JPS58135356A - Electronically controlled fuel injector for engine - Google Patents

Electronically controlled fuel injector for engine

Info

Publication number
JPS58135356A
JPS58135356A JP57017062A JP1706282A JPS58135356A JP S58135356 A JPS58135356 A JP S58135356A JP 57017062 A JP57017062 A JP 57017062A JP 1706282 A JP1706282 A JP 1706282A JP S58135356 A JPS58135356 A JP S58135356A
Authority
JP
Japan
Prior art keywords
fuel
engine
pressure
air
flow meter
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
JP57017062A
Other languages
Japanese (ja)
Inventor
Yoshiaki Asayama
浅山 嘉明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP57017062A priority Critical patent/JPS58135356A/en
Publication of JPS58135356A publication Critical patent/JPS58135356A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/16Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors
    • F02M69/18Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors the means being metering valves throttling fuel passages to injectors or by-pass valves throttling overflow passages, the metering valves being actuated by a device responsive to the engine working parameters, e.g. engine load, speed, temperature or quantity of air

Landscapes

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

Abstract

PURPOSE:To effectively correct even air-fuel ratios during high-land running period by correcting the dispersions of a vortex flow meter to detect the flow rate of intake air and also of fuel metering. CONSTITUTION:Fuel sent under pressure is injected into an air inlet pipe 3 syncyronously with the frequency output of a vortex flow meter 4. At the same time as current is supplied to a mobile coil 22 according to the output signals of an exhaust gas sensor 33, the output signals of a vortex flow meter 6 and a revolving number detector 31 are input, and the operating region of engine is judged. In such an electronic controller 34, air-fuel ratios are converted into fuel pressures by the output signals of the exhaust gas sensor 33 and controllably fed back to a nearly theoretical air-fuel ratio. The fuel pressure in the operation region of engine, where no feed-back control is made, is regulated and held at almost average value of the fuel pressure in the operation region where feed- back control is made, and thereby the dispersion in the amounts of fuel weighed can be corrected.

Description

【発明の詳細な説明】 この発明は自動車用内燃機関の電子制卸燃料噴射装置に
係り、特に機関の吸入空気型を便用する渦流量h1とこ
の渦流11計の周波数出力に同期し所定時1ハ1駆tl
U]さ口て士1己機関に燃料を供給する燃料噴射用電磁
弁と、この飴、(ミ弁に供給される燃料圧力を制御する
燃料圧力制御装置と、上記at関の排気ガス成分を検知
する排気センサを備え、上記機関の空燃比を上記排気セ
ンサの出力信号により上記燃料圧力を変えてほぼflj
I論空燃比にフィードバック制御するようにし、このフ
ィードバック制卸を行なわない機関の運転域における上
記燃料圧力はフィードバック制(111を行なっている
運転域における燃ね圧力のほぼ平均値に調整保持するこ
とにより、上記渦流量計ふ・よひ上記燃料噴射用電磁弁
による燃料計重のバラツキを補正し、また高地走行時の
ように大気圧力が変化した場合にも自動的に空燃比を補
正するようにした機関の電子制卸燃料噴射装置を提供す
るものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an electronically controlled fuel injection system for an internal combustion engine for automobiles, and in particular to an electronically controlled fuel injection system for an internal combustion engine, in particular, a vortex flow rate h1 which conveniently utilizes the intake air type of the engine, and a vortex flow rate h1 that is synchronized with the frequency output of this vortex flow meter at a predetermined time. 1ha 1wd tl
U] A solenoid valve for fuel injection that supplies fuel to the engine, this candy, a fuel pressure control device that controls the fuel pressure supplied to the mi-valve, and the exhaust gas components of the above AT The air-fuel ratio of the engine is adjusted to approximately flj by changing the fuel pressure according to the output signal of the exhaust sensor.
Feedback control is applied to the air-fuel ratio of I theory, and the fuel pressure in the operating range of the engine where this feedback control is not performed is adjusted and maintained at approximately the average value of the fuel pressure in the operating range where feedback control (111) is performed. The above-mentioned vortex flow meter corrects the variation in fuel weight due to the above-mentioned fuel injection solenoid valve, and also automatically corrects the air-fuel ratio when atmospheric pressure changes such as when driving at high altitudes. The present invention provides an electronic control fuel injection system for an engine that has been developed.

衆知のように渦流量計は計測すべき吸入空気の体槓流凰
に比例する高速度(渦発生数)に対応した周波数の出力
が得ら口る。この吸入空気量(に比例した周波数出力に
同期して一定量の燃料を機関に噴射供給する方法は、機
関の加速時における急檄な吸入空気量の変化に追従して
燃料を噴射することができるので上記機関は加速性能の
優J’したものとなる特長を有している。ところで高地
走行]I41のように大気圧が低下する場合、あるいは
上記吸入空気の温度が変わる場合は、上記渦流、1計の
出力は上記大気圧あるいは温度に応じて補正する必要が
あるので上記大気圧を検知する大気圧検出器および吸入
空気検出器が必要となる。
As is well known, a vortex flowmeter produces an output at a frequency corresponding to a high velocity (vortex generation number) that is proportional to the body flow rate of the intake air to be measured. This method of injecting and supplying a constant amount of fuel to the engine in synchronization with the frequency output proportional to the intake air amount () makes it possible to inject fuel to follow sudden changes in the intake air amount when the engine accelerates. Therefore, the above-mentioned engine has the feature of having excellent acceleration performance.By the way, when the atmospheric pressure decreases as in I41 when driving at high altitude, or when the temperature of the above-mentioned intake air changes, the above-mentioned vortex flow , 1 meter output needs to be corrected according to the atmospheric pressure or temperature, so an atmospheric pressure detector and an intake air detector are required to detect the atmospheric pressure.

この発明はこのような大気圧検出器および吸入空気検出
器が無くても上記機関の空燃比を所定値に保つようにし
たものである。
This invention maintains the air-fuel ratio of the engine at a predetermined value even without such an atmospheric pressure detector and an intake air detector.

以下、図に不すこの発明の一実施例について説明する。An embodiment of the present invention not shown in the drawings will be described below.

図中、(1)は機関、(2)は目動車のアクセルペダル
に連動したスロットル弁、(3)は吸気管、(4)は上
記機関(1)に吸入さ口る吸入空気量を検出する渦#L
鍬計、(5)は燃料噴射用電磁弁であり、圧送されてく
る燃料を上記渦流量計(4)の周波数出力に同期して上
記吸気管(3)内に噴射する。(6〕は上記電磁弁(5
)を上記周波数出力に同期して所定時間するit!、磁
弁駆動装置fi、(7)はエアクリーナ、(8)は該エ
アクリーナ(7)内に収納さ第1たクリーナエレメント
(′oM紙)、(9)は燃料タンク、(11は燃料ポン
プでありその吸入側はバイブ0υにより上記燃料タンク
(9)に結合しである。(12は上記燃料ポンプ0(j
の吐出側に結合したバイブ、02やは燃料圧力制仰装誼
である。04)は該燃料圧力調整室*、 O’Wlの本
体ケースであシ、上記バイブQ功に結合した燃粋1圧力
調整室(14a)を構成している。この燃料圧力高1整
室(14a)はバイブaGで十配燃料噴射用電磁弁(5
ンに連通している。OQは上記燃料圧力制御装置03の
差汁調整冨(16a)を描成するケースで舌)シバイブ
0ηによシ上記吸気管(3)内に連通している。081
はスプリング、ag)はダイアフラムであり、上記燃料
圧力調整室(14a )と上記差圧調整室(16a)を
区画している。α))は圧力調整弁であり、上記ダイア
フラム09に一体的に取付けら口ている。Qυは上記本
体ケース041に同右さ口ているモータケース、(2)
は可動コイルであり、永久磁石(2)とコア曽、ヨーク
(7)と共に衆知のりニアモータを構成している。(4
)は上記本体ケース(+4)に対して気密を保って貴通
し摺動自在に設けられた圧力制@10ツドであり、アー
ム勾を介して上記可動コイル(イ)が連結しており、こ
のiJ動コイル(2)の移動に従って矢印の方向に移動
するように描成さ口ている。また上記圧力制御ロッド(
ホ)は中空となっており、その一端は上記圧力調整弁−
に当接し、該圧力調整弁−と共に上記圧力謔整室(14
a)内の燃料圧力を制御する作用をする。−万他畑は伸
縮自在のジャバラ(ハ)を介してバイブ(2)に連結し
ており、さらに上記燃料タンク(9)に連通している。
In the figure, (1) is the engine, (2) is the throttle valve linked to the accelerator pedal of the moving vehicle, (3) is the intake pipe, and (4) is the detection of the amount of intake air taken into the engine (1). Whirlpool #L
The hoe meter (5) is a solenoid valve for fuel injection, which injects the pressure-fed fuel into the intake pipe (3) in synchronization with the frequency output of the vortex flow meter (4). (6) is the above solenoid valve (5)
) for a predetermined period of time in synchronization with the above frequency output! , magnetic valve drive device fi, (7) is an air cleaner, (8) is a first cleaner element ('oM paper) housed in the air cleaner (7), (9) is a fuel tank, (11 is a fuel pump) Its suction side is connected to the fuel tank (9) by a vibrator 0υ. (12 is the fuel pump 0(j
The vibrator 02 connected to the discharge side of the fuel pressure control device is a fuel pressure control device. 04) is the main body case of the fuel pressure adjustment chamber*, O'Wl, and constitutes the fuel 1 pressure adjustment chamber (14a) connected to the vibe Q-gong. This fuel pressure high 1 adjustment chamber (14a) is a 10-distribution fuel injection solenoid valve (5
It communicates with the OQ communicates with the air intake pipe (3) through the air pressure control unit (16a) of the fuel pressure control device (03). 081
is a spring, and ag) is a diaphragm, which partitions the fuel pressure adjustment chamber (14a) and the differential pressure adjustment chamber (16a). α)) is a pressure regulating valve, which is integrally attached to the diaphragm 09. Qυ is the motor case that is opened to the right of the main body case 041 above, (2)
is a moving coil, which together with a permanent magnet (2), a core and a yoke (7) constitutes a well-known linear motor. (4
) is a pressure control @10 which is installed in the main body case (+4) so as to be able to slide freely through the main body case (+4) while maintaining airtightness. It is drawn to move in the direction of the arrow as the iJ moving coil (2) moves. In addition, the above pressure control rod (
E) is hollow, and one end of it is connected to the pressure regulating valve -
and the pressure regulating chamber (14) together with the pressure regulating valve.
a) acts to control the fuel pressure in the - The mandai field is connected to the vibrator (2) via a telescopic bellows (c), and further communicates with the fuel tank (9).

G[jはスプリングである。6υは上記機関(1)の回
転数便用器、曽は排気管、冑は排気センサであり上記機
関(1)の排気ガス成分を検知し1、¥質的に上記機関
(1)の運転窄燃比を押出する。図は上記排気ナンサ曽
の出力信号に対応してL記可動コイル(2)に石、流を
供・給すると同時に上記渦流量計(6)および回1獣数
棟出器6υの出力信号を入力し上記機関(1)の運転域
を判別する電子制御装置である。
G[j is a spring. 6υ is the rotation speed toilet of the engine (1), Z is the exhaust pipe, and 充 is the exhaust sensor that detects the exhaust gas components of the engine (1). Push out a narrow fuel ratio. The figure shows that stones and flow are supplied to the movable coil (2) in accordance with the output signal of the above-mentioned exhaust nancer, and at the same time, the output signal of the above-mentioned vortex flow meter (6) and the 1st number feeder 6υ is supplied. This is an electronic control device that inputs information and determines the operating range of the engine (1).

以上のように構成さJ’した装置の動作について説1明
する。ます、m l!I (1)が始M i rすると
吸入空気はエアクリーナ(7)をJJ3]す、’lt+
jA fir、1計(4)内に入り該渦流量計(4)に
より吸入空費(搬が検出さ■て吸気管(3)から上記機
関(1)に導入さfしる。−万、燃料タンク(9)内の
燃料は燃料ポンプOQによ多燃料圧力調整室(Ha)に
圧送さtする。託送された燃料の圧力が所定値以上にな
るとダイアフラムαつに加わる力が増大し、スプリング
θ〜の力に抗して該スプリングQ81を圧縮する方間に
上記タイアフラムα鋳が移動する。
The operation of the apparatus configured as described above will now be described. Masu, m l! When I (1) starts, the intake air passes through the air cleaner (7).
The air enters the engine (4) and is detected by the vortex flowmeter (4) and introduced into the engine (1) from the intake pipe (3). The fuel in the fuel tank (9) is pressure-fed to the fuel pressure adjustment chamber (Ha) by the fuel pump OQ.When the pressure of the delivered fuel exceeds a predetermined value, the force applied to the diaphragm α increases, The tire flamm α cast moves in a direction that compresses the spring Q81 against the force of the spring θ~.

この時圧力調整弁いルは圧力制御ロッド翰から都nる。At this time, the pressure regulating valve is removed from the pressure control rod.

そして畠圧の燃料は上記圧力制御ロッド翰の中空部から
−L記燻料タンク(99に溢流し上記圧力調整’4(1
4a)円の圧力をドける。圧力が下がると再ひ上記圧力
調整弁い勿か上記圧力制御ロッド(イ)に当接し、中空
部は開じらjLる。このような上記圧力、iI+!+l
整弁翰の開閉動作により上記圧力調整室(14a)の燃
料圧力がはは−正に保たれる。調圧された燃利はバイ1
0句から燃料噴射用電磁弁(5)に供給灯れ吸気%l′
(3)内に噴射される。この燃オコ[が噴射さイ]、る
吸気室(3)内の圧力を基準として上記燃料注力をeS
tは一定に保つために、上記吸気管(3)内の圧力を差
圧調整室(16a、)に導き、上記タイアフラム(l!
Jlに作用させている。以上の動作は従来装置と同様で
ある。上ril:!燃N I+@射用石′6イ社弁(5
)は石、磁弁1[1tlt装置M (61により上記渦
流量計(4)の周波数出力に同期してRr定時間駆動さ
口て燃料を噴射する。他方、ffjl気センサ曽の出力
信号を入力した゛申子制伺1装血C匈は上記出力信号に
対応した石、流を可動コイル(4)に供給し、この’r
4=’、 tAi It良Vこ応じて上記圧力制伸ロッ
ド翰が移動する。その結果圧力9M整弁い夛と上記圧力
制σ410ッド呟1が当接する位置が変わシ、圧力調整
室(14a)内の燃料圧力が変更きねる。すなわち上記
燃相唱射用−値弁(5)に供給さ口る燃料噴射圧力が変
史さ口噴射さ口る燃料量が制伺1される。この制御は上
記機関(υの運転空燃比かほぼ理論空燃比になるように
、上記排気センサ曽の出力信号によりフィードバック制
$1される。このフィードバック8ill 1ffll
lが行なわ口ている上記機関(1)の運転域では実質的
に上記渦流鼠gf(4)に尋人される吸入空気の大気j
土、温度および該渦流量計(4)と燃料lI!を射用石
5磁弁(5)による燃料針足のバラツキ等を運転空燃比
がほぼ理論空燃比となるように上記燃料圧力を変えて袖
正しているのである。したがって上記フィードバック制
御が行なわれている運転状態での上記燃料圧力は上記燃
ネ+#1重のバラツキ等を総合的に?+ti正したもの
である。−ト記連軌状態の燃料圧力に調整するのに必要
なp(動コイル(イ)に供給される電流値は石、千制仰
装置M(ロ)に記憶さ口る。そして、上記機関(1)が
高速運転域となり上記渦流重訂(4)の出力信号と同転
数検出’a’、31)の出力信号が所定値に達すると上
d己フィードバンクl用641は停止妊口る。そして、
このようなフィードバック制伺1を行なわない運転域で
の運転空燃比は上記理論空燃比以外の所望の空燃比で運
転さ口る。この時の上記燃料圧力は上記フィードバック
制御1111を行なっていた時に上記電子側(i11装
置C陣に記憶さ口た電流値が可動コイル(イ)に供給さ
It上記フィードバック制#Jを行なっていた運転域で
の燃料圧力のほぼ平均(ulに保持さ口る。すなわち上
記フィードバック制御を行なわない高速運転域において
も上記燃料針足のバラツキ等を抽圧するのである。
Then, the fuel under the pressure control rod overflows from the hollow part of the pressure control rod into the smoke tank (99) and the pressure adjustment '4 (1).
4a) Apply circular pressure. When the pressure decreases, the pressure regulating valve again comes into contact with the pressure control rod (a), and the hollow part is not opened. Such the above pressure, iI+! +l
The fuel pressure in the pressure adjustment chamber (14a) is maintained at a positive level by opening and closing the valve control rod. The regulated fuel is by 1
From the 0th clause, the fuel injection solenoid valve (5) is supplied with the intake air %l'
(3) Injected within. This fuel injection is based on the pressure in the intake chamber (3), and the above fuel concentration is eS.
In order to keep t constant, the pressure in the intake pipe (3) is guided to the differential pressure adjustment chamber (16a,), and the tire flamm (l!
It is acting on Jl. The above operation is similar to that of the conventional device. Upper ril:! MoN I+ @ shooting stone'6 ishaben (5
) is a stone, magnetic valve 1 [1tlt device M (61) drives Rr for a fixed time in synchronization with the frequency output of the vortex flow meter (4) and injects fuel.On the other hand, the output signal of the ffjl gas sensor The input ``Shinshi control signal 1 blood supply C'' supplies stones and streams corresponding to the above output signal to the movable coil (4), and this 'r
4=', tAi It is good. Accordingly, the pressure-reducing rod holder moves. As a result, the contact position of the pressure 9M valve regulator and the pressure regulator σ410 valve 1 changes, and the fuel pressure in the pressure adjustment chamber (14a) changes. In other words, the fuel injection pressure supplied to the fuel phase injection value valve (5) changes and the amount of fuel injected is controlled. This control is controlled by feedback control based on the output signal of the exhaust sensor so that the operating air-fuel ratio of the engine (υ) becomes approximately the stoichiometric air-fuel ratio.This feedback 8ill 1ffll
In the operating range of the engine (1) where the engine (1) is being operated, the atmosphere of the intake air flowing into the whirlpool gf (4) is substantially
Soil, temperature and the vortex flow meter (4) and fuel lI! Variations in the fuel needle due to the injection stone 5 solenoid valve (5) are corrected by changing the fuel pressure so that the operating air-fuel ratio becomes approximately the stoichiometric air-fuel ratio. Therefore, in the operating state where the feedback control is performed, is the fuel pressure determined by taking into account the fuel pressure + #1 weight variation, etc.? +ti corrected. - The current value supplied to the moving coil (A) necessary to adjust the fuel pressure in the continuous state is stored in the mechanical control device M (B). (1) becomes a high-speed operation region, and when the output signal of the above-mentioned eddy current correction (4) and the output signal of the same rotation speed detection 'a', 31) reach a predetermined value, the upper d self feed bank l 641 stops. Ru. and,
The operating air-fuel ratio in the operating range where such feedback control 1 is not performed is determined at a desired air-fuel ratio other than the stoichiometric air-fuel ratio. At this time, the fuel pressure was determined by the current value stored in the electronic side (i11 device C group) when the feedback control 1111 was being performed, and the current value stored in the C group of the electronic side (i11) was supplied to the movable coil (a), and the feedback control #J was being performed. The fuel pressure in the operating range is maintained at approximately the average (ul). That is, even in the high-speed operating range where the feedback control is not performed, variations in the fuel pressure are eliminated.

以上のようにこの発明は機関の吸入空気坦を検出する渦
流量計とこの渦流量計の周波数出力に同期し所定時間駆
動さ口て上記機関に燃料を供給する燃料噴射用電磁弁と
、この市、母方に供給される燃料圧力を?Id制御する
燃料圧力制御装置と、上記機関の排気ガス成分を便知す
る排気センサを備え、上記機関の空燃比を上記排気セン
サの出力信号により上記燃料圧力を変えて、はぼ理論空
燃比にフィードバック制御するようにし、このフィード
バック制御を行なわない機関の運転域における上記燃料
圧力はフィードバック開側1を行なっている運転域にお
ける燃料圧力のほぼ平均値に謔整保持することにより、
上記機関の全運転域において、」―記簡流加−計および
燃料噴射用電磁弁による燃料針足のバラツキを袖正し、
また尚地走行時のように大気圧力が変化した場合にも目
動的に空燃比を抽圧することができるのである。
As described above, the present invention includes a vortex flowmeter for detecting the level of intake air of an engine, a fuel injection solenoid valve that is synchronized with the frequency output of the vortex flowmeter and is driven for a predetermined period of time to supply fuel to the engine, and City, the fuel pressure supplied to the maternal side? A fuel pressure control device for Id control and an exhaust sensor for detecting exhaust gas components of the engine are provided, and the air-fuel ratio of the engine is changed to the stoichiometric air-fuel ratio by changing the fuel pressure according to the output signal of the exhaust sensor. Feedback control is performed, and the fuel pressure in the operating range of the engine where this feedback control is not performed is adjusted and maintained at approximately the average value of the fuel pressure in the operating range where feedback opening side 1 is performed.
In all operating ranges of the above engine, the fluctuations in the fuel needle due to the flow meter and fuel injection solenoid valve are corrected.
Furthermore, even when the atmospheric pressure changes, such as when the vehicle is driving in a rural area, it is possible to manually extract the air-fuel ratio.

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

図はこの発明の一′:#旌例を示す構成図である。 図中、(1)は機関、(4)は渦流重訂、(5)は燃料
噴射用電磁弁、(7)はエアクリーナ、QCIはfPN
f+ポンプ、Qニヤは燃料圧力制伸装誼、(幻は排気セ
ンサ、(ロ)は電子制御製電である。
The figure is a block diagram showing one example of this invention. In the figure, (1) is the engine, (4) is the vortex revision, (5) is the fuel injection solenoid valve, (7) is the air cleaner, and QCI is fPN.
F + pump, Q near are fuel pressure control equipment, (phantom is exhaust sensor, (b) is electronically controlled electrical equipment.

Claims (1)

【特許請求の範囲】[Claims] 機関の吸入空気流重に応じて高速度に対応した周波数の
出力を発生して上記吸入空気流i1を検知する渦流量計
と、該渦流量計の周波数出力に同期し所定時間駆動さ口
て上記機関に燃料を供給する燃料噴射用*i弁と、該電
磁弁に燃料を圧送する燃料ポンプと、該圧送さ口る燃料
の燃ネデ1汁力を制卸する燃料圧力制御1141装置と
、−に組機W−1の排気ガス成分を検知する排気センサ
を備え、」−rIL!機関の草燃比を上記排気センサの
出力伯月により上記燃ネ・)圧力を変えてほぼ理論空燃
比にフィードバック制御するようにした上記機関の電子
制佃I燃料噴射装置において、上記フィードバック制卸
を行なわない上記機関の運転域における上記燃もi圧力
は上記フィードバック側倒1を行なっている連軌域斡二
おける燃料圧力のほぼ平均値に調整保持さ口ることを待
機とする機関の市、子制御燃料噴射装置。
a vortex flow meter that detects the intake air flow i1 by generating an output with a frequency corresponding to high speed according to the intake air flow weight of the engine; A fuel injection *i valve that supplies fuel to the engine, a fuel pump that pumps fuel to the solenoid valve, and a fuel pressure control device 1141 that controls the fuel pressure of the pumped fuel. , - is equipped with an exhaust sensor for detecting exhaust gas components of assembly machine W-1, and "-rIL! In the electronically controlled fuel injection system for the engine, the air-fuel ratio of the engine is feedback-controlled to approximately the stoichiometric air-fuel ratio by changing the air-fuel pressure according to the output ratio of the exhaust sensor. The fuel pressure in the operating range of the engine in which the feedback is not performed is adjusted to approximately the average value of the fuel pressure in the linked rail region in which the feedback is performed, and the engine is on standby. Child-controlled fuel injection system.
JP57017062A 1982-02-04 1982-02-04 Electronically controlled fuel injector for engine Pending JPS58135356A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57017062A JPS58135356A (en) 1982-02-04 1982-02-04 Electronically controlled fuel injector for engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57017062A JPS58135356A (en) 1982-02-04 1982-02-04 Electronically controlled fuel injector for engine

Publications (1)

Publication Number Publication Date
JPS58135356A true JPS58135356A (en) 1983-08-11

Family

ID=11933494

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57017062A Pending JPS58135356A (en) 1982-02-04 1982-02-04 Electronically controlled fuel injector for engine

Country Status (1)

Country Link
JP (1) JPS58135356A (en)

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