JPH0514104B2 - - Google Patents

Info

Publication number
JPH0514104B2
JPH0514104B2 JP57144884A JP14488482A JPH0514104B2 JP H0514104 B2 JPH0514104 B2 JP H0514104B2 JP 57144884 A JP57144884 A JP 57144884A JP 14488482 A JP14488482 A JP 14488482A JP H0514104 B2 JPH0514104 B2 JP H0514104B2
Authority
JP
Japan
Prior art keywords
pressure
valve
fuel
fuel injection
air
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
JP57144884A
Other languages
Japanese (ja)
Other versions
JPS5844262A (en
Inventor
Shuroru Ruudorufu
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Publication of JPS5844262A publication Critical patent/JPS5844262A/en
Publication of JPH0514104B2 publication Critical patent/JPH0514104B2/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
    • 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
    • F02M59/20Varying fuel delivery in quantity or timing
    • F02M59/36Varying fuel delivery in quantity or timing by variably-timed valves controlling fuel passages to pumping elements or overflow passages
    • F02M59/366Valves being actuated electrically
    • 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
    • F02M59/107Pumps 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 pneumatic drive, e.g. crankcase pressure drive

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)

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、内燃機関用の燃料噴射ポンプであつ
て、各機関シリンダに1つの燃料噴射弁が設けら
れていて、該燃料噴射弁の弁ニードルが、供給さ
れる燃料の圧力によつて閉鎖ばねの力に抗して開
放方向に運動せしめられるようになつており、燃
料噴射弁の燃料貯え室が、供給導管を介して燃料
噴射ポンプのポンプ作業室に接続されており、該
ポンプ作業室が、最大噴射燃料の収容を可能にす
る容積を有していて、該ポンプ作業室の方向に向
かつてしか開放しない逆止弁を有する燃料供給導
管を介して、常に燃料フイードポンプと接続され
ており、該燃料フイードポンプの吐出圧が一定
で、燃料噴射弁の開放圧よりも低く設定されてお
り、燃料が燃料噴射ポンプのポンプ作業室から、
内燃機関のサイクルで圧力空気によつて作動可能
な圧力伝達ピストンを用いて、燃料噴射弁に供給
可能であり、ポンプ作業室がポンプシリンダによ
つて形成されていて、圧力伝達ピストンに、該ポ
ンプシリンダ内を摺動しかつポンプ作業室を制限
する吐出ピストンが設けられており、該吐出ピス
トンには、ポンプ作業室とは反対の側において、
圧力シリンダ内を摺動する大径のサーボピストン
が設けられていて、該サーボピストンが、吐出ピ
ストンとは反対の側に位置する空気圧力室を制限
しており、該空気圧力室が、電磁作動式の2方向
切換え制御弁の出口に接続されていて、該2方向
切換え制御弁を介して、圧力伝達ピストンを作動
させるために空気タンクに接続されるか、又は切
換えによつて、放圧導管に接続されるようになつ
ている形式のものに関する。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to a fuel injection pump for an internal combustion engine, in which each engine cylinder is provided with one fuel injection valve, and the valve needle of the fuel injection valve is , the fuel reservoir of the fuel injection valve is moved in the opening direction by the pressure of the supplied fuel against the force of the closing spring, and the fuel reservoir of the fuel injection valve is connected to the pumping operation of the fuel injection pump via the supply conduit. a fuel supply conduit connected to a chamber, the pump working chamber having a volume that allows accommodation of a maximum amount of injected fuel, and having a check valve that opens only in the direction of the pump working chamber; The fuel feed pump is always connected to the fuel feed pump via the fuel feed pump, and the discharge pressure of the fuel feed pump is constant and set lower than the opening pressure of the fuel injection valve, and the fuel is supplied from the pump working chamber of the fuel injection pump.
The fuel injection valve can be supplied with a pressure transmission piston operable by pressurized air in the cycle of the internal combustion engine, the pump working chamber being formed by the pump cylinder, and the pressure transmission piston being connected to the pump. A discharge piston is provided which slides within the cylinder and delimits the pump working chamber, the discharge piston having, on the side opposite the pump working chamber,
A large diameter servo-piston is provided that slides within the pressure cylinder, the servo-piston delimiting a pneumatic chamber located opposite the discharge piston, the pneumatic pressure chamber being actuated by an electromagnetic actuator. a pressure relief conduit connected to the outlet of a two-way switching control valve of the type and, via said two-way switching control valve, being connected to an air tank for actuating a pressure transmitting piston, or by switching a pressure relief conduit; Concerning a type of thing that has become connected to.

従来の技術 ドイツ連邦共和国特許出願公開第2012202号明
細書に基づいて公知の上記形式の燃料噴射装置で
は、切換え弁を用いて圧力室にはサーボピストン
を介して、燃料供給ポンプから吐出された燃料が
制御されて供給されるようになつている。この場
合もつぱら切換え弁によつて制御される噴射動作
時に、サーボピストンと協働するポンププランジ
ヤが燃料圧を提供するようになつている。この燃
料圧は、切換え弁によつて制御される噴射開始時
期の後で初めて、この燃料圧が燃料噴射弁の弁ニ
ードルを閉鎖ばねの力に抗して開放方向に運動さ
せるのに十分になるまで、上昇する。しかしなが
らこの場合既に弁ニードルの開放運動の開始直後
に、燃料は燃焼室に流出することができるので、
この際に開放圧が再び降下し、完全に開放した位
置への弁ニードルの移動が急激には行われず、噴
射過程中、弁ニードルが中途半端な位置に留まる
おそれがある。
Prior Art In the above-mentioned fuel injection device known from German Patent Application No. 2012202, a switching valve is used to supply fuel discharged from a fuel supply pump to a pressure chamber via a servo piston. is being supplied in a controlled manner. A pump plunger cooperating with a servo piston provides fuel pressure during the injection operation, which is again controlled by the switching valve. Only after the injection start time controlled by the switching valve does this fuel pressure become sufficient to move the valve needle of the fuel injector in the opening direction against the force of the closing spring. rise until. However, in this case already immediately after the start of the opening movement of the valve needle, fuel can flow into the combustion chamber, so that
At this time, the opening pressure drops again, and the valve needle does not move quickly to the fully open position, and there is a risk that the valve needle may remain in a halfway position during the injection process.

発明が解決しようとする手段 ゆえに本発明の課題は、冒頭に述べた形式の燃
料噴射装置を改良して、燃料噴射開始時期を噴射
圧の形成とは無関係にして、噴射動作の開始時
に、燃料噴射弁に所望の噴射圧を供給することが
でき、しかもこの噴射圧を噴射過程の終了時まで
維持することができる燃料噴射装置を提供するこ
とである。
Means to be Solved by the Invention Therefore, an object of the present invention is to improve the fuel injection device of the type mentioned at the beginning, to make the fuel injection start timing independent of the formation of the injection pressure, and to make the fuel injection start timing independent of the formation of the injection pressure. It is an object of the present invention to provide a fuel injection device that can supply a desired injection pressure to an injection valve and maintain this injection pressure until the end of an injection process.

課題を解決するための手段 この課題を解決するために本発明の構成では、
冒頭に述べた形式の燃料噴射装置において、圧力
空気室に2方向切換え制御弁を介して圧力空気を
供給するために、電磁作動式のコンプレツサによ
つて連続的に圧力空気を供給される空気タンクが
設けられており、ポンプ作業室と燃料噴射弁との
間における供給導管が、内燃機関のサイクルで、
2方向切換え制御弁によつて制御された空気圧力
室の圧力負荷時間内において任意に切換え可能な
前置弁を用いて、開閉制御可能であり、燃料流れ
方向で見て該前置弁に後置された放圧弁を用い
て、前置弁の閉鎖後に放圧可能である。
Means for Solving the Problem In order to solve this problem, the configuration of the present invention includes:
In a fuel injection device of the type mentioned at the outset, an air tank is continuously supplied with pressurized air by an electromagnetically actuated compressor in order to supply the pressurized air chamber with pressurized air via a two-way control valve. is provided, and the supply conduit between the pump working chamber and the fuel injection valve is operated during the cycle of the internal combustion engine.
Opening and closing can be controlled using a front valve that can be switched arbitrarily during the pressure load time of the air pressure chamber controlled by a two-way switching control valve. With the aid of a pressure relief valve placed in the front end, pressure relief can be achieved after the front valve has been closed.

発明の効果 本発明のように構成されていると、既に噴射開
始前に吐出ピストンを用いて生ぜしめられている
圧力を、前置弁の開放後にも引き続き燃料噴射弁
に供給することができ、しかもこの圧力が、前置
弁の閉鎖によつて終了する全噴射時間にわたつて
維持されるので、噴射開始時に燃料噴射弁を急激
に開放すること及び全噴射時間中に弁ニードルを
その完全な開放位置に留めることが可能である。
また、圧力空気室に圧力空気を供給するためつま
り圧力伝達ピストンを作動させるために、従来技
術におけるように燃料圧によつて作動する供給装
置を使用する代わりに、本発明では電磁作動式の
コンプレツサによつて連続的に圧力空気を供給さ
れる空気タンクを用いることによつて、制御を確
実かつ容易に行うことが可能である。
Effects of the Invention With the configuration of the present invention, the pressure already generated using the discharge piston before the start of injection can be continuously supplied to the fuel injection valve even after the pre-valve is opened. Moreover, since this pressure is maintained over the entire injection period, which ends with the closing of the pre-valve, it is necessary to open the fuel injector suddenly at the start of injection and to close the valve needle to its full extent during the entire injection period. It is possible to keep it in the open position.
Furthermore, instead of using a supply device actuated by fuel pressure as in the prior art to supply pressurized air to the pressurized air chamber, ie to actuate the pressure transfer piston, the invention uses an electromagnetically actuated compressor. By using an air tank that is continuously supplied with pressurized air by a pump, control can be carried out reliably and easily.

実施例 次に図面につき本発明の実施例を説明する。Example Next, embodiments of the present invention will be described with reference to the drawings.

図面において燃料を通す導管は交互に白黒の部
分を備えたダブルラインで示されているのに対し
て、空気を通す導管は白抜きのダブルラインで示
され、電流を通す導線はシングルラインで示され
ている。さらに図面に描かれている矢印は燃料を
通す導管及び空気を通す導管では燃料の流れ方向
ないしは空気の圧力方向を示し、電流を通す導線
では信号伝達の方向を示している。
In the drawings, conduits carrying fuel are shown as double lines with alternating black and white sections, while conduits carrying air are shown as double white lines and conductors carrying current are shown as single lines. has been done. Furthermore, the arrows drawn in the drawings indicate the direction of fuel flow or air pressure in the fuel and air conduits, and the direction of signal transmission in the case of electrical conductors.

図面には内燃機関用の図示の燃料噴射装置の一
部として、機関シリンダに配属された1つの燃料
噴射弁が示されている。この燃料噴射弁の弁ニー
ドル2は、供給導管5を介して燃料貯え室4に供
給された燃料の力によつて閉鎖ばね3の力に抗し
て開放方向に運動可能である。本発明によれば燃
料噴射弁に、噴射される燃料量を収容するための
ポンプ作業室6が前置されている。ポンプ作業室
6は、有利には電動機7によつて駆動される燃料
フイードポンプ8に接続されていて、この燃料フ
イードポンプ8から連続的に燃料を供給されるよ
うになつている。この供給される燃料の吐出圧は
燃料噴射弁1の開放圧よりも低く設定されてい
る。燃料はポンプ作業室6から、機関サイクルに
合わせてニユーマチツク式に作動される圧力伝達
ピストン9を介して燃料噴射弁1に供給される。
ポンプ作業室6と燃料噴射弁1との間の導管10
には、この導管10を機関サイクルに合わせて開
閉制御する前置弁11が取り付けられている。導
管10はさらに前置弁11の閉鎖後にその都度流
れ方向で見て前置弁11に後置されている放圧弁
12によつて、導管10から分岐していて燃料タ
ンク13に燃料を戻す放圧導管14を介して放圧
されるようになつている。
The drawing shows a fuel injection valve assigned to an engine cylinder as part of the illustrated fuel injection system for an internal combustion engine. The valve needle 2 of this fuel injection valve is movable in the opening direction against the force of the closing spring 3 by the force of the fuel supplied to the fuel reservoir 4 via the supply conduit 5 . According to the invention, the fuel injection valve is provided with a pump working chamber 6 for accommodating the amount of fuel to be injected. The pump work chamber 6 is connected to a fuel feed pump 8, preferably driven by an electric motor 7, from which it is continuously supplied with fuel. The discharge pressure of the supplied fuel is set lower than the opening pressure of the fuel injection valve 1. Fuel is supplied from the pump work chamber 6 to the fuel injection valve 1 via a pressure-transmitting piston 9 which is actuated pneumatically in accordance with the engine cycle.
Conduit 10 between pump working chamber 6 and fuel injection valve 1
A front valve 11 is installed to control the opening and closing of the conduit 10 in accordance with the engine cycle. The line 10 is furthermore branched off from the line 10 by means of a pressure relief valve 12 which is downstream of the upstream valve 11 in the flow direction in each case after the closing of the upstream valve 11 and which returns the fuel to the fuel tank 13. The pressure is released through a pressure conduit 14.

ポンプ作業室6はポンプシリンダ15によつて
形成されており、このポンプシリンダ15内では
圧力伝達ピストン9の吐出ピストン16が作業し
ている。吐出ピストン16の後ろ側には、圧力シ
リンダ17内で作業する大径のサーボピストン1
8が接続されており、このサーボピストン18は
圧力シリンダ17の壁と協働して空気圧力室19
を制限している。ポンプシリンダ15からは一方
では導管10が分岐し、他方ではポンプシリンダ
15に燃料供給導管20が開口している。燃料供
給導管20は、燃料フイードポンプ8の吐出部に
接続されていてかつすべての燃料噴射弁に燃料を
供給するために働く燃料搬送導管21から分岐し
ている。燃料搬送導管20には、燃料供給方向に
だけ通過を許しひいては圧力伝達ピストン9の吐
出行程時にポンプ作業室6から燃料搬送導管21
への燃料の逆流を阻止する逆止弁22が設けられ
ている。燃料フイードポンプ8はフイルタ23及
び吸込み導管24を介して燃料タンク13から燃
料を吸い込み、この燃料を、燃料噴射弁1の開放
圧よりも約10〜20%低い圧力で燃料搬送導管21
に吐出する。所望の吐出圧を調節及び維持するた
めに燃料フイードポンプ8には圧力調整弁25が
配属されている。この圧力調整弁25は圧力監視
導管に設けられており、この圧力監視導管は燃料
フイードポンプ8の下流で燃料搬送導管21から
分岐し、流れ方向で見て燃料フイードポンプ8の
前で再び吸込み導管24に開口している。
The pump working chamber 6 is formed by a pump cylinder 15 in which the delivery piston 16 of the pressure-transmitting piston 9 operates. Behind the discharge piston 16 is a large-diameter servo piston 1 that works in a pressure cylinder 17.
8 is connected, and this servo piston 18 cooperates with the wall of the pressure cylinder 17 to open the air pressure chamber 19.
is restricted. A conduit 10 branches off from the pump cylinder 15 on the one hand, and a fuel supply conduit 20 opens into the pump cylinder 15 on the other hand. The fuel supply conduit 20 branches off from a fuel conveying conduit 21 which is connected to the outlet of the fuel feed pump 8 and serves to supply all fuel injection valves with fuel. The fuel conveying conduit 20 is allowed to pass only in the fuel supply direction, and therefore, the fuel conveying conduit 21 is allowed to pass from the pump working chamber 6 during the discharge stroke of the pressure transmitting piston 9.
A check valve 22 is provided to prevent backflow of fuel to. The fuel feed pump 8 sucks fuel from the fuel tank 13 via a filter 23 and a suction conduit 24 and transfers this fuel to the fuel delivery conduit 21 at a pressure approximately 10-20% lower than the opening pressure of the fuel injection valve 1.
Discharge into. A pressure regulating valve 25 is assigned to the fuel feed pump 8 in order to regulate and maintain the desired discharge pressure. This pressure regulating valve 25 is arranged in a pressure monitoring line which branches off from the fuel conveying line 21 downstream of the fuel feed pump 8 and again into the suction line 24 before the fuel feed pump 8 in the flow direction. It's open.

各空気圧力室19に圧力空気を供給するために
空気タンク26が設けられており、この空気タン
ク26には、電動機27によつて駆動されるコン
プレツサ28によつて圧力空気が供給されるよう
になつている。コンプレツサ28は必要な空気を
空気フイルタ29及び吸込み導管30を介して吸
い込み、圧縮された空気を搬送導管31を介して
空気タンク26に圧送する。搬送導管31には、
搬送方向に開放する逆止弁32及び圧力調整弁3
3が設けられており、圧力調整弁33は内燃機関
の所定の運転フアクタに関連して調節されるよう
になつている。
An air tank 26 is provided to supply pressurized air to each air pressure chamber 19, and this air tank 26 is supplied with pressurized air by a compressor 28 driven by an electric motor 27. It's summery. Compressor 28 sucks in the required air via air filter 29 and suction conduit 30 and pumps the compressed air via conveying conduit 31 to air tank 26 . The conveyance conduit 31 includes
Check valve 32 and pressure regulating valve 3 that open in the conveying direction
3 is provided, and the pressure regulating valve 33 is adapted to be adjusted in relation to certain operating factors of the internal combustion engine.

空気タンク26からは、すべての空気圧力室1
9に圧力空気を供給するために働く空気主導管3
4が延びている。各空気圧力室19には、空気主
導管34から分岐している空気供給導管35を介
して圧力空気が供給される。空気供給導管35に
は、電磁石によつて作動される2方向切換え制御
弁36が設けられており、この2方向切換え制御
弁36は1つの入口と2つの出口を有しており、
この場合入口には空気供給導管35が、第1の出
口には空気圧力室19と接続された加圧兼放圧導
管37が、そして第2の出口には放圧導管38が
接続されている。空気損失を回避するために、空
気圧力室19の放圧時に生じる空気は放圧導管3
8及び主集合導管40を介して共通の空気集合タ
ンク39に送られ、この空気集合タンク39か
ら、吸込み導管30に開口している流出導管41
を介してコンプレツサ28によつて吸い込まれ
る。空気集合タンク39における圧力は大気圧よ
りも高いので、吸込み導管30には流出導管41
の開口箇所の前後に、吸込み方向に開放する逆止
弁42,43が1つずつ設けられている。このこ
とに関して付け加えておくと、空気圧力室19の
放圧が大気中に行われることも可能である。ポン
プシリンダ15から、すなわち、圧力伝達ピスト
ン9の往復動時に圧力伝達ピストン9の吐出ピス
トン16によつて解放されないポンプシリンダ範
囲からは、燃料タンク13に通じている漏れ燃料
導管44が分岐している。この漏れ燃料導管44
には圧力調整弁45が設けられており、この圧力
調整弁45は、漏れ燃料圧が燃料噴射弁の開放圧
と等しいか又はそれよりも高くなるように調節さ
れている。
From the air tank 26, all air pressure chambers 1
Air main pipe 3 serving to supply pressurized air to 9
4 is extended. Each air pressure chamber 19 is supplied with pressurized air via an air supply conduit 35 branching from the main air conduit 34 . The air supply conduit 35 is provided with a two-way switching control valve 36 actuated by an electromagnet, the two-way switching control valve 36 having one inlet and two outlets;
In this case, an air supply conduit 35 is connected to the inlet, a pressurization/relief conduit 37 connected to the air pressure chamber 19 is connected to the first outlet, and a pressure relief conduit 38 is connected to the second outlet. . In order to avoid air losses, the air generated when the air pressure chamber 19 is relieved is transferred to the relief conduit 3.
8 and a main collecting conduit 40 to a common air collecting tank 39 , from which an outflow conduit 41 opens into the suction conduit 30 .
The air is sucked in by the compressor 28 through the air. Since the pressure in the air collection tank 39 is higher than atmospheric pressure, the suction conduit 30 is connected to the outflow conduit 41.
One check valve 42, 43, which opens in the suction direction, is provided before and after the opening location. It should be noted in this connection that it is also possible for the air pressure chamber 19 to be depressurized to the atmosphere. From the pump cylinder 15 , that is to say from the pump cylinder region which is not released by the delivery piston 16 of the pressure-transmitting piston 9 during the reciprocating movement of the pressure-transmitting piston 9 , a leakage fuel line 44 , which leads to the fuel tank 13 , branches off. . This leakage fuel conduit 44
is provided with a pressure regulating valve 45, which is adjusted so that the leakage fuel pressure is equal to or higher than the opening pressure of the fuel injection valve.

ポンプ作業室6と燃料噴射弁1との間の導管1
0には、流れ方向で見て前置弁11の後ろに圧力
監視装置46が接続されている。この圧力監視装
置46は、噴射過程において起こり得る不規則性
を信号化するためにアラーム装置47と及び(又
は)、非常停止処置をトリガすることができしか
もマイクロプロセツサを有していて燃料噴射装置
に固有な電子式の調整兼制御装置48と接続され
ていてもよい。
Conduit 1 between pump working chamber 6 and fuel injection valve 1
0, a pressure monitoring device 46 is connected behind the upstream valve 11 in the flow direction. This pressure monitoring device 46 has an alarm device 47 to signal possible irregularities in the injection process and/or can trigger an emergency shutdown procedure and has a microprocessor to control the fuel injection. It may also be connected to an electronic regulation and control device 48 specific to the device.

前置弁11、放圧弁12及び2方向切換え制御
弁36はそれぞれ過励磁されるリフテイング磁石
によつて作動させられるようになつており、この
リフテイング磁石は圧力調整弁33並びに場合に
よつては燃料噴射装置の別の2つの圧力調整弁2
5,45と同様に、電子式の調整兼制御装置48
から制御命令を与えられる。圧力調整弁33はこ
の場合機関の運転フアクタ例えば回転数、吸気圧
又はこれに類したものに関連して調節され、この
結果各空気圧力室19には、機関の現在の又は望
まれる運転条件にその都度適合した圧力で空気が
供給されるようになつている。このような空気圧
が可変であることによつて、燃料側において噴射
過程に適当な影響を与えること、ひいては噴射過
程を機関の現在の又は所望の運転条件に適合させ
ることが保証されている。
The front valve 11, the pressure relief valve 12 and the two-way control valve 36 are each actuated by an overexcited lifting magnet, which lifts the pressure regulating valve 33 and, if necessary, the fuel. Another two pressure regulating valves 2 of the injector
Similar to 5 and 45, electronic adjustment and control device 48
Control commands are given by. The pressure regulating valve 33 is adjusted in this case in relation to operating factors of the engine, such as rotational speed, intake pressure or the like, so that each air pressure chamber 19 is supplied with air depending on the current or desired operating conditions of the engine. Air is supplied at the appropriate pressure each time. This variable air pressure ensures a suitable influence on the injection process on the fuel side and thus adaptation of the injection process to the current or desired operating conditions of the engine.

次に本発明による燃料噴射装置の作用形式を完
全な噴射サイクルに基づいて記載する。出発位置
は次のように仮定されている。ポンプ作業室6は
既に燃料によつて満たされており、さらに前置弁
11は閉鎖位置に、放圧弁12は開放位置に位置
しており、2方向切換え制御弁36は放圧のため
の切換え位置を占めている。これによつて空気圧
力室19は放圧されており、さらに2方向切換制
御弁36の入口には所望の圧力の空気がある。
The mode of operation of the fuel injection device according to the invention will now be described on the basis of a complete injection cycle. The starting position is assumed as follows. The pump work chamber 6 is already filled with fuel, the prevalve 11 is in the closed position, the pressure relief valve 12 is in the open position, and the two-way control valve 36 is switched for pressure relief. occupying a position. As a result, the air pressure chamber 19 is depressurized and, furthermore, air at the desired pressure is present at the inlet of the two-way control valve 36.

噴射過程を行うことが望まれると、調整兼制御
装置48から制御導線49を介して2方向切換え
制御弁36にパルス信号が送られ、制御導線49
に接続されているリフテイング磁石が2方向切換
え制御弁36を引き寄せて、図面に示されている
貫流位置に移動させる。これによつて、空気供給
導管35内で2方向切換え制御弁36の入口にあ
る圧力空気は加圧兼放圧導管37を介して空気圧
力室19に供給される。適当な時期に調整兼制御
装置48から制御導線50を介して前置弁11の
リフテイング磁石にパルス信号が送られ、この結
果前置弁11は開放し、燃料路はポンプ作業室6
から導管10を介して燃料噴射弁1に向かつて開
放される。同時に制御導線51を介して放圧弁1
2のリフテイング磁石にパルス信号が送られ、放
圧弁12は閉鎖して放圧導管14は遮断される。
空気圧力室19における圧力空気によつて圧力伝
達ピストン9は図面で見て下に向かつて移動せし
められ、圧力伝達ピストン9の吐出ピストン16
はポンプ作業室6内の燃料を該ポンプ作業室6か
ら押し出し、燃料噴射弁1に圧送する。燃料噴射
弁1の燃料貯え室4における燃料圧が燃料噴射弁
1の開放圧を越えるやいなや、燃料噴射弁1は開
放して噴射過程が完了する。この場合、あらかじ
めポンプ作業室6に貯えられていた燃料量が最大
限に噴射され得る。噴射過程が終了すると、前置
弁11は再び閉鎖され、同時に調整兼制御装置4
8からは制御導線51を介して放圧弁12のリフ
テイング磁石にパルス信号が送られ、この結果放
圧弁12は開放し、前置弁11の下流の燃料路に
おける圧力は放圧導管14を介して降下する。同
時に調整兼制御装置48は制御導線52を介して
2方向切換え制御弁36の他方のリフテイング磁
石に命令が与えられて、2方向切換え制御弁36
は放圧位置に移動せしめられる。この放圧位置で
は加圧兼放圧導管37は放圧導管38と接続され
て、空気圧力室19内の空気圧は接続された導管
路を介して低下せしめられる。次いでポンプ作業
室6は燃料供給導管20を介して新たに燃料を満
たされ、圧力伝達ピストン9は再び出発位置に戻
される。これによつて燃料噴射装置は新たな噴射
過程のための準備状態になる。
When it is desired to carry out an injection process, a pulse signal is sent from the regulator and control device 48 via a control line 49 to the two-way control valve 36;
A lifting magnet connected to pulls the two-way switching control valve 36 into the flow-through position shown in the drawings. Thereby, the pressurized air present in the air supply conduit 35 at the inlet of the two-way control valve 36 is supplied to the air pressure chamber 19 via the pressurization and pressure relief conduit 37. At the appropriate time, a pulse signal is sent from the regulator and control device 48 via the control line 50 to the lifting magnet of the front valve 11, so that the front valve 11 is opened and the fuel line is opened to the pump work chamber 6.
The fuel injection valve 1 is opened from the fuel injection valve 1 via a conduit 10. At the same time, via the control line 51, the pressure relief valve 1 is
A pulse signal is sent to the lifting magnet No. 2, the pressure relief valve 12 is closed and the pressure relief conduit 14 is cut off.
The pressure transmission piston 9 is moved downward in the drawing by the pressurized air in the air pressure chamber 19, and the discharge piston 16 of the pressure transmission piston 9 is moved downward.
pushes the fuel in the pump working chamber 6 out of the pump working chamber 6 and forcefully feeds it to the fuel injection valve 1. As soon as the fuel pressure in the fuel storage chamber 4 of the fuel injection valve 1 exceeds the opening pressure of the fuel injection valve 1, the fuel injection valve 1 opens and the injection process is completed. In this case, the maximum amount of fuel previously stored in the pump working chamber 6 can be injected. At the end of the injection process, the prevalve 11 is closed again and at the same time the regulating and control device 4 is closed.
8 sends a pulse signal via a control line 51 to the lifting magnet of the pressure relief valve 12, so that the pressure relief valve 12 opens and the pressure in the fuel line downstream of the front valve 11 is reduced via the pressure relief line 14. Descend. At the same time, the regulating and controlling device 48 is commanded via a control line 52 to the other lifting magnet of the two-way control valve 36 .
is moved to the pressure release position. In this pressure relief position, the pressurization and pressure relief line 37 is connected to the pressure relief line 38, and the air pressure in the air pressure chamber 19 is reduced via the connected line. The pump working chamber 6 is then refilled with fuel via the fuel supply line 20 and the pressure-transmitting piston 9 is returned to its starting position again. This prepares the fuel injection system for a new injection process.

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

図面は本発明による燃料噴射装置の原理的な構
成を略示する回路図である。 1…燃料噴射弁、2…弁ニードル、3…閉鎖ば
ね、4…燃料貯え室、5…供給導管、6…ポンプ
作業室、7,27…電動機、8…燃料フイードポ
ンプ、9…圧力伝達ピストン、10…導管、11
…前置弁、12…放圧弁、13…燃料タンク、1
4…放圧導管、15…ポンプシリンダ、16…吐
出ピストン、17…圧力シリンダ、18…サーボ
ピストン、19…空気圧力室、20…空気供給導
管、21…燃料搬送導管、22,32,42,4
3…逆止弁、23…フイルタ、24…吸込み導
管、25…圧力調整弁、26…空気タンク、28
…コンプレツサ、29…空気フイルタ、30…吸
込み導管、31…搬送導管、33…圧力調整弁、
34…空気主導管、35…空気供給導管、36…
2方向切換え制御弁、37…加圧兼放圧導管、3
8…放圧導管、39…空気集合タンク、40…主
集合導管、41…流出導管、44…漏れ燃料導
管、45…圧力調整弁、46…圧力監視装置、4
7…アラーム装置、48…調整兼制御装置、4
9,50,51,52…制御導線。
The drawing is a circuit diagram schematically showing the basic structure of a fuel injection device according to the present invention. DESCRIPTION OF SYMBOLS 1... Fuel injection valve, 2... Valve needle, 3... Closing spring, 4... Fuel storage chamber, 5... Supply conduit, 6... Pump working chamber, 7, 27... Electric motor, 8... Fuel feed pump, 9... Pressure transmission piston, 10... conduit, 11
... Front valve, 12 ... Pressure relief valve, 13 ... Fuel tank, 1
4...Pressure conduit, 15...Pump cylinder, 16...Discharge piston, 17...Pressure cylinder, 18...Servo piston, 19...Air pressure chamber, 20...Air supply conduit, 21...Fuel transfer conduit, 22, 32, 42, 4
3... Check valve, 23... Filter, 24... Suction conduit, 25... Pressure regulating valve, 26... Air tank, 28
... Compressor, 29... Air filter, 30... Suction conduit, 31... Conveyance conduit, 33... Pressure regulating valve,
34...Air main conduit, 35...Air supply conduit, 36...
Two-way switching control valve, 37... Pressurization and pressure relief conduit, 3
8... Pressure relief pipe, 39... Air collecting tank, 40... Main collecting pipe, 41... Outflow pipe, 44... Leakage fuel pipe, 45... Pressure regulating valve, 46... Pressure monitoring device, 4
7...Alarm device, 48...Adjustment and control device, 4
9, 50, 51, 52...control conductor.

Claims (1)

【特許請求の範囲】 1 内燃機関用の燃料噴射装置であつて、各機関
シリンダに1つの燃料噴射弁1が設けられてい
て、該燃料噴射弁1の弁ニードル2が、供給され
る燃料の圧力によつて閉鎖ばねの力に抗して開放
方向に運動せしめられるようになつており、 燃料噴射弁1の燃料貯え室4が、供給導管5,
10を介して燃料噴射装置のポンプ作業室6に接
続されており、該ポンプ作業室6が、最大噴射燃
料量の収容を可能にする容積を有していて、該ポ
ンプ作業室6の方向に向かつてしか開放しない逆
止弁22を有する燃料供給導管20を介して、常
に燃料フイードポンプ8と接続されており、 該燃料フイードポンプ8の吐出圧が一定で、燃
料噴射弁1の開放圧よりも低く設定されており、 燃料が燃料噴射装置のポンプ作業室6から、内
燃機関のサイクルで圧力空気によつて作動可能な
圧力伝達ピストン9を用いて、燃料噴射弁1に供
給可能であり、 ポンプ作業室6がポンプシリンダ15によつて
形成されていて、圧力伝達ピストン9に、該ポン
プシリンダ15内を摺動しかつポンプ作業室6を
制限する吐出ピストン16が設けられており、該
吐出ピストン16には、ポンプ作業室6とは反対
の側において、圧力シリンダ17内を摺動する大
径のサーボピストン18が設けられていて、該サ
ーボピストン18が、吐出ピストン16とは反対
の側に位置する空気圧力室19を制限しており、 該空気圧力室19が、電磁作動式の2方向切換
え制御弁36の出口に接続されていて、該2方向
切換え制御弁36を介して、圧力伝達ピストン9
を作動させるために空気タンク26に接続される
か、又は切換えによつて、放圧導管38に接続さ
れるようになつている形式のものにおいて、 空気圧力室19に2方向切換え制御弁36を介
して圧力空気を供給するために、電磁作動式のコ
ンプレツサ28によつて連続的に圧力空気を供給
される空気タンク26が設けられており、ポンプ
作業室6と燃料噴射弁1との間における供給導管
10が、内燃機関のサイクルで、2方向切換え制
御弁36によつて制御された空気圧力室19の圧
力負荷時間内において任意に切換え可能な前置弁
11を用いて、開閉制御可能であり、燃料流れ方
向で見て該前置弁11に後置された放圧弁12を
用いて、前置弁11の閉鎖後に放圧可能である ことを特徴とする、内燃機関用の燃料噴射装置。 2 コンプレツサ28から空気タンク26に通じ
る搬送導管31に、搬送方向に開放する逆止弁3
2と、内燃機関の規定の運転フアクタに関連して
調節可能な圧力調整弁33とが配置されている、
特許請求の範囲第1項記載の燃料噴射装置。 3 2方向切換え制御弁36の放圧導管38が第
2の空気タンク39と接続されており、該空気タ
ンク39から放圧導管38を介して戻される圧力
空気が、コンプレツサ28によつて吸込み可能で
あり、2方向切換え制御弁36と接続された空気
タンク26に新たに導入可能である、特許請求の
範囲第1項又は第2項記載の燃料噴射装置。 4 前置弁11と放圧弁12と2方向切換え制御
弁36とが、過励磁されるリフテイング磁石によ
つて作動されるようになつており、該リフテイン
グ磁石及び圧力調整弁33が、マイクロプロセツ
サを備えた電子式の調整兼制御装置48の制御信
号によつて、制御可能である、特許請求の範囲第
2項又は第3項記載の燃料噴射装置。 5 ポンプ作業室6と燃料噴射弁1との間の供給
導管10に、流れ方向で見て前置弁11及び放圧
導管14の後ろ側に圧力監視装置46が接続され
ており、該圧力監視装置46が、噴射過程中に起
こり得る不規則性を信号化するために、緊急停止
処置をトリガする調整兼制御装置48及びアラー
ム装置47と又はいずれか一方の装置と接続され
ている、特許請求の範囲第1項から第4項までの
いずれか1項記載の燃料噴射装置。 6 燃料フイードポンプ8が電動機によつて駆動
されるようになつており、調節される吐出圧を一
定に保つために燃料フイードポンプ8に圧力調整
弁25が配属されている、特許請求の範囲第1項
から第5項までのいずれか1項記載の燃料噴射装
置。
[Scope of Claims] 1. A fuel injection device for an internal combustion engine, in which each engine cylinder is provided with one fuel injection valve 1, and a valve needle 2 of the fuel injection valve 1 is configured to inject fuel to be supplied. The fuel storage chamber 4 of the fuel injection valve 1 is moved in the opening direction by pressure against the force of the closing spring, and the fuel storage chamber 4 of the fuel injection valve 1 is connected to the supply conduit 5,
10 to the pump working chamber 6 of the fuel injection device, which pump working chamber 6 has a volume that makes it possible to accommodate the maximum amount of injected fuel, and which has a volume in the direction of the pump working chamber 6. It is always connected to a fuel feed pump 8 via a fuel supply conduit 20 having a check valve 22 that opens only when it is in the opposite direction, and the discharge pressure of the fuel feed pump 8 is constant and lower than the opening pressure of the fuel injection valve 1. and fuel can be supplied from the pump working chamber 6 of the fuel injector to the fuel injection valve 1 by means of a pressure transmission piston 9 actuatable by pressurized air in the cycle of the internal combustion engine, and the pump working A chamber 6 is formed by a pump cylinder 15 , and the pressure-transmitting piston 9 is provided with a delivery piston 16 that slides in the pump cylinder 15 and delimits the pump working space 6 . is provided with a large-diameter servo piston 18 sliding in the pressure cylinder 17 on the side opposite the pump working chamber 6, the servo piston 18 being located on the side opposite the discharge piston 16. The air pressure chamber 19 is connected to the outlet of an electromagnetically actuated two-way switching control valve 36, and via the two-way switching control valve 36, a pressure transmitting piston is connected. 9
A two-way switching control valve 36 is provided in the air pressure chamber 19, in the version that is adapted to be connected to the air tank 26 or, by switching, to the pressure relief conduit 38 for actuating the air pressure chamber 19. An air tank 26 is provided which is continuously supplied with pressurized air by an electromagnetically actuated compressor 28 in order to supply pressurized air between the pump working chamber 6 and the fuel injection valve 1. The supply conduit 10 can be controlled to open and close during the cycle of the internal combustion engine using a front valve 11 which can be switched at will during the pressure load time of the air pressure chamber 19 controlled by the two-way control valve 36. A fuel injection device for an internal combustion engine, characterized in that the pressure can be released after the front valve 11 is closed, using a pressure relief valve 12 located after the front valve 11 when viewed in the fuel flow direction. . 2 A check valve 3 that opens in the conveying direction is installed in the conveying conduit 31 leading from the compressor 28 to the air tank 26.
2 and a pressure regulating valve 33 which is adjustable in relation to the defined operating factors of the internal combustion engine,
A fuel injection device according to claim 1. 3. The pressure relief line 38 of the two-way control valve 36 is connected to a second air tank 39, from which the pressurized air returned via the pressure relief line 38 can be sucked in by the compressor 28. The fuel injection device according to claim 1 or 2, which can be newly introduced into the air tank 26 connected to the two-way switching control valve 36. 4. The front valve 11, the pressure relief valve 12, and the two-way switching control valve 36 are operated by a lifting magnet that is overexcited, and the lifting magnet and the pressure regulating valve 33 are operated by a microprocessor. 4. The fuel injection device according to claim 2, wherein the fuel injection device is controllable by a control signal of an electronic adjustment and control device 48 having a control signal. 5 A pressure monitoring device 46 is connected to the supply conduit 10 between the pump working chamber 6 and the fuel injection valve 1 behind the upstream valve 11 and the pressure relief conduit 14, viewed in the flow direction, and which pressure monitoring device 46 It is claimed that the device 46 is connected to a regulating and controlling device 48 and/or an alarm device 47 to signal irregularities that may occur during the injection process, triggering an emergency shutdown procedure. The fuel injection device according to any one of the ranges 1 to 4. 6. The fuel feed pump 8 is adapted to be driven by an electric motor, and a pressure regulating valve 25 is assigned to the fuel feed pump 8 in order to keep the adjusted discharge pressure constant. 5. The fuel injection device according to any one of items 1 to 5.
JP14488482A 1981-08-22 1982-08-23 Fuel injector for internal combustion engine Granted JPS5844262A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813133288 DE3133288A1 (en) 1981-08-22 1981-08-22 Fuel injection system on an internal combustion engine
DE31332889 1981-08-22

Publications (2)

Publication Number Publication Date
JPS5844262A JPS5844262A (en) 1983-03-15
JPH0514104B2 true JPH0514104B2 (en) 1993-02-24

Family

ID=6139905

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14488482A Granted JPS5844262A (en) 1981-08-22 1982-08-23 Fuel injector for internal combustion engine

Country Status (3)

Country Link
JP (1) JPS5844262A (en)
CH (1) CH657422A5 (en)
DE (1) DE3133288A1 (en)

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JPS60162021A (en) * 1984-01-31 1985-08-23 Kawasaki Heavy Ind Ltd Fuel injection control device of internal-combustion engine
JPH071029B2 (en) * 1987-07-29 1995-01-11 いすゞ自動車株式会社 Accumulation type fuel injection device
EP0371759A3 (en) * 1988-11-29 1990-08-22 The University Of British Columbia Intensifier-injector for gaseous fuel for positive displacement engines
US5479901A (en) * 1994-06-27 1996-01-02 Caterpillar Inc. Electro-hydraulic spool control valve assembly adapted for a fuel injector
EP0962649A1 (en) * 1998-06-04 1999-12-08 Wolfgang Dr. Heimberg Fuel injection apparatus
DE19948464A1 (en) * 1999-10-08 2001-04-12 Bosch Gmbh Robert Common rail fuel injection system

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JPS522032B2 (en) * 1972-03-11 1977-01-19
JPS53109021A (en) * 1977-03-07 1978-09-22 Nippon Denso Co Ltd Fuel injection device for internal combustion engine
JPS555419A (en) * 1978-06-23 1980-01-16 Mitsubishi Heavy Ind Ltd Fuel injection system of pressure accumulation type

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Also Published As

Publication number Publication date
DE3133288C2 (en) 1989-02-23
CH657422A5 (en) 1986-08-29
JPS5844262A (en) 1983-03-15
DE3133288A1 (en) 1983-03-03

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