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JPH0544539B2 - - Google Patents
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JPH0544539B2 - - Google Patents

Info

Publication number
JPH0544539B2
JPH0544539B2 JP59015745A JP1574584A JPH0544539B2 JP H0544539 B2 JPH0544539 B2 JP H0544539B2 JP 59015745 A JP59015745 A JP 59015745A JP 1574584 A JP1574584 A JP 1574584A JP H0544539 B2 JPH0544539 B2 JP H0544539B2
Authority
JP
Japan
Prior art keywords
pressure
valve
fuel
passage
injection
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
Application number
JP59015745A
Other languages
Japanese (ja)
Other versions
JPS60162021A (en
Inventor
Hideaki Nakano
Tadanori Azuma
Shuichi Sato
So Kashima
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.)
Kawasaki Heavy Industries Ltd
Original Assignee
Kawasaki Heavy Industries Ltd
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 Kawasaki Heavy Industries Ltd filed Critical Kawasaki Heavy Industries Ltd
Priority to JP1574584A priority Critical patent/JPS60162021A/en
Publication of JPS60162021A publication Critical patent/JPS60162021A/en
Publication of JPH0544539B2 publication Critical patent/JPH0544539B2/ja
Granted 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0003Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure
    • 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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/02Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
    • F02M59/10Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
    • F02M59/105Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive hydraulic drive

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】 技術分野 本発明は、内燃機関を停止することなく、また
内燃機関の回転速度に依存せず、燃料噴射時期お
よび燃料噴射量、燃料噴射圧力を容易に調節でき
る内燃機関の燃料噴射制御装置に関する。
Detailed Description of the Invention Technical Field The present invention relates to an internal combustion engine in which fuel injection timing, fuel injection amount, and fuel injection pressure can be easily adjusted without stopping the internal combustion engine and independent of the rotational speed of the internal combustion engine. The present invention relates to a fuel injection control device.

背景技術 一般に内燃機関、特にデイーゼル機関において
は、燃料噴射時期は機関性能特に燃料消費率に大
きく影響する。また燃料噴射圧力は高圧力化して
燃料噴霧の微細化と噴射期間の短縮を図り燃料効
率を高めることにより燃料消費率の低減が図れる
が、内燃機関が低負荷のときの高圧力噴射は、デ
イーゼルノツクの原因となり内燃機関に無理が生
じ、内燃機関の寿命の短縮や過大な騒音につなが
る。噴射の時期や圧力の最適値は、内燃機関の運
転状態や燃料油の質により大きく変化するので、
内燃機関の運転中でも燃料噴射時期や燃料噴射圧
力が自由に調節できれば、燃料の大幅な節約が内
燃機関に無理に強いることなく可能となり、石油
価格の高騰する現状から考え、大きな利益を生
む。
BACKGROUND ART In general, in internal combustion engines, and in diesel engines in particular, fuel injection timing greatly affects engine performance, particularly fuel consumption rate. In addition, the fuel injection pressure can be increased to make the fuel spray finer and the injection period shorter, increasing fuel efficiency and reducing the fuel consumption rate. However, when the internal combustion engine is under low load, high-pressure injection This causes knocking and puts strain on the internal combustion engine, leading to a shortened engine life and excessive noise. The optimum injection timing and pressure vary greatly depending on the operating conditions of the internal combustion engine and the quality of the fuel oil.
If the fuel injection timing and fuel injection pressure could be adjusted freely even while the internal combustion engine is running, it would be possible to save a large amount of fuel without forcing the internal combustion engine to do so, and considering the current situation of soaring oil prices, this would generate large profits.

従来、内燃機関の運転に同期して駆動される定
行程式燃料噴射ポンプと、閉止弁付自動噴射ノズ
ルとを直接燃料噴射管を介して接続して構成され
る内燃機関の燃料噴射装置は、広く世界で採用さ
れている。この従来式の燃料噴射装置において、
燃料噴射時期はカムの設定位置により定まり、燃
料噴射時期を変更する場合、カムのカム軸への設
定位置を変えることが必要であり、一旦内燃機関
を停止しなければならない。また燃料噴射圧力
は、内燃機関の回転速度と噴射ノズルの寸法とに
よつて定まり、自由に調節することはできない。
Conventionally, a fuel injection device for an internal combustion engine is configured by directly connecting a fixed stroke fuel injection pump that is driven in synchronization with the operation of the internal combustion engine and an automatic injection nozzle with a shutoff valve via a fuel injection pipe. Widely adopted around the world. In this conventional fuel injection device,
The fuel injection timing is determined by the set position of the cam, and when changing the fuel injection timing, it is necessary to change the set position of the cam on the camshaft, and the internal combustion engine must be temporarily stopped. Furthermore, the fuel injection pressure is determined by the rotational speed of the internal combustion engine and the dimensions of the injection nozzle, and cannot be freely adjusted.

一方、特開昭56−143344においてすでに公知で
あり燃料噴射装置では、閉止弁付噴射ノズルに電
気油圧式サーボ弁を装備し、燃料とは別の液体圧
を利用して燃料流路を切換えることにより、高圧
力燃料源に蓄圧された燃料を噴射ノズルから気筒
内に噴射供給し、その噴射の開始および終了は前
記電気油圧式サーボ弁に与える電気パルス信号で
制御される燃料噴射装置があるが、このような装
置によれば、燃料噴射時期および燃料噴射量は前
記電気パルス信号の送出時期とパルス幅とにより
決まり、また高圧力燃料源に蓄圧された燃料圧力
により燃料噴射圧力が決まるので、燃料噴射時
期、燃料噴射量および燃料噴射圧力は内燃機関の
速度やカムの取付けに関係なく自由に調節するこ
とができる。しかしながらこのような装置では、
噴射期間にかかわりなく常時、高圧力燃料源に噴
射圧相当の高圧力燃料を蓄圧した状態を保持して
おく必要があり、高圧力燃料源と燃料弁の間の配
管による圧力損失と燃料噴射時の吐出による瞬間
的な圧力降下とを補償しなければ燃料弁からの高
い燃料噴射率を維持できず、噴射圧力の高圧化が
達成できない。
On the other hand, in a fuel injection device already known in JP-A-56-143344, an injection nozzle with a shutoff valve is equipped with an electro-hydraulic servo valve, and the fuel flow path is switched using liquid pressure other than the fuel. There is a fuel injection device that injects and supplies fuel accumulated in a high-pressure fuel source into a cylinder from an injection nozzle, and the start and end of the injection is controlled by an electric pulse signal applied to the electrohydraulic servo valve. According to such a device, the fuel injection timing and fuel injection amount are determined by the transmission timing and pulse width of the electric pulse signal, and the fuel injection pressure is determined by the fuel pressure accumulated in the high-pressure fuel source. The fuel injection timing, fuel injection amount, and fuel injection pressure can be freely adjusted regardless of the speed of the internal combustion engine or the installation of the cam. However, in such a device,
Regardless of the injection period, it is necessary to maintain a state in which high-pressure fuel equivalent to the injection pressure is stored in the high-pressure fuel source at all times, and pressure loss due to piping between the high-pressure fuel source and the fuel valve and during fuel injection must be maintained. Unless the instantaneous pressure drop caused by the discharge of fuel is compensated for, a high fuel injection rate from the fuel valve cannot be maintained and a high injection pressure cannot be achieved.

舶用機関での燃料噴射圧力は通常600〜1500
Kg/cm2と非常に高い圧力かつ可燃物質であるた
め、高圧力燃料源の圧力変動を緩和する手段は通
常油圧管路系に使用されるガス圧によるアキユム
レータではなく燃料自身の体積弾性を利用した圧
力容器とせざるを得ない。
Fuel injection pressure in marine engines is usually 600 to 1500
Because it is a combustible material and has a very high pressure of Kg/cm 2 , the means to alleviate pressure fluctuations in high-pressure fuel sources uses the bulk elasticity of the fuel itself, rather than the gas-pressure accumulator normally used in hydraulic pipeline systems. There is no choice but to use a pressure vessel with a high temperature.

したがつて圧力容器の容積は、最大吐出量と供
給量とのバランスにおいて圧力変動幅をどの程度
まで許容するかによつて定まる。舶用機関での燃
料噴射期間は約30度クランク角であるので、機関
回転数を500rpmとすれば約10msの時間となる。
このような短い時間内における圧力変動を考える
場合、実用上供給量は無視できるので、例えば1
サイクルあたりの吐出量を15mlとして、噴射期間
内における許容圧力変動幅を30Kg/cm2とすれば、
単純計算では約8.5の容積が必要となる。
Therefore, the volume of the pressure vessel is determined by how much pressure fluctuation range is allowed in the balance between the maximum discharge amount and the supply amount. The fuel injection period in a marine engine is approximately 30 degrees of crank angle, so if the engine speed is 500 rpm, the period is approximately 10 ms.
When considering pressure fluctuations within such a short period of time, the supply amount can be ignored in practice, so for example 1
If the discharge amount per cycle is 15ml and the allowable pressure fluctuation range within the injection period is 30Kg/ cm2 , then
A simple calculation requires a volume of approximately 8.5.

このように多量のしかも超高圧力の燃料を保持
する圧力容器の構造寸法は、強度上内燃機関の従
来の燃料噴射ポンプの寸法に比較してかなり大き
くならざるを得ず、製作コストおよび機関への配
設方法に問題がある。また上記圧力容器はその寸
法の大きさゆえに、燃料噴射弁の配設されるシリ
ンダヘツドとは離れて配設せざるを得ないので、
超高圧燃料は噴射管によつて圧力容器と燃料噴射
弁を連通せしめられるが、超高圧力に耐え得るよ
うな噴射管や継手部の強度およびシール性能を高
める必要がある。さらに比較的長い噴射管を通し
て超高圧燃料を非常に短い時間内に供給する必要
があり、管内流速が早くなるので前述したように
圧力損失が大きくなつてその分所定の噴射圧力よ
りも圧力容器における元圧を高くする必要がある
ばかりでなく、噴射管内における圧力脈動のため
噴射管内圧力が異常に高くなつたり低くなつたり
して噴射管および継手部において破損の危険性が
生じるとともに、2次、3次噴射等の不整噴射を
生じるという問題がある。さらに高圧の燃料を蓄
圧した容器が大型化し、高圧の燃料が通る噴射管
も長くなればそれだけ、燃料のもれる機会も多く
なる。高圧の燃料がもれに場合、霧化されること
が多く、それだけ火災に対する危険性も大きくな
る。船上における火災は、船および乗員の生命に
多大の損害を与える。
The structural dimensions of a pressure vessel that holds such a large amount of fuel under ultra-high pressure must be considerably larger than the dimensions of a conventional fuel injection pump for an internal combustion engine due to its strength, which increases manufacturing costs and reduces the impact on the engine. There is a problem with the installation method. Furthermore, due to the size of the pressure vessel, it is necessary to install it separately from the cylinder head where the fuel injection valve is installed.
Ultra-high pressure fuel is communicated between a pressure vessel and a fuel injection valve through an injection pipe, but it is necessary to improve the strength and sealing performance of the injection pipe and joints so that they can withstand the ultra-high pressure. Furthermore, it is necessary to supply ultra-high pressure fuel in a very short time through a relatively long injection pipe, and the flow velocity in the pipe increases, so as mentioned above, the pressure loss increases, and the pressure drop in the pressure vessel becomes higher than the predetermined injection pressure. Not only is it necessary to increase the original pressure, but pressure pulsations within the injection pipe can cause the pressure inside the injection pipe to become abnormally high or low, creating a risk of damage to the injection pipe and joints. There is a problem that irregular injection such as tertiary injection occurs. Furthermore, as the container holding the high-pressure fuel becomes larger and the injection pipe through which the high-pressure fuel passes becomes longer, the chances of fuel leaking increase. When high-pressure fuel leaks, it often becomes atomized, increasing the risk of fire. A fire on a ship causes great damage to the ship and the lives of its crew.

一方、上記問題を解決するために燃料の噴射圧
力を超高圧化する手段としてパスカルの原理を応
用したブースターによる増圧構造を採用している
先行技術がある。この先行技術では、低圧力であ
る駆動側の圧力室に供給する作動油の供給量は燃
料の噴射量よりも増圧比分だけ多くなる。
On the other hand, in order to solve the above-mentioned problem, there is a prior art that employs a pressure increasing structure using a booster applying Pascal's principle as a means for increasing the fuel injection pressure to an ultra-high pressure. In this prior art, the amount of hydraulic oil supplied to the drive-side pressure chamber at low pressure is greater than the amount of fuel injection by the pressure increase ratio.

例えば噴射圧1500Kg/cm2の燃料の必要噴射量を
10msの噴射時間で15mlとすれば、増圧比7の場
合、単純に計算すれば約214Kg/cm2の作動油を10
msのうちに105mlだけ供給する必要があるとい
うことになる。燃料噴射の開始は上記作動油を圧
力源とブースターの駆動側圧力室を電磁弁により
連通せしめることによつて達成されるから、電磁
弁の圧油の通過流量は約630/minとなる。
For example, the required injection amount of fuel with an injection pressure of 1500Kg/cm 2 is
If the injection time is 10ms and the injection time is 15ml, then if the pressure increase ratio is 7, then by simple calculation, approximately 214Kg/ cm2 of hydraulic oil will be
This means that only 105ml needs to be supplied within ms. Since the start of fuel injection is achieved by communicating the hydraulic oil between the pressure source and the drive side pressure chamber of the booster through the solenoid valve, the flow rate of the pressure oil through the solenoid valve is about 630/min.

電磁弁には電磁力によりスプールを動かして圧
油の流路を切換える直動式と直動式電磁弁により
切換えた圧油の駆動力によりメインスプールを動
かして圧油の流路の切換えを行なうパイロツト式
とがある。高圧、大流量の場合直動式では切換え
動作時、流体力がスプールに作用して切換え不能
となるので通常、パイロツト式が採用される。と
ころがパイロツト式の場合、複数段階操作である
ため構造上速い応答性を得るには限界がある。一
方、内燃機関の燃料噴射に要求される制御精度は
1〜2度クランク角であり、500rpmの回転数で
は0.3〜0.7msの極端に微少な時間精度となる。
したがつて上記のような高圧力、大流量を扱う電
磁弁により、内燃機関の精度の高い燃料噴射制御
を行なうことは現状の技術では不可能である。
Direct-acting type solenoid valves use electromagnetic force to move the spool to switch the pressure oil flow path. Direct-acting type solenoid valves use the driving force of the switched pressure oil to move the main spool and switch the pressure oil flow path. There is a pilot type. In the case of high pressure and large flow rates, the pilot type is usually used because the direct acting type would be unable to switch due to the fluid force acting on the spool during the switching operation. However, in the case of a pilot type, there is a limit to how fast response can be achieved due to its structure, since it requires multiple steps of operation. On the other hand, the control accuracy required for fuel injection in an internal combustion engine is 1 to 2 degrees of crank angle, and at a rotation speed of 500 rpm, the time accuracy is extremely small, 0.3 to 0.7 ms.
Therefore, with the current technology, it is impossible to perform highly accurate fuel injection control of an internal combustion engine using a solenoid valve that handles high pressure and large flow rate as described above.

目 的 本発明は、上記従来技術の問題点に鑑み、燃料
の超高圧力化に要する増圧構造ブースタへ送給す
る大流量の圧油の制御を行なう電磁弁と内燃機関
の精度の高い燃料噴射制御を行なう少流量の電磁
弁とに燃料噴射の機能を分担せしめることによ
り、上記問題点の解決を図つたものであり、内燃
機関を停止することなく、また内燃機関の回転速
度に依存せず、燃料噴射時期および燃料噴射量、
燃料噴射圧力を容易に調節でき、かつ燃料圧力が
高圧化でき高信頼度で安価な内燃機関の燃料噴射
制御装置を提供することを目的とする。
Purpose: In view of the problems of the prior art described above, the present invention provides a solenoid valve that controls a large flow of pressure oil to be fed to a booster with a pressure increase structure required to increase the pressure of fuel to an ultra-high pressure, and a highly accurate fuel for an internal combustion engine. This problem is solved by sharing the fuel injection function with a small-flow solenoid valve that performs injection control, without stopping the internal combustion engine, and without depending on the rotational speed of the internal combustion engine. First, fuel injection timing and fuel injection amount,
It is an object of the present invention to provide a highly reliable and inexpensive fuel injection control device for an internal combustion engine that can easily adjust fuel injection pressure and increase the fuel pressure.

本発明は、第1圧力源1からの作動油を、少な
くとも燃料噴射期間W1以上の期間W2だけ開弁
状態となる第1電磁弁5を介して、ブースタ3に
おける移動体7,8の一端の大径受圧面71側に
導き、移動体7,8の他端の小径受圧面72側の
圧力室10には、第2圧力源2から燃料油を第1
逆止弁13を介して導入し、この圧力室10から
の燃料油は第2逆止弁11を介して蓄圧室12に
与え、蓄圧室12からの燃料油は第1通路22か
ら制御弁31および第2通路35を介してノズル
孔51から噴射され、 ノズル孔51には、第2通路35に連なる燃料
貯め48に臨む噴射弁体47が弁ばね46のばね
力によつて閉じる方向に付勢され、 制御弁31は、第1通路22と第2通路35と
の間に設けられた座面32に、第2通路35に連
通する圧力室34に設けられた弁体31aが着座
して閉弁可能に設けられて構成され、 弁体31aには、環状溝33が設けられ、第2
通路35は、制御弁31の閉弁時に環状溝33を
介して第3通路36が開いて排油され、制御弁3
1の開弁時に第3通路36を閉じ、 弁体31aは、第1圧力源1からの第2電磁弁
6を介して制御ピストン37の受圧面73,10
1に与えられる作動油によつて、制御ピストン3
7に結合された弁体31aが閉じる方向にパイロ
ツト作動されることを特徴とする内燃機関の燃料
噴射制御装置である。
The present invention supplies hydraulic oil from the first pressure source 1 to one end of the movable bodies 7 and 8 in the booster 3 via the first electromagnetic valve 5 that is open for at least a period W2 that is longer than the fuel injection period W1. Fuel oil is introduced from the second pressure source 2 into the pressure chamber 10 on the side of the small-diameter pressure-receiving surface 72 at the other end of the movable bodies 7 and 8.
The fuel oil from the pressure chamber 10 is introduced via the check valve 13 and is supplied to the pressure accumulation chamber 12 via the second check valve 11, and the fuel oil from the pressure accumulation chamber 12 is introduced from the first passage 22 to the control valve 31. The fuel is injected from the nozzle hole 51 via the second passage 35, and the injection valve body 47 facing the fuel reservoir 48 connected to the second passage 35 is attached to the nozzle hole 51 in the closing direction by the spring force of the valve spring 46. The control valve 31 has a valve element 31a provided in a pressure chamber 34 communicating with the second passage 35 seated on a seat surface 32 provided between the first passage 22 and the second passage 35. The valve body 31a is provided with an annular groove 33, and a second
When the control valve 31 is closed, the third passage 36 is opened through the annular groove 33 and oil is drained from the passage 35.
When the valve 1 is opened, the third passage 36 is closed, and the valve body 31a receives pressure from the control piston 37 through the second electromagnetic valve 6 from the first pressure source 1.
1, the control piston 3
This fuel injection control device for an internal combustion engine is characterized in that a valve body 31a connected to a valve 7 is pilot operated in a closing direction.

実施例 図面によつて本発明の実施例を説明する。第1
図は本発明の第1の実施例を示す構成図である。
第1圧力源1は、導管55、逆止弁17および第
1電磁弁5を介して導管15によりブースタ3の
接続口19から圧力室9に接続されており、導管
55から分岐する導管43により逆止弁42およ
び第2電磁弁6を介して燃料噴射弁4の接続口3
9から通路41を経て圧力室38に接続可能にな
つている。導管15,43には、管路内の圧力脈
動を吸収するためのアキユームレータ18,44
が接続される。第2圧力源2は、導管27を介し
て、ブースタ3の接続口21から、ばね付勢され
ている逆止弁13を経て、圧力室10に接続され
る。
Embodiments Embodiments of the present invention will be described with reference to the drawings. 1st
The figure is a configuration diagram showing a first embodiment of the present invention.
The first pressure source 1 is connected to the pressure chamber 9 from the connection port 19 of the booster 3 by the conduit 15 via the conduit 55, the check valve 17, and the first electromagnetic valve 5, and is connected to the pressure chamber 9 by the conduit 43 branching from the conduit 55. Connection port 3 of fuel injection valve 4 via check valve 42 and second solenoid valve 6
9 can be connected to the pressure chamber 38 via a passage 41. The conduits 15, 43 are provided with accumulators 18, 44 for absorbing pressure pulsations within the conduits.
is connected. The second pressure source 2 is connected to the pressure chamber 10 via a conduit 27 from the connection 21 of the booster 3 via a spring-loaded check valve 13 .

ブースタ3内には、上部シリンダ66を滑動す
るピストン7と、下部シリンダ67を滑動するプ
ランジヤ8が配設されており、ピストン7とプラ
ンジヤ8は押接している。シリンダ66とピスト
ン7の上端部の大径受圧面である頂面71とによ
つて形成される圧力室9には、第1圧力源1から
供給される作動油が第1電磁弁5を介して供給可
能となつている。シリンダ67とプランジヤ8の
下端部の小径受圧面である面72によつて形成さ
れる圧力室10には、第2圧力源2から前述のよ
うに逆止弁13を介して供給される燃料油が充満
可能になつている。圧力室10は、ばねつきの逆
止弁11を介してブースタ3下部に配設された蓄
圧室12に接続されている。蓄圧室12には通路
22によつて燃料噴射弁4に連通している。通路
22は通路35によつて燃料貯め48に連通して
いる。
Inside the booster 3, a piston 7 that slides on an upper cylinder 66 and a plunger 8 that slides on a lower cylinder 67 are disposed, and the piston 7 and the plunger 8 are pressed against each other. Hydraulic oil supplied from the first pressure source 1 is supplied to the pressure chamber 9 formed by the cylinder 66 and the top surface 71, which is a large-diameter pressure receiving surface at the upper end of the piston 7, through the first solenoid valve 5. It is now available to supply. The pressure chamber 10 formed by the cylinder 67 and the small diameter pressure receiving surface 72 at the lower end of the plunger 8 is filled with fuel oil supplied from the second pressure source 2 via the check valve 13 as described above. is becoming available. The pressure chamber 10 is connected to a pressure accumulation chamber 12 disposed below the booster 3 via a check valve 11 with a spring. The pressure accumulation chamber 12 is connected to the fuel injection valve 4 through a passage 22 . The passage 22 communicates with a fuel reservoir 48 by a passage 35.

燃料噴射弁4は制御部Aと弁部Bから構成され
る。制御部Aには、シリンダ69を滑動する制御
弁31と、シリンダ68を滑動する制御ピストン
37が押接して配設されている。シリンダ68と
制御ピストン37の面73によつて制御弁31の
反対側に形成される圧力室38には、第1圧力源
1から接続口39を介して供給される作動油が充
満している。弁部Bには、シリンダ70を滑動す
る噴射弁体47と、噴射弁体47をノズル孔51
の座面50に押圧する方向に付勢する弁ばね46
が設けられている。
The fuel injection valve 4 is composed of a control section A and a valve section B. In the control section A, a control valve 31 that slides on a cylinder 69 and a control piston 37 that slides on a cylinder 68 are disposed in pressure contact with each other. A pressure chamber 38 formed on the opposite side of the control valve 31 by the cylinder 68 and the surface 73 of the control piston 37 is filled with hydraulic oil supplied from the first pressure source 1 via the connection port 39. . The valve part B includes an injection valve body 47 that slides on the cylinder 70 and a nozzle hole 51 that connects the injection valve body 47 to the nozzle hole 51.
Valve spring 46 biased in the direction of pressing against the seat surface 50 of
is provided.

第1圧力源1では、作動油はタンク61からフ
イルタ59を介してポンプ58によつて昇圧され
る。調圧弁57によつて圧力調整された圧油はフ
イルタ56を介して導管55に供給される。
In the first pressure source 1, the pressure of hydraulic oil is increased from the tank 61 through the filter 59 by the pump 58. Pressure oil whose pressure is regulated by the pressure regulating valve 57 is supplied to the conduit 55 via the filter 56.

第2圧力源2では、燃料油はタンク65からフ
イルタ64を介してポンプ63によつて高圧化さ
れ、調圧弁62によつて圧力調整された圧油が導
管27に供給される。
In the second pressure source 2 , fuel oil is increased in pressure from the tank 65 through the filter 64 by the pump 63 , and the pressure oil whose pressure is regulated by the pressure regulating valve 62 is supplied to the conduit 27 .

ピストン14は、シリンダ24内で第1図の上
下に移動可能であり、弁ばね25によつて蓄圧室
12に連通する圧力室23が小さくなるように第
1図の上方に付勢されている。ピストン14がば
ね25のばね力に抗して変位し圧力室23が大き
くなると、この圧力室23は通路76から導管2
9に連通する。制御弁31の弁体31aが座面3
2に着座して閉弁状態にあるとき、弁体31aに
形成された環状溝33によつて通路36は接続口
52からドレン管53,54を介してタンク65
に連通する。制御弁31が開くと通路36と接続
口52とは遮断される。
The piston 14 is movable up and down in FIG. 1 within the cylinder 24, and is urged upward in FIG. 1 by a valve spring 25 so that the pressure chamber 23 communicating with the pressure accumulation chamber 12 becomes smaller. . When the piston 14 is displaced against the spring force of the spring 25 and the pressure chamber 23 becomes larger, this pressure chamber 23 is moved from the passage 76 to the conduit 2.
Connects to 9. The valve body 31a of the control valve 31 is the seat surface 3
2 and the valve is in the closed state, the passage 36 is connected to the tank 65 from the connection port 52 via the drain pipes 53 and 54 by the annular groove 33 formed in the valve body 31a.
communicate with. When the control valve 31 opens, the passage 36 and the connection port 52 are cut off.

なお、ピストン7およびプランジヤ8の最大ス
トロークは、プランジヤ8の最大ストロークボリ
ユームが1回の最大噴射量と高圧蓄圧に要する燃
料の圧縮容積の合計よりも若干大きくなるように
選ばれる。
The maximum strokes of the piston 7 and the plunger 8 are selected such that the maximum stroke volume of the plunger 8 is slightly larger than the sum of the maximum injection amount per injection and the compressed volume of fuel required for high-pressure accumulation.

次に作用を第1図にしたがい説明する。 Next, the operation will be explained according to FIG.

第1電磁弁5の左側のソレノイドが励磁されて
位置5bにあるとき、圧力室9に関して絞り弁6
0が介在されている戻り導管16を介してブース
タ3の接続口19をタンク61に連通するように
流路を切換えている。このときブースタ3の圧力
室10には、逆止弁13のクラツキング圧以上の
圧力で第2圧力源2から導管27、ブースタ3の
接続口21および逆止弁13を介して燃料が供給
され、その圧力でプランジヤ8およびピストン7
が圧力室9の容積を小さくする方向に押しあげら
れ、ピストン7の頂面71がシリンダ66の端面
74に圧接して停止する。プランジヤ8およびピ
ストン7の移動速度は、戻り導管16の途中に配
設された絞り弁60によつて制限されているの
で、ポンプ63により高圧化された燃料によりピ
ストン7が暴走するのを防止しストロークエンド
における衝撃力が緩和される。
When the left-hand solenoid of the first solenoid valve 5 is energized and in position 5b, the throttle valve 6 with respect to the pressure chamber 9
The flow path is switched so that the connection port 19 of the booster 3 is communicated with the tank 61 via the return conduit 16 in which the 0 is interposed. At this time, fuel is supplied to the pressure chamber 10 of the booster 3 from the second pressure source 2 at a pressure higher than the cracking pressure of the check valve 13 via the conduit 27, the connection port 21 of the booster 3, and the check valve 13, With that pressure, plunger 8 and piston 7
is pushed up in a direction to reduce the volume of the pressure chamber 9, and the top surface 71 of the piston 7 comes into pressure contact with the end surface 74 of the cylinder 66 and stops. The moving speeds of the plunger 8 and the piston 7 are limited by a throttle valve 60 disposed in the middle of the return conduit 16, so that the piston 7 is prevented from running out of control due to the fuel pressurized by the pump 63. The impact force at the end of the stroke is alleviated.

第2電磁弁6は、左側のソレノイドが励磁され
て位置6bにあつて、圧力室38の接続口39が
導管43に連通するよう流路を切換えている。そ
のため燃料噴射弁4の制御弁31では、第1圧力
源1からの圧油は制御ピストン37の面73に作
用してその駆動力により制御ピストン37は第1
図の左方に付勢されており、制御弁31の弁体3
1aは制御部Aの弁体31aに対向した座面32
に圧接されており、接続口22と通路35は制御
弁31により遮断されている。
The second electromagnetic valve 6 switches the flow path so that the connection port 39 of the pressure chamber 38 communicates with the conduit 43 when the left solenoid is energized and is in position 6b. Therefore, in the control valve 31 of the fuel injection valve 4, the pressure oil from the first pressure source 1 acts on the surface 73 of the control piston 37, and its driving force causes the control piston 37 to move to the first
The valve body 3 of the control valve 31 is biased to the left in the figure.
1a is a seat surface 32 facing the valve body 31a of the control section A
The connection port 22 and the passage 35 are closed off by the control valve 31.

ブースタ3の蓄圧室12には、第2動力源2か
らの供給圧力よりも高い超高圧力が蓄圧される。
蓄圧室12は、ばね付勢された逆止弁11によつ
て圧力室10と遮断され、かつ、安全弁80によ
つて通路76と遮断され、かつ、制御弁31によ
り通路35と遮断されている。
An extremely high pressure higher than the supply pressure from the second power source 2 is accumulated in the pressure accumulation chamber 12 of the booster 3 .
The pressure accumulation chamber 12 is isolated from the pressure chamber 10 by a spring-biased check valve 11, from the passage 76 by a safety valve 80, and from the passage 35 by a control valve 31. .

燃料噴射弁4の通路35の途中から分岐する通
路36は、制御弁31の弁体31aに形成された
環状溝35によつて、接続口52からドレン管5
3,54を介してタンク65に連通する。制御弁
31、圧力室34、通路35,36,52、およ
び燃料貯め48は、大気圧に開放された燃料が充
満している。
A passage 36 that branches off from the middle of the passage 35 of the fuel injection valve 4 is connected from the connection port 52 to the drain pipe 5 by an annular groove 35 formed in the valve body 31a of the control valve 31.
It communicates with a tank 65 via 3 and 54. The control valve 31, the pressure chamber 34, the passages 35, 36, 52, and the fuel reservoir 48 are filled with fuel open to atmospheric pressure.

弁部Bの噴射弁47は弁ばね46により付勢さ
れており、噴射弁47の先端部49が座面50に
圧接され、燃料貯め48をノズル孔51から遮断
している。
The injection valve 47 of the valve portion B is biased by the valve spring 46, and the tip 49 of the injection valve 47 is pressed against the seat surface 50, thereby blocking the fuel reservoir 48 from the nozzle hole 51.

次に、第1電磁弁5の右側ソレノイドが付勢さ
れて第2図1のように時刻t1〜t4で期間W2
だけ第1電磁弁5の流路が切換つて位置5aとな
ると導管15と接続口19が連通して第1圧力源
1から圧油が圧力室9に供給される。そのためピ
ストン7およびプランジヤ8が第1図の下方に押
し下げられ、圧力室10に充満した燃料を圧縮す
る。この際、アキユムレータ18は導管15内の
圧油の圧力の瞬間的な低下を防ぐために有効に働
く。プランジヤ8の面72に対するピストン7の
頂面71の面積比をK(K>1)とすると、圧力
室10には圧力室9の圧力K倍の圧力が発生す
る。Kを増圧比と言う。このとき制御弁31は遮
断状態にあるので、ピストン7およびプランジヤ
8は停止している。圧力室10の圧力は、接続口
21の圧力よりも高いので、逆止弁13は閉じら
れる。圧力室10の圧力と蓄圧室12の圧力はほ
とんど同じになるので、逆止弁11はばね力によ
り閉弁している。第2電流弁6は位置6bにあ
り、弁体31aと制御ピストン37の面積比は、
接続口22の圧力による開弁方向の駆動力より
も、ピストン37の面73に作用する圧力室38
の圧力による閉弁方向の駆動力が充分大きくなる
ように選ばれる。そのため制御弁31は閉弁状態
を維持している。
Next, the right solenoid of the first solenoid valve 5 is energized, and the period W2 is from time t1 to t4 as shown in FIG.
When the flow path of the first electromagnetic valve 5 is switched to position 5a, the conduit 15 and the connection port 19 communicate with each other, and pressure oil is supplied from the first pressure source 1 to the pressure chamber 9. Therefore, the piston 7 and the plunger 8 are pushed downward in FIG. 1, compressing the fuel filling the pressure chamber 10. At this time, the accumulator 18 effectively works to prevent the pressure of the pressure oil within the conduit 15 from dropping momentarily. If the area ratio of the top surface 71 of the piston 7 to the surface 72 of the plunger 8 is K (K>1), a pressure K times the pressure of the pressure chamber 9 is generated in the pressure chamber 10 . K is called the pressure increase ratio. At this time, the control valve 31 is in the cutoff state, so the piston 7 and plunger 8 are stopped. Since the pressure in the pressure chamber 10 is higher than the pressure in the connection port 21, the check valve 13 is closed. Since the pressure in the pressure chamber 10 and the pressure in the pressure accumulation chamber 12 are almost the same, the check valve 11 is closed by the spring force. The second current valve 6 is at position 6b, and the area ratio between the valve body 31a and the control piston 37 is
The pressure chamber 38 that acts on the surface 73 of the piston 37 is stronger than the driving force in the valve opening direction due to the pressure of the connection port 22.
is selected so that the driving force in the valve closing direction due to the pressure is sufficiently large. Therefore, the control valve 31 remains closed.

その後、第2電磁弁6の右側ソレノイドが励磁
されると、第2電磁弁6の流路が切換つて位置6
aとなり、接続口39が戻り導管45に連通して
圧力室38の圧油がタンク61に排出される。そ
のため接続口22側からの圧油の駆動力により、
制御弁31が第2図2の時刻t2〜t3で開弁す
る。弁体31aの第1図右方への開弁方向の移動
に伴ない、制御弁31の滑動面によりシリンダ6
9に開口した通路36と通路52が遮断されると
ともに、通路22と圧力室34とが連通して通路
35に蓄圧室12から高圧燃料油が流入する。そ
の結果、圧力室48内の圧力が高くなつて、噴射
弁47の段付き部75に作用する駆動力が閉弁方
向に付勢している弁ばね46のばね力に打ち勝つ
て、噴射弁47を開弁し、ノズル孔51から高圧
燃料が噴射される。
Thereafter, when the right solenoid of the second solenoid valve 6 is energized, the flow path of the second solenoid valve 6 is switched to position 6.
a, the connection port 39 communicates with the return conduit 45, and the pressure oil in the pressure chamber 38 is discharged to the tank 61. Therefore, due to the driving force of the pressure oil from the connection port 22 side,
The control valve 31 opens between times t2 and t3 in FIG. As the valve body 31a moves to the right in FIG. 1 in the valve opening direction, the sliding surface of the control valve 31 causes the cylinder 6 to
9 and the passage 52 are cut off, the passage 22 and the pressure chamber 34 communicate with each other, and high-pressure fuel oil flows into the passage 35 from the pressure accumulation chamber 12. As a result, the pressure within the pressure chamber 48 increases, and the driving force acting on the stepped portion 75 of the injection valve 47 overcomes the spring force of the valve spring 46 biasing the injection valve 47 in the valve closing direction. The valve is opened and high pressure fuel is injected from the nozzle hole 51.

噴射開始後蓄圧室12から通路35を介してノ
ズル孔51に燃料が供給排出されるとともに、逆
止弁11が開き蓄圧室12には圧力室10から高
圧の燃料が補給される。第1圧力源1から充分な
圧油の供給をうけてピストン7はプランジヤ8を
移動させる。そのため圧力室10は高圧に保持さ
れており、燃料はその噴射圧力が高圧に保たれた
ままでノズル孔51に補給される。
After the injection starts, fuel is supplied and discharged from the pressure accumulation chamber 12 to the nozzle hole 51 via the passage 35, and at the same time, the check valve 11 is opened and the pressure accumulation chamber 12 is supplied with high pressure fuel from the pressure chamber 10. The piston 7 moves the plunger 8 when supplied with sufficient pressure oil from the first pressure source 1. Therefore, the pressure chamber 10 is maintained at a high pressure, and fuel is supplied to the nozzle hole 51 while its injection pressure is maintained at a high pressure.

所定の噴射時間W1の経過の後、時刻t3で第
2電磁弁6の左側ソレノイドが励磁され、流路が
接続口39と導管43が連通するように位置6b
に切換る。そのため圧力室38には、第1圧力源
1からの圧油が供給される。したがつて制御ピス
トン37の駆動力によつて制御ピストン37およ
び弁体31aは閉弁方向に付勢され、弁座32に
弁体31aを押圧して接続口22を通路35から
遮断する。この際、弁体31aの閉弁方向への移
動に伴ない、環状溝33によつて通路36と接続
口52が連通せしめられるので、通路35に充満
する高圧燃料油はドレン管53,54に排出さ
れ、圧力が急激に下がる。その結果、燃料貯め4
8において噴射弁47に開弁方向に作用していた
駆動力が瞬時に小さくなつて、弁ばね46の閉弁
方向のばね力により、噴射弁47は閉弁方向に付
勢され、弁座50に噴射弁47の先端部49が押
圧されて閉弁する。そのためノズル孔51からの
燃料噴射が完了する。環状溝33からの排油は、
いわゆる「燃料の切れ」をよくするのに役立ち、
燃料効率の向上に効果がある。
After the predetermined injection time W1 has elapsed, the left solenoid of the second electromagnetic valve 6 is energized at time t3, and the flow path is moved to position 6b so that the connection port 39 and the conduit 43 communicate with each other.
Switch to. Therefore, pressure oil from the first pressure source 1 is supplied to the pressure chamber 38 . Therefore, the control piston 37 and the valve body 31a are urged in the valve closing direction by the driving force of the control piston 37, and the valve body 31a is pressed against the valve seat 32, thereby blocking the connection port 22 from the passage 35. At this time, as the valve body 31a moves in the valve closing direction, the passage 36 and the connection port 52 are brought into communication by the annular groove 33, so that the high-pressure fuel oil filling the passage 35 flows into the drain pipes 53, 54. is discharged and the pressure drops rapidly. As a result, fuel storage 4
At 8, the driving force acting on the injection valve 47 in the valve opening direction instantly becomes smaller, and the injection valve 47 is urged in the valve closing direction by the spring force of the valve spring 46 in the valve closing direction, and the valve seat 50 The tip 49 of the injection valve 47 is pressed to close the valve. Therefore, fuel injection from the nozzle hole 51 is completed. The drained oil from the annular groove 33 is
It helps to improve the so-called "fuel shortage",
Effective in improving fuel efficiency.

制御ピストン37のストロークはごくわずかで
あり、たとえば1mm程度である。したがつて第2
電磁弁6を通過する作動油の流量は小さい。その
ため作動油による駆動力は小さくてよく直動形の
電磁弁を使用することができる。これによつて噴
射タイミングおよび調整の精度を向上することが
可能となる。
The stroke of the control piston 37 is very small, for example on the order of 1 mm. Therefore, the second
The flow rate of hydraulic oil passing through the solenoid valve 6 is small. Therefore, the driving force required by the hydraulic oil is small and a direct-acting solenoid valve can be used. This makes it possible to improve the accuracy of injection timing and adjustment.

弁部Bの閉弁時に、蓄圧室12および圧力室1
0にはピストン7およびプランジヤ8の加速度に
より瞬間的に高圧が発生する。このとき、蓄圧室
12に開口している安全弁80の圧力室23の容
積はばね25のばね力に抗して滑動するピストン
14の変位によつて大きくなり、そのため衝撃圧
力が吸収される。つまり、圧力室23は緩衝ボリ
ユームとして働く何らかの異常によりピストン1
4が或る一定値以上第1図の下方に移動すると、
通路76が圧力室23に連通して高圧燃料が導管
29からタンク65に排出される。そのため蓄圧
室12が異常に高圧になるのが防止される。蓄圧
室12の圧力がピストン7およびプランジヤ8の
停止に伴なつて平準化されるに従い、ピストン1
4はばね25によつて押し戻される。
When valve part B is closed, pressure accumulator chamber 12 and pressure chamber 1
At zero, high pressure is instantaneously generated due to the acceleration of the piston 7 and plunger 8. At this time, the volume of the pressure chamber 23 of the safety valve 80 that opens to the pressure accumulation chamber 12 increases due to the displacement of the piston 14 that slides against the spring force of the spring 25, so that the impact pressure is absorbed. In other words, the pressure chamber 23 acts as a buffer volume due to some abnormality and the piston 1
4 moves downward in Figure 1 by more than a certain value,
Passage 76 communicates with pressure chamber 23 and high pressure fuel is discharged from conduit 29 into tank 65 . Therefore, the pressure accumulation chamber 12 is prevented from becoming abnormally high pressure. As the pressure in the pressure storage chamber 12 is equalized as the piston 7 and plunger 8 stop, the piston 1
4 is pushed back by spring 25.

燃料噴射の終了後、第2図1の時刻t4で、第
1電磁弁5が切換えられて位置5bとなり、流路
が接続口19と戻り導管16が連通するように切
換ると圧力室9の圧油は、戻り導管16から絞り
弁60を介してタンク61に排出される。この
際、圧力室9からの圧油の排出に伴ない、圧力室
10の燃料の駆動力により、ピストン7およびプ
ランジヤ8は上方に移動し、圧力室10の容積が
増大して圧力が下がる。圧力室10は、逆止弁1
1によつて蓄圧室12とは遮断されているので、
蓄圧室12には高圧力が保持される。圧力室10
の圧力が接続口21の圧力よりも逆止弁13のク
ラツキング圧だけ低くなると、逆止弁13が開弁
し、第2圧力源から高圧燃料が補充され、ピスト
ン頂面71がシリンダ66の座面74に押圧され
て停止する。戻り導管16の途中に配設された絞
り弁60の開度は、圧力室10の圧油の駆動力に
よるピストン7およびプランジヤ8の移動速度を
制限するように調整されている。
After the fuel injection ends, at time t4 in FIG. The pressure oil is discharged from the return conduit 16 via a throttle valve 60 into a tank 61 . At this time, as the pressure oil is discharged from the pressure chamber 9, the piston 7 and the plunger 8 move upward due to the driving force of the fuel in the pressure chamber 10, the volume of the pressure chamber 10 increases, and the pressure decreases. The pressure chamber 10 has a check valve 1
Since it is cut off from the pressure accumulation chamber 12 by 1,
High pressure is maintained in the pressure accumulation chamber 12 . Pressure chamber 10
When the pressure at the connecting port 21 becomes lower than the pressure at the connection port 21 by the cracking pressure of the check valve 13, the check valve 13 opens, high-pressure fuel is replenished from the second pressure source, and the piston top surface 71 is brought into contact with the seat of the cylinder 66. It is pressed against the surface 74 and stops. The opening degree of the throttle valve 60 disposed midway through the return conduit 16 is adjusted so as to limit the movement speed of the piston 7 and the plunger 8 due to the driving force of the pressure oil in the pressure chamber 10.

第1電磁弁5を通過する作動油の流量は、燃焼
性能を向上させるための増圧比を大きくとりかつ
大きい噴射量を短時間に出すため大流量となる。
回転数500rpmで、11c.c.の燃料をクランク角25度
で噴射するとき、増圧比を8とすると、 Q=6×500/25×11×60/1000×8=633/min ……(1) このため第1電磁弁5は、パイロツト作動方式
にせざるを得ず、パイロツト作動式の電磁弁は応
答性が悪いが、圧力室10への燃料の補充は噴射
期間以外の充分長い時間内で行なえばよく、第1
電磁弁5の切換えに第2電磁弁6のような高速性
が要求されない。事実、500rpmで回転する内燃
機関において噴射期間や噴射時期をクランク角1
度単位で制御する場合 1000/500×6=0.33ms ……(2) 程度の応答性が第2電磁弁6に要求されるが、第
1電磁弁5は噴射時期を25度とすると、 (360−25)×1000/500×6=112ms ……(3) の間に流路を切換え、燃料を圧力室10に補給す
ればよいので、第2電磁弁6と比べ応答性は1/10
以下でよい。
The flow rate of the hydraulic oil passing through the first electromagnetic valve 5 is large because the pressure increase ratio is large to improve combustion performance and a large injection amount is produced in a short period of time.
When injecting 11 c.c. of fuel at a crank angle of 25 degrees at a rotation speed of 500 rpm, and the pressure increase ratio is 8, Q = 6 x 500/25 x 11 x 60/1000 x 8 = 633/min... ( 1) For this reason, the first solenoid valve 5 has to be pilot operated, and although pilot operated solenoid valves have poor response, the pressure chamber 10 can be refilled with fuel within a sufficiently long period of time other than the injection period. You can do it in the first step.
Switching of the solenoid valve 5 does not require high speed as in the case of the second solenoid valve 6. In fact, in an internal combustion engine that rotates at 500 rpm, the injection period and injection timing are adjusted by 1 crank angle.
When controlling in degree units, the second solenoid valve 6 is required to have a response of 1000/500×6=0.33ms (2), but if the first solenoid valve 5 has an injection timing of 25 degrees, ( 360-25) x 1000/500 x 6 = 112 ms... (3) Since it is only necessary to switch the flow path and replenish fuel to the pressure chamber 10, the response is 1/10 compared to the second solenoid valve 6.
The following is fine.

上記のごとく構成された実施例では 1回の噴射周期ごとに超高圧燃料を蓄圧し、
噴射期間内に燃料を常に補充するようにブース
タ3が作用するので、安定した噴射率が得られ
る。大容量の超高圧圧力容器が不要である。
In the embodiment configured as described above, ultra-high pressure fuel is accumulated for each injection cycle,
Since the booster 3 acts to constantly replenish fuel within the injection period, a stable injection rate can be obtained. A large-capacity ultra-high-pressure pressure vessel is not required.

蓄圧容器であるブースタ3が小型化できるの
で、ブースタ3を噴射弁4と近接あるいは直接
結合できる。そのため圧力容器である蓄圧室1
2から噴射弁4までの噴射通路が短くでき、噴
射通路での圧力損失を小さくしうるとともに、
また配管の省略によつて燃料漏れの発生を抑
え、火災の発生を防ぐことができる。
Since the booster 3, which is a pressure accumulating container, can be miniaturized, the booster 3 can be placed close to or directly connected to the injection valve 4. Therefore, the pressure accumulation chamber 1 which is a pressure vessel
The injection passage from the injection valve 2 to the injection valve 4 can be shortened, and the pressure loss in the injection passage can be reduced.
Furthermore, by omitting piping, it is possible to suppress the occurrence of fuel leakage and prevent the occurrence of fire.

大容量の超高圧圧力容器が不要で作動油圧力
源からブースタまでは噴射圧力に比べ小さな圧
力配管でよいので、配管継手は従来のものが使
用でき、安価である。
A large-capacity ultra-high-pressure pressure vessel is not required, and pressure piping that is smaller than the injection pressure is sufficient from the hydraulic oil pressure source to the booster, so conventional piping joints can be used and are inexpensive.

従来の油圧作動による増圧式燃料噴射装置で
はブースタのピストンやプランジヤの着座時に
発生する衝撃力が問題であつたが、本発明の場
合、増圧部に関して蓄圧室12に配設した衝撃
吸収ピストンと安全弁を構成するピストン14
により蓄圧室12の過圧を防止することができ
る。
In conventional hydraulically actuated pressure booster fuel injection devices, the impact force generated when the booster piston or plunger is seated has been a problem, but in the case of the present invention, the pressure increaser has a shock absorbing piston disposed in the pressure accumulation chamber 12 and Piston 14 constituting a safety valve
This makes it possible to prevent overpressure in the pressure accumulation chamber 12.

蓄圧室12に逆止弁11,13を配設するこ
とにより、燃料の供給が可能となり、少量の噴
射も可能となる。
By disposing the check valves 11 and 13 in the pressure accumulation chamber 12, fuel can be supplied and a small amount of fuel can be injected.

増圧のための高圧作動油の供給には、大容量
の電磁弁が必要であるが、従来の場合、応答
性、再現性ともに非常に高い制御精度の要求さ
れる噴射タイミングの制御を単一の電磁弁で行
なわしめているので、大容量と精度を同時に達
成することは両立しない。本発明では、増圧に
要する油圧駆動力を発生させる機能と噴射期間
の制御を行なう機能を個別の電磁弁5,6によ
り分担せしめることにより、油圧作動による燃
料噴射を達成し得る。
A large-capacity solenoid valve is required to supply high-pressure hydraulic oil for pressure increase, but in the past, injection timing control, which requires extremely high control accuracy in both response and repeatability, was performed using a single unit. Since this is done using a solenoid valve, it is not compatible to achieve large capacity and accuracy at the same time. In the present invention, fuel injection by hydraulic operation can be achieved by having individual electromagnetic valves 5 and 6 share the function of generating the hydraulic driving force required for pressure increase and the function of controlling the injection period.

1気筒毎にブースタ3と噴射弁4とが設けら
れ噴射系が気筒毎に独立しているので高圧式噴
射装置のように気筒間の干渉が防げるととも
に、1気筒分のこのような構成が故障しても、
内燃機関の運転を他の気筒で続行することがで
きるので、エンジンの信頼性が高い。
Since a booster 3 and an injection valve 4 are provided for each cylinder, and the injection system is independent for each cylinder, it is possible to prevent interference between cylinders like in a high-pressure injection system, and this configuration for one cylinder also prevents failure. Even if
Since the internal combustion engine can continue to operate in other cylinders, the reliability of the engine is high.

制御部Aと弁部Bとを一体的に組合せて燃料
噴射弁4を構成するので、配管が省略される。
そのため燃料漏れが防がれるとともに、燃料漏
れに起因した火災の発生が防がれる。
Since the fuel injection valve 4 is constructed by integrally combining the control section A and the valve section B, piping is omitted.
Therefore, fuel leakage is prevented, and the occurrence of a fire due to fuel leakage is also prevented.

第3図は本発明の他の実施例の構成図である。 FIG. 3 is a block diagram of another embodiment of the present invention.

この実施例は、第1図および第2図示の実施例
に類似し、対応する部分には同一の参照符を付
す。注目すべきは、蓄圧室12の燃料の圧力によ
つて、制御弁31の弁体31aの段付き部には、
第3図の上への力が作用して開弁状態となるよう
に構成される。
This embodiment is similar to the embodiment shown in FIGS. 1 and 2, and corresponding parts are provided with the same reference numerals. What should be noted is that due to the pressure of the fuel in the pressure accumulation chamber 12, the stepped portion of the valve body 31a of the control valve 31 has a
The valve is configured so that an upward force as shown in FIG. 3 acts to open the valve.

本発明のさらに他の実施例として、絞り弁60
を導管16に介在する代りに、導管27に介在し
てもよい。
As yet another embodiment of the present invention, a throttle valve 60
Instead of intervening in the conduit 16, it may be interposed in the conduit 27.

第4図は、本発明の更に他の実施例を示す構成
図である。これら実施例は前述の実施例に類似し
ており、対応する部分には同一の参照符を付す。
注目すべきは、第2電磁弁6に4方向弁を用いた
ことであり、制御ピストン37の両側に配した第
1受圧面100と第2受圧面101を有する圧力
室38a,38bは第2電磁弁6により圧力のか
かつた導管43と逃し導管45にそれぞれ交互に
接続可能になつていて、制御ピストン37は切換
え位置6aでは右方向へ、切換え位置6bでは左
方向へそれぞれ付勢される。第4図示は、第1電
磁弁5が切換え位置5aに、第2電磁弁6が切換
え位置6bにあり、第3図における時刻t1とt
2の間にある状態を示している。圧力室10と蓄
圧室12にはブースタ3により増圧された燃料油
が保持されていて弁部Bは閉じている。つまり、
通路22を介して制御弁31を右方向へ付勢する
燃料油による力は、制御ピストン37を左方向へ
付勢する作動油による力よりも小さく、制御弁3
1は閉じている。このため通路35の圧力はタン
クに開放されており、弁体47はばね46に付勢
され閉じている。時刻t2において第2電磁弁6
が切換えられ6aに示す状態になると、圧力室3
8aに圧力導管43が、圧力室38bに逃し導管
45が接続され制御ピストン37は右方向へ付勢
されるので、制御弁31は右へ移動し、蓄圧室1
2の燃料は通路22から燃料貯め48へ流れる。
弁体47は燃料圧力に付勢さればね46の抗力に
反して上昇し図示しないシリンダ室へ噴射が行な
われる。時刻t3になると第2電磁弁6は再び切
換えられ、第4図示の状態となり、制御弁31は
左へ移動し、閉弁されるので噴射は終了する。
FIG. 4 is a configuration diagram showing still another embodiment of the present invention. These embodiments are similar to the previously described embodiments and corresponding parts are provided with the same reference numerals.
What should be noted is that a four-way valve is used as the second electromagnetic valve 6, and the pressure chambers 38a and 38b, which have the first pressure receiving surface 100 and the second pressure receiving surface 101 arranged on both sides of the control piston 37, are the second solenoid valve 6. The solenoid valve 6 can be connected alternately to the pressurized conduit 43 and the relief conduit 45, so that the control piston 37 is urged to the right in the switching position 6a and to the left in the switching position 6b. In the fourth illustration, the first solenoid valve 5 is at the switching position 5a, the second solenoid valve 6 is at the switching position 6b, and the times t1 and t in FIG.
It shows a state between 2. Fuel oil pressurized by the booster 3 is held in the pressure chamber 10 and the pressure accumulation chamber 12, and the valve portion B is closed. In other words,
The force of the fuel oil that urges the control valve 31 to the right through the passage 22 is smaller than the force of the hydraulic oil that urges the control piston 37 to the left.
1 is closed. Therefore, the pressure in the passage 35 is released to the tank, and the valve body 47 is biased by the spring 46 and closed. At time t2, the second solenoid valve 6
is switched to the state shown in 6a, the pressure chamber 3
The pressure conduit 43 is connected to the pressure chamber 8a, and the relief conduit 45 is connected to the pressure chamber 38b, and the control piston 37 is urged to the right, so the control valve 31 moves to the right and the pressure accumulation chamber 1
2 flows from passage 22 to fuel reservoir 48 .
The valve body 47 is biased by the fuel pressure and rises against the resistance of the spring 46, causing injection into a cylinder chamber (not shown). At time t3, the second electromagnetic valve 6 is switched again and enters the state shown in the fourth figure, and the control valve 31 moves to the left and is closed, thus ending the injection.

第5図は本発明の他の実施例を示す構成図であ
る。これら実施例は前述の実施例に類似してお
り、対応する部分には同一の参照符を付す。注目
すべきは、第2電磁弁6に4方向弁を用いたこと
であり、制御ピストン37の両側に配した第1受
圧面100と第2受圧面101を有する圧力室3
8a,38bは第2電磁弁6により圧力のかかつ
た導管43と逃し導管45にそれぞれ交互に接続
可能になつていて、制御ピストン37は切換え位
置6aでは上方向へ、切換え位置6bでは下方向
へそれぞれ付勢される。第5図示は、第1電磁弁
5が切換え位置5aに、第2電磁弁が切換え位置
6bにあり、第3図における時刻t1とt2の間
にある状態を示している。圧力室10と蓄圧室1
2にはブースタ3により増圧された燃料油が保持
されていて、弁部Bは閉じている。つまり、通路
22を介して制御弁31を上方向へ付勢する燃料
油による力は、制御ピストン37を下方向へ付勢
する作動油による力よりも小さく、制御弁31は
閉じている。このため通路35の圧力はタンクに
開放されており弁体47はばね46に付勢され閉
じている。時刻t2において第2電磁弁6が切換
えられ6aに示す状態になると、圧力室38aに
圧力導管43が圧力室38bに逃し導管45が接
続され制御ピストン37は上方向へ付勢されるの
で、制御弁31は上へ移動し、蓄圧室12の燃料
は通路22から燃料貯め48へ流れる。弁体47
は燃料圧力に付勢さればね46の抗力に反して上
昇し、図示しないシリンダ室へ噴射が行なわれ
る。時刻t3になると第2電磁弁6は再び切換え
られ第5図示に示す状態となり、制御弁31は下
へ移動し、閉弁されるので噴射は終了する。
FIG. 5 is a block diagram showing another embodiment of the present invention. These embodiments are similar to the previously described embodiments and corresponding parts are provided with the same reference numerals. What should be noted is that a four-way valve is used as the second electromagnetic valve 6, and the pressure chamber 3 has a first pressure receiving surface 100 and a second pressure receiving surface 101 arranged on both sides of the control piston 37.
8a and 38b can be connected alternately to the pressured conduit 43 and the relief conduit 45 by the second solenoid valve 6, and the control piston 37 moves upward in the switching position 6a and downward in the switching position 6b. Each is energized. The fifth illustration shows a state in which the first solenoid valve 5 is at the switching position 5a and the second solenoid valve is at the switching position 6b, between times t1 and t2 in FIG. Pressure chamber 10 and pressure accumulation chamber 1
2 holds fuel oil whose pressure has been increased by the booster 3, and the valve portion B is closed. That is, the force of the fuel oil that urges the control valve 31 upward through the passage 22 is smaller than the force of the hydraulic oil that urges the control piston 37 downward, and the control valve 31 is closed. Therefore, the pressure in the passage 35 is released to the tank, and the valve body 47 is biased by the spring 46 and closed. When the second electromagnetic valve 6 is switched to the state shown in 6a at time t2, the pressure conduit 43 is connected to the pressure chamber 38a and the relief conduit 45 is connected to the pressure chamber 38b, and the control piston 37 is urged upward, so that the control Valve 31 moves upwards and fuel in accumulator chamber 12 flows from passage 22 to fuel reservoir 48 . Valve body 47
is urged by the fuel pressure and rises against the resistance of the spring 46, and injection is performed into a cylinder chamber (not shown). At time t3, the second electromagnetic valve 6 is switched again to the state shown in FIG. 5, and the control valve 31 is moved downward and closed, thus ending the injection.

以上のように本発明によれば、内燃機関を停止
することなく、また内燃機関の回転速度に依存せ
ず、燃料噴射時期および燃料噴射量、燃料噴射圧
力を容易に調節でき、しかも燃料圧力が高圧化で
きるようになる。
As described above, according to the present invention, the fuel injection timing, fuel injection amount, and fuel injection pressure can be easily adjusted without stopping the internal combustion engine and without depending on the rotational speed of the internal combustion engine. It becomes possible to increase the pressure.

特に本発明によれば、噴射弁体47は弁ばね4
6によつてノズル孔51を閉じる方向に付勢さ
れ、燃料噴射終了時には、第2電磁弁6からの作
動油によつて蓄圧室12からの燃料油が遮断さ
れ、しかも燃料貯め48内の燃料油は、第2通路
35から環状溝33を介して第3通路36から排
油され、したがつて燃料切れが良好となり、希望
する期間だけ、燃料油を供給することが可能とな
る。しかもこのような構成は簡単であり、実現が
容易である。
In particular, according to the invention, the injection valve body 47 is connected to the valve spring 4
6 in the direction of closing the nozzle hole 51, and at the end of fuel injection, the hydraulic oil from the second solenoid valve 6 blocks off the fuel oil from the pressure accumulation chamber 12, and the fuel in the fuel reservoir 48 The oil is drained from the second passage 35 through the annular groove 33 and from the third passage 36, so that fuel runs out easily and it becomes possible to supply fuel oil only for a desired period. Moreover, such a configuration is simple and easy to implement.

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

第1図は本発明の一実施例の構成図、第2図は
第1図に示された実施例の動作を説明するための
グラフ、第3図は本発明の他の実施例の構成図、
第4図は本発明の更に他の実施例の構成図、第5
図は本発明の他の実施例の構成図である。 1……第1圧力源、2……第2圧力源、3……
ブースタ、4……燃料噴射弁、5,6……電磁
弁、7……ピストン、8……プランジヤ、10…
…圧力室、11,13……逆止弁、12……蓄圧
室、31……制御弁、35……通路、51……ノ
ズル孔、A……制御部、B……弁部。
Fig. 1 is a block diagram of one embodiment of the present invention, Fig. 2 is a graph for explaining the operation of the embodiment shown in Fig. 1, and Fig. 3 is a block diagram of another embodiment of the present invention. ,
FIG. 4 is a configuration diagram of still another embodiment of the present invention, and FIG.
The figure is a configuration diagram of another embodiment of the present invention. 1...First pressure source, 2...Second pressure source, 3...
Booster, 4... Fuel injection valve, 5, 6... Solenoid valve, 7... Piston, 8... Plunger, 10...
... Pressure chamber, 11, 13 ... Check valve, 12 ... Pressure accumulation chamber, 31 ... Control valve, 35 ... Passage, 51 ... Nozzle hole, A ... Control section, B ... Valve section.

Claims (1)

【特許請求の範囲】 1 第1圧力源1からの作動油を、少なくとも燃
料噴射期間W1以上の期間W2だけ開弁状態とな
る第1電磁弁5を介して、ブースタ3における移
動体7,8の一端の大径受圧面71側に導き、移
動体7,8の他端の小径受圧面72側の圧力室1
0には、第2圧力源2から燃料油を第1逆止弁1
3を介して導入し、この圧力室10からの燃料油
は第2逆止弁11を介して蓄圧室12に与え、蓄
圧室12からの燃料油は第1通路22から制御弁
31および第2通路35を介してノズル孔51か
ら噴射され、 ノズル孔51には、第2通路35に連なる燃料
貯め48に臨む噴射弁体47が弁ばね46のばね
力によつて閉じる方向に付勢され、 制御弁31は、第1通路22と第2通路35と
の間に設けられた座面32に、第2通路35に連
通する圧力室34に設けられた弁体31aが着座
して閉弁可能に設けられて構成され、 弁体31aには、環状溝33が設けられ、第2
通路35は、制御弁31の閉弁時に環状溝33を
介して第3通路36が開いて排油され、制御弁3
1の開弁時に第3通路36を閉じ、 弁体31aは、第1圧力源1からの第2電磁弁
6を介して制御ピストン37の受圧面73,10
1に与えられる作動油によつて、制御ピストン3
7に結合された弁体31aが閉じる方向にパイロ
ツト作動されることを特徴とする内燃機関の燃料
噴射制御装置。
[Scope of Claims] 1. Hydraulic oil from the first pressure source 1 is supplied to the movable bodies 7, 8 in the booster 3 via the first solenoid valve 5, which remains open for at least a period W2 that is longer than the fuel injection period W1. The pressure chamber 1 is guided to the large-diameter pressure-receiving surface 71 side at one end, and the pressure chamber 1 is guided to the small-diameter pressure-receiving surface 72 side at the other end of the movable bodies 7 and 8.
0, fuel oil is supplied from the second pressure source 2 to the first check valve 1.
3, the fuel oil from the pressure chamber 10 is supplied to the pressure accumulation chamber 12 via the second check valve 11, and the fuel oil from the pressure accumulation chamber 12 is introduced from the first passage 22 to the control valve 31 and the second check valve 11. The fuel is injected from the nozzle hole 51 through the passage 35, and the injection valve body 47 facing the fuel reservoir 48 connected to the second passage 35 is biased in the closing direction by the spring force of the valve spring 46. The control valve 31 can be closed by seating a valve body 31a provided in a pressure chamber 34 communicating with the second passage 35 on a seat surface 32 provided between the first passage 22 and the second passage 35. The valve body 31a is provided with an annular groove 33, and a second
When the control valve 31 is closed, the third passage 36 is opened through the annular groove 33 and oil is drained from the passage 35.
When the valve 1 is opened, the third passage 36 is closed, and the valve body 31a receives pressure from the control piston 37 through the second electromagnetic valve 6 from the first pressure source 1.
1, the control piston 3
A fuel injection control device for an internal combustion engine, characterized in that a valve body 31a coupled to a valve body 31a is pilot operated in a closing direction.
JP1574584A 1984-01-31 1984-01-31 Fuel injection control device of internal-combustion engine Granted JPS60162021A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1574584A JPS60162021A (en) 1984-01-31 1984-01-31 Fuel injection control device of internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1574584A JPS60162021A (en) 1984-01-31 1984-01-31 Fuel injection control device of internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS60162021A JPS60162021A (en) 1985-08-23
JPH0544539B2 true JPH0544539B2 (en) 1993-07-06

Family

ID=11897297

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1574584A Granted JPS60162021A (en) 1984-01-31 1984-01-31 Fuel injection control device of internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS60162021A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002527676A (en) * 1998-10-16 2002-08-27 インターナショナル トラック アンド エンジン コーポレイション Fuel injector with direct control of needle valve

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5526791A (en) * 1995-06-07 1996-06-18 Diesel Technology Company High-pressure electromagnetic fuel injector
JP4574762B2 (en) * 1998-08-28 2010-11-04 ヴェルトジィレ シュヴァイツ アクチェンゲゼルシャフト Fuel injection device for reciprocating piston engine
KR20130027996A (en) * 2011-09-08 2013-03-18 바르질라 스위츠랜드 리미티드 Fuel injection system for an internal combustion engine, method for injecting fuel, as well as an internal combustion engine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57124032A (en) * 1981-01-24 1982-08-02 Diesel Kiki Co Ltd Fuel injector
DE3133288A1 (en) * 1981-08-22 1983-03-03 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8900 Augsburg Fuel injection system on an internal combustion engine
JPS58119961A (en) * 1982-01-11 1983-07-16 Kawasaki Heavy Ind Ltd Fuel injection device in diesel engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002527676A (en) * 1998-10-16 2002-08-27 インターナショナル トラック アンド エンジン コーポレイション Fuel injector with direct control of needle valve

Also Published As

Publication number Publication date
JPS60162021A (en) 1985-08-23

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