JPH0617653B2 - Fuel injection control device - Google Patents
Fuel injection control deviceInfo
- Publication number
- JPH0617653B2 JPH0617653B2 JP59141408A JP14140884A JPH0617653B2 JP H0617653 B2 JPH0617653 B2 JP H0617653B2 JP 59141408 A JP59141408 A JP 59141408A JP 14140884 A JP14140884 A JP 14140884A JP H0617653 B2 JPH0617653 B2 JP H0617653B2
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- fuel injection
- flow rate
- injection pump
- control valve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1813—Discharge orifices having different orientations with respect to valve member direction of movement, e.g. orientations being such that fuel jets emerging from discharge orifices collide with each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
- F02D1/02—Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
- F02D1/08—Transmission of control impulse to pump control, e.g. with power drive or power assistance
-
- 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
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/40—Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
- F02D41/401—Controlling injection timing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M41/00—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
- F02M41/08—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
- F02M41/10—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined pump pistons acting as the distributor
- F02M41/12—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined pump pistons acting as the distributor the pistons rotating to act as the distributor
- F02M41/123—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined pump pistons acting as the distributor the pistons rotating to act as the distributor characterised by means for varying fuel delivery or injection timing
- F02M41/125—Variably-timed valves controlling fuel passages
- F02M41/126—Variably-timed valves controlling fuel passages valves being mechanically or electrically adjustable sleeves slidably mounted on rotary piston
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M55/00—Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
- F02M55/02—Conduits between injection pumps and injectors, e.g. conduits between pump and common-rail or conduits between common-rail and injectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/182—Discharge orifices being situated in different transversal planes with respect to valve member direction of movement
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- High-Pressure Fuel Injection Pump Control (AREA)
- Fuel-Injection Apparatus (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明はディーゼルエンジン等内燃機関に用いられる燃
料噴射制御装置に関する。The present invention relates to a fuel injection control device used in an internal combustion engine such as a diesel engine.
[従来の技術] 従来より、噴射ポンプから燃料を圧送し、噴射ノズルで
エンジンシリンダ内に燃料を噴射する燃料噴射装置で、
低回転・低負荷時の噴射燃料の微粒化対策として、噴射
口断面積を可変とするスロットル機関付き噴射ノズルを
用いた燃料噴射制御装置が提案されている。また、燃料
噴射弁の圧力を制御するという意味では実開昭58−8
1375号の燃料噴射弁等が提案されている。[Prior Art] Conventionally, in a fuel injection device that pumps fuel from an injection pump and injects the fuel into an engine cylinder with an injection nozzle,
A fuel injection control device using an injection nozzle with a throttle engine having a variable injection port cross-sectional area has been proposed as a measure against atomization of injected fuel at low rotation speed and low load. Also, in the sense that the pressure of the fuel injection valve is controlled
No. 1375 fuel injection valve and the like have been proposed.
[発明が解決しようとする課題] しかし、前記スロットル機関付き噴射ノズルでは、その
噴射装置の構成、つまり、噴射ポンプで燃料を調量・圧
送して噴射ノズルから噴射させる方法では、おのずと回
転数と負荷によって、噴射ノズルから噴射される燃料の
噴射圧力が大きく変化してしまい、スロットル機構が有
効に作用する範囲が限定され、特に、極低回転・低負荷
時には、噴射ポンプで圧縮圧送される燃料の圧力が十分
に上昇せず、噴霧の流出速度が落ち、噴射燃料の微粒化
不足から、排出HCが多量に発生するという欠点があっ
た。また、実開昭58−81375号の燃料噴射弁は、
噴射圧力の上り過ぎを防止するものであり、下がり過ぎ
を問題とする本発明の問題点を解決するものではなかっ
た。[Problems to be Solved by the Invention] However, in the injection nozzle with the throttle engine, in the configuration of the injection device, that is, in the method of injecting fuel from the injection nozzle by metering and pressure-feeding the fuel with the injection pump, the number of revolutions is naturally increased. The load changes the injection pressure of the fuel injected from the injection nozzle significantly, limiting the range in which the throttle mechanism works effectively. Especially, at the time of extremely low rotation and low load, the fuel compressed by the injection pump is sent. However, there is a drawback that a large amount of exhausted HC is generated due to insufficient increase in the pressure of No. 3, the decrease in the outflow rate of the spray, and insufficient atomization of the injected fuel. In addition, the fuel injection valve of Jiukai Sho 58-81375 is
The purpose of the present invention is to prevent the injection pressure from rising too high, and it has not solved the problem of the present invention in which the pressure is too low.
本発明の目的は、機関の極低回転、低負荷においても、
噴射燃料を十分に微粒化し、HCの排出を抑制すると同
時に、安定した燃焼を得ることができる燃料噴射制御装
置を提供することにある。The object of the present invention is to achieve extremely low engine speed and low load.
It is an object of the present invention to provide a fuel injection control device capable of sufficiently atomizing the injected fuel, suppressing the discharge of HC, and obtaining stable combustion.
[課題を解決するための手段] この目的を達成する本発明の燃料噴射制御装置は、次の
装置から成る。すなわち、 燃料タンクと、吸入口と吐出口を有し吸入口が前記燃料
タンクと接続され吐出口から燃料を高圧で送出する燃料
噴射ポンプと、該燃料噴射ポンプの吐出口と接続されニ
ードル先端円錐部と前記円錐部に当接するノズルボディ
の内周円錐部とによって形成されるシート部と該シート
部に開口し前記ニードル上昇時に前記シート部を前記燃
料噴射ポンプをバイパスして前記燃料タンクへと連通す
るバイパス通路とを有する燃料噴射ノズルと、前記燃料
噴射ノズルのバイパス通路と前記燃料タンクとを連通す
る通路上に設けられた流量制御弁と、機関の負荷検出手
段と、機関のまたは前記燃料噴射ポンプの回転数検出手
段と、前記燃料噴射ポンプに設けられた送出燃料流量調
節手段及び流量検出手段と、前記流量制御弁に設けられ
た該流量制御弁の調節手段及び流量検出手段と、前記燃
料噴射ポンプの送出燃料流量調節手段及び流量検出手段
と前記流量制御弁の調節手段及び流量検出手段に電気的
に接続されたマイクロコンピュータと、から成り、機関
の負荷状態及び機関または燃料噴射ポンプの回転数に応
じて前記燃料噴射ポンプの流量調節と前記流量制御弁の
流量調節を前記マイクロコンピュータにて行うようにし
たものから成る。[Means for Solving the Problems] A fuel injection control device of the present invention that achieves this object includes the following device. That is, a fuel tank, a fuel injection pump having an inlet and an outlet, the inlet being connected to the fuel tank and delivering fuel at high pressure from the outlet, and a needle tip cone connected to the outlet of the fuel injection pump. And a seat formed by an inner peripheral conical part of the nozzle body that abuts on the conical part and the seat is opened to the seat when the needle rises and bypasses the fuel injection pump to the fuel tank. A fuel injection nozzle having a bypass passage communicating with the fuel injection nozzle, a flow control valve provided on a passage communicating the bypass passage of the fuel injection nozzle with the fuel tank, a load detecting means of the engine, the engine or the fuel. An injection pump rotation speed detecting means, a delivery fuel flow rate adjusting means and a flow rate detecting means provided in the fuel injection pump, and the flow provided in the flow rate control valve. A quantity control valve adjusting means and a flow rate detecting means; a delivery fuel flow rate adjusting means and a flow rate detecting means of the fuel injection pump; and a microcomputer electrically connected to the flow rate control valve adjusting means and the flow rate detecting means. The flow control of the fuel injection pump and the flow control of the flow control valve are performed by the microcomputer according to the load condition of the engine and the rotation speed of the engine or the fuel injection pump.
[作用] 上記本発明の装置においては、エンジンの低回転数時及
び低負荷時においても、燃料噴射ポンプを全負荷運転す
ると共に、バイパス通路を通って逃げる燃料量を制御す
ることにより、高圧燃料を送供する燃料噴射ポンプの圧
送圧力を、回転数、負荷に関係なく、十分に高めること
ができ、噴射燃料の微粒化が改善されることによって、
排出HCの低減が可能になる。[Operation] In the above-described device of the present invention, the high-pressure fuel is controlled by operating the fuel injection pump at full load and controlling the amount of fuel escaping through the bypass passage even at low engine speed and low load. The pressure-feeding pressure of the fuel injection pump that delivers the fuel can be sufficiently increased regardless of the number of rotations and the load, and atomization of the injected fuel is improved,
It is possible to reduce the exhausted HC.
[実施例] 以下本発明の望ましい実施例を図面を参照して説明す
る。[Embodiment] A preferred embodiment of the present invention will be described below with reference to the drawings.
第1図は本発明の電子制御燃料噴射装置を示したもの
で、1は燃料タンク、2は燃料タンク1からの燃料をパ
イプ28を介して吸入し高圧圧送する電子制御燃料噴射
ポンプである。燃料噴射ポンプ2内には、燃料を高圧圧
送するプランジャ3と、該プランジャで圧送される燃料
量を調節するスピルリング4が組込まれる。このスピル
リング4は支点6を支点にしたレバー5でプランジャ3
の軸上を平行移動する。レバー5の上端は、リニアソレ
ノイド7に当接しており、リニアソレノイド7の動きに
よってスピルリング4の移動量が決定される。さらに8
のスピル位置センサによってその移動量が検出される。
検出された信号は信号線35によってマイクロコンピュ
ータ25に伝えられる。又、プランジャ3と同軸上にギ
ア9が取り付けられ、回転数センサ10によって、回転
数が検出される。回転数センサ10の信号は信号線34
によってマイクロコンピュータ25に伝えられる。燃料
噴射ポンプ2の吐出口11はパイプ29を介して燃料噴
射ノズル12につながっている。FIG. 1 shows an electronically controlled fuel injection device according to the present invention. Reference numeral 1 is a fuel tank, and 2 is an electronically controlled fuel injection pump that sucks fuel from the fuel tank 1 through a pipe 28 and sends it under high pressure. In the fuel injection pump 2, a plunger 3 for pressure-feeding fuel and a spill ring 4 for adjusting the amount of fuel pressure-fed by the plunger are incorporated. This spill ring 4 is a lever 5 with a fulcrum 6 as a fulcrum, and a plunger 3
Translate on the axis of. The upper end of the lever 5 is in contact with the linear solenoid 7, and the movement amount of the spill ring 4 is determined by the movement of the linear solenoid 7. 8 more
The spill position sensor detects the amount of movement.
The detected signal is transmitted to the microcomputer 25 by the signal line 35. Further, a gear 9 is mounted coaxially with the plunger 3, and a rotation speed sensor 10 detects the rotation speed. The signal of the rotation speed sensor 10 is the signal line 34.
Is transmitted to the microcomputer 25. The discharge port 11 of the fuel injection pump 2 is connected to the fuel injection nozzle 12 via a pipe 29.
この噴射ポンプ2から圧送された燃料を噴射する燃料噴
射ノズル12は、ノズルボディ13とニードル14から
成っており、その先端には噴孔16が開口し、ニードル
14の先端とノズルボディ13の当接によって形成され
るシート部15によって、図示しないばねによってニー
ドル14が通常図中下方に付勢され、その密封を保持し
ている。燃料の供給は、連通路19を介して燃料供給通
路17に行なわれるが、ニードル14が上昇すると、ニ
ードル14の軸中心に開口する燃料バイパス通路18と
も連通し、連通路20にも燃料が満たされる。The fuel injection nozzle 12 for injecting the fuel pumped from the injection pump 2 is composed of a nozzle body 13 and a needle 14. An injection hole 16 is opened at the tip of the fuel injection nozzle 12, and the tip of the needle 14 and the nozzle body 13 come into contact with each other. By the seat portion 15 formed by the contact, the needle 14 is normally urged downward in the drawing by a spring (not shown), and the sealing is maintained. The fuel is supplied to the fuel supply passage 17 through the communication passage 19. When the needle 14 rises, the fuel is also communicated with the fuel bypass passage 18 that opens in the axial center of the needle 14, and the communication passage 20 is also filled with the fuel. Be done.
第2図でノズル先端の詳細構造を説明すると、燃料噴射
ノズル12の先端のノズルボディ13には、ニードル1
4が挿入され、その先端円錐部40に当接するように、
ノズルボディ13にも内周円錐部41が形成され、噴口
16と、燃料供給通路17の燃料を遮断するシート部1
5が形成される。ニードル14の中心には燃料バイパス
通路18が軸に平行に貫通し、その末端は連通路39に
開口する。連通路39はシート部15に向って開口して
おり、ニードル14がシート部15に密着閉塞している
時は、燃料供給通路17及び噴口16のいずれとも連通
することはないが、ニードル14が上昇してシート部1
5が開放されると、連通路39は燃料供給通路17及び
噴口16と連通し、バイパス通路18とも連通する。The detailed structure of the nozzle tip will be described with reference to FIG. 2. The needle 1 is attached to the nozzle body 13 at the tip of the fuel injection nozzle 12.
4 is inserted and touches the tip conical portion 40,
An inner peripheral conical portion 41 is also formed in the nozzle body 13, and the seat portion 1 that shuts off the fuel in the injection port 16 and the fuel supply passage 17 is formed.
5 is formed. A fuel bypass passage 18 passes through the center of the needle 14 in parallel with the axis, and its end opens into a communication passage 39. The communication passage 39 opens toward the seat portion 15, and when the needle 14 is tightly closed to the seat portion 15, it does not communicate with either the fuel supply passage 17 or the injection port 16, but the needle 14 Seat part 1
When 5 is opened, the communication passage 39 communicates with the fuel supply passage 17 and the injection port 16, and also communicates with the bypass passage 18.
第2図(ロ)は別の態様に係るノズル先端の構造を示し
ている。本態様では、燃料バイパス通路18がノズルボ
ディ13中に形成されている。39は連通路、39a、
39bは通路を形成するためのめくら栓である。FIG. 2B shows the structure of the nozzle tip according to another aspect. In this aspect, the fuel bypass passage 18 is formed in the nozzle body 13. 39 is a communication passage, 39a,
39b is a blind plug for forming a passage.
以上のようなノズル構造を有する燃料噴射ノズル12の
燃料バイパス通路18は、第1図に示すように、連通路
20に接続され、パイプ30で、バイパス弁21に導か
れる。バイパス弁21は流路断面積を可変にできる流量
制御式弁よりなっている。バイパス弁21でバイパスさ
れた燃料はパイプ31を通って燃料タンク1に戻され
る。又、バイパス弁21は、電流値変化によってその吸
収力を自在に変化しうるリニアソレノイド23にロッド
22によって連結される。24はロッド位置センサであ
り、バイパス弁21の変化量を信号線36を介してマイ
クロコンピュータ25に伝達する役目をする。As shown in FIG. 1, the fuel bypass passage 18 of the fuel injection nozzle 12 having the above-described nozzle structure is connected to the communication passage 20 and guided to the bypass valve 21 by the pipe 30. The bypass valve 21 is composed of a flow rate control valve capable of varying the flow passage cross-sectional area. The fuel bypassed by the bypass valve 21 is returned to the fuel tank 1 through the pipe 31. Further, the bypass valve 21 is connected by a rod 22 to a linear solenoid 23 whose absorption force can be freely changed by changing the current value. Reference numeral 24 denotes a rod position sensor, which serves to transmit the amount of change of the bypass valve 21 to the microcomputer 25 via the signal line 36.
26は、アクセルペダルでその動きはワイヤー32でア
クセル開度センサ27に伝えられ、電気信号に変換後信
号線33でマイクロコンピュータ25に伝達される。Reference numeral 26 denotes an accelerator pedal, the movement of which is transmitted to the accelerator opening sensor 27 by a wire 32 and is transmitted to the microcomputer 25 by a signal line 33 after being converted into an electric signal.
マイクロコンピュータ25の出力信号は、信号線37,
38を介してそれぞれ燃料噴射ポンプ2のリニアソレノ
イド7およびバイパス弁21のリニアソレノイド23に
送られ、それぞれの流量を制御する。The output signal of the microcomputer 25 is the signal line 37,
They are sent to the linear solenoid 7 of the fuel injection pump 2 and the linear solenoid 23 of the bypass valve 21 via 38 to control the respective flow rates.
以下作用を説明する。The operation will be described below.
燃料は、燃料タンク1から、パイプ28で燃料噴射ポン
プ2に供給され、プランジャ3で高圧圧縮された後、吐
出口11よりパイプ29で噴射ノズル12に供給され
る。連通路19、燃料供給通路17に充満した燃料によ
って、ニードル14にかかる圧力が上昇してばねに抗し
てニードル14が上昇すると、シート部15が開放さ
れ、噴口16から燃料が噴射される。同時に、燃料バイ
パス通路18にも高圧の燃料が供給され、連通路20を
介してパイプ30でバイパス弁21に導入され、流量調
節後パイプ31で再び燃料タンク1に戻される。The fuel is supplied from the fuel tank 1 to the fuel injection pump 2 via the pipe 28, compressed to a high pressure by the plunger 3, and then supplied from the discharge port 11 to the injection nozzle 12 via the pipe 29. When the pressure applied to the needle 14 increases due to the fuel filled in the communication passage 19 and the fuel supply passage 17 and the needle 14 rises against the spring, the seat portion 15 is opened and the fuel is injected from the injection port 16. At the same time, high-pressure fuel is also supplied to the fuel bypass passage 18, is introduced into the bypass valve 21 through the communication passage 20 through the pipe 30, and is returned to the fuel tank 1 through the pipe 31 after the flow rate is adjusted.
マイクロコンピュータ25には、アクセル開度センサ2
7からの出力信号、噴射ポンプ2に取り付けられた回転
数センサ10からの出力信号、同じく噴射ポンプ2のス
ピルリング4を移動させるリニアソレノイド7に直結し
たスピル位置センサ8から出力信号、バイパス弁21駆
動用リニアソレノイド23に直結してロッド位置センサ
24かの出力信号が、信号線33、34、35、36で
それぞれ取り入れられ、あらかじめマイクロコンピュー
タ25に記憶された制御内容に従って、スピルリング4
を駆動するリニアソレノイド7と、バイパス弁21を駆
動するリニアソレノイド23とをそれぞれ独立に駆動す
るように、制御信号を信号線37、38を介して出力す
る。The microcomputer 25 includes an accelerator opening sensor 2
7, an output signal from a rotation speed sensor 10 attached to the injection pump 2, an output signal from a spill position sensor 8 directly connected to a linear solenoid 7 for moving the spill ring 4 of the injection pump 2, and a bypass valve 21. The output signals of the rod position sensor 24, which are directly connected to the driving linear solenoid 23, are taken in through the signal lines 33, 34, 35 and 36, respectively, and the spill ring 4 is supplied in accordance with the control contents stored in the microcomputer 25 in advance.
A control signal is output via the signal lines 37 and 38 so that the linear solenoid 7 that drives the control valve and the linear solenoid 23 that drives the bypass valve 21 are driven independently of each other.
具体的には、第6図に示す如くマイクロコンピュータの
回路がスタートすると(ステップ100)、噴射ポンプ
2に取り付けられた回転数センサ10の回転数Neが読
み込まれる(ステップ101)。又、何らかの原因でエ
ンジンが停止している場合は回転数Neを判定すること
によって(ステップ102)、ステップ101に戻るよ
うになっている。Specifically, when the circuit of the microcomputer is started as shown in FIG. 6 (step 100), the rotation speed Ne of the rotation speed sensor 10 attached to the injection pump 2 is read (step 101). If the engine is stopped for some reason, the number of revolutions Ne is determined (step 102), and the process returns to step 101.
エンジンが回転しており、回転数Neが読み込まれる
と、次に、アクセル開度センサー27のアセル開度θa
が読み込まれる(ステップ103)。一般の燃料噴射装
置におけるエンジン回転数と噴射ノズルの噴射圧力の関
係は、第3図に示すように、回転数及び噴射量によって
大きく変化し低回転、低噴射量の領域においては、図中
斜線で示す如く、燃料噴霧の微粒化を達成するのに最低
限必要である圧力レベルに成らず、微粒化が十分になさ
れない領域があった。そこで、本発明は、該領域におい
て、燃料噴射ポンプ2を微粒化のための最低圧力レベル
以上になる噴射量になるように調整し、圧力を確保した
上で、燃料量の調整を、燃料噴射ノズル12とバイパス
弁21で行なうものである。再び、第6図にもどってそ
の制御内容を説明すれば、ステップ101、ステップ1
03でそれぞれ回転数Ne及びアクセル開度θaを入力
すると、先に説明した制御内容に基いた、第4図に示す
エンジン回転数と噴射ポンプ吐出力の図(Ne−Qp
図)からNe、θaに相当する噴射ポンプ吐出力Qpを
読み出す(ステップ104)。次に、Qpの値に係数α
をかけて燃料噴射ポンプ2のスピルリング4の変化量で
あるスピル位置Spに値を変換する(ステップ10
5)。さらに、燃料噴射ポンプ2のスピル位置センサ8
から、実際のスピル位置Sp′を読み込み(ステップ1
06)、最終スピル位置移動量(Sp)を算出(ステッ
プ107)、出力(ステップ108)し、燃料噴射ポン
プ2から燃料噴射ノズル12への燃料供給量が第4図に
示す斜線内の範囲に制御される。一方、バイパス弁21
は、ステップ104と同時に、第5図に示すエンジン回
転数とバイパス弁排出量の図(Ne−Qb図)からN
e、θaに相当するバイパス弁排出量Qbを読み出す
(ステップ109)。この時の排出量は、周知の通り、
第4図のポンプ吐出量と逆の関係になっており、燃料噴
射ノズル12から噴射される燃料量が従来通り、アクセ
ル角度に応じて、変化するようになっている。次に、Q
bの値をバイパス弁のロッド位置値に変換し(ステップ
110)、ステップ111で、実際のロッド位置をセン
サ24から読み取る。さらに最終のロッド移動量(L
b)を算出して(ステップ112)、リニアソレノイド
23に(LB)を出力する(ステップ113)。こうし
て、バイパス弁21は、リニアソレノイド23によって
軸42のまわりを矢印43の如く回転し、パイプ30と
パイプ31の間の燃料の流量を制御する。上記ステップ
104〜ステップ108までとステップ109〜ステッ
プ113の動きは同じに行なわれ、(Sp)、(LB)
をそれぞさ出力すると再びステップ114でリターンさ
れ、ステップ100のスタートに戻る繰り返しとなる。When the engine is rotating and the rotation speed Ne is read, next, the accelerator opening θa of the accelerator opening sensor 27 is read.
Is read (step 103). As shown in FIG. 3, the relationship between the engine rotation speed and the injection pressure of the injection nozzle in a general fuel injection device greatly changes depending on the rotation speed and the injection amount. As shown in (3), there was a region where the pressure level that was the minimum required to achieve atomization of the fuel spray was not achieved and atomization was not sufficiently performed. Therefore, in the present invention, the fuel injection pump 2 is adjusted so that the injection amount becomes equal to or higher than the minimum pressure level for atomization in this region, the pressure is secured, and then the fuel amount is adjusted. The nozzle 12 and the bypass valve 21 are used. Referring again to FIG. 6, the control contents will be described. Step 101, step 1
When the rotation speed Ne and the accelerator opening degree θa are input in 03, respectively, the engine rotation speed and the injection pump discharge force (Ne-Qp) shown in FIG. 4 based on the control content described above (Ne-Qp
The injection pump discharge force Qp corresponding to Ne and θa is read from the figure) (step 104). Next, for the value of Qp, the coefficient α
The value is converted to the spill position Sp, which is the change amount of the spill ring 4 of the fuel injection pump 2 by multiplying (step 10).
5). Further, the spill position sensor 8 of the fuel injection pump 2
The actual spill position Sp 'is read from (step 1
06), the final spill position movement amount (Sp) is calculated (step 107), output (step 108), and the fuel supply amount from the fuel injection pump 2 to the fuel injection nozzle 12 falls within the range within the hatched area shown in FIG. 4. Controlled. On the other hand, the bypass valve 21
At the same time as step 104, the engine speed and the bypass valve discharge amount (Ne-Qb diagram) shown in FIG.
The bypass valve discharge amount Qb corresponding to e and θa is read (step 109). The discharge amount at this time is, as is well known,
It has an inverse relationship with the pump discharge amount shown in FIG. 4, and the fuel amount injected from the fuel injection nozzle 12 changes according to the accelerator angle as in the conventional case. Then Q
The value of b is converted into the rod position value of the bypass valve (step 110), and the actual rod position is read from the sensor 24 in step 111. Furthermore, the final rod movement amount (L
b) is calculated (step 112), and (LB) is output to the linear solenoid 23 (step 113). In this way, the bypass valve 21 is rotated around the shaft 42 by the linear solenoid 23 as indicated by an arrow 43 to control the flow rate of fuel between the pipe 30 and the pipe 31. The above steps 104 to 108 and steps 109 to 113 are performed in the same manner, and (Sp), (LB)
When each is output, the process returns again to step 114, and the process returns to the start of step 100.
[発明の効果] 本発明によれば、燃料噴射ノズルにバイパス通路を設
け、該バイパス通路にバイパス弁を設け、該バイパス弁
と燃料噴射ポンプをマイクロコンピュータで制御するこ
とにより、エンジンの低回転数時及び低負荷時において
も高圧燃料を送供するようにし、噴射ポンプの圧送圧力
を負荷に関係なく充分に高めることができ、噴射燃料の
微粒化が改善されることによって排出HCの低減が可能
になるという効果が得られる。EFFECTS OF THE INVENTION According to the present invention, a bypass passage is provided in the fuel injection nozzle, a bypass valve is provided in the bypass passage, and the bypass valve and the fuel injection pump are controlled by a microcomputer, so that the engine speed is low. Even when the load is low and the load is high, the pressure of the injection pump can be sufficiently increased regardless of the load, and the atomization of the injected fuel can be improved to reduce the exhaust HC. The effect of becoming
第1図は本発明の実施例を示すシステム全体図、 第2図(イ)、(ロ)はそれぞれ噴射ノズル先端部分の
拡大断面図、 第3図はエンジン回転数と噴射圧力の関係図、 第4図はエンジン回転数と噴射ポンプ吐出力の関係図、 第5図はエンジン回転数とバイパス弁排出量の関係図、 第6図は本発明による各リニアソレノイドの制御を示す
流れ図、 である。 1……燃料タンク 2……燃料噴射ポンプ 3……プランジャ 4……スピルリング 5……レバー 6……支点 7……リニアソレノイド 8……スピル位置センサ 9……ギア 10……回転数センサ 11……吐出口 12……燃料噴射ノズル 13……ノズルボディ 14……ニードル 15……シート部 16……噴口 17……燃料供給通路 18……燃料バイパス通路 19、20……連通路 21……バイパス弁 22……ロッド 23……リニアソレノイド 24……ロッド位置センサ 25……マイクロコンピュータ 26……アクセルペダル 27……アクセル開度センサ 28、29、30、31……パイプ 32……ワイヤー 33、34、35、 36、37、38……信号線 39……連通路 40……先端 41……円錐部 42……軸 43……矢印FIG. 1 is an overall system view showing an embodiment of the present invention, FIGS. 2 (a) and 2 (b) are enlarged cross-sectional views of a tip portion of an injection nozzle, respectively, and FIG. 3 is a relationship diagram between engine speed and injection pressure, FIG. 4 is a relationship diagram between engine speed and injection pump discharge force, FIG. 5 is a relationship diagram between engine speed and bypass valve discharge amount, and FIG. 6 is a flow chart showing control of each linear solenoid according to the present invention. . 1 ... Fuel tank 2 ... Fuel injection pump 3 ... Plunger 4 ... Spill ring 5 ... Lever 6 ... Support point 7 ... Linear solenoid 8 ... Spill position sensor 9 ... Gear 10 ... Rotation speed sensor 11 ...... Discharge port 12 ...... Fuel injection nozzle 13 ...... Nozzle body 14 ...... Needle 15 ...... Seat part 16 ...... Injection port 17 ...... Fuel supply passage 18 ...... Fuel bypass passage 19, 20 ...... Communication passage 21 ...... Bypass valve 22 ... Rod 23 ... Linear solenoid 24 ... Rod position sensor 25 ... Microcomputer 26 ... Accelerator pedal 27 ... Accelerator opening sensor 28, 29, 30, 31 ... Pipe 32 ... Wire 33, 34, 35, 36, 37, 38 ... Signal line 39 ... Communication path 40 ... Tip 41 ... Cone 42 ... Shaft 43 ... Arrow
フロントページの続き (51)Int.Cl.5 識別記号 庁内整理番号 FI 技術表示箇所 F02M 61/18 350 D 9248−3G Continuation of the front page (51) Int.Cl. 5 Identification code Office reference number FI technical display location F02M 61/18 350 D 9248-3G
Claims (1)
口が前記燃料タンクと接続され吐出口から燃料を高圧で
送出する燃料噴射ポンプと、該燃料噴射ポンプの吐出口
と接続されニードル先端円錐部と前記円錐部に当接する
ノズルボディの内周円錐部とによって形成されるシート
部と該シート部に開口し前記ニードル上昇時に前記シー
ト部を前記燃料噴射ポンプをバイパスして前記燃料タン
クへと連通するバイパス通路とを有する燃料噴射ノズル
と、前記燃料噴射ノズルのバイパス通路と前記燃料タン
クとを連通する通路上に設けられた流量制御弁と、機関
の負荷検出手段と、機関のまたは前記燃料噴射ポンプの
回転数検出手段と、前記燃料噴射ポンプに設けられた送
出燃料流量調節手段及び流量検出手段と、前記流量制御
弁に設けられた該流量制御弁の調節手段及び流量検出手
段と、前記燃料噴射ポンプの送出燃料流量調節手段及び
流量検出手段と前記流量制御弁の調節手段及び流量検出
手段に電気的に接続されたマイクロコンピュータと、か
ら成り、機関の負荷状態及び機関または燃料噴射ポンプ
の回転数に応じて前記燃料噴射ポンプの流量調節と前記
流量制御弁の流量調節を前記マイクロコンピュータにて
行うようにしたことを特徴とする燃料噴射制御装置。1. A fuel tank, a fuel injection pump having a suction port and a discharge port, the suction port being connected to the fuel tank and delivering fuel at a high pressure from the discharge port, and being connected to the discharge port of the fuel injection pump. A seat formed by a needle tip conical part and an inner peripheral conical part of the nozzle body that abuts the conical part, and an opening in the seat part, and when the needle rises, the seat part bypasses the fuel injection pump and the fuel A fuel injection nozzle having a bypass passage communicating with the tank, a flow control valve provided on a passage communicating the bypass passage of the fuel injection nozzle with the fuel tank, an engine load detection unit, and an engine load detector. Alternatively, the rotation speed detection means of the fuel injection pump, the delivery fuel flow rate adjustment means and flow rate detection means provided in the fuel injection pump, and the flow rate control valve provided A quantity control valve adjusting means and a flow rate detecting means; a delivery fuel flow rate adjusting means and a flow rate detecting means of the fuel injection pump; and a microcomputer electrically connected to the flow rate control valve adjusting means and the flow rate detecting means. The fuel injection is characterized in that the flow rate of the fuel injection pump and the flow rate of the flow control valve are adjusted by the microcomputer according to the load condition of the engine and the rotation speed of the engine or the fuel injection pump. Control device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59141408A JPH0617653B2 (en) | 1984-07-10 | 1984-07-10 | Fuel injection control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59141408A JPH0617653B2 (en) | 1984-07-10 | 1984-07-10 | Fuel injection control device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6123836A JPS6123836A (en) | 1986-02-01 |
| JPH0617653B2 true JPH0617653B2 (en) | 1994-03-09 |
Family
ID=15291310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59141408A Expired - Lifetime JPH0617653B2 (en) | 1984-07-10 | 1984-07-10 | Fuel injection control device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0617653B2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008064051A (en) * | 2006-09-08 | 2008-03-21 | Toyota Motor Corp | Fuel injection valve for internal combustion engine with oil repellent coating |
| GB0805263D0 (en) * | 2008-03-25 | 2008-04-30 | Delphi Tech Inc | Sensor arrangement |
| WO2014080265A1 (en) * | 2012-11-20 | 2014-05-30 | Nostrum Energy Pte. Ltd. | Liquid injector atomizer with colliding jets |
-
1984
- 1984-07-10 JP JP59141408A patent/JPH0617653B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6123836A (en) | 1986-02-01 |
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