と連動して開閉J”るよう
にされた、吸入空気の流量を制御Jるためのスロワ1〜
ル弁16と、 該スロットル弁16の開度を検出覆るためのスL1ット
ルセンサ18と、 吸気干渉を防止づるためのサージタンク20と、該サー
ジタンク20内の吸入空気の圧力を検出Jるための吸気
賃圧力センサ22と、 吸気ン二ホルド24に配設された、エンジン10の各気
筒の吸気ポートに向け°C1加圧燃料を間欠的に噴射ツ
るICめのインジェクタ26と、エンジン燃焼至1’ 
OA内に導入された混合気に社火りるための点火プラグ
28と、 排気ンーホルド30と、 Ljj火−」イル32ぐ発生された高圧の点火2送信号
をエンジン10の各気筒の点火プラグ28に配’tN4
るための、Jレジン10のクランク軸の回転と連動し℃
回転覆るデストリピユータllll34Aをイ1するデ
ス1〜リビ」−夕34と、 該デストリピユータ34に内蔵された、前記デストリピ
ユータ軸34Aの回転状態からエンジン゛10の回転状
態を検知づるためのクランク角度センサ36と、 エンジノ10のシリンダブロック10Bに配設された、
エンジン冷h1水堀を検知りるための水温セッサ38と
、 [)0記吸気芭・圧力センサ22出力から検知されるU
ンジン負荷や+iQ記クランク角1爽センサ36出力か
ら求められるエンジン回転速度等に応じて同期噴射時間
を計東し、エンジン(ロ)転と同期して定期的に前記イ
ンシュ1クタ26に開弁詩間伯号を出力しで同期鴫剣を
行うとともに、スロットル弁開度れる加速時は、スロッ
トル弁開度の変化速度に56じた琶の非同期@剣を行う
ための電子制御ユニツU−(以下ECIJと称づる)4
0と、から構成されでいる。
As shown in FIG. 2, this embodiment includes an intake temperature sensor 12 for detecting the humidity a of intake air taken in from the outside, an accelerator disposed in the throttle body 14, and an accelerator disposed in the driver's seat. Thrower 1 for controlling the flow rate of intake air, which opens and closes in conjunction with a pedal (not shown).
a throttle valve 16, a throttle sensor 18 for detecting the opening of the throttle valve 16, a surge tank 20 for preventing intake interference, and a surge tank 20 for detecting the pressure of intake air in the surge tank 20. an IC injector 26 that intermittently injects pressurized fuel at °C toward the intake port of each cylinder of the engine 10, which is disposed in the intake hold 24; To 1'
A spark plug 28 for igniting the air-fuel mixture introduced into the OA, an exhaust hold 30, and a high-pressure ignition signal 32 are sent to the spark plugs of each cylinder of the engine 10. Assigned to 28'tN4
It is linked to the rotation of the crankshaft of J Resin 10 in order to
A crank angle sensor 36 for detecting the rotational state of the engine 10 from the rotational state of the destroyer shaft 34A built in the destroyer 34; , arranged in the cylinder block 10B of the engine 10,
A water temperature sensor 38 for detecting the engine cold h1 water hole, and U detected from the output of the intake pressure sensor 22.
The synchronous injection time is calculated according to the engine load and the engine rotational speed determined from the +iQ crank angle 1 freshness sensor 36 output, and the valve is opened periodically in synchronization with the engine rotation. The electronic control unit U-( (hereinafter referred to as ECIJ)4
It is composed of 0 and .

^ら記ECIJ40は、第3図に詳細に示づ如く、各種
演算処理を行うための、例えばンイクロゾロセツサから
なる中央処理ユニット(以下CPUと称づる)40Δと
、 制御プログラムや各種データ等を記憶づるためのリード
オンリーメモリ(以下ROfVIと称゛づる)40Bと
、 前記CPU40Aにおける演算データ等を一時的に記憶
づるためのランダムアクセスメモリ(以下RAMと称づ
る)40Gと、 エンジン停止時にも補助電源から給電されて記憶を保持
できるバックアップRA M 4.01)と、前記吸気
温センサ12、吸気管圧力センサ22、水温センサ38
等から入力されるアナログ信号をデジタル信号に変換し
て順次取込むための、lルチノ°レクサ機能を崗えたア
ナログ−デジタル変換器(以ドΔ、/’ D Llンバ
ータと称づる)40Eと、前記スーツ1〜ルセンサ18
、クランク角度センサ36等から人ノJされるデジタル
信号を取込むとともに、Cl−’ U 40 Aの演算
結果に応じて、前記インジェクタ26等に制御信号を出
力するだめの、ハラノア機能をt6えIこ入出力小−1
〜(以下I7′0ボートと称づる)40Fと、 oIj記各構成機器間を接続して、データや命令を転送
−4るための−」モンバス40Gと、から構成され(い
る。
As shown in detail in Figure 3, the ECIJ 40 includes a central processing unit (hereinafter referred to as CPU) 40Δ consisting of, for example, a microprocessor for performing various arithmetic processing, control programs, various data, etc. A read-only memory (hereinafter referred to as ROofVI) 40B for storing data, a random access memory (hereinafter referred to as RAM) 40G for temporarily storing calculation data etc. in the CPU 40A, and Backup RAM 4.01) which is powered by an auxiliary power source and can hold memory, the intake temperature sensor 12, the intake pipe pressure sensor 22, and the water temperature sensor 38.
an analog-to-digital converter (hereinafter referred to as a Δ,/' D Ll inverter) 40E equipped with a lrutino° lexer function for converting analog signals input from, etc. into digital signals and sequentially capturing them; Said suits 1 to 18
, the Haranoa function that takes in digital signals from the crank angle sensor 36, etc., and outputs control signals to the injector 26, etc. according to the calculation result of Cl-' U 40 A is installed at t6. I input/output small -1
(hereinafter referred to as I7'0 boat) 40F, and a mon bus 40G for connecting each component and transferring data and instructions.

以下作用を説明−づる。The action will be explained below.

本実111!!例にa3りる加速時の非同期噴射は、第
4図に承づような所定時間毎の割込みルーチンに従つ−
(大行される。即ち、所定時間経過毎にステップ110
に進み、前記スロットルセンサ18の出力から求められ
るスロットル弁開度TAの所定時間毎の変化1△T A
が、所定値A以上であるか百731を判定覆る。判定結
果が正である場合、即ち、加速時の非同期噴射を行うべ
き状態にあると判断される時には、ステップ112に進
み、前回のスロットル弁開度変化量ΔTAが、既に所定
1i![A以上ぐあったか否かを判定づる。判定結果が
否である場合、即ら、今回初めて加速状態になったと判
断される時には、ステップ114に進み、例えば、第5
図に実線で示1ような、エンジン回転速度と制限回数の
関係、第6図に示づような、吸気管圧力と制限回数の関
係、及び、第7図に示すような、エンジン冷却水温と制
限回数の関係を含む、エンジン回転速度、吸気管圧力及
びエンジン冷却水温と制限回数の関係を表わした三次元
マツプを用いで、制限回数を求め、一連の非同期噴射回
数を計数しでいるカウンタに初期値として入れる。−)
5、前出ステップ112の判定結果が正である場合、即
ち、今回の処理が一連の非同期噴射処理にJハブる2回
目以障の処理であると判断される時には、ステップ11
6に進み、前記カウンタを1だりカウトダウンタる。次
いでステップ118に進み、前記カウンタの計数値が零
となったが否かを判定Jる。
Honji 111! ! For example, asynchronous injection during acceleration, such as a3, follows an interrupt routine at predetermined time intervals as shown in Figure 4.
(Step 110 is executed repeatedly. That is, step 110 is executed every predetermined period of time.)
Then, the change 1ΔTA in the throttle valve opening degree TA determined from the output of the throttle sensor 18 for each predetermined time is determined.
is greater than or equal to the predetermined value A or 10731 is determined. If the determination result is positive, that is, if it is determined that asynchronous injection during acceleration should be performed, the process proceeds to step 112, and the previous throttle valve opening change amount ΔTA has already reached the predetermined value 1i! [Determine whether or not there is an error greater than or equal to A.] If the determination result is negative, that is, if it is determined that the current acceleration state is reached for the first time, the process proceeds to step 114, and, for example, the fifth
The relationship between the engine rotation speed and the limit number of times as shown by the solid line 1 in the figure, the relationship between the intake pipe pressure and the limit number of times as shown in Figure 6, and the relationship between the engine cooling water temperature and the number of times as shown in Figure 7. Using a three-dimensional map showing the relationship between the engine rotation speed, intake pipe pressure, and engine cooling water temperature, including the relationship between the limit number of times, and the limit number of times, the limit number of times is calculated, and the number of times of asynchronous injection is counted. Enter it as the initial value. −)
5. If the determination result in step 112 is positive, that is, if it is determined that the current process is the second or subsequent J hub failure in a series of asynchronous injection processes, step 11
Proceed to step 6 and count down the counter by 1. Next, the process proceeds to step 118, where it is determined whether the count value of the counter has become zero.

前出ステップ114終了後、又は、6り出ステップ11
8の判定結果か否である場合、即ち、今回の処理7j1
初め(の非同期噴射処理ひあるか、又は、制御i回数内
の非同期1ljI則処理であると判断される時には、ス
Tツブ120に進み、非同期噴射実行フラグをレットづ
る。一方、前出ステップ118の判定結果が正である場
合、即ち、今回の一連の非同期噴射処理において、既に
、制限回数の非同期噴射を1丁つl、−と判面される時
には、ステップ122に進み、非同期噴射実行フラグを
リセットづる。
After the above step 114 or 6 exit step 11
8, that is, the current process 7j1
If there is an asynchronous injection process at the beginning (or if it is determined that it is an asynchronous 1ljI law process within the i number of controls), the process proceeds to the step 120 and sets the asynchronous injection execution flag. On the other hand, in step 118 If the determination result is positive, that is, in the current series of asynchronous injection processing, one asynchronous injection of the limited number of times has already been performed, the process proceeds to step 122, and the asynchronous injection execution flag is set. Reset.

ステップ120又は122柊了後、ステップ124に進
み、非同期噴射実行フラグがセットさ才′1(いか台か
を判γづる。判定結果が正である場合には、スTツブ1
26に進み、前記インジェクタ26に出力される開弁時
間信号をオンとして、非同期噴射を開始覆る。次いでス
テップ128に進み、例えば次式の関係を用いて、スロ
ットル弁開度の変化司△TAに応じた非同期噴射量ゴー
を求める。
After completing step 120 or 122, the process proceeds to step 124, where the asynchronous injection execution flag is set.
26, the valve opening time signal output to the injector 26 is turned on to start asynchronous injection. Next, the process proceeds to step 128, and the asynchronous injection amount go corresponding to the change in throttle valve opening ΔTA is determined using, for example, the following equation.

ここひ、B、Cは定数である。Here, B and C are constants.

次いでステップ130に進み、シンペアレジスタに、前
記非同期噴射量Tに対応覆る非Ih]則噴射終了時刻を
セラ1〜して、所定時間後にインジェクタ26の開弁時
間信号がオフとされるようにづる。
Next, the process proceeds to step 130, and the non-Ih law injection end time corresponding to the asynchronous injection amount T is entered in the compare register so that the valve opening time signal of the injector 26 is turned off after a predetermined time. Zuru.

ステラージ130終了後、又は、前出ステップ110.
124の判定結果が否である場合には、このルーチンを
抜(プる。
After completion of Sterage 130, or after step 110.
If the determination result at step 124 is negative, this routine is skipped.

本実施例における加速時の空燃比の変化状態の一例を第
8図に破線りで承り。+81しく第8図に貰&Eで示づ
従来例と比べて、加速時のオーバーリッチ現数が解消さ
れ、良好な空燃比が得られていることが明らかである。
An example of how the air-fuel ratio changes during acceleration in this embodiment is shown in broken lines in FIG. It is clear that the over-rich current ratio during acceleration is eliminated and a good air-fuel ratio is obtained compared to the conventional example shown by +81 and E in FIG.

尚前記実施例においては、非同期噴射回数の制限値を、
[ンジン回転速度、吸気管圧力及びエンジン冷却水温に
応じて、三次元マツプから求めるようにしていたが、非
同期@剣の制限回数を求める方法はこれに限定されず、
例えば、エンジン+o+転速麿のみに応じた一次元\ノ
ツゾ、或いは、Lンジン回Φム速反及び吸気管圧力に応
じた二次元マツプから求めることも可能て・ある。又、
エンジン回転速1哀等と制限回数の関係し、前記実施例
のように、上ンシン回転速度等が高くなるにつれて制限
回数が徐々に低くなるものに限γされず、例えば、前出
第す図に破線Fで示づ如く、エンジン回転速度等に応じ
−C1制限回数を段階的に変えることも勿論可能(゛め
る。
In the above embodiment, the limit value of the number of asynchronous injections is
[Although it was calculated from a three-dimensional map according to the engine rotation speed, intake pipe pressure, and engine cooling water temperature, the method of calculating the limit number of asynchronous @ swords is not limited to this.
For example, it is possible to obtain it from a one-dimensional map that corresponds only to the engine + engine speed + rotation speed, or a two-dimensional map that corresponds to the engine speed and reaction and intake pipe pressure. or,
The relationship between the engine rotational speed, etc. and the number of limits is not limited to that in which the number of limits is gradually lowered as the engine rotational speed, etc. increases, as in the above embodiment. As shown by the broken line F, it is of course possible to change the -C1 limit number of times in stages depending on the engine speed, etc.

前記実施例にあい−では、本発明が、スロットル弁1バ
j度の変化速度に応じIC非同期噴射に適用され(いた
が、本発明の適用a5囲はこれに限定されず、吸気冶圧
力の変化速度に応じた非同期噴射や、吸入空気量の変化
速度に応じた非同期@川に+)同(、Aに)所用できる
ことは明らかである。
In the above embodiment, the present invention was applied to IC asynchronous injection according to the rate of change of the throttle valve 1 degree (although the application of the present invention is not limited to this, and It is clear that the same (and A) can be used for asynchronous injection according to the rate of change and asynchronous injection according to the rate of change of the intake air amount.

又、前記実施例においては、非161期r@躬爺1が、
ス1」ットル弁開度変化量△王Aに応じて、゛前出〈]
)工(に示りような関係を用いて算出されていたが、−
1ンジン運転状態に応じて非同期噴射量ゴを求める′h
法はこれに限定されず、吸気管圧力や吸入空気量の変化
速度等に応じて、前出(1)式と類似の関係により非同
期噴射量Tを求めるようにしicす、或いは、非同期用
!)J 2−rを一定(旧と−づることム可能である。
In addition, in the above example, non-161st period r@Yuji1 is
1) The amount of change in the throttle valve opening △Depending on A,
) was calculated using the relationship shown in (), but -
1 Find the asynchronous injection amount according to the engine operating condition'h
The method is not limited to this, but the asynchronous injection amount T may be determined by a relationship similar to the above equation (1) depending on the intake pipe pressure, the rate of change of the intake air amount, etc. ) J2-r can be termed constant (old).

前記実施例においては、本発明か、吸気芭I−iカ感知
式の電子制御燃料噴射装置を備えた自動牛用エンジンに
適用されていたが、A発明の’rB用範囲はこれに限定
されず、例えば、吸入空気星感知工(の電子制御燃料噴
射装置を備えた自動車用エンジンに用いることも可能で
ある。この場合に(ま、当然前出第6図に示した、吸気
賀圧力と制限回数の関係を、吸入空気量と制限回数の関
係に変える必要がある。又、本発明が、他の形式の電子
制御燃料噴用式1”ンジンにも同様に適用できることは
明らかである。
In the above embodiment, the present invention was applied to an automatic cattle engine equipped with an electronically controlled fuel injection device that senses the intake air flow, but the scope of the 'rB application of the A invention is limited to this. For example, it can also be used in an automobile engine equipped with an electronically controlled fuel injection device that detects an intake air star.In this case, of course, the intake air pressure and It is necessary to change the relationship between the limit number of times to a relationship between the intake air amount and the limit number of times. It is clear that the present invention is equally applicable to other types of electronically controlled fuel injection type 1" engines.

以上説明した通り、本発明によれば、加速時の非同期用
!)J uを、容易に、且つ確実に制限Jることができ
、従って、エンジン運転状態に応じた適切な非同期噴用
組を、容易に得ることができる。
As explained above, according to the present invention, for asynchronous use during acceleration! ) J u can be easily and reliably limited, and therefore, an appropriate asynchronous injection set depending on the engine operating condition can be easily obtained.

よつ′C,急加速時のオーバーリッチ用船等を確実に防
止づることができるという優れた効果を有りる。
This has the excellent effect of reliably preventing overrich chartering during sudden acceleration.

【図面の簡単な説明】 第1図は、本発明に係る電子制御燃料噴射式土ンジンの
加速時非同期噴射制御方法の要旨を示づ流れ図。 第2図は、本発明が採用きれた、吸気管圧力感。 知式の゛吊f制御燃料噴射装置を備えた自動単用rンシ
ンの実施例を示づ、一部ブロック線図を含む断面図、 第3図は、前記実施例で用いられている電子制御ユーツ
トの崩成を示づブロック線図、第4図は、1jil 1
.; <、非同期1墳剛を行うだめの所定吋間細の11
込みルーチンを示1流れ図、M’S 5図【よ、前記ル
ーチンで用いられている、相同11iJ IIβ剣の制
限回数を求めるための三次元マツプにJlプる、−1ン
シン回転速度と制限回数の関係の例をボ゛9粉図、 第6図は、同じく、吸気管圧力と制限回数の関係の例を
ボづ線区、 第712.lは、16]じく、エンジン冷却水温と制限
同第8図は、前記実施例及び従来例における、加速時の
空燃比の変化状態の例を比較して示″CJ線図である。 △T A、・・・スロットル弁開痕変化量、A・・・所
定値、 10・・・二1ンジン、     16・・・スロット
ル弁、18・・・ス1」ットルセンサ、 22・・・吸気管圧力センサ、 26・・・インジェク
タ、34・・・デストリヒュータ、 36・・・クランク角度センサ、38・・・水温センサ
、40・・・電子制御ユニット(、ECU)。 代理人  畠 矢  論 くほか1名)
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a flowchart showing the gist of a method for controlling asynchronous injection during acceleration of an electronically controlled fuel injection soil engine according to the present invention. Figure 2 shows the intake pipe pressure feeling that the present invention has been successfully adopted. FIG. 3 is a sectional view including a partial block diagram, showing an embodiment of an automatic single-use engine equipped with an intelligent-type suspension f-control fuel injection device. The block diagram showing the collapse of the unit, Figure 4, is 1jil 1
.. ; <, 11 of the specified width for performing asynchronous one-mounding
Figure 1 shows the flowchart of the routine, M'S 5 shows the three-dimensional map used in the above routine to find the limit number of times for the homologous 11iJ IIβ sword. Figure 6 shows an example of the relationship between the intake pipe pressure and the limit number of times in the box section. l is 16] Figure 8 is a ``CJ'' diagram that compares examples of changes in the air-fuel ratio during acceleration in the embodiment and the conventional example. △ T A,... Throttle valve opening change amount, A... Predetermined value, 10... 21 engine, 16... Throttle valve, 18... Throttle sensor, 22... Intake pipe Pressure sensor, 26... Injector, 34... Distributor, 36... Crank angle sensor, 38... Water temperature sensor, 40... Electronic control unit (ECU). Agent: Ronku Hatake and 1 other person)

Claims (2)

【特許請求の範囲】[Claims] (1)エンジン同転と同期して定期的に行われる1iJ
I 111噴則に加え(、加速時は非1i;J期@射を
行うようにしIこ電子制御燃料噴射式エンジンの加速時
算量111J @則制御力法にJ、iいて、エンジン運
転状態が加速時の非同期噴射を行うl\き状態にあるか
否かを判定する手順と、非同期噴射を行うべき状態にあ
る時は、少くとしエンジン回IP7i速度に応じて、続
(プで行われる非Ia1期噴射回故の制限値を求める手
順と、111」記制限価の範囲内で一連の非同期噴射を
実行づる手順と、 を含むことを特徴とづる電子制御燃料IIR剣式上式エ
ンジンlJ速時非1ii1期噴剣制御方法。
(1) 1iJ performed periodically in synchronization with engine rotation
In addition to the I 111 injection rule (, non-1i during acceleration; J period @ injection is performed, the acceleration calculation of an electronically controlled fuel injection type engine 111J @ law control force method, J, i, and the engine operating state The procedure for determining whether or not the engine is in a state where asynchronous injection is performed during acceleration, and when it is in a state where asynchronous injection should be performed, are performed in a series of steps depending on the engine speed and IP7i speed. An electronically controlled fuel IIR sword-type upper type engine lJ characterized by comprising: a procedure for determining a limit value for non-Ia1 stage injection rotation; and a procedure for executing a series of asynchronous injections within the limit value specified in 111. Fast time non-1ii1 period spout control method.
(2)前記非fn]tilJ l’FJ剣回数の制限値
を、エンジン回転速度、エンジン温度、吸気筐圧力又は
吸入空気俣等に応じて求めるようにした特許B?I 5
Jこの範囲第1項記載の電子らり御燃料噴射式エンジン
の加速性非同期噴射制御方法。
(2) Patent B in which the limit value of the number of times of non-fn]tilJ l'FJ is determined according to engine speed, engine temperature, intake casing pressure, intake air flow, etc.? I 5
J. A method for controlling acceleration asynchronous injection of an electronically controlled fuel injection type engine according to item 1 of this scope.
JP58081290A 1983-05-10 1983-05-10 Asynchronous injection control method during acceleration of an electronically controlled fuel injection engine Expired - Lifetime JPH0647957B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58081290A JPH0647957B2 (en) 1983-05-10 1983-05-10 Asynchronous injection control method during acceleration of an electronically controlled fuel injection engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58081290A JPH0647957B2 (en) 1983-05-10 1983-05-10 Asynchronous injection control method during acceleration of an electronically controlled fuel injection engine

Publications (2)

Publication Number Publication Date
JPS59206630A true JPS59206630A (en) 1984-11-22
JPH0647957B2 JPH0647957B2 (en) 1994-06-22

Family

ID=13742246

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58081290A Expired - Lifetime JPH0647957B2 (en) 1983-05-10 1983-05-10 Asynchronous injection control method during acceleration of an electronically controlled fuel injection engine

Country Status (1)

Country Link
JP (1) JPH0647957B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007327408A (en) * 2006-06-07 2007-12-20 Denso Corp Fuel injection control device
JP2009108774A (en) * 2007-10-30 2009-05-21 Honda Motor Co Ltd Fuel injection quantity control system for general-purpose engine

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5848730A (en) * 1981-09-14 1983-03-22 Toyota Motor Corp Fuel injection method for electronically controlled type fuel-injection internal-combustion engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5848730A (en) * 1981-09-14 1983-03-22 Toyota Motor Corp Fuel injection method for electronically controlled type fuel-injection internal-combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007327408A (en) * 2006-06-07 2007-12-20 Denso Corp Fuel injection control device
JP2009108774A (en) * 2007-10-30 2009-05-21 Honda Motor Co Ltd Fuel injection quantity control system for general-purpose engine

Also Published As

Publication number Publication date
JPH0647957B2 (en) 1994-06-22

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