JPS5910747A - Fuel cut device for electronically controlled engine - Google Patents

Fuel cut device for electronically controlled engine

Info

Publication number
JPS5910747A
JPS5910747A JP11839882A JP11839882A JPS5910747A JP S5910747 A JPS5910747 A JP S5910747A JP 11839882 A JP11839882 A JP 11839882A JP 11839882 A JP11839882 A JP 11839882A JP S5910747 A JPS5910747 A JP S5910747A
Authority
JP
Japan
Prior art keywords
fuel
engine
reference value
synchronous
fuel cutoff
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
JP11839882A
Other languages
Japanese (ja)
Inventor
Nobuo Habu
土生 信男
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 JP11839882A priority Critical patent/JPS5910747A/en
Publication of JPS5910747A publication Critical patent/JPS5910747A/en
Pending 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
    • F02D41/12Introducing corrections for particular operating conditions for deceleration
    • F02D41/123Introducing corrections for particular operating conditions for deceleration the fuel injection being cut-off

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 reduce variation of the output torque of an engine by cutting fuel when synchronous fuel injection amount is less than a reference value. CONSTITUTION:In step 66 is read an engine speed Ne. In step 67 is obtained the reference fuel injection time taucut from the engine seed Ne. In step 68 is read synchronous injection time tau, and in step 69 is judged whether or not tau<taucut. When tau<taucut and the engine speed Ne>=N1, fuel is cut. When Ne<N1 even though tau<taucut, fuel is not cut. When tau>=taucut, fuel is not cut. Thus, the variation of the output torque of the engine can be reduced.

Description

【発明の詳細な説明】 本発明は、減速期間に燃料の供給を中止して排気ガスの
浄化および燃料消費効率を改善する電子制御機関の燃料
遮断(フューエルカット)装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fuel cut device for an electronically controlled engine that stops supplying fuel during a deceleration period to improve exhaust gas purification and fuel consumption efficiency.

従来の燃料遮断装置では、燃料遮断が、絞り弁のアイド
リング開度を検出するアイドルスイッチのオン、オフに
応動して実施されている。
In conventional fuel cutoff devices, fuel cutoff is performed in response to turning on and off of an idle switch that detects the idling opening of a throttle valve.

アイドルスイッチは、絞り弁の軸に連動して接点を開閉
する機械式であり、所定の接点圧力を確保する/こめに
絞り弁開度がアイドリング開度より少し大きい1〜2°
からオンになっている。
The idle switch is a mechanical type that opens and closes the contacts in conjunction with the shaft of the throttle valve, ensuring a predetermined contact pressure.
It has been turned on since.

したがって従来の燃料遮断装置では、特に機関の低回転
速度領域における燃)1遮断の場合、機関の出力トルク
が機関の摩擦トルクへ十分に近旧く前に燃料遮断が開始
され、あるいは減速から加速へ移る場合には絞り弁が1
〜2゛の開度になってから燃料供給が再開され、燃料遮
断の開始、および減速から加速へ移る際の衝撃が増大し
ている。寸だ、絞り弁が完全にアイドリング開度になっ
ていないわずかな開度にある状態で燃享1遮断が行なわ
れることは、機関の低回転軽負荷の運転領域を狭めてい
る。
Therefore, in the conventional fuel cutoff device, especially in the case of fuel cutoff in the low engine speed region, the fuel cutoff is started before the engine's output torque becomes sufficiently close to the engine's friction torque, or the fuel cutoff is started before the engine's output torque becomes sufficiently close to the engine's friction torque, or the fuel cutoff is started before the engine's output torque becomes sufficiently close to the engine's friction torque. If it moves, the throttle valve is 1
The fuel supply is resumed after the opening degree reaches ~2°, and the shock at the start of fuel cutoff and when transitioning from deceleration to acceleration increases. Indeed, the fact that the fuel 1 cutoff is performed when the throttle valve is not fully idling but at a slight opening narrows the engine's low-speed, light-load operating range.

本発明の目的d:、アイドルスイッチがアイドリング開
度より少し大きい開度からオンになる/こめに生じてい
た従来の燃料遮断装置のこのような欠点を除去すること
である。
An object of the present invention is to eliminate such drawbacks of the conventional fuel cutoff device, which occurs when the idle switch is turned on from an opening slightly larger than the idling opening.

この目的を達成するだめに本発明によれば、機関の回転
に同期して噴射弁から吸気系へ供給する燃料の同期燃料
噴射量が吸入空気流量の関数として削q、される電子制
御機関の燃料遮断装置において、機関回転速度の関数で
ある基準値を、検出シ7フξ1穴関回転速度から算出し
、回期燃利噴射計か基準値未満であれば燃料遮断を行な
い、同1υ1燃料噴射計か基準値以−1−であれd、燃
ネIを吸気系へ供給する。
In order to achieve this object, the present invention provides an electronically controlled engine in which the synchronous fuel injection amount of fuel supplied from the injection valve to the intake system in synchronization with the rotation of the engine is reduced as a function of the intake air flow rate. In the fuel cutoff device, a reference value, which is a function of the engine rotational speed, is calculated from the detection shift ξ1 hole rotational speed, and if the periodic fuel injection meter is less than the reference value, the fuel is cut off, and the same 1υ1 fuel If the injection meter is below the standard value, it will supply fuel I to the intake system.

図面を参照して本発明の実施例をt)a明する。Embodiments of the present invention will be explained with reference to the drawings.

第1図は本発明が適用される’i[Y1制ml I箋関
の全体の概略図である。エアクリーナ1から吸入されだ
電気はエアフローメータ2、絞り弁3、ザーノタンク・
1、吸気ボート5、および吸気弁6を含む吸気通路12
を介して機関本体7の燃焼室8へ送られる6、絞り弁6
は運転室の加速ペダル1,3に連動する。燃焼室8はシ
リンダヘッド9、シリンダブロック10、およびピスト
ン11によって画定され、混合気の燃焼によって生成さ
れ/こ排気ガスは制気弁15、排気ボート16、排気分
岐管17、および排気管18を介して大気へ放出される
。バイパス通路21は絞り弁3の上流とザージタンク4
とを接続し、バイパス流量制御弁22はバイパス通路2
1の流通断面積を制御し7てアイドリンク時の機関回転
速度を一定に維持する。窒素酸化物の発生を抑制するだ
めに排気ガスを吸気系へ導くυ1気ガス再循環(EGR
)通路2:3 ij、排気分岐′(τ17とザー/・4
ンク4とを接続し、オンオフ弁形式の排気ガス再循環(
EGR)制御弁2・I tfot:電気パルスに応動し
てEGR通路2;)を開閉する。)!ジ気IM1センザ
281(1、エアフローメータ2内に設けられて吸気温
を検出し、スロットル位置センザ29 t/i、絞り弁
:3の開度を検出する。水温センサ30 (4ンリンダ
ブロツク10に取付けられて冷却水温度、すなわち機関
温度を検出し7、酸素濃度センサとしての周知の空燃比
センサ31は411気分岐管17の集合部分に取付けら
れて集合部分における酸素濃度を検出し、クランク角セ
ンサ32は、機関本体7のクランク軸(図示せず)に結
合する配電器33の軸;3・1の回転からクランク軸の
クランク角を検出する。これらのセン′v2+ ”8+
29.30.31.32の出力は電子制御装置40へ送
られる。燃旧噴種弁旧は各気筒に対応して各吸気ボート
5の近傍にそれぞれ設けられ、ポンプ42は燃料タンク
43からの燃料通路44を介して燃料噴射弁旧へ送る。
FIG. 1 is a schematic diagram of the entire Y1 system to which the present invention is applied. The electricity sucked in from the air cleaner 1 is sent to the air flow meter 2, throttle valve 3, Zano tank,
1, an intake passage 12 including an intake boat 5 and an intake valve 6
6, which is sent to the combustion chamber 8 of the engine body 7 via the throttle valve 6.
is linked to accelerator pedals 1 and 3 in the driver's cab. A combustion chamber 8 is defined by a cylinder head 9, a cylinder block 10, and a piston 11, and the exhaust gas produced by the combustion of the air-fuel mixture passes through a control valve 15, an exhaust boat 16, an exhaust branch pipe 17, and an exhaust pipe 18. released into the atmosphere via The bypass passage 21 connects the upstream side of the throttle valve 3 and the surge tank 4.
The bypass flow control valve 22 is connected to the bypass passage 2.
The flow cross-sectional area of 1 is controlled to maintain a constant engine rotational speed during idling. In order to suppress the generation of nitrogen oxides, exhaust gas is guided to the intake system by υ1 gas recirculation (EGR).
) Passage 2:3 ij, exhaust branch' (τ17 and ther/・4
connection 4, and perform on-off valve type exhaust gas recirculation (
EGR) control valve 2・Itfot: Opens and closes the EGR passage 2;) in response to electric pulses. )! Water temperature sensor 281 (1, installed in the air flow meter 2 to detect the intake air temperature, throttle position sensor 29 t/i, throttle valve: 3 opening degree), water temperature sensor 30 (4 cylinder block 10) A well-known air-fuel ratio sensor 31 as an oxygen concentration sensor is attached to the collecting part of the 411 air branch pipe 17 to detect the oxygen concentration in the collecting part, and detects the cooling water temperature, that is, the engine temperature. The angle sensor 32 detects the crank angle of the crankshaft from the rotation of the shaft of the power distributor 33 connected to the crankshaft (not shown) of the engine body 7; 3.1.
The outputs of 29.30.31.32 are sent to the electronic control unit 40. Fuel and injection valves are provided near each intake boat 5 in correspondence with each cylinder, and the pump 42 supplies fuel from a fuel tank 43 to the fuel injection valves through a fuel passage 44.

電子jlil制御装簡4(1iJ、各センサからの一人
力信弓に基ついて燃れ(噴QA’ ti’iを唱豹し7
、青1■しだ燃オ′・1噴Q1.5+4に月見、しブこ
パルス幅の燃第1噴射パルスを燃料噴射弁41−8送る
。電−r’ :Il僧1装置=lO11だ、バイパス流
に制御弁22、F: G R:li’l伺弁2・1.お
A、ひ点火装置・1Gを開側)する。点火装置バ4(i
の点すくコイルの三次Th1ll lql:配電器3;
3−\接続されている。。
Electronic jlil control system 4 (1iJ, burning based on one person's strength bow from each sensor (reciting jet QA'ti'i 7
, Blue 1 ■ Shida Fuel O'・1 injection Q1.5+4 sends the first fuel injection pulse with a Tsukimi and Shibu pulse width to the fuel injection valve 41-8. E-r': Il monk 1 device = lO11, control valve 22 for bypass flow, F: G R:li'l visit valve 2.1. A, Ignition device/1G open side). Ignition device bar 4 (i
Tertiary Th1ll lql of the spotting coil: Distributor 3;
3-\Connected. .

第2図((1、電子−制御装置の内部のブ「1ツク図で
ある。 CP U 5に 、 ROM 57、RAM 
58 、541、マルチプレクザ利きA/I) (アナ
ログ/テゾ′タル)変換器60、およびl10(人出力
)インクフェース61は、バス62を介して互いに接続
されている。RAM5!1←l1、補助電源へ接続され
ており、点火スイッチか開かれて機関が停市している期
間も所定の電力を供給されて記憶を保持することができ
る。
Figure 2 (1) is a block diagram of the internal components of the electronic control unit. CPU 5, ROM 57, RAM
58 , 541 , a multiplexer (A/I) (analog/tezotal) converter 60 , and an I10 (human output) ink face 61 are connected to each other via a bus 62 . RAM5!1←l1 is connected to the auxiliary power source, and even when the ignition switch is opened and the engine is stopped, a predetermined amount of power is supplied and the memory can be retained.

ニーアフロ−メータ2、吸気温センサ28、水温センサ
30、および空燃比センサ31からのアナログ信号はA
/D変換器60へ送られる。スロットル位置センサ2(
]およびクランク角セノザ32の出力はI10インタフ
ェース6Iへ送られ、バイパス流量制御I fp 22
、EGR制御弁24、燃料噴射弁旧、および点火装置4
al(、J、入出力インタフエーヌ61から入カイ言号
を送られる。
Analog signals from the knee flow meter 2, intake temperature sensor 28, water temperature sensor 30, and air-fuel ratio sensor 31 are A.
/D converter 60. Throttle position sensor 2 (
] and the output of the crank angle sensor 32 are sent to the I10 interface 6I, and the bypass flow control I fp 22
, EGR control valve 24, old fuel injection valve, and ignition system 4
al(, J, an input signal is sent from the input/output interface 61.

第3図d、本発明のプログラムのフローチャートである
。ステップ66では機関回転速度Neを読込む。機関回
転速度Neはクランク角センザ32からの人力から検出
される。ステップ67では燃料遮断のだめの基準燃料噴
射時間でcutを算出する。
FIG. 3d is a flowchart of the program of the present invention. In step 66, the engine rotational speed Ne is read. The engine rotational speed Ne is detected from human power from the crank angle sensor 32. In step 67, cut is calculated using the standard fuel injection time for fuel cutoff.

τc u tにl:第4図に示されているようにNeの
関数であり、次式により定義される。
τc u t l: As shown in FIG. 4, it is a function of Ne and is defined by the following equation.

τcut=Ne X (−K )+T const/こ
だしK if正の定数、τconstけ第4図のT c
onstに列名する同期燃料噴射時間τであり定藪であ
る。なお同期燃料噴射時間τとは、機関回転速度に同+
lJ+ して噴射弁11が燃料を噴射する時間を意味し
、噴射弁旧はでたけ開状態に維持される。
τcut=Ne
The synchronous fuel injection time τ listed in onst is constant. Note that the synchronous fuel injection time τ is the same as the engine rotation speed.
lJ+ means the time during which the injection valve 11 injects fuel, and the injection valve old is kept fully open.

第4図において横軸は機関回転速度Ne、縦軸は機関の
出力トルクTであり、等τ線は横軸に対して・1行にな
る。機関の摩擦トルクは、Neに関係1〜ており、Ne
か小さいとき1′−1減少(摩擦トルクは負で表現する
ため)する。τcut(r、J摩擦)・ルクの線に沿っ
て設定されている1、機関の出力トルクTか負というこ
とは、トルクか駆動輪から機関のカへ伝達されているこ
とを意味する。
In FIG. 4, the horizontal axis is the engine rotational speed Ne, the vertical axis is the engine output torque T, and the iso-tau line is in one line with respect to the horizontal axis. The friction torque of an engine is related to Ne, and Ne
When it is small, it decreases by 1'-1 (because friction torque is expressed as a negative value). The engine output torque T, which is set along the line τcut(r, J friction) · torque, is negative, which means that the torque is being transmitted from the drive wheels to the engine force.

ステップ(58では、同量噴射時間τを読込む。τは吸
入空気流量−Qの関数である。吸入空気計はエアフロ・
−メータ2から直接、あるいは吸気管負側から間接的に
検出できる。ステップ69でd、τ〈τcutか否かを
判別して〈τcutてあればステップ70へ進み、τ、
τcutであればステップ76へ進んでフラグF cu
tを0にする。ステップ70ではNe 、NIであるか
否かを判別しNe 、Q−3Nlであればステップ74
へ進んでフラグF cutを1にし、N〈N1てあれば
ステップ71へ進む。Nl1J:、2000 r、p、
m。
Step (58) reads the same amount injection time τ. τ is a function of the intake air flow rate - Q.
- It can be detected directly from the meter 2 or indirectly from the negative side of the intake pipe. In step 69, it is determined whether d, τ<τcut, and if it is, the process proceeds to step 70, and τ,
If τcut, proceed to step 76 and set the flag F cu
Set t to 0. In step 70, it is determined whether Ne is NI or not, and if Ne is Q-3Nl, step 74
Step 71 sets the flag F cut to 1, and if N<N1, the flow advances to step 71. Nl1J:, 2000 r, p,
m.

以下であり、例えばl300r、p、m、である。ステ
ップ71ではN−1−N2かつF cut−1か否かを
判別し、N−;−N2かつF cut−=1であればプ
ロゲラ11を終了し、N(N2あるいiJ、’ F c
ut = 0であればステップ76へ進んでp cut
 = Oとする。N2はI 800 r、p、+n、以
下であり、Nl  −N2  /100てあり、N2(
d例えば!I F3(] r、 p、m、である。Fc
uヒ1の場合は燃1;l遮断が実倫され、F C1l 
t−0の場合は燃料が燃料噴射弁旧から供給される。燃
料遮断の実施には機関回転速度に関するヒステリシスが
設けら九、Ne(Nlの場合では燃料遮断は開始されず
、1だ、燃本・I退所は−/こん開始されるとNeがN
2に減少する寸で継続さhる。従来の燃料遮断装置では
第4図の破線で示されるようにアイドルスイッチがオフ
からオフになると、すなわち絞り弁3がアイドリング開
度になる前の1〜2°の開度の時に燃料遮断が開始され
、機関の出力トルクTが破線の位置から摩擦トルクの位
置(二点釦線)へ大きく変化し、大きな衝撃が発生して
いた。本発明では機関の出力トルクTがその時の機関回
転速度Neにおける摩擦トルクに十分に近付いてから燃
料遮断が実施されるので、燃料遮断の開始に伴う機関の
出力トルクの変化が小さく、衝撃が抑制される。
For example, l300r, p, m. In step 71, it is determined whether or not N-1-N2 and F cut-1. If N-;-N2 and F cut-=1, Progera 11 is terminated and N(N2 or iJ,'
If ut = 0, proceed to step 76 and p cut
= O. N2 is less than or equal to I 800 r, p, +n, Nl - N2 /100, and N2 (
dFor example! I F3(] r, p, m, Fc
In the case of u Hi 1, it is practical to shut off the fuel 1;l, and F C1l
In the case of t-0, fuel is supplied from the old fuel injection valve. A hysteresis regarding the engine rotational speed is provided for the implementation of the fuel cutoff.If Ne(Nl), the fuel cutoff will not be started, but if Ne is
It continues decreasing to 2 hours. In the conventional fuel cutoff device, the fuel cutoff starts when the idle switch is turned off from OFF, as shown by the broken line in Fig. 4, that is, when the throttle valve 3 is opened 1 to 2 degrees before reaching the idling opening. As a result, the engine output torque T changed significantly from the position of the broken line to the position of friction torque (the two-dot button line), and a large impact was generated. In the present invention, the fuel cutoff is performed after the engine output torque T sufficiently approaches the friction torque at the engine rotational speed Ne at that time, so the change in the engine output torque accompanying the start of the fuel cutoff is small, and the impact is suppressed. be done.

第5図はNeがそれぞれNea 、 Neb 、 Ne
c (Nea (Neb (Nec)の」場合における
機関の出力トルクTと絞り弁開度との関係を示(2てい
る。実線は本発明、破線d、〒l′r−来装置の!時性
を71にし、ている02本発明でi−1、アイドルスイ
ッチかオンU(二なる開度以後も、燃j′−1供給が継
続され、機関の出力l・ルクが摩擦トルクに十分に接近
してから燃81遮断が開始され、この特徴はNeが小さ
い場合程、顕著となる。
In Figure 5, Ne is Nea, Neb, Ne, respectively.
c shows the relationship between the engine output torque T and the throttle valve opening in the case of Nea (Neb (Nec)). In the present invention, i-1, the idle switch is turned on U (even after the second opening, the fuel j'-1 continues to be supplied, and the engine's output l/ruq is sufficient for the friction torque). The fuel 81 cut-off starts after the approach, and this feature becomes more pronounced as Ne is smaller.

第6図はスロットル弁をアイドリング開度まで除々に閉
じアイドリング開度から円び除々に開くときの車速およ
び機関の出力トルクの時間変化を示している。実線は本
発明、破線は従来装置の変化をそれぞれ示している。t
l 、 t2はそれぞれ従来装置および本発明において
燃料遮断が開始される時刻、t3 、 t4はそれぞれ
本発明および従来装置において燃料供給が再開される時
刻である。燃料遮断中は機関回転速度が減少するので機
関出力は時間とともに増大する。本発明により、機関の
出力トルクが十分に減少してから燃料遮断が実施され、
まだ、加速時d1、アイドルスイッチがオフになる絞り
弁開度1〜2゜以前に燃料供給が速やかに再開されるの
で、燃料遮断の開始、終了に伴う機関出力トルクの変化
が減少し、衝撃が抑制される。
FIG. 6 shows changes over time in vehicle speed and engine output torque when the throttle valve is gradually closed to the idling opening and then gradually opened from the idling opening. The solid line shows the present invention, and the broken line shows the change in the conventional device. t
1 and t2 are the times at which fuel cutoff is started in the conventional device and the present invention, respectively, and t3 and t4 are the times at which fuel supply is restarted in the present invention and the conventional device, respectively. During fuel cutoff, the engine speed decreases, so the engine output increases over time. According to the present invention, the fuel cutoff is performed after the output torque of the engine is sufficiently reduced;
However, during acceleration d1, the fuel supply is quickly resumed before the throttle valve opening degree is 1 to 2 degrees when the idle switch is turned off, so the change in engine output torque due to the start and end of fuel cut-off is reduced, and the impact is reduced. is suppressed.

このように本発明によれは、吸入空気流量の関数として
言1算された同期燃料噴射計を、機関回転速度の関数と
して計算された基準値と比較して燃料遮断の実施を決定
するので、燃料遮断の開始および燃料供給の再開に伴う
機関出力トルクの断続的な変化量を減少さぜ、衝撃を抑
制することができる。寸だ、アイドルスイッチがオンと
なるような極めて小さい開度において燃料供給を維持す
ることができるので、機関の低負荷における運転領域を
拡大することができる。
Thus, according to the present invention, the synchronous fuel injector calculated as a function of the intake air flow rate is compared with a reference value calculated as a function of the engine speed to determine whether to perform a fuel cutoff. It is possible to reduce the amount of intermittent change in engine output torque accompanying the start of fuel cutoff and resumption of fuel supply, thereby suppressing impact. Since fuel supply can be maintained at extremely small openings, such as when the idle switch is turned on, the operating range of the engine at low loads can be expanded.

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

第1図は本発明が適用される電子制御機関の全体の概略
図、第2図は第1図の電子制御装置のブロック図、第3
図は本発明に基づくプログラムのフローチャート、第4
図は燃料遮断の実施領域を示す図、第5図−は本発明と
従来装置とを対比して絞り弁開度と機関の出力トルりと
の関係を示すグラフ、第6図は緩減速から緩力11速−
\移行する場合の重速、絞り弁開度、および機関の出力
トルクの時間変化を示すグラノーである。 2・工rフローメータ、7・・・機関本体、・10・・
電子制御装置、41・燃料噴射弁。
FIG. 1 is a schematic diagram of the entire electronic control engine to which the present invention is applied, FIG. 2 is a block diagram of the electronic control device shown in FIG. 1, and FIG.
Figure 4 is a flowchart of a program based on the present invention.
The figure shows the implementation range of fuel cutoff, Figure 5- is a graph showing the relationship between the throttle valve opening and the engine output torque comparing the present invention and the conventional device, and Figure 6 shows the relationship between the throttle valve opening and the engine output torque. Slow force 11 speed-
This is a graph that shows the time changes in heavy speed, throttle valve opening, and engine output torque when shifting. 2. Flow meter, 7. Engine body, 10.
Electronic control unit, 41・Fuel injection valve.

Claims (1)

【特許請求の範囲】 1 機関の回転に同期して噴射弁から吸気系へ供給する
燃料の同期燃料噴射量が吸入空気流樋の関数として計算
される電子制御機関の燃料遮断装置において、機関回転
速度の関数である基準値を、検出した機関回転速度から
算出し、同期燃料噴射量が基準値未満であれば燃料遮断
を行ない、同期燃料噴射量が基準値以」二であれば燃料
を吸気系へ供給することを特徴とする、電子制御機関の
燃料遮断装置。 2 噴射弁へ送られるべき燃料噴射パルスが、同期燃料
噴射量に対応するパルス幅を有し、該パルス幅が前記基
準値と比較されることを特徴とする特許請求の範囲第1
項記載の燃料遮断装置。 3 前記基準値は、機関回転速度の増大に連れて減少す
るような関数として設定されていることを特徴とする特
許請求の範囲第1項あるいは第2項記載の燃料遮断装置
。 4 前記基準値τcutが、次式 %式% た/としNe:機関回転速度、K:正の定数、τcon
st :定数とする。 から勢出されることを特徴とする特許請求の範囲第3項
記載の燃料遮断装置。
[Scope of Claims] 1. A fuel cutoff system for an electronically controlled engine in which a synchronous fuel injection amount of fuel supplied from an injection valve to an intake system in synchronization with engine rotation is calculated as a function of an intake air flow gutter. A reference value, which is a function of speed, is calculated from the detected engine rotational speed, and if the synchronous fuel injection amount is less than the reference value, fuel is cut off, and if the synchronous fuel injection amount is less than or equal to the reference value, fuel is taken into intake. A fuel cutoff device for an electronically controlled engine, characterized by supplying fuel to the system. 2. Claim 1, characterized in that the fuel injection pulse to be sent to the injection valve has a pulse width corresponding to the synchronous fuel injection amount, and the pulse width is compared with the reference value.
Fuel cutoff device as described in section. 3. The fuel cutoff device according to claim 1 or 2, wherein the reference value is set as a function that decreases as the engine rotational speed increases. 4 The reference value τcut is determined by the following formula % formula % Ne: engine rotation speed, K: positive constant, τcon
st: A constant. 4. The fuel cutoff device according to claim 3, wherein the fuel is discharged from the fuel cutoff device.
JP11839882A 1982-07-09 1982-07-09 Fuel cut device for electronically controlled engine Pending JPS5910747A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11839882A JPS5910747A (en) 1982-07-09 1982-07-09 Fuel cut device for electronically controlled engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11839882A JPS5910747A (en) 1982-07-09 1982-07-09 Fuel cut device for electronically controlled engine

Publications (1)

Publication Number Publication Date
JPS5910747A true JPS5910747A (en) 1984-01-20

Family

ID=14735672

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11839882A Pending JPS5910747A (en) 1982-07-09 1982-07-09 Fuel cut device for electronically controlled engine

Country Status (1)

Country Link
JP (1) JPS5910747A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61113941U (en) * 1984-12-26 1986-07-18

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5219821A (en) * 1975-08-08 1977-02-15 Nippon Denso Co Ltd Electronic control system fuel injection apparatus
JPS5618035A (en) * 1979-07-19 1981-02-20 Nissan Motor Co Ltd Fuel controller

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5219821A (en) * 1975-08-08 1977-02-15 Nippon Denso Co Ltd Electronic control system fuel injection apparatus
JPS5618035A (en) * 1979-07-19 1981-02-20 Nissan Motor Co Ltd Fuel controller

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61113941U (en) * 1984-12-26 1986-07-18
JPH0447400Y2 (en) * 1984-12-26 1992-11-09

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