JPS6093153A - Fuel shut-off device - Google Patents
Fuel shut-off deviceInfo
- Publication number
- JPS6093153A JPS6093153A JP20217883A JP20217883A JPS6093153A JP S6093153 A JPS6093153 A JP S6093153A JP 20217883 A JP20217883 A JP 20217883A JP 20217883 A JP20217883 A JP 20217883A JP S6093153 A JPS6093153 A JP S6093153A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- engine
- fuel injection
- injection
- cylinder
- 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
Links
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
- F02D41/12—Introducing corrections for particular operating conditions for deceleration
- F02D41/123—Introducing corrections for particular operating conditions for deceleration the fuel injection being cut-off
-
- 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
- F02D41/008—Controlling each cylinder individually
- F02D41/0087—Selective cylinder activation, i.e. partial cylinder operation
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
Description
【発明の詳細な説明】
(技術分野)
本発明は電子制御により燃料噴射を行なう、特に単点燃
料噴射を行なう自動車用機関において、減速運転時の燃
料遮断装置の改良に関する。DETAILED DESCRIPTION OF THE INVENTION (Technical Field) The present invention relates to an improvement of a fuel cutoff device during deceleration operation in an automobile engine that performs fuel injection under electronic control, particularly single point fuel injection.
(従来技術)
車両の減速運転時には機関の駆動力が不要になることか
ら燃料の供給を停止し、減速時の燃費節減を図ることが
一般的に行なわれている。(Prior Art) Since the driving force of the engine is no longer needed when a vehicle is decelerating, it is common practice to stop the supply of fuel to reduce fuel consumption during deceleration.
この場合、車両の減速状態を絞弁が全閉、もしくけ全閉
からあるーポの開度以下になったときに州となる絞弁ス
イッチにより検出し、この検出信号ヲ受けるとコントロ
ールユニットはその時の機関回転数が遮断回転数N1以
上であれば、燃料噴射弁への噴射信号を停止して燃料遮
断を行ない、燃料遮断稜、機関回転数が解除回転数Nm
(ただしNs < Nl )まで下がると、噴射信号
の停止を解除し、燃料噴射を再開するようになっている
(例えば特開昭57−140542号公報参照)Qなお
、噴射時期は機関1回転毎に、全気筒で燃焼に必要な燃
料のしを噴射するので、たとえば、4サイクル機関では
クランク軸の1回転毎に1回噴射が行なわれることに々
る。In this case, the deceleration state of the vehicle is detected by the throttle valve switch, which is the state when the throttle valve is fully closed, or when the throttle valve becomes less than a certain opening from fully closed, and when this detection signal is received, the control unit If the engine speed at that time is equal to or higher than the cutoff rotational speed N1, the injection signal to the fuel injector is stopped to shut off the fuel, and the engine speed at the fuel cutoff edge reaches the release rotational speed Nm.
(However, when the temperature drops to Ns < Nl), the stoppage of the injection signal is canceled and fuel injection is restarted (for example, see Japanese Patent Application Laid-Open No. 140542/1983). In addition, the amount of fuel necessary for combustion is injected into all cylinders, so in a four-stroke engine, for example, injection is often performed once per revolution of the crankshaft.
ところで、気筒毎に燃料噴射弁を備える多点燃料噴射シ
ステムと異なシ、吸気マニホールドの枝管集合部よシ上
流の吸気通路に1個の燃料噴射弁を備えるのみの単点燃
料噴射システムでは、燃料噴射弁による燃料遮断、燃料
遮断解除が全気筒の燃料遮断、燃料供給再開を意味する
ので、燃料供給再開前後でのトルク変動が大きく、この
ため、車両に前後方向の衝撃が発生して運転のつながシ
が悪く、運転者に不快感を与えるという問題があった。By the way, unlike a multi-point fuel injection system that has a fuel injection valve for each cylinder, a single-point fuel injection system that only has one fuel injection valve in the intake passage upstream of the branch pipe collection part of the intake manifold, Since fuel cutoff and release of fuel cutoff by the fuel injector means fuel cutoff for all cylinders and restart of fuel supply, torque fluctuations are large before and after fuel supply is restarted, and as a result, a shock occurs in the front and rear directions of the vehicle, making it difficult to operate the vehicle. There was a problem that the connections were poor and caused discomfort to the driver.
また、気筒毎に燃料噴射弁を備える多点燃料噴射システ
ムでは、2グループに分けた噴射弁グループのそれぞれ
に制御回路を設け、機関回転数がN1とN3の間に設定
される一部気筒の燃料遮断解除回転数N2以下になると
、一方の噴射弁グループへの噴射信号の停止を解除する
ようにして燃料供給再開前後でのトルク変動による車両
の衝撃や回転数の落込みを防IFするものがあるが、こ
の場合、単点燃料噴射システムと比べ、噴射弁の数量の
多いこと、燃料配管、制(1111回路が著しく複雑と
なることなどから生産性が悪く、コスト胃を免れない。In addition, in a multi-point fuel injection system that includes a fuel injection valve for each cylinder, a control circuit is provided for each of the two injection valve groups, and some cylinders whose engine speed is set between N1 and N3 When the fuel cutoff release rotation speed drops below N2, the stoppage of the injection signal to one of the injector groups is canceled to prevent vehicle impact and rotation speed drop due to torque fluctuations before and after resuming fuel supply. However, in this case, compared to a single-point fuel injection system, the number of injection valves is large, and the fuel piping and control circuit (1111) are extremely complicated, resulting in poor productivity and high costs.
(発明の目的)
本発明は各気筒の吸気行程毎に噴射弁に噴射信号を出力
するとともに、燃料遮断後に、機関回転数がN2 (N
! <N2 <Nl )以下になると、噴射信号の回数
を気筒数の半分に低減して半数気筒の燃料供給を再会す
ることにより、燃料供給再開時の急激なトルク変動によ
る車両の衝撃を最小限に抑えて運転性の向−ヒな図り、
また、単点燃料噴射システムであっても多点燃料噴射シ
ステムと同様の作用を達成することにより、配管や制御
回路を簡素化し、生産性、制御性の改善を図る燃料遮断
装置を提供することを目的とする。(Object of the Invention) The present invention outputs an injection signal to the injection valve for each intake stroke of each cylinder, and after the fuel is cut off, the engine speed is reduced to N2 (N
! <N2 <Nl), the number of injection signals is reduced to half the number of cylinders and fuel supply to half the cylinders is resumed, thereby minimizing the shock to the vehicle due to sudden torque fluctuations when fuel supply is resumed. Designed to improve driveability by suppressing
Furthermore, it is an object of the present invention to provide a fuel cutoff device that achieves the same effect as a multipoint fuel injection system even in a single point fuel injection system, simplifies piping and control circuits, and improves productivity and controllability. With the goal.
3−
(発明の構成並びに作用)
第1図は本発明の構成を明示するための全体構成図であ
る。3- (Structure and operation of the invention) FIG. 1 is an overall block diagram for clearly showing the structure of the present invention.
すなわち、本発明は、吸気マニホールド2の枝管集合部
3よシ土流の吸気通路4に介装される1個の燃料噴射弁
6と、吸入空気量を検出するエアフローメータ13と、
機関回転数を検出するクランク角センサ14と、絞弁5
の全閉位置を検出する絞弁スイッチ17と、吸入空気量
と機関回転数に基づいて所定の燃料噴射信号を出力する
とともに、機関の減速時に機関回転数が遮断回転数N1
よシも高い場合に前記噴射信号を遮断しN1よシも低い
遮断解除回転数N3になると再び前記噴射信号を供給ス
るコントロールユニット20を備えた燃料遮断装置を前
提とする。That is, the present invention includes one fuel injection valve 6 interposed in the intake passage 4 flowing from the branch pipe collecting portion 3 of the intake manifold 2, an air flow meter 13 for detecting the amount of intake air,
A crank angle sensor 14 that detects the engine speed and a throttle valve 5
The throttle valve switch 17 detects the fully closed position of the engine, outputs a predetermined fuel injection signal based on the intake air amount and engine speed, and when the engine decelerates, the engine speed changes to the cut-off speed N1.
The present invention is based on a fuel cutoff device including a control unit 20 which cuts off the injection signal when the rotational speed is higher than N1 and supplies the injection signal again when the cutoff release rotational speed N3 is lower than N1.
そして、本発明は、この装置に、各気筒の吸気行程毎に
前記噴射弁6が1気筒分の燃料噴射を行な°うように制
御する燃料噴射制御手段28と、前記N1とN3の間に
1部気筒の燃料遮断を解除する回転数N2を設定する解
除回転数設定手段29と、機 4−
開回転数がNsからN2の回転域にあシかつ減速時にあ
ることを判別する回転域判別手段26と、この判別結果
に基づき機関回転数がN、からN2の回転域したがって
、俗気筒の吸気行程にあわせて燃料が供給されるので、
単点燃料噴射であ夛ながら、各気筒への燃料供給を制御
できることになル、このため、噴射回数をさらに制御す
ると、特定気筒の燃料供給、燃料遮断が制御されるので
ある。Further, the present invention provides this device with a fuel injection control means 28 that controls the injection valve 6 to inject fuel for one cylinder every intake stroke of each cylinder, and a fuel injection control means 28 between the N1 and N3. a release rotation speed setting means 29 for setting the rotation speed N2 at which the fuel cutoff of the first cylinder is canceled; Based on the discrimination means 26 and the discrimination result, the engine speed is determined in the rotation range from N to N2.Therefore, fuel is supplied in accordance with the intake stroke of the common cylinder.
It is possible to control the fuel supply to each cylinder while using single-point fuel injection, so if the number of injections is further controlled, fuel supply and fuel cut-off to a specific cylinder can be controlled.
(実施例)
第2図(A)は本発明の一実施例の概11r7構成図で
、4気筒機関に適用されたものである。ただし第2図B
)は第2図(〜の部分平面図である図中、燃料噴射弁6
け吸気マニホールド2の枝管集合部3より上流の吸気通
路4(たとえば絞弁5は枝管集合部3のすぐ上流に介装
されるので、この絞弁5のさらに上流の吸り、通路)に
介装され、燃料供給系の燃料ポンシフによって圧送され
た燃料を、エアクリーナ11を介して流入する吸気に向
けて供給する 々お、8は燃料フィルタ、9は燃料タン
ク、10は圧力X部器である。(Embodiment) FIG. 2(A) is a schematic 11r7 configuration diagram of an embodiment of the present invention, which is applied to a four-cylinder engine. However, Figure 2B
) is a partial plan view of FIG.
An intake passage 4 upstream of the branch pipe collection part 3 of the intake manifold 2 (for example, since the throttle valve 5 is installed immediately upstream of the branch pipe collection part 3, the intake passage further upstream of the throttle valve 5) , the fuel pumped by the fuel pump in the fuel supply system is supplied to the intake air flowing in through the air cleaner 11. 8 is a fuel filter, 9 is a fuel tank, and 10 is a pressure X component. It is.
20は燃料噴射量及び噴射時期を制御するコントロール
ユニットで、主にマイクロプロセッサ(中央演算装置)
と、メモリ(記憶装置)と、インターフェイス(入出力
信号処理回路)とから構成され、吸入空気量Qを検出す
るエアフローメータ13からの信号、機関回転数N及び
クランク角の基準位置を検出するクランク角センサ14
からの単位クランク角パルス及びクランク角基準ハルス
、機関冷却水温を検出する水温センサ15からの信号、
排気中の酸素濃度を検出する酸素濃度センサ16からの
信号、絞弁5の全閉(もしくは所定の小開度以下)を検
出する絞弁スイッチ17からの信号がそれぞれ入力され
、これらの信号にもとづいて基本的には機関回転に同期
しかつ吸入空気量に対、応したパルス幅をもつ燃料噴射
信号をつくシ、この信号により燃料噴射弁6を駆動する
。20 is a control unit that controls the fuel injection amount and injection timing, and is mainly a microprocessor (central processing unit).
, a memory (storage device), and an interface (input/output signal processing circuit), which detects the signal from the air flow meter 13 that detects the intake air amount Q, the engine speed N, and the crank angle that detects the reference position of the crank angle. Angle sensor 14
unit crank angle pulse and crank angle reference Hals from, a signal from the water temperature sensor 15 that detects the engine cooling water temperature,
A signal from the oxygen concentration sensor 16 that detects the oxygen concentration in the exhaust gas and a signal from the throttle valve switch 17 that detects when the throttle valve 5 is fully closed (or below a predetermined small opening) are input, and these signals are Basically, a fuel injection signal is generated which is synchronized with the engine rotation and has a pulse width corresponding to the amount of intake air, and the fuel injection valve 6 is driven by this signal.
同時に、コントロールユニット20では絞弁スイッチ1
7の信号とクランク角センサ14からの回転数信号にも
とづき減速時に燃料遮断を行なうが、これについて、第
3図のコントロールユニット20のブロック図に基づき
説明する。At the same time, the control unit 20 switches the throttle valve switch 1
7 and the rotational speed signal from the crank angle sensor 14, the fuel is cut off during deceleration. This will be explained based on the block diagram of the control unit 20 in FIG.
21は減速時検出手段で、絞弁スイッチ17からの信号
を入力し、絞弁スイッチ17がONである場合(絞弁5
は全閉状態にある)に減速時であることを検出する。21 is deceleration detecting means which inputs the signal from the throttle valve switch 17, and when the throttle valve switch 17 is ON (throttle valve 5
(in the fully closed state), it is detected that deceleration is occurring.
22は回転数検出手段で、一定時間の間に発生するクラ
ンク角センサ14からの単位角・そルス(回転数信号)
をH4数し、この泪数値を機関回転数Nを示す信号とし
て出力する。Reference numeral 22 denotes a rotation speed detection means, which detects the unit angle/solus (rotation speed signal) from the crank angle sensor 14 that occurs during a certain period of time.
is expressed as H4, and this value is output as a signal indicating the engine speed N.
24は燃料遮断を行なう回転数を設定する遮断回転数設
定手段で、機関水温(機関水温検出手段23にて検出さ
れる)に応じて予め設定される遮断回転数N、のマッシ
(第4図参照)から、その時のN1を読み出す。Reference numeral 24 denotes a cutoff rotational speed setting means for setting the rotational speed at which fuel cutoff is performed, and the cutoff rotational speed N is set in advance according to the engine water temperature (detected by the engine water temperature detection means 23). (see), read N1 at that time.
25は燃料遮断を解除する回転数を設定する解除回転数
設定手段で、同様に、機関水温に応じて予め設定される
解除回転数Na(ただしNs <Nl )のマツプ(第
4図参照)からその時のNsを読み出す。Reference numeral 25 denotes a release rotation speed setting means for setting the rotation speed at which the fuel cutoff is canceled, and similarly, the release rotation speed is determined from a map (see Fig. 4) of the release rotation speed Na (however, Ns < Nl), which is preset according to the engine water temperature. Read out Ns at that time.
7−
回転域判別手段26は減速時検出手段21が減速時を検
出した場合に、機関回転数Nと設定回転数N、、N、を
比較し、燃料遮断を行なう回転域を判別する。7- When the deceleration detection means 21 detects deceleration, the rotation range determination means 26 compares the engine rotation speed N and the set rotation speed N, , N, and determines the rotation range in which the fuel is cut off.
全気筒遮断設定手段30、全気筒解除設定手段32は燃
料遮断係数α(通常の燃料噴射時を1、燃料遮断時を0
とする係数である)を判別手段260判別結果に基づき
、それぞれ設定する。The all-cylinder cutoff setting means 30 and the all-cylinder release setting means 32 set a fuel cutoff coefficient α (1 during normal fuel injection and 0 during fuel cutoff).
are respectively set based on the determination result of the determining means 260.
具体的には、NがNs (例えば1600 rpm)以
上からの減速時には、全気筒遮断設定手段30にてαが
0に設定され、Na (例えば11000rp )まで
下がると、全気筒解除設定手段32にてαが再び1に設
定される(したがって、NがN1よ勺低い回転数からの
減速時にはαは0に設定されない)。Specifically, when N is decelerating from Ns (for example, 1600 rpm) or more, α is set to 0 in the all cylinder cutoff setting means 30, and when it decreases to Na (for example, 11000 rpm), α is set to 0 in the all cylinder cutoff setting means 32. Then α is set to 1 again (therefore, α is not set to 0 when decelerating from a rotational speed where N is much lower than N1).
燃料噴射制御手段28は吸入空気量Q(吸入空気量検出
手段27にて検出される)と機関回転数Nとから演算さ
れる基本噴射・母ルス幅T、(=に−Q/NfcだしK
は定数)に、他の運転ノリメータから得られる補正係数
桐、並びに前述のαを乗算して通常の噴射・9ルス幅T
i=Tp−に・αをめTiミラ 8−
噴射パルス幅とする駆11bilルス(噴射信号)を燃
料噴射弁6に供給する。The fuel injection control means 28 calculates the basic injection/main pulse width T, which is calculated from the intake air amount Q (detected by the intake air amount detection means 27) and the engine speed N, (= -Q/Nfc and K
is a constant), the correction coefficient Kiri obtained from other driving norm meters, and the above-mentioned α are multiplied to determine the normal injection 9-rus width T.
An injection pulse (injection signal) with an injection pulse width of 8- is supplied to the fuel injection valve 6 so that i=Tp- and α.
したがって、通常の燃料噴射時はα−1であるため、噴
射弁6はTi (= ’[’p −に、 )の値に対応
する時間だけ開かれ、この開弁時間に比例した燃料が噴
射供給されるが、遮断回転域の判別によりα=Oの場合
は、’ri=oとなり駆動パルスは出力され、ない。Therefore, since α-1 during normal fuel injection, the injection valve 6 is opened for a time corresponding to the value of Ti (='['p-, ), and fuel proportional to this valve opening time is injected. However, if α=O based on the determination of the cut-off rotation range, 'ri=o, and no drive pulse is output.
すなわち、減速状態が判別され−かつその時の機関回転
数NがNs (例えば1600 rpm)以上である場
合は全気筒の燃料遮断を行ない、Ns (例えば100
0 rpm) iで下がると、全気筒の燃料噴射を再開
するようになっている(したがって、NがN1より小さ
い場合には燃料遮断は行なわない)。That is, if a deceleration state is determined and the engine speed N at that time is greater than or equal to Ns (for example, 1600 rpm), fuel is cut off for all cylinders, and the engine speed is increased to Ns (for example, 100 rpm).
0 rpm) i, fuel injection in all cylinders is restarted (therefore, if N is smaller than N1, fuel cutoff is not performed).
以−にの構成については従来と同じであるが、本発明で
は、これに、燃料噴射制御手段28と、解除回転数設定
手段29と、回転域判別手段26と。The following configuration is the same as the conventional one, but in the present invention, it additionally includes a fuel injection control means 28, a release rotation speed setting means 29, and a rotation range determination means 26.
一部気筒解除設定手段31が設けられる。A partial cylinder release setting means 31 is provided.
解除回転数設定手段29はN、とN、の間に一部気筒の
燃料遮断を解除する回転数N2 (Nl >N2 〉N
3)を設定するもので、機関水温に応じて予め設定され
る遮断回転数N2のマツプ(第4図)からその時のN2
を読み出す。The release rotation speed setting means 29 sets the rotation speed N2 (Nl >N2 >N) at which fuel cutoff of some cylinders is canceled between N and N.
3), the current N2 is determined from the map (Fig. 4) of the cut-off rotation speed N2, which is preset according to the engine water temperature.
Read out.
燃料噴射制御手段28は前述した噴射パルス幅Tiを演
算する機能に、さらに燃料噴射時期を制御する機能が追
加されるもので、クランク角センサ14のクランク角基
準パルスにもとづき各気筒の吸入行程毎に噴射弁6が開
弁して噴射を行なう。The fuel injection control means 28 has a function of calculating the injection pulse width Ti described above, and a function of controlling the fuel injection timing.The fuel injection control means 28 has a function of calculating the injection pulse width Ti described above, and a function of controlling the fuel injection timing. The injection valve 6 opens to perform injection.
回転域判別手段26も、従来の機能に本発明の機能が加
わるもので、NがN3からN2の回転域にあシかつ減速
時であることを判別する。The rotation range determining means 26 also has the function of the present invention added to the conventional function, and determines whether N is in the rotation range from N3 to N2 and the vehicle is decelerating.
一部気筒解除設定手段31は、この判別結果に基づき制
聯p手段2Bからの噴射回数を気筒数の半分にするよう
前述のαを設定する。Based on this determination result, the partial cylinder release setting means 31 sets the above-mentioned α so that the number of injections from the control p means 2B is half the number of cylinders.
具体的には、機関1回転に1回の噴射が行なわれるよう
αが1と0に交互に設定されるのである。Specifically, α is alternately set to 1 and 0 so that one injection is performed per engine revolution.
次に作用を第5図のフローチャートに基づいて説明する
。なお、図中のP1〜l”+2は各ステップを示し、制
御演算は機関回転に同期して実行される。Next, the operation will be explained based on the flowchart of FIG. Note that P1 to l''+2 in the figure indicate each step, and control calculations are executed in synchronization with engine rotation.
機関の通常趣転時にはP、で絞弁スイッチ17がONで
ないため、pHで遮断係数αは1となり、P3にて噴射
ノ卆ルス幅TiはTp−KI(りだしTpU吸入空気量
Qと機関回転数Nから演算される基本パルス鼠殉は運転
パラメータによる補正係数である)となシ、このTiを
噴射パルス幅として噴射弁6が開閉駆動される、
この場合、噴射時期は各気筒の吸気行程毎に行なわれる
。つまり、吸気弁の開弁よシ所定りランク角度前になる
と、噴射弁6が開弁作動し、噴射された燃料は絞弁5を
経て吸気マニホールド2内に拡散し、続いて吸気弁の開
いた気筒に供給される。When the engine is running normally, the throttle valve switch 17 is not ON at P, so the shutoff coefficient α is 1 at pH, and the injection nozzle width Ti is Tp-KI (starting TpU intake air amount Q and engine The basic pulse width calculated from the rotational speed N is a correction coefficient based on the operating parameters), and the injection valve 6 is driven to open and close using this injection pulse width. In this case, the injection timing is set according to the intake air of each cylinder. This is done for each step. In other words, when the intake valve is opened by a predetermined rank angle, the injection valve 6 is opened, the injected fuel passes through the throttle valve 5, diffuses into the intake manifold 2, and then the intake valve is opened. is supplied to the cylinder.
今、4気筒機関の点火順序を41=1→3−≠4−≠2
として、噴射弁6の噴射時期を示すと第6図のように各
気筒の吸気行程毎に噴射が行なわれ、単点燃料噴射にか
かわらず、多点燃料噴射の一方法であるシーケンシャル
インジェクションに相当する作用が得られることになる
。Now, the ignition order of a 4-cylinder engine is 41=1→3−≠4−≠2
As shown in Figure 6, the injection timing of the injector 6 is shown. Injection is performed every intake stroke of each cylinder, and regardless of single-point fuel injection, it corresponds to sequential injection, which is a method of multi-point fuel injection. This results in the effect of
次に、機関回転数NがN+ (例えば1600 rpm
)以上の高回転域からアクセルペダルを離して減速を1
1−
行なうと、絞弁スイッチ17がONとなり(絞弁5が閉
弁する〕、かつN≧N、であるので、P9にてαはOK
設定される。Next, the engine speed N is N+ (for example, 1600 rpm
) Release the accelerator pedal from the high rotation range above to decelerate by 1.
1- When done, the throttle valve switch 17 turns ON (throttle valve 5 closes) and N≧N, so α is OK at P9.
Set.
このためP8でTi=0となシ、駆動パルスは出力され
ず、全気筒の燃料遮断が行なわれる。Therefore, when Ti=0 at P8, no drive pulse is output and fuel is cut off for all cylinders.
この全気筒燃料遮断によシ機関回転数Nが低下し、N2
〉N≧N3になると、Ploでαは1点火毎に0と1が
交互に設定される。Due to this all-cylinder fuel cutoff, the engine speed N decreases, and N2
> When N≧N3, α is alternately set to 0 and 1 for each ignition in Plo.
すなわち、機関1回転に1回は燃料遮断が解除される(
通常の半分の噴射回数で噴射される)ことにな勺、点火
順序に従い+1.≠4気筒の吸気行程に応じる噴射のみ
が再開されたとすると、第7図のように、噴射溶料の大
部分は11.44 気筒に吸入され、部分気筒燃焼を行
々う。このため、機関1回転に1回はトルクを生じるこ
とになる。In other words, the fuel cutoff is canceled once per engine revolution (
+1 according to the ignition order (injected at half the normal number of injections). If only the injection corresponding to the intake stroke of the ≠4 cylinders is restarted, most of the injected solvent will be taken into the 11.44 cylinders and partial cylinder combustion will occur, as shown in FIG. Therefore, torque is generated once per engine revolution.
この場合、吸気行程にある受筒以外の気筒にも吸気の脈
動や干渉により極めて微量の噴射燃料が供給されるが、
排気通路の触媒等に悪影響を及ばすものではない。In this case, a very small amount of injected fuel is supplied to cylinders other than the receiver cylinder during the intake stroke due to intake pulsation and interference.
It does not have a negative effect on the catalyst in the exhaust passage.
減速状態が維持され、P8でNがNs (例えは12−
1000 rpm ) VCなると、PIIKてαが再
び1に設定され、機関1回転に2回噴射が行なわれるこ
とになり、全気筒の燃料供給が再開される通常の燃料噴
射が行なわれる。When the deceleration state is maintained and N becomes Ns (for example, 12-1000 rpm) VC at P8, α is set to 1 again at PIIK, and injection is performed twice per engine revolution, so that all cylinders are injected with fuel. Normal fuel injection takes place with the supply resumed.
したがって、全気筒燃料遮断回転数N1と全気筒遮断解
除回転数N3の間に一部気筒遮断解除回転域A(第4図
)が形成されることになシ、燃料遮断からの回復時には
、−挙に全気筒の燃料供給が再開されるのではなく、半
数気筒の燃料供給の再開を必ず経るため、燃料再Jt給
前後のトルク変動が緩和され、車両の衝撃を最小限に抑
えられるのである。Therefore, a partial cylinder cut-off rotation speed range A (Fig. 4) is formed between the all-cylinder fuel cut-off rotation speed N1 and the all-cylinder cut-off release rotation speed N3, and when recovering from the fuel cut-off, - Instead of restarting fuel supply to all cylinders at once, fuel supply is always restarted to half of the cylinders, which alleviates torque fluctuations before and after refueling and minimizes shock to the vehicle. .
なお、噴射弁6の単打位置が吸気ポートよシ離れている
ので、噴射された燃料の挙動を、吸気弁の開弁時間との
関係で考慮しておく必要があり、このため、機関回転数
に対する吸気弁の開弁時間を第8図に示す。Furthermore, since the single stroke position of the injection valve 6 is far away from the intake port, it is necessary to consider the behavior of the injected fuel in relation to the opening time of the intake valve. FIG. 8 shows the opening time of the intake valve.
一部気筒噴射解除回転域A (1000〜1500 r
pm )では噴射ノfルス幅i’i(噴射弁の開所時間
で、例えば120Orpmで1.2 m5ec 程度)
に対し吸気弁の開弁時間Tは急激に大きくなる(例えば
240Orpmで12.5 m5ecが120Orpm
で25 m5ecとなる)。Partial cylinder injection release rotation range A (1000 to 1500 r
pm), the injection nozzle width i'i (opening time of the injection valve, for example, about 1.2 m5ec at 120Orpm)
On the other hand, the opening time T of the intake valve suddenly increases (for example, 12.5 m5ec at 240Orpm becomes 120Orpm).
25 m5ec).
一方、噴射弁6と吸気弁との間の通路距離は約0.3m
あυ、減速時の気化燃料は音速で流れるので、噴射によ
り即座に気化した燃料が吸気弁の開口部に達するに要す
る時間は約1 m5ec、 i fc噴射により吸気通
路の内壁に付着した壁面燃料が同じく開口部に達するに
要する時間Tj(第8図の鎖線)は約I Q m5ec
となり、これらの所要時間を前述の噴射弁開弁時間T
iに加算しても、なお吸気弁の開弁時間Tに比較すれば
充分小さい。このため、一部気筒には演算された燃料量
がほとんど供給されることになり燃焼状態は良好に維持
される。したがって、噴射弁6の取付位置が離れたもの
であっても一部1(気筒遮断解除回転域A (1000
〜1500rpm)の設定は容易に可能となるのである
。On the other hand, the passage distance between the injection valve 6 and the intake valve is approximately 0.3 m.
Aυ, since vaporized fuel flows at the speed of sound during deceleration, the time required for the fuel vaporized immediately by injection to reach the opening of the intake valve is approximately 1 m5ec. The time Tj (dashed line in Fig. 8) required for the same to reach the opening is approximately IQ m5ec.
These required times are defined as the injection valve opening time T
Even if added to i, it is still sufficiently small compared to the opening time T of the intake valve. Therefore, most of the calculated amount of fuel is supplied to some cylinders, and the combustion state is maintained in good condition. Therefore, even if the injection valve 6 is installed at a remote location, part 1 (cylinder cutoff release rotation range A (1000
~1500 rpm) can be easily set.
々お、絞弁スイッチ17は絞弁5の下流の吸入負圧を検
出する負圧センサに代えてもよく、この場合には吸入負
圧により減速状態が検出されることになる。Alternatively, the throttle valve switch 17 may be replaced with a negative pressure sensor that detects the suction negative pressure downstream of the throttle valve 5, and in this case, the deceleration state will be detected by the suction negative pressure.
また、一部気筒の燃料遮断解除は+3.+2気筒につい
て行なってもよいし、均一なトルク変動でなくともよい
場合は、=ll−11+−2気筒あるいは+−3,+1
気筒の一方を燃料遮断解除することも可能である。Also, release of fuel cutoff for some cylinders is +3. It may be done for +2 cylinders, or if uniform torque fluctuation is not required, =ll-11+-2 cylinders or +-3, +1
It is also possible to release fuel cut-off for one of the cylinders.
(発明の効果)
以上のように本発明によれば、単点燃料噴射弁の燃料噴
射を各気筒の吸気行程毎に行なうとともに、減速時の燃
料遮断回転数N、と燃料遮断解除回転数N、の間に一部
気筒遮断解除回転数N2を設定し、N2とN3の間を一
部気筒遮断解除回転域として減速時に全気筒の燃料遮断
が行なわれた俵、回転数の低下に伴い全気筒の溶料供給
が再開される前にまず半数気筒の燃料供給が再開される
ようにしたので、トルク変動が緩和され、従来例のよう
に燃料供給再開前後の急激なトルク変動が発生せず、こ
れにより著しく運転性の同上が図れるという効果が得ら
れる。(Effects of the Invention) As described above, according to the present invention, fuel is injected by the single-point fuel injection valve every intake stroke of each cylinder, and the fuel cut-off rotation speed N during deceleration and the fuel cut-off release rotation speed N are , the partial cylinder cutoff release rotation speed N2 is set between N2 and N3, and the partial cylinder cutoff release rotation speed range is set between N2 and N3. Since the fuel supply to half of the cylinders is restarted before the solvent supply to the cylinders is restarted, torque fluctuations are alleviated and the sudden torque fluctuations before and after fuel supply restarts do not occur as in the conventional case. This has the effect of significantly improving drivability.
tri公知の多点燃料噴射システムによシ行なわれる笥
1分気筒遮断解除と同一の作用が本発明により行なわれ
るので、この多点燃料噴射システムと15−
は較べものにならない程配管や制御回路が簡素化でき、
生産性、制御性が改善できるという効果も得られる。Since the same effect as the one-minute cylinder cut-off release performed by the known multi-point fuel injection system is performed by the present invention, the piping and control circuits are incomparably different from this multi-point fuel injection system. can be simplified,
It also has the effect of improving productivity and controllability.
第1図は本発明の全体構成図である。
第2図へ)は本発明の1実施例の全体図、第2図0は第
2図(5)の部分平面図、第3図は第2図(5)中のコ
ントロールユニットのブロック図である。
第4図は機関水温に対する設定回転数の特性図、第5図
は第2図(5)中のコントロールユニットの演算処理を
示すフローチャート、第6図は通常時の燃料噴射時期を
説明する図、第7図は一部気筒の燃料遮断解除時の燃料
噴射時期を説明する図、第8図は機関回転数に対する吸
気弁開弁時間、噴射弁開弁時間、壁面燃料流による所要
時間をそれぞれ示す特性図である。
2・吸気マニホールド、3・・・枝管集合惟、4・・・
吸シ通路、5・・・絞弁、6・・・燃料噴射弁、13・
・・エアフローメータ、14・・・クランク角センサ、
17・・・絞弁スイッチ、20・・・コントロールユニ
ット、16−
21・・・減速時検出手段、22・・・回転数検出手段
、24・・・遮断回転数設定手段、25.29・・・解
除回転数設定手段、26・・何E11転載判別手段、2
7・・・吸入空惣量検出手段、28・・・燃料噴射制御
手段、3061.全気筒遮1tノr設定手段、31・・
・一部気筒解l!、1′−,設定手段、32・・・全気
筒解除設定手段。
特許出願人 日産自動車株式会社FIG. 1 is an overall configuration diagram of the present invention. Figure 2) is an overall view of one embodiment of the present invention, Figure 20 is a partial plan view of Figure 2 (5), and Figure 3 is a block diagram of the control unit in Figure 2 (5). be. Fig. 4 is a characteristic diagram of the set rotation speed with respect to engine water temperature, Fig. 5 is a flowchart showing the arithmetic processing of the control unit in Fig. 2 (5), Fig. 6 is a diagram explaining the fuel injection timing in normal conditions, Fig. 7 is a diagram explaining the fuel injection timing when fuel cutoff is released for some cylinders, and Fig. 8 shows the intake valve opening time, injection valve opening time, and time required by wall fuel flow with respect to engine speed, respectively. It is a characteristic diagram. 2. Intake manifold, 3. Branch pipe collection, 4.
Suction passage, 5... Throttle valve, 6... Fuel injection valve, 13.
...Air flow meter, 14...Crank angle sensor,
17... Throttle valve switch, 20... Control unit, 16-21... Deceleration detection means, 22... Rotation speed detection means, 24... Cutoff rotation speed setting means, 25.29... - Release rotation speed setting means, 26...What E11 reprinting determining means, 2
7... Intake air amount detection means, 28... Fuel injection control means, 3061. All cylinder shutoff 1 ton r setting means, 31...
・Partial cylinder disassembly! , 1'-, setting means, 32... all cylinder release setting means. Patent applicant Nissan Motor Co., Ltd.
Claims (1)
装される1個の燃料噴射弁と、吸入空気量を検出するエ
ア70−メータと、機関回転数を検出するクランク角セ
ンサと、絞弁の全閉位置を検出する絞弁スイッチと、吸
入空気量と機関回転数に基づいて所定の燃料噴射信号を
出力するとともに、機関の減速時に機関回転数が遮断回
転数N。 よシも高い場合に前記噴射信号を遮断しN1よりも低い
遮断解除回転数N3になると再び前記噴射信号を供給す
るコントロールユニットヲ備えた燃料遮断装置において
、各気筒の吸気行程毎に前記噴射弁が1気筒分の燃料噴
射を行なうように制御する燃料噴射制御手段と、前記N
1とN、の間に1部気筒の燃料遮断を解除する回転数N
を設定する解除回転数設定手段と、機関回転数がN8か
らN2の回転域にあシかつ減速時にあることを判別する
回転域判別手段と、この判別結果に基づき襞間回転数が
N、からN2の回転域になると、前記噴射弁の噴射回数
を気筒数の半分にする一部気筒解除設定手段を設けたこ
とを特徴とする燃料遮断装置。[Scope of Claims] One fuel injection valve installed in the intake passage upstream of the branch pipe collection part of the intake manifold, an air 70-meter for detecting the amount of intake air, and a crank for detecting the engine speed. An angle sensor, a throttle valve switch that detects the fully closed position of the throttle valve, outputs a predetermined fuel injection signal based on the intake air amount and engine speed, and when the engine decelerates, the engine speed changes to the cutoff speed N. . In the fuel cutoff device, the fuel cutoff device includes a control unit that cuts off the injection signal when the rotational speed is higher than N1 and supplies the injection signal again when the cutoff release rotation speed N3 is lower than N1. a fuel injection control means for injecting fuel for one cylinder;
Between 1 and N, the rotation speed N at which the fuel cutoff of the first cylinder is released.
a release rotation speed setting means for setting the engine rotation speed; a rotation range determination means for determining that the engine rotation speed is in the rotation range from N8 to N2 and during deceleration; A fuel cutoff device characterized in that a partial cylinder release setting means is provided which reduces the number of injections of the injection valve to half the number of cylinders when the engine speed reaches the N2 rotation range.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20217883A JPS6093153A (en) | 1983-10-28 | 1983-10-28 | Fuel shut-off device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20217883A JPS6093153A (en) | 1983-10-28 | 1983-10-28 | Fuel shut-off device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6093153A true JPS6093153A (en) | 1985-05-24 |
Family
ID=16453250
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP20217883A Pending JPS6093153A (en) | 1983-10-28 | 1983-10-28 | Fuel shut-off device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6093153A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7086387B2 (en) * | 2001-06-01 | 2006-08-08 | Hitachi, Ltd. | Control apparatus of internal combustion engine |
-
1983
- 1983-10-28 JP JP20217883A patent/JPS6093153A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7086387B2 (en) * | 2001-06-01 | 2006-08-08 | Hitachi, Ltd. | Control apparatus of internal combustion engine |
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