EP1123463B1 - Fuel injection system for an internal combustion engine - Google Patents

Fuel injection system for an internal combustion engine Download PDF

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Publication number
EP1123463B1
EP1123463B1 EP00958211A EP00958211A EP1123463B1 EP 1123463 B1 EP1123463 B1 EP 1123463B1 EP 00958211 A EP00958211 A EP 00958211A EP 00958211 A EP00958211 A EP 00958211A EP 1123463 B1 EP1123463 B1 EP 1123463B1
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EP
European Patent Office
Prior art keywords
pressure
fuel
injection system
fuel injection
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP00958211A
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German (de)
French (fr)
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EP1123463A1 (en
Inventor
Bernd Mahr
Martin Kropp
Hans-Christoph Magel
Wolfgang Otterbach
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Robert Bosch GmbH
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Robert Bosch GmbH
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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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/022Injectors structurally combined with fuel-injection pumps characterised by the pump drive
    • F02M57/025Injectors structurally combined with fuel-injection pumps characterised by the pump drive hydraulic, e.g. with pressure amplification
    • F02M57/026Construction details of pressure amplifiers, e.g. fuel passages or check valves arranged in the intensifier piston or head, particular diameter relationships, stop members, arrangement of ports or conduits
    • 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
    • F02M41/00Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
    • F02M41/02Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor being spaced from pumping elements
    • F02M41/06Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor being spaced from pumping elements the distributor rotating
    • 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
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • 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
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
    • F02M47/027Electrically actuated valves draining the chamber to release the closing 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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/022Injectors structurally combined with fuel-injection pumps characterised by the pump drive
    • F02M57/025Injectors structurally combined with fuel-injection pumps characterised by the pump drive hydraulic, e.g. with pressure amplification
    • 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
    • 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
    • F02M63/02Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
    • F02M63/0225Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails

Definitions

  • the invention is based on a fuel injection system for an internal combustion engine according to the preamble of the claim 1.
  • Such an injection system is for example by the DE 41 18 237 A has become known.
  • a pressure-controlled fuel injection system is controlled by the pressure prevailing in the nozzle chamber of an injector fuel pressure valve body (eg a nozzle needle) against the action of a closing force and thus released the injection port for injection of the fuel.
  • the pressure with which fuel exits the nozzle chamber into the cylinder is referred to as injection pressure.
  • a stroke-controlled fuel injection system is understood to mean that the opening and closing of the injection opening of an injector take place by means of a displaceable valve member due to the hydraulic interaction of the fuel pressures in a nozzle space and in a control space.
  • an arrangement will be referred to as central if it is common to all cylinders, and local if provided for only a single cylinder.
  • a disadvantage of this known fuel injection system is that first of all the fuel only to the higher Pressure level must be compressed, then one Part of the fuel back to the lower pressure level relieve.
  • two pressure accumulators are required to store the two fuel pressures.
  • the high pressure pump is because it is driven by the camshaft of the engine is, permanently in the enterprise and also then, if the desired pressure in the respective accumulator already is constructed. This permanent high pressure generation and the subsequent relief to the low pressure level a better efficiency.
  • High pressure accumulator is the fuel pressure for strength reasons currently limited to a maximum of about 1800 bar.
  • WO 98/09068 From WO 98/09068 is a stroke-controlled injection system known, in which also two pressure accumulator for storage the two fuel pressures are provided. For each Accumulator is provided its own high-pressure pump, which is permanently in operation and even if the desired pressure already built up in the respective accumulator is.
  • the invention is defined by the features of claim 1.
  • a second higher pressure level by means of a pressure booster generated. Because this translated pressure is not in one Pressure accumulator is stored, can be a higher injection pressure be achieved. Both pressure levels can be used for Representation of a flexible injection such as a boat-shaped Injection, pre and post injection used become.
  • first embodiment of a pressure-controlled fuel injection system 1 promotes a high pressure pump 2 fuel 3 from a storage tank 4 via a feed line 5 to a central pressure booster unit 6 at high pressure, which is constructed by energizing a 2/2-way valve 7 ,
  • the high-pressure pump 2 can produce a first (lower) fuel pressure of about 300 to about 1000 bar and, for example, be a cam pump with injection adjuster similar to the distributor injection pump known from DE 35 16 867 A1.
  • an even higher fuel pressure can be generated via the central pressure booster unit 6.
  • an injection pressure of more than 2000 bar can be realized.
  • the respectively present fuel pressure is then distributed from a central distribution device 8 to a plurality of high-pressure lines 9 corresponding to the number of individual cylinders, which discharge to the individual injectors 10 (injection device) projecting into the combustion chamber of the internal combustion engine to be supplied.
  • a central distribution device 8 to a plurality of high-pressure lines 9 corresponding to the number of individual cylinders, which discharge to the individual injectors 10 (injection device) projecting into the combustion chamber of the internal combustion engine to be supplied.
  • Fig. 1 only one of the injectors 10 is shown in more detail.
  • the central pressure booster unit 6 comprises a pressure booster 11 with a pressure means 12 in the form of a displaceable piston element, which can be connected at one end to the delivery line 5 by means of a valve unit 13 , so that it is pressurized by the fuel located in a primary chamber 14 at one end.
  • a differential space 15 is depressurized by means of a leakage line 16 , so that the pressure medium 12 can be displaced in the compression direction to reduce the volume of a pressure chamber 17 .
  • the fuel in the pressure chamber 17 is compressed corresponding to the area ratio of the primary chamber 14 and the pressure chamber 17 to the higher fuel pressure.
  • the pressure booster 11 can be bypassed by a parallel bypass line 19 , which can be activated or deactivated by means of the valve unit 13.
  • the valve unit 13 is formed in front of the pressure booster 11 and as a 3/2-way valve.
  • the parts 11, 13 and 19 form the central pressure booster unit 6.
  • the respectively present at the manifold 8 fuel pressure is passed through the pressure line 9 into a nozzle chamber 20 of the injector 10.
  • the injection is pressure-controlled by means of an axially displaceable in a guide bore piston-shaped valve member 21 (nozzle needle), the conical valve sealing surface 22 cooperates with a valve seat surface on the injector and thus closes the injection openings 23 provided there.
  • the nozzle chamber 20 a in the opening direction of the valve member 21 facing pressure surface of the valve member 21 is exposed to the pressure prevailing there, wherein the nozzle chamber 20 continues through an annular gap between the valve member 21 and the guide bore to the valve sealing surface 22 of the injector 10.
  • each injector 10 By the pressure prevailing in the nozzle chamber 20 pressure, the injection openings 23 sealing valve member 21 is controlled against the action of a closing force (closing spring 24 ), wherein the spring chamber 25 is depressurized by means of a leakage line 26 .
  • a check valve assembly 27 Behind the manifold 8 for each injector 10 each still a check valve assembly 27 is provided which allows the fuel in the direction of the injector 10 via a first check valve 28 and the return of fuel from the injector 10 by means of a throttle 29 and a second check valve 30 to relieve the Distributor 8 and the pressure reduction permits.
  • a pre-injection with the lower fuel pressure takes place in de-energized valve unit 13 by energizing the 2/2-way valve 7. By energizing also the valve unit 13 then takes the main injection with the higher Fuel pressure. For a post-injection with the deeper Fuel pressure, the valve unit 13 back in switched back to the de-energized state. Will the primary chamber 14 with the help of the valve unit 13 at no-current 2/2-way valve 7 connected to the input of the high pressure pump 2, so the provision of the pressure medium done 12 and the refilling of the pressure chamber 17, over the check valve 18 is connected to the delivery line 5 is.
  • valve unit 13a is formed behind the pressure booster 11 and a 2/2-way valve, which is decoupled from the bypass line 19 via a check valve 31 .
  • the parts 11, 13a, 19 and 31 form the central pressure booster unit 6a.
  • the pressure booster unit 41 is not provided centrally but locally for each injector 10 individually.
  • the local pressure booster unit 41 like the central pressure booster unit 6 shown in FIG. 1 a, comprises a pressure booster 42 with a check valve 43 and a valve unit 44 for switching between the pressure booster 42 and the bypass duct 45.
  • the high-pressure pump 2 conveys the fuel via the delivery line 5 into a central pressure accumulator 51 (common rail), in which the fuel is stored under a pressure of approximately 300 to approximately 600 bar.
  • a central valve unit 52 eg, a 3/2-way valve
  • the fuel from the pressure accumulator 51 via the central distribution device 8 is forwarded to the individual pressure-controlled injectors 10.
  • Each injector 10 is associated with a local pressure booster unit 53 with a pressure booster 54 , by means of which, if necessary from the lower fuel pressure of the pressure accumulator 51, a higher fuel pressure can be generated.
  • the local pressure booster 54 Via the valve unit 55 (3/2-way valve), the local pressure booster 54, which is constructed analogously to the central pressure booster 11, are activated.
  • the pressure chamber 56 of the local pressure booster 54 is filled with fuel from the pressure accumulator 51, wherein a check valve 57 in a bypass line 58 parallel to the pressure booster 54 prevents the return of compressed fuel back into the pressure accumulator 51.
  • the parts 54, 55, 57 and 58 form the local pressure booster unit 53, which may be either inside the injector housing ( FIG. 3a ) or outside ( FIG. 3b ).
  • a pilot injection with the lower fuel pressure of the central pressure accumulator 51 takes place with currentless valve unit 55 by energizing the central 3/2-way valve 52. By energizing the valve unit 55 and then the main injection with the higher fuel pressure. For a post-injection with the lower fuel pressure, the valve unit 55 is switched back to the de-energized state. At the end of the injection, the central valve unit 52 is switched back to leakage 59 and thus the manifold 8 and the injector 10 relieved.
  • the injection system 60 shown in Fig. 4 differs by the use of stroke-controlled injectors 61 and the formation of the central valve unit 62 as a 2/2-way valve.
  • the pressure-controlled injector 10 of FIG. 1 engages in a stroke-controlled injector 61 on the valve member 21 coaxial with the valve spring 23 to a pressure piece 63 , which limits the valve sealing surface 22 remote from the end face 64 a control chamber 65.
  • the control chamber 65 has a fuel inlet from the pressure line 9 with a first throttle 66 and a fuel outlet to a pressure relief line 67 with a second throttle 68, which is controllable by a 2/2-way valve 69 to 70 leakage.
  • the pressure piece 63 is pressurized in the closing direction. Under the lower or higher fuel pressure stagnant fuel constantly fills the nozzle chamber 20 and the control chamber 65.
  • the pressure in the control chamber 65 can be reduced, so that in the sequence on the opening direction the valve member 21 acting pressure force in the nozzle chamber 20 exceeds the force acting in the closing direction on the valve member 21 pressing force.
  • the valve sealing surface 22 lifts off the valve seat surface and fuel is injected. In this case, the pressure relief process of the control chamber 65 and thus the stroke control of the valve member 21 via the dimensioning of the two throttles 66 and 68 can be influenced.
  • the end of the injection is initiated by renewed actuation (closing) of the 2/2-way valve 69, which decouples the control chamber 65 again from the leakage line 70, so that in the control chamber 65 again a pressure builds up, the pressure piece 63 in the closing direction can move.
  • the switching of the fuel to either the lower or the higher fuel pressure occurs for each injector 61 in the local pressure booster unit 53 through the valve unit 55.
  • the pressure booster unit 53 can be arranged either inside the injector housing ( FIG. 4a ) or outside ( FIG. 4b ).
  • a fuel injection system 1 for an internal combustion engine different with the fuel with at least two high fuel pressures via injectors 10 in the combustion chamber of the internal combustion engine to be injected can, parallel to a bypass line 19 is a hydraulic Pressure booster 11 for generating the higher fuel pressure provided, wherein the pressure booster 11 via a valve unit 13 can be activated and deactivated. Since the intensifier is not permanently in operation and even the losses are reduced by friction, is the Improved efficiency.

Abstract

In a fuel injection system for an internal combustion engine, in which fuel at at least two differently high fuel pressures can be injected via injectors into the combustion chamber of the engine, parallel to a bypass line a hydraulic pressure booster is provided for generating the higher fuel pressure; the pressure booster is actuatable and deactuatable via a valve unit. Since the pressure booster is not constantly in operation, and the losses from friction are also reduced, the efficiency is improved.

Description

Stand der TechnikState of the art

Die Erfindung geht aus von einem Kraftstoffeinspritzsystem für eine Brennkraftmaschine nach der Gattung des Patentanspruchs 1. The invention is based on a fuel injection system for an internal combustion engine according to the preamble of the claim 1.

Ein derartiges Einpritzsystem ist beispielsweise durch die DE 41 18 237 A bekanntgeworden.Such an injection system is for example by the DE 41 18 237 A has become known.

Zum besseren Verständnis der nachfolgenden Beschreibung werden zunächst einige Begriffe näher erläutert: Bei einem druckgesteuerten Kraftstoffeinspritzsystem wird durch den im Düsenraum eines Injektors herrschenden Kraftstoffdruck ein Ventilkörper (z.B. eine Düsennadel) gegen die Wirkung einer Schließkraft aufgesteuert und so die Einspritzöffnung für eine Einspritzung des Kraftstoffes freigegeben. Der Druck, mit dem Kraftstoff aus dem Düsenraum in den Zylinder austritt, wird als Einspritzdruck bezeichnet. Unter einem hubgesteuerten Kraftstoffeinspritzsystem wird im Rahmen der Erfindung verstanden, daß das Öffnen und Schließen der Einspritzöffnung eines Injektors mit Hilfe eines verschieblichen Ventilglieds aufgrund des hydraulischen Zusammenwirkens der Kraftstoffdrücke in einem Düsenraum und in einem Steuerraum erfolgen. Weiterhin ist im folgenden eine Anordnung als zentral bezeichnet, wenn sie gemeinsam für alle Zylinder vorgesehen ist, und als lokal, wenn sie für nur einen einzelnen Zylinder vorgesehen ist.For a better understanding of the following description, some terms are first explained in more detail: In a pressure-controlled fuel injection system is controlled by the pressure prevailing in the nozzle chamber of an injector fuel pressure valve body (eg a nozzle needle) against the action of a closing force and thus released the injection port for injection of the fuel. The pressure with which fuel exits the nozzle chamber into the cylinder is referred to as injection pressure. In the context of the invention, a stroke-controlled fuel injection system is understood to mean that the opening and closing of the injection opening of an injector take place by means of a displaceable valve member due to the hydraulic interaction of the fuel pressures in a nozzle space and in a control space. Further, hereinafter, an arrangement will be referred to as central if it is common to all cylinders, and local if provided for only a single cylinder.

Bei dem aus der EP 0 711 914 A1 bekannten druckgesteuerten Kraftstoffeinspritzsystem wird mit Hilfe einer Hochdruckpumpe Kraftstoff auf einen ersten hohen Kraftstoffdruck von etwa 1200 bar komprimiert und in einem ersten Druckspeicher gespeichert. Weiterhin wird der unter Hochdruck stehende Kraftstoff auch in einen zweiten Druckspeicher gefördert, in welchem durch Regelung seiner Kraftstoffzufuhr mittels eines 2/2-Wegventils ein zweiter hoher Kraftstoffdruck von ca. 400 bar aufrechterhalten wird. Über eine Ventilsteuereinheit wird entweder der tiefere oder höhere Kraftstoffdruck in den Düsenraum eines Injektors geleitet. Dort wird durch den Druck ein federbelasteter Ventilkörper von seinem Ventilsitz abgehoben, so daß Kraftstoff aus der Düsenöffnung austreten kann.In the known from EP 0 711 914 A1 pressure controlled Fuel injection system is using a high pressure pump Fuel to a first high fuel pressure compressed from about 1200 bar and in a first accumulator saved. Furthermore, the under high pressure standing fuel also in a second pressure accumulator promoted in which by regulating its fuel supply by means of a 2/2-way valve, a second high fuel pressure of about 400 bar is maintained. Over a Valve control unit is either the lower or higher Fuel pressure passed into the nozzle chamber of an injector. There is a spring-loaded valve body by the pressure lifted off its valve seat so that fuel can escape from the nozzle opening.

Nachteilig bei diesem bekannten Kraftstoffeinspritzsystem ist, daß zunächst der gesamte Kraftstoff erst auf das höhere Druckniveau komprimiert werden muß, um dann einen Teil des Kraftstoffs wieder auf das tiefere Druckniveau zu entlasten. Außerdem sind zwei Druckspeicher erforderlich, um die beiden Kraftstoffdrücke zu lagern. Die Hochdruckpumpe ist, da sie von der Nockenwelle des Motors angetrieben wird, dauerhaft im Betrieb und zwar auch dann, wenn der gewünschte Druck im jeweiligen Druckspeicher bereits aufgebaut ist. Diese permanente Hochdruckerzeugung und die nachfolgende Entlastung auf das Niederdruckniveau stehen einem besseren Wirkungsgrad entgegen. Bei Verwendung von Hochdruckspeichern ist der Kraftstoffdruck aus Festigkeitsgründen derzeit auf maximal ca. 1800 bar beschränkt.A disadvantage of this known fuel injection system is that first of all the fuel only to the higher Pressure level must be compressed, then one Part of the fuel back to the lower pressure level relieve. In addition, two pressure accumulators are required to store the two fuel pressures. The high pressure pump is because it is driven by the camshaft of the engine is, permanently in the enterprise and also then, if the desired pressure in the respective accumulator already is constructed. This permanent high pressure generation and the subsequent relief to the low pressure level a better efficiency. When using High pressure accumulator is the fuel pressure for strength reasons currently limited to a maximum of about 1800 bar.

Aus der WO 98/09068 ist ein hubgesteuertes Einspritzsystem bekannt, bei dem ebenfalls zwei Druckspeicher zur Lagerung der beiden Kraftstoffdrücke vorgesehen sind. Für jeden Druckspeicher ist eine eigene Hochdruckpumpe vorgesehen, die dauerhaft im Betrieb ist und zwar auch dann, wenn der gewünschte Druck im jeweiligen Druckspeicher bereits aufgebaut ist.From WO 98/09068 is a stroke-controlled injection system known, in which also two pressure accumulator for storage the two fuel pressures are provided. For each Accumulator is provided its own high-pressure pump, which is permanently in operation and even if the desired pressure already built up in the respective accumulator is.

Vorteile der ErfindungAdvantages of the invention

Die Erfindung wird durch die Merkamle des Anspruchs 1 definiert. Zur Verbesserung des Wirkungsgrads wird erfindungsgemäß ein zweites höheres Druckniveau mittels eines Druckübersetzers erzeugt. Da dieser übersetzte Druck nicht in einem Druckspeicher gelagert wird, kann ein höherer Einspritzdruck erreicht werden. Die beiden Druckniveaus können zur Darstellung einer flexiblen Einspritzung wie einer boot-förmigen Einspritzung, Vor- und Nacheinspritzung verwendet werden.The invention is defined by the features of claim 1. To improve the efficiency is according to the invention a second higher pressure level by means of a pressure booster generated. Because this translated pressure is not in one Pressure accumulator is stored, can be a higher injection pressure be achieved. Both pressure levels can be used for Representation of a flexible injection such as a boat-shaped Injection, pre and post injection used become.

Weitere Vorteile und vorteilhafte Ausgestaltungen des Gegenstands der Erfindung sind der Beschreibung, der Zeichnung und den Ansprüchen entnehmbar.Further advantages and advantageous embodiments of the subject The invention are the description, the drawing and the claims.

Zeichnungdrawing

Verschiedene Beispiele von Kraftstoffeinspritzsystemen mit einer hydraulischen Druckübersetzungseinheit, bei denen Kraftstoff mit zwei unterschiedlich hohen Kraftstoffdrücken eingespritzt wird, sind in der Zeichnung schematisch dargestellt und in der nachfolgenden Beschreibung erläutert. Es zeigen:

Fig. 1a und 1b
ein erstes, erfindungsgemäßes Kraftstoffeinspritzsystem mit druckgesteuerten Injektoren und einer zentralen Druckübersetzungseinheit;
Fig. 2
ein zweites, nicht erfindungsgemäßes Einspritzsystem mit druckgesteuerten Injektoren und jeweils einer für jeden Injektor vorgesehenen lokalen Druckübersetzungseinheit;
Fig. 3a und 3b
ein drittes, nicht erfindungsgemäßes Einspritzsystem mit druckgesteuerten Injektoren und jeweils einer modifizierten lokalen Druckübersetzungseinheit für jeden Injektor; und
Fig. 4a und 4b
ein viertes, nicht erfindungsgemäßes Einspritzsystem mit hubgesteuerten Injektoren und jeweils der modifizierten lokalen Druckübersetzungseinheit für jeden Injektor.
Various examples of fuel injection systems with a hydraulic pressure booster unit, in which fuel is injected with two different levels of fuel pressure, are shown schematically in the drawing and explained in the following description. Show it:
Fig. 1a and 1b
a first, inventive fuel injection system with pressure-controlled injectors and a central pressure booster unit;
Fig. 2
a second, non-inventive injection system with pressure-controlled injectors and each provided for each injector local pressure booster unit;
Fig. 3a and 3b
a third, not according to the invention injection system with pressure-controlled injectors and in each case a modified local pressure booster unit for each injector; and
Fig. 4a and 4b
a fourth, not inventive injection system with stroke-controlled injectors and each of the modified local pressure booster unit for each injector.

Beschreibung der AusführungsbeispieleDescription of the embodiments

Bei dem in Fig. 1a dargestellten ersten Ausführungsbeispiel eines druckgesteuerten Kraftstoffeinspritzsystems 1 fördert eine Hochdruckpumpe 2 Kraftstoff 3 aus einem Vorratstank 4 über eine Förderleitung 5 zu einer zentralen Druckübersetzungseinheit 6 mit hohem Druck, der durch Bestromen eines 2/2-Wege-Ventils 7 aufgebaut wird. Die Hochdruckpumpe 2 kann einen ersten (tieferen) Kraftstoffdruck von ca. 300 bis ca. 1000 bar erzeugen und z.B. eine Nokkenpumpe mit Spritzversteller ähnlich der aus DE 35 16 867 A1 bekannten Verteilereinspritzpumpe sein.In the illustrated in Fig. 1a first embodiment of a pressure-controlled fuel injection system 1 promotes a high pressure pump 2 fuel 3 from a storage tank 4 via a feed line 5 to a central pressure booster unit 6 at high pressure, which is constructed by energizing a 2/2-way valve 7 , The high-pressure pump 2 can produce a first (lower) fuel pressure of about 300 to about 1000 bar and, for example, be a cam pump with injection adjuster similar to the distributor injection pump known from DE 35 16 867 A1.

Über die zentrale Druckübersetzungseinheit 6 kann bei Bedarf ein noch höherer Kraftstoffdruck erzeugt werden. Durch Nutzung von Wellenausbreitungseffekten läßt sich ein Einspritzdruck von über 2000 bar realisieren. Der jeweils anstehende Kraftstoffdruck wird dann von einer zentralen Verteilereinrichtung 8 auf mehrere, der Anzahl einzelner Zylinder entsprechende Hochdruckleitungen 9 verteilt, die zu den einzelnen, in den Brennraum der zu versorgenden Brennkraftmaschine ragenden Injektoren 10 (Einspritzeinrichtung) abführen. In Fig. 1 ist lediglich einer der Injektoren 10 näher dargestellt.If required, an even higher fuel pressure can be generated via the central pressure booster unit 6. By utilizing wave propagation effects, an injection pressure of more than 2000 bar can be realized. The respectively present fuel pressure is then distributed from a central distribution device 8 to a plurality of high-pressure lines 9 corresponding to the number of individual cylinders, which discharge to the individual injectors 10 (injection device) projecting into the combustion chamber of the internal combustion engine to be supplied. In Fig. 1, only one of the injectors 10 is shown in more detail.

Die zentrale Druckübersetzungseinheit 6 umfaßt einen Druckübersetzer 11 mit einem Druckmittel 12 in Form eines verschieblichen Kolbenelements, das einenends mit Hilfe einer Ventileinheit 13 an die Förderleitung 5 angeschlossen werden kann, so daß es durch den in einer Primärkammer 14 befindlichen Kraftstoff einenends druckbeaufschlagt wird. Ein Differenzraum 15 ist mittels einer Leckageleitung 16 druckentlastet, so daß das Druckmittel 12 zur Verringerung des Volumens einer Druckkammer 17 in Kompressionsrichtung verschoben werden kann. Dadurch wird der in der Druckkammer 17 befindliche Kraftstoff entsprechend entsprechend dem Flächenverhältnis von Primärkammer 14 und Druckkammer 17 auf den höheren Kraftstoffdruck verdichtet. Die Befüllung der Druckkammer 17 erfolgt über ein im Druckmittel 17 vorgesehenes Rückschlagventil 18. Der Druckübersetzer 11 kann durch eine parallele Bypaßleitung 19 umgangen werden, die mittels der Ventileinheit 13 aktivierbar bzw. deaktivierbar ist. In Fig. 1a ist die Ventileinheit 13 vor dem Druckübersetzer 11 und als 3/2-Wege-Ventil ausgebildet. Die Teile 11, 13 und 19 bilden die zentrale Druckübersetzungseinheit 6.The central pressure booster unit 6 comprises a pressure booster 11 with a pressure means 12 in the form of a displaceable piston element, which can be connected at one end to the delivery line 5 by means of a valve unit 13 , so that it is pressurized by the fuel located in a primary chamber 14 at one end. A differential space 15 is depressurized by means of a leakage line 16 , so that the pressure medium 12 can be displaced in the compression direction to reduce the volume of a pressure chamber 17 . As a result, the fuel in the pressure chamber 17 is compressed corresponding to the area ratio of the primary chamber 14 and the pressure chamber 17 to the higher fuel pressure. The filling of the pressure chamber 17 via a pressure medium 17 provided in the check valve 18th The pressure booster 11 can be bypassed by a parallel bypass line 19 , which can be activated or deactivated by means of the valve unit 13. In Fig. 1a , the valve unit 13 is formed in front of the pressure booster 11 and as a 3/2-way valve. The parts 11, 13 and 19 form the central pressure booster unit 6.

Der an der Verteilereinrichtung 8 jeweils anstehende Kraftstoffdruck wird über die Druckleitung 9 in einen Düsenraum 20 des Injektors 10 geleitet. Die Einspritzung erfolgt druckgesteuert mit Hilfe eines in einer Führungsbohrung axial verschiebbaren kolbenförmigen Ventilglieds 21 (Düsennadel), dessen konische Ventildichtfläche 22 mit einer Ventilsitzfläche am Injektorgehäuse zusammenwirkt und so die dort vorgesehenen Einspritzöffnungen 23 verschließt. Innerhalb des Düsenraums 20 ist eine in Öffnungsrichtung des Ventilglieds 21 weisende Druckfläche des Ventilgliedes 21 dem dort herrschenden Druck ausgesetzt, wobei sich der Düsenraum 20 über einen Ringspalt zwischen dem Ventilglied 21 und der Führungsbohrung bis an die Ventildichtfläche 22 des Injektors 10 fortsetzt. Durch den im Düsenraum 20 herrschenden Druck wird das die Einspritzöffnungen 23 abdichtende Ventilglied 21 gegen die Wirkung einer Schließkraft (Schließfeder 24) aufgesteuert, wobei der Federraum 25 mittels einer Leckageleitung 26 druckentlastet ist. Hinter der Verteilereinrichtung 8 ist für jeden Injektor 10 jeweils noch eine Rückschlagventilanordnung 27 vorgesehen, die den Kraftstoff in Richtung Injektor 10 über ein erstes Rückschlagventil 28 durchläßt und den Rückfluß von Kraftstoff aus dem Injektor 10 mittels einer Drossel 29 und eines zweiten Rückschlagventils 30 zur Entlastung der Verteilereinrichtung 8 und zum Druckabbau zuläßt.The respectively present at the manifold 8 fuel pressure is passed through the pressure line 9 into a nozzle chamber 20 of the injector 10. The injection is pressure-controlled by means of an axially displaceable in a guide bore piston-shaped valve member 21 (nozzle needle), the conical valve sealing surface 22 cooperates with a valve seat surface on the injector and thus closes the injection openings 23 provided there. Within the nozzle chamber 20 a in the opening direction of the valve member 21 facing pressure surface of the valve member 21 is exposed to the pressure prevailing there, wherein the nozzle chamber 20 continues through an annular gap between the valve member 21 and the guide bore to the valve sealing surface 22 of the injector 10. By the pressure prevailing in the nozzle chamber 20 pressure, the injection openings 23 sealing valve member 21 is controlled against the action of a closing force (closing spring 24 ), wherein the spring chamber 25 is depressurized by means of a leakage line 26 . Behind the manifold 8 for each injector 10 each still a check valve assembly 27 is provided which allows the fuel in the direction of the injector 10 via a first check valve 28 and the return of fuel from the injector 10 by means of a throttle 29 and a second check valve 30 to relieve the Distributor 8 and the pressure reduction permits.

Eine Voreinspritzung mit dem tieferen Kraftstoffdruck erfolgt bei stromloser Ventileinheit 13 durch Bestromen des 2/2-Wege-Ventils 7. Durch Bestromen auch der Ventileinheit 13 erfolgt dann die Haupteinspritzung mit dem höheren Kraftstoffdruck. Für eine Nacheinspritzung mit dem tieferen Kraftstoffdruck wird die Ventileinheit 13 wieder in den stromlosen Zustand zurückgeschaltet. Wird die Primärkammer 14 mit Hilfe der Ventileinheit 13 bei unbestromtem 2/2-Wege-Ventil 7 an den Eingang der Hochdruckpumpe 2 angeschlossen, so erfolgen die Rückstellung des Druckmittels 12 und die Wiederbefüllung der Druckkammer 17, die über das Rückschlagventil 18 an die Förderleitung 5 angeschlossen ist. Aufgrund der Druckverhältnisse in der Primärkammer 14 und in der Druckkammer 17 öffnet das Rückschlagventil 18, so daß die Druckkammer 17 unter dem Kraftstoffdruck der Hochdruckpumpe 2 steht und das Druckmittel 12 hydraulisch in seine Ausgangsstellung zurückgefahren wird. Zur Verbesserung des Rückstellverhaltens können eine oder mehrere Federn in den Räumen 14, 15 und 17 angeordnet sein. A pre-injection with the lower fuel pressure takes place in de-energized valve unit 13 by energizing the 2/2-way valve 7. By energizing also the valve unit 13 then takes the main injection with the higher Fuel pressure. For a post-injection with the deeper Fuel pressure, the valve unit 13 back in switched back to the de-energized state. Will the primary chamber 14 with the help of the valve unit 13 at no-current 2/2-way valve 7 connected to the input of the high pressure pump 2, so the provision of the pressure medium done 12 and the refilling of the pressure chamber 17, over the check valve 18 is connected to the delivery line 5 is. Due to the pressure conditions in the primary chamber 14 and in the pressure chamber 17 opens the check valve 18, so that the pressure chamber 17 under the fuel pressure the high-pressure pump 2 is and the pressure medium 12th hydraulically returned to its original position. To improve the restoring behavior, one or more several springs in the rooms 14, 15 and 17 arranged be.

In Fig. 1b ist die Ventileinheit 13a hinter dem Druckübersetzer 11 und als 2/2-Wege-Ventil ausgebildet, welches von der Bypaßleitung 19 über ein Rückschlagventil 31 abgekoppelt ist. Die Teile 11, 13a, 19 und 31 bilden die zentrale Druckübersetzungseinheit 6a. In Fig. 1b , the valve unit 13a is formed behind the pressure booster 11 and a 2/2-way valve, which is decoupled from the bypass line 19 via a check valve 31 . The parts 11, 13a, 19 and 31 form the central pressure booster unit 6a.

Nachfolgend werden in der Beschreibung zu den weiteren Figuren lediglich die Unterschiede zum Kraftstoffeinspritzsystem nach Fig. 1 behandelt. Identische bzw. funktionsgleiche Bauteile sind mit gleichen Bezugsziffern bezeichnet und werden nicht näher erläutert.Hereinafter, in the description of the other figures only the differences to the fuel injection system treated according to FIG. 1. Identical or functionally identical Components are designated by the same reference numerals and are not explained in detail.

Bei dem in Fig. 2 gezeigten Einspritzsystem 40 ist die Druckübersetzungseinheit 41 nicht zentral, sondern lokal für jeden Injektor 10 einzeln vorgesehen. Die lokale Druckübersetzungseinheit 41 umfaßt wie die in Fig. 1a gezeigte zentrale Druckübersetzungseinheit 6 einen Druckübersetzer 42 mit Rückschlagventil 43 sowie eine Ventileinheit 44 zum Umschalten zwischen dem Druckübersetzer 42 und der Bypaßleitung 45. In the injection system 40 shown in FIG. 2 , the pressure booster unit 41 is not provided centrally but locally for each injector 10 individually. The local pressure booster unit 41, like the central pressure booster unit 6 shown in FIG. 1 a, comprises a pressure booster 42 with a check valve 43 and a valve unit 44 for switching between the pressure booster 42 and the bypass duct 45.

Bei dem in Fig. 3 dargestellten Einspritzsystem 50 fördert die Hochdruckpumpe 2 den Kraftstoff über die Förderleitung 5 in einen zentralen Druckspeicher 51 (Common-Rail), in dem der Kraftstoff unter einem Druck von ca. 300 bis ca. 600 bar gelagert wird. Gesteuert über eine zentrale Ventileinheit 52 (z.B. ein 3/2-Wegventil), wird der Kraftstoff aus dem Druckspeicher 51 über die zentrale Verteilereinrichtung 8 an die einzelnen druckgesteuerten Injektoren 10 weitergeleitet. Jedem Injektor 10 ist eine lokale Druckübersetzungseinheit 53 mit einem Druckübersetzer 54 zugeordnet, mittels dem bei Bedarf aus dem tieferen Kraftstoffdruck des Druckspeichers 51 ein höherer Kraftstoffdruck erzeugt werden kann. Über die Ventileinheit 55 (3/2-Wegeventil) kann der lokale Druckübersetzer 54, der analog dem zentralen Druckübersetzer 11 aufgebaut ist, aktiviert werden. Die Druckkammer 56 des lokalen Druckübersetzers 54 wird mit Kraftstoff aus dem Druckspeicher 51 befüllt, wobei ein Rückschlagventil 57 in einer zum Druckübersetzer 54 parallelen Bypaßleitung 58 den Rücklauf von komprimiertem Kraftstoff zurück in den Druckspeicher 51 verhindert. Die Teile 54, 55, 57 und 58 bilden die lokale Druckübersetzungseinheit 53, die sich entweder innerhalb des Injektorgehäuses (Fig. 3a) oder außerhalb (Fig. 3b) befinden kann.In the injection system 50 shown in FIG. 3 , the high-pressure pump 2 conveys the fuel via the delivery line 5 into a central pressure accumulator 51 (common rail), in which the fuel is stored under a pressure of approximately 300 to approximately 600 bar. Controlled via a central valve unit 52 (eg, a 3/2-way valve), the fuel from the pressure accumulator 51 via the central distribution device 8 is forwarded to the individual pressure-controlled injectors 10. Each injector 10 is associated with a local pressure booster unit 53 with a pressure booster 54 , by means of which, if necessary from the lower fuel pressure of the pressure accumulator 51, a higher fuel pressure can be generated. Via the valve unit 55 (3/2-way valve), the local pressure booster 54, which is constructed analogously to the central pressure booster 11, are activated. The pressure chamber 56 of the local pressure booster 54 is filled with fuel from the pressure accumulator 51, wherein a check valve 57 in a bypass line 58 parallel to the pressure booster 54 prevents the return of compressed fuel back into the pressure accumulator 51. The parts 54, 55, 57 and 58 form the local pressure booster unit 53, which may be either inside the injector housing ( FIG. 3a ) or outside ( FIG. 3b ).

Eine Voreinspritzung mit dem tieferen Kraftstoffdruck des zentralen Druckspeichers 51 erfolgt bei stromloser Ventileinheit 55 durch Bestromen des zentralen 3/2-Wege-Ventils 52. Durch Bestromen auch der Ventileinheit 55 erfolgt dann die Haupteinspritzung mit dem höheren Kraftstoffdruck. Für eine Nacheinspritzung mit dem tieferen Kraftstoffdruck wird die Ventileinheit 55 wieder in den stromlosen Zustand zurückgeschaltet. Am Ende der Einspritzung wird die zentrale Ventileinheit 52 auf Leckage 59 zurückgeschaltet und damit die Verteilereinrichtung 8 und der Injektor 10 entlastet.A pilot injection with the lower fuel pressure of the central pressure accumulator 51 takes place with currentless valve unit 55 by energizing the central 3/2-way valve 52. By energizing the valve unit 55 and then the main injection with the higher fuel pressure. For a post-injection with the lower fuel pressure, the valve unit 55 is switched back to the de-energized state. At the end of the injection, the central valve unit 52 is switched back to leakage 59 and thus the manifold 8 and the injector 10 relieved.

Vom Einspritzsystem 50 unterscheidet sich das in Fig. 4 gezeigte Einspritzsystem 60 durch die Verwendung hubgesteuerter Injektoren 61 und die Ausbildung der zentralen Ventileinheit 62 als 2/2-Wege-Ventil. Ausgehend von dem druckgesteuerten Injektor 10 der Fig. 1 greift bei einem hubgesteuerten Injektor 61 an dem Ventilglied 21 koaxial zur Ventilfeder 23 ein Druckstück 63 an, das mit seiner der Ventildichtfläche 22 abgewandten Stirnseite 64 einen Steuerraum 65 begrenzt. Der Steuerraum 65 hat von der Druckleitung 9 her einen Kraftstoffzulauf mit einer ersten Drossel 66 und einen Kraftstoffablauf zu einer Druckentlastungsleitung 67 mit einer zweiten Drossel 68, die durch ein 2/2-Wege-Ventil 69 auf Leckage 70 steuerbar ist. Über den Druck im Steuerraum 65 wird das Druckstück 63 in Schließrichtung druckbeaufschlagt. Unter dem tieferen oder höheren Kraftstoffdruck stehender Kraftstoff füllt ständig den Düsenraum 20 und den Steuerraum 65. Bei Betätigung (Öffnen) des 2/2-Wege-Ventils 69 kann der Druck im Steuerraum 65 abgebaut werden, so daß in der Folge die in Öffnungsrichtung auf das Ventilglied 21 wirkende Druckkraft im Düsenraum 20 die in Schließrichtung auf das Ventilglied 21 wirkende Druckkraft übersteigt. Die Ventildichtfläche 22 hebt von der Ventilsitzfläche ab, und Kraftstoff wird eingespritzt. Dabei läßt sich der Druckentlastungsvorgang des Steuerraums 65 und somit die Hubsteuerung des Ventilglieds 21 über die Dimensionierung der beiden Drosseln 66 und 68 beeinflussen. Das Ende der Einspritzung wird durch erneutes Betätigen (Schließen) des 2/2-Wege-Ventils 69 eingeleitet, das den Steuerraum 65 wieder von der Leckageleitung 70 abkoppelt, so daß sich im Steuerraum 65 erneut ein Druck aufbaut, der das Druckstück 63 in Schließrichtung bewegen kann. Die Umschaltung des Kraftstoffs auf entweder den tieferen oder den höheren Kraftstoffdruck erfolgt für jeden Injektor 61 in der lokalen Druckübersetzungseinheit 53 durch die Ventileinheit 55. Die Druckübersetzungseinheit 53 kann entweder innerhalb des Injektorgehäuses (Fig. 4a) oder außerhalb (Fig. 4b) angeordnet sein.From the injection system 50, the injection system 60 shown in Fig. 4 differs by the use of stroke-controlled injectors 61 and the formation of the central valve unit 62 as a 2/2-way valve. Starting from the pressure-controlled injector 10 of FIG. 1 engages in a stroke-controlled injector 61 on the valve member 21 coaxial with the valve spring 23 to a pressure piece 63 , which limits the valve sealing surface 22 remote from the end face 64 a control chamber 65. The control chamber 65 has a fuel inlet from the pressure line 9 with a first throttle 66 and a fuel outlet to a pressure relief line 67 with a second throttle 68, which is controllable by a 2/2-way valve 69 to 70 leakage. About the pressure in the control chamber 65, the pressure piece 63 is pressurized in the closing direction. Under the lower or higher fuel pressure stagnant fuel constantly fills the nozzle chamber 20 and the control chamber 65. Upon actuation (opening) of the 2/2-way valve 69, the pressure in the control chamber 65 can be reduced, so that in the sequence on the opening direction the valve member 21 acting pressure force in the nozzle chamber 20 exceeds the force acting in the closing direction on the valve member 21 pressing force. The valve sealing surface 22 lifts off the valve seat surface and fuel is injected. In this case, the pressure relief process of the control chamber 65 and thus the stroke control of the valve member 21 via the dimensioning of the two throttles 66 and 68 can be influenced. The end of the injection is initiated by renewed actuation (closing) of the 2/2-way valve 69, which decouples the control chamber 65 again from the leakage line 70, so that in the control chamber 65 again a pressure builds up, the pressure piece 63 in the closing direction can move. The switching of the fuel to either the lower or the higher fuel pressure occurs for each injector 61 in the local pressure booster unit 53 through the valve unit 55. The pressure booster unit 53 can be arranged either inside the injector housing ( FIG. 4a ) or outside ( FIG. 4b ).

Bei einem Kraftstoffeinspritzsystem 1 für eine Brennkraftmaschine, bei dem Kraftstoff mit mindestens zwei unterschiedlich hohen Kraftstoffdrücken über Injektoren 10 in den Brennraum der Brennkraftmaschine eingespritzt werden kann, ist parallel zu einer Bypaßleitung 19 ein hydraulischer Druckübersetzer 11 zur Erzeugung des höheren Kraftstoffdruckes vorgesehen, wobei der Druckübersetzer 11 über eine Ventileinheit 13 aktivierbar und deaktivierbar ist. Da der Druckübersetzer nicht permanent im Betrieb ist und auch die Verluste durch Reibung reduziert sind, ist der Wirkungsgrad verbessert.In a fuel injection system 1 for an internal combustion engine, different with the fuel with at least two high fuel pressures via injectors 10 in the combustion chamber of the internal combustion engine to be injected can, parallel to a bypass line 19 is a hydraulic Pressure booster 11 for generating the higher fuel pressure provided, wherein the pressure booster 11 via a valve unit 13 can be activated and deactivated. Since the intensifier is not permanently in operation and even the losses are reduced by friction, is the Improved efficiency.

Claims (7)

  1. Fuel injection system (1) for an internal combustion engine, in which fuel can be injected into the combustion chamber of the internal combustion engine via injectors (10) at at least two different fuel pressures, a hydraulic pressure intensifier (11) for generating the higher fuel pressure being provided in parallel with a bypass line (19) and it being possible to activate and de-activate the pressure intensifier (11) via a valve unit (13; 13a), characterized in that the pressure intensifier (11) is provided centrally for all injectors (10), and in that a central distributor device (8) is provided to distribute the fuel pressure to the individual injectors (10).
  2. Fuel injection system according to Claim 1, characterized in that the bypass line (19) is closed when the pressure intensifier (11) is activated.
  3. Fuel injection system according to Claim 1 or 2, characterized in that the valve unit (13) is arranged in front of the pressure intensifier (11).
  4. Fuel injection system according to Claim 1 or 2, characterized in that the valve unit (13a) is arranged behind the pressure intensifier (11).
  5. Fuel injection system according to one of the preceding claims, characterized in that at least one central pressure accumulator is provided for storing the lower fuel pressure.
  6. Fuel injection system according to one of the preceding claims, characterized in that the injectors (10) are configured for pressure control.
  7. Fuel injection system according to one of the preceding claims, characterized in that the injectors are configured for stroke control.
EP00958211A 1999-08-20 2000-08-02 Fuel injection system for an internal combustion engine Expired - Lifetime EP1123463B1 (en)

Applications Claiming Priority (3)

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DE19939423 1999-08-20
DE19939423A DE19939423A1 (en) 1999-08-20 1999-08-20 Fuel injection system for an internal combustion engine
PCT/DE2000/002581 WO2001014727A1 (en) 1999-08-20 2000-08-02 Fuel injection system for an internal combustion engine

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EP1123463A1 EP1123463A1 (en) 2001-08-16
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AT (1) ATE292238T1 (en)
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WO2001014727A1 (en) 2001-03-01
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ATE292238T1 (en) 2005-04-15
US6688277B1 (en) 2004-02-10

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