EP1682769B1 - Fuel injector with a multipart, directly controlled injection valve element - Google Patents

Fuel injector with a multipart, directly controlled injection valve element Download PDF

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Publication number
EP1682769B1
EP1682769B1 EP04786717A EP04786717A EP1682769B1 EP 1682769 B1 EP1682769 B1 EP 1682769B1 EP 04786717 A EP04786717 A EP 04786717A EP 04786717 A EP04786717 A EP 04786717A EP 1682769 B1 EP1682769 B1 EP 1682769B1
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EP
European Patent Office
Prior art keywords
injection valve
fuel injector
valve member
needle part
chamber
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
EP04786717A
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German (de)
French (fr)
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EP1682769A1 (en
Inventor
Friedrich Boecking
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Robert Bosch GmbH
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Robert Bosch GmbH
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    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/0603Injectors peculiar thereto with means directly operating the valve needle using piezoelectric or magnetostrictive operating means
    • 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
    • F02M45/02Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
    • F02M45/04Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
    • F02M45/08Injectors peculiar thereto
    • F02M45/086Having more than one injection-valve controlling discharge orifices
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/21Fuel-injection apparatus with piezoelectric or magnetostrictive elements
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/46Valves, e.g. injectors, with concentric valve bodies
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/70Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
    • F02M2200/703Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic

Definitions

  • Verbrennungsltraftmaschinen storage injection systems are used for fuel injection, which allow a speed and load-independent adjustment of the injection pressure.
  • Conunon-Rail are pressure generation and injection and locally decoupled.
  • the injection pressure is generated by a separate high-pressure pump. This does not have to be driven synchronously with the injections.
  • the pressure can be adjusted independently of the engine speed and the injection quantity.
  • electrically actuated injectors with their An horrzeittician and An Kunststoffdauer the start of injection and the injection quantities are determined in the combustion chambers of the internal combustion engine.
  • common-rail injection systems there is a high degree of freedom with regard to the design and formation of multiple or split injection processes.
  • Out DE-190 55 271 A1 is a pressure / stroke controlled injector with hydraulic translator known.
  • 2/2-way control valves are included, the vertical movement is mechanically coupled via a bridge to each other.
  • the 2/2-way control valves are arranged on the inlet side and on the outlet side and upstream of a hydraulic booster.
  • the hydraulic booster pressurizes a pressure chamber surrounding a nozzle needle with high pressure fuel.
  • the two 2/2-way control valves are housed opposite to each other in the injector of the fuel injector.
  • a disadvantage of the DE 190 55 271 A1 known solution is the large number of items that are required to implement a pressure / stroke controlled Injektoran horrung according to this solution.
  • a valve for controlling fluids comprises a valve member axially displaceable in a bore of a valve body. This has a valve closing member forming the valve head, which cooperates with a provided on the valve body seat for opening and closing the valve. Furthermore, a piezoelectric unit for actuating the valve member and a tolerance compensation element to compensate for elongation tolerances of the piezoelectric unit and / or other valve components is provided.
  • the piezoelectric unit is arranged essentially at right angles to the axial movement direction of the valve member and can be acted upon by an electric current such that the piezoelectric unit exerts a tilting movement on an actuator serving as a lever arm, which is operatively connected to the valve member.
  • the proposed solution according to the invention is characterized in that different injection cross-sections in the combustion chamber of a self-igniting internal combustion engine can be released with a multi-part, needle-shaped injection valve member, wherein the multi-part injection valve member is in particular controlled directly.
  • a hydraulic transmission arrangement is provided between a piezoelectric actuator and the multi-part, needle-shaped injection valve member, which has two booster chambers.
  • Each of the two translator chambers acts on a control chamber for controlling an inner needle part and for driving an outer needle part of the multi-part, needle-shaped injection valve member.
  • the inner and the outer needle part of the multipart injection valve member have pressure stages which allow for pressurization of a nozzle chamber in the nozzle body and pressure relief of the control chambers a time-delayed opening of the needle parts of the multi-part injection valve member.
  • the hydraulic forces acting on the outer needle part can be adjusted such that the smallest quantity capability of the fuel injector is ensured even at very low pressures. Due to the formation of two pressure stages on the outer needle part of the multi-part injection valve member this opens very early, whereas the inner needle part of the multi-part injection valve member opens later, since the pressure formed at this stage is designed to be very small. Due to this design of the two pressure levels on the outer needle part and the pressure level on the inner needle part can be achieved that the two needle parts of the multi-part, needle-shaped injection valve member can be switched to different pressure levels.
  • the single FIGURE shows a section through the present invention proposed fuel injector with multi-part trained, needle-shaped injection valve member and a hydraulic transmission arrangement on the booster chambers control spaces which are respectively associated with the inner and the outer needle portion of the multipart injection valve, pressure relieving or druckbeaufschlagbar.
  • the fuel injector 1 shown in the drawing comprises an injector body 2 and a nozzle body 3.
  • the injector body 2 and the nozzle body 3 are in the assembled state at a butt joint 4 to each other.
  • the fuel flows through a high-pressure accumulator injection system, not shown in the drawing (common rail), to the injector body 2 via a fuel inlet 5.
  • an actuator 6 is accommodated, to which a hydraulic transmission device 9 is assigned.
  • a high-pressure feed line 7 branches off in the injector body 2, via which the high-pressure fuel flowing to the injector body 2 flows into a nozzle chamber 8.
  • the nozzle chamber 8 is located in the nozzle body 3 and encloses a multi-part injection valve member 21, which is movably received in the nozzle body 3 in the vertical direction.
  • the hydraulic transmission device 9 comprises a booster piston 10.
  • the booster piston 10 has a first end face 11, which is opposite to the actuator 6.
  • a second end face 12 of the booster piston 10 defines a first booster chamber 13 of the hydraulic transmission device 9.
  • On the booster piston 10 is a booster piston extension 14, which is formed in a smaller diameter compared to the diameter of the booster piston 10.
  • An end face 15 of the translator piston extension 14 projects into a second translator chamber 17. From the second booster chamber 17 from a channel 16 which opens into a first control chamber 19 extends. Parallel to the channel 16 extends an overflow 18, via which the first booster chamber 13 and a second control chamber 20 communicate with each other hydraulically.
  • the multi-part needle-shaped injection valve member 21 has an outer needle part 22 and an inner needle part 23 arranged movably in this needle part.
  • the inner needle part 23 is acted upon by the first control chamber 19, which is in communication with the second booster chamber 17 of the hydraulic transmission arrangement, while the outer needle part 22 via the second control chamber 20 which communicates via the overflow 18 with the first booster chamber 13, is pressed.
  • the outer needle part 22 has a second control chamber 20 limiting control-space-side end face 24 and a first pressure step 25 on the outside and a further, second pressure step 26, which is formed on the inside of the outer needle member 22.
  • a pressure chamber 29 is formed, which is bounded by an annular part 27 formed on the inner needle part 23.
  • a seat 31 is formed on the outer circumference, which has a first seat diameter 32.
  • the seat edge formed in the first seat diameter 32 interacts with the wall of the nozzle body 3.
  • the seat diameter of the seat 33 of the inner needle member 23 is formed in a second seat diameter 34 (d 1 ) which is considerably smaller than the first seat diameter 32 of the outer needle member 22.
  • first injection ports 35 are separated by the closed seat 31 of the outer needle member 22 of an annular gap 41, in which over the nozzle chamber 8 is under high pressure fuel.
  • second injection openings 36 are likewise closed against the fuel which is present in the annular gap 41 and is under high pressure.
  • closed state of the multi-part needle-shaped injection valve member 21, 23 forms a wedge-shaped annular space 42 between the seat 31 of the outer needle member 22 and the seat 33 of the inner needle member.
  • the combustion chamber in which fuel is injected either via the first injection openings 35 or via the opened first and second injection openings 35, 36 when the multi-part injection valve member 21 is open, is identified by reference number 43.
  • the outer needle part 22 of the multi-part, needle-shaped injection valve member 21 is received in a guide length 37 in the nozzle body 3, while the inner needle member 23 in a guide length 38 extending between the Druckraumzuidentn 30 of the outer needle member 23 and its seat 31 in this body 3 , is limited.
  • the outer needle member 22 may be performed in the nozzle body 3 in a plurality of, for example, 120 ° offset from each other formed guide surfaces.
  • the inner needle part 23 of the multi-part, needle-shaped injection valve member 21 has a second diameter 39 (d 2 ) in the region above the inner pressure chamber 29, which exceeds the second seat diameter 34 (d 1 ), ie d 2 > d 1 .
  • the actuator 6 In the closed state of the multi-part injection valve member 21 shown in the drawing, the actuator 6 is energized and extended. Due to the energization of the actuator 6, which is preferably designed as a piezoelectric actuator, its piezocrystals length, which are arranged one above the other in the form of a stack and thus act on the booster piston 10. Its second end face 12 moves into the first booster room 13 a. By the second end face 12 of the booster piston 10 and the booster piston extension 14 is retracted into the second booster chamber 17 of the hydraulic booster assembly 9. The first booster chamber 13 and the second booster chamber 17 are filled via the guide leaks between the outer needle part 22 and the nozzle body 3, the guide leak between the inner needle part 23 and the injector body 2 and the guide leakage between the booster piston 10 and the fuel inlet 5.
  • the booster piston 10 including the translator piston extension 14 moves in the vertical direction upwards.
  • the stroke of the booster piston 10 and the booster piston extension 14 is in the range between 40 and 160 .mu.m.
  • the outer needle part 22 opens sooner, since at this an outer first pressure stage 25 and an inner second pressure stage 26 are formed above the inner pressure chamber 29.
  • the annular space 42 comes into communication with the annular gap 41, in which high-pressure fuel is present.
  • the high-pressure fuel can be injected into the combustion chamber 43 via the first injection openings 35 during a first phase of the injection process.
  • the inner needle portion 23 of the multipart, needle-shaped injection valve member 21 remains in its closed position, d. H. the seat 33 of the inner needle part 23 remains closed.
  • the inner needle part 23 of the multi-part injection valve member 21 opens, since the pressure stage 28 formed thereon is very small.
  • high-pressure fuel flows into the inner pressure space 29 between the outer needle part 22 and the inner needle part 23 via the pressure chamber inlets 30.
  • the fuel flowing into the interior pressure chamber 29 is in contact with the annular surface 27 of the inner needle part 23 and continues to act on it in the closing direction.
  • the annular gap 41 enters the annular space 42 in connection.
  • an effective in the opening direction hydraulic force at the pressure stage 28 at the combustion chamber end of the inner needle member 23 is effective, which moves this in the opening direction.
  • the second seat 33 of the inner needle part 23 is also opened and fuel flows via the now opened second seat 33 to the second injection openings 36.
  • the diameter of the inner needle part 23, i. the first diameter 39 is in the range between 1.5 and 2.5 mm, while the diameter of the second control chamber 20 may be between 3.5 and 5.6 mm, depending on the design of the fuel injector.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

A fuel injector for a common rail injection system for injecting fuel into a combustion chamber of an internal combustion engine includes an injector body and a nozzle body with an injection valve member embodied in multiple parts received in the nozzle body. A hydraulic booster assembly connected downstream of a piezoelectric actuator. Control chambers are associated with the multi-part injection valve member for actuating it. The hydraulic booster assembly actuated by the piezoelectric actuator has booster chambers, which are each directly connected hydraulically with control chambers that actuate the needle parts of the injection valve member.

Description

Technisches GebietTechnical area

An selbstzündenden Verbrennungsltraftmaschinen werden Speichereinspritzsysteme zur Kraftstoffeinspritzung eingesetzt, die eine drehzahl- und lastunabhängige Einstellung des Einspritzdrucks erlauben. Bei den Speichereinspritzsystemen (Conunon-Rail) sind Druckerzeugung und Einspritzung und örtlich voneinander entkoppelt. Der Einspritzdruck wird von einer separaten Hochdruckpumpe erzeugt. Diese muss nicht synchron zu den Einspritzungen angetrieben werden. Der Druck kann unabhängig von der Motordrehzahl und der Einspritzmenge eingestellt werden. An die Stelle druckgesteuelier Einspritzventile treten bei diesem Kraftstoffeinspritzsystem elektrisch betätigte Injektoren, mit deren Ansteuerzeitpunkt und Ansteuerdauer der Einspritzbeginn und die Einspritzmengen in die Brennräume der Verbrennungskraftmaschine bestimmt werden. Bei Common-Rail-Einspritzsystemen besteht ein hoher Freiheitsgrad bezüglich der Gestaltung und Formung von mehrfach- oder geteilten Einspritzvorgängen.On self-igniting Verbrennungsltraftmaschinen storage injection systems are used for fuel injection, which allow a speed and load-independent adjustment of the injection pressure. In the storage injection systems (Conunon-Rail) are pressure generation and injection and locally decoupled. The injection pressure is generated by a separate high-pressure pump. This does not have to be driven synchronously with the injections. The pressure can be adjusted independently of the engine speed and the injection quantity. In place of druckgesteuelier injectors occur in this fuel injection system electrically actuated injectors, with their Ansteuerzeitpunkt and Ansteuerdauer the start of injection and the injection quantities are determined in the combustion chambers of the internal combustion engine. In common-rail injection systems, there is a high degree of freedom with regard to the design and formation of multiple or split injection processes.

Stand der TechnikState of the art

Aus DE-190 55 271 A1 ist ein druck-/hubgesteuerter Injektor mit hydraulischem Übersetzer bekannt. In einem Injektorgehäuse sind 2/2-Wege-Steuerventile aufgenommen, deren vertikale Bewegung mechanisch über eine Brücke aneinander gekoppelt ist. Die 2/2-Wege-Steuerventile sind zulaufseitig und ablaufseitig angeordnet und einem hydraulischen Übersetzer vorgeschaltet. Der hydraulische Übersetzer beaufschlagt einen eine Düsennadel umgebenden Druckraum mit unter hohem Druck stehenden Kraftstoff. Die beiden 2/2-Wege-Steuerventile sind im Injektorgehäuse des Kraftstoffinjektors gegengleich zueinander aufgenommen.Out DE-190 55 271 A1 is a pressure / stroke controlled injector with hydraulic translator known. In an injector 2/2-way control valves are included, the vertical movement is mechanically coupled via a bridge to each other. The 2/2-way control valves are arranged on the inlet side and on the outlet side and upstream of a hydraulic booster. The hydraulic booster pressurizes a pressure chamber surrounding a nozzle needle with high pressure fuel. The two 2/2-way control valves are housed opposite to each other in the injector of the fuel injector.

Nachteilig an der aus DE 190 55 271 A1 bekannten Lösung ist die Vielzahl von Einzelteilen, die zur Realisierung einer druck-/hubgesteuerten Injektoransteuerung gemäß dieser Lösung erforderlich sind.A disadvantage of the DE 190 55 271 A1 known solution is the large number of items that are required to implement a pressure / stroke controlled Injektoransteuerung according to this solution.

Aus DE 199 46 838 C1 ist ein Ventil zum Steuern von Flüssigkeiten bekannt. Das Ventil umfasst ein in einer Bohrung eines Ventilkörpers axial verschiebbares Ventilglied. Dieses weist einen das Ventilschließglied bildenden Ventilkopf auf, der mit einem an dem Ventilkörper vorgesehenen Sitz zum Öffnen und Schließen des Ventiles zusammenwirkt. Des weiteren wird eine piezoelektrische Einheit zur Betätigung des Ventilgliedes sowie ein Toleranzausgleichselement zum Ausgleich von Längungstoleranzen der piezoelektrischen Einheit und/oder anderer Ventilbauteile vorgesehen. Die piezoelektrische Einheit ist hinsichtlich ihrer Wirkrichtung im Wesentlichen im rechten Winkel zur axialen Bewegungsrichtung des Ventilgliedes angeordnet und mit einem elektrischen Strom derart beaufschlagbar, dass die piezoelektrische Einheit auf ein als Hebelarm dienendes, mit dem Ventilglied in Wirkverbindung stehendes Stellglied eine Kippbewegung ausübt.Out DE 199 46 838 C1 a valve for controlling fluids is known. The valve comprises a valve member axially displaceable in a bore of a valve body. This has a valve closing member forming the valve head, which cooperates with a provided on the valve body seat for opening and closing the valve. Furthermore, a piezoelectric unit for actuating the valve member and a tolerance compensation element to compensate for elongation tolerances of the piezoelectric unit and / or other valve components is provided. With regard to its direction of action, the piezoelectric unit is arranged essentially at right angles to the axial movement direction of the valve member and can be acted upon by an electric current such that the piezoelectric unit exerts a tilting movement on an actuator serving as a lever arm, which is operatively connected to the valve member.

Darstellung der ErfindungPresentation of the invention

Die erfindungsgemäß vorgeschlagene Lösung zeichnet sich dadurch aus, dass mit einem mehrteilig ausgebildeten, nadelförmigen Einspritzventilglied unterschiedliche Einspritzquerschnitte in den Brennraum einer selbstzündenden Verbrennungskraftmaschine freigebbar sind, wobei das mehrteilig ausgebildete Einspritzventilglied insbesondere direkt angesteuert ist. Zur Direktansteuerung des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes ist zwischen einem Piezoaktor und der dem mehrteilig ausgebildeten, nadelförmigen Einspritzventilglied eine hydraulische Übersetzungsanordnung vorgesehen, die zwei Übersetzerräume aufweist. Jeder der beiden Übersetzerräume beaufschlagt einen Steuerraum zur Ansteuerung eines inneren Nadelteiles und zur Ansteuerung eines äußeren Nadelteiles des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes.The proposed solution according to the invention is characterized in that different injection cross-sections in the combustion chamber of a self-igniting internal combustion engine can be released with a multi-part, needle-shaped injection valve member, wherein the multi-part injection valve member is in particular controlled directly. For direct control of the multi-part, needle-shaped injection valve member, a hydraulic transmission arrangement is provided between a piezoelectric actuator and the multi-part, needle-shaped injection valve member, which has two booster chambers. Each of the two translator chambers acts on a control chamber for controlling an inner needle part and for driving an outer needle part of the multi-part, needle-shaped injection valve member.

Der innere und der äußere Nadelteil des mehrteilig ausgebildeten Einspritzventilgliedes weisen Druckstufen auf, die bei Druckbeaufschlagung eines Düsenraumes im Düsenkörper und bei Druckentlastung der Steuerräume ein zeitlich versetztes Öffnen der Nadelteile des mehrteilig ausgebildeten Einspritzventilgliedes ermöglichen. Dadurch erfolgt während einer ersten Phase der Einspritzung von Kraftstoff in den Brennraum einer selbstzündenden Verbrennungskraftmaschine über einen ersten Einspritzöffnungsquerschnitt und im weiteren Verlauf der Einspritzung beim zeitlich später erfolgenden Öffnen des inneren Nadelteiles des mehrteilig ausgebildeten Einspritzventilgliedes die Freigabe eines weiteren Öffnungsquerschnittes, so dass gegen Ende des Einspritzvorganges mehr Kraftstoff in den Brennraum gelangt, als zu Beginn des Einspritzvorganges. Demnach ist im Teillastbetrieb der Verbrennungskraftmaschine nur ein Einspritzquerschnitt freigegeben während bei Volllast der Verbrennungskraftmaschine beide Nadelteile des mehrteilig ausgebildeten Einspritzventilgliedes offen stehen, so dass die maximale Einspritzmenge in den Brennraum der Verbrennungskraftmaschine eingespritzt werden kann.The inner and the outer needle part of the multipart injection valve member have pressure stages which allow for pressurization of a nozzle chamber in the nozzle body and pressure relief of the control chambers a time-delayed opening of the needle parts of the multi-part injection valve member. As a result, during a first phase of the injection of fuel into the combustion chamber of a self-igniting internal combustion engine via a first Einspritzöffnungsquerschnitt and later in the injection at later time opening the inner needle part of the multi-part injection valve member, the release of a further opening cross-section, so that towards the end of the injection process more fuel enters the combustion chamber, as at the beginning of the injection process. Accordingly, in the partial load operation of the internal combustion engine only one injection cross-section is released while at full load of the internal combustion engine both needle parts of the multi-part design Injection valve member are open, so that the maximum injection quantity can be injected into the combustion chamber of the internal combustion engine.

Durch die Auslegung von am äußeren Nadelteil des mehrteilig ausgebildeten Einspritzventilglied ausgebildeten Druckstufen, können die auf das äußere Nadelteil einwirkenden hydraulischen Kräfte derart eingestellt werden, dass auch bei geringsten Drücken die Kleinstmengenfähigkeit des Kraftstoffinjektors gewährleistet ist. Aufgrund der Ausbildung zweier Druckstufen am äußeren Nadelteil des mehrteiligen Einspritzventilgliedes öffnet dieses sehr früh, wohingegen das innere Nadelteil des mehrteilig ausgebildeten Einspritzventilgliedes später öffnet, da die an diesem ausgebildete Druckstufe sehr klein ausgelegt ist. Aufgrund dieser Auslegung der beiden Druckstufen am äußeren Nadelteil und der Druckstufe am inneren Nadelteil kann erreicht werden, dass die beiden Nadelteile des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes auf voneinander verschiedenen Druckniveaus geschaltet werden können.By designing pressure stages formed on the outer needle part of the multi-part injection valve member, the hydraulic forces acting on the outer needle part can be adjusted such that the smallest quantity capability of the fuel injector is ensured even at very low pressures. Due to the formation of two pressure stages on the outer needle part of the multi-part injection valve member this opens very early, whereas the inner needle part of the multi-part injection valve member opens later, since the pressure formed at this stage is designed to be very small. Due to this design of the two pressure levels on the outer needle part and the pressure level on the inner needle part can be achieved that the two needle parts of the multi-part, needle-shaped injection valve member can be switched to different pressure levels.

Zeichnungdrawing

Anhand der Zeichnung wird die Erfindung nachstehend eingehender erläutert.With reference to the drawing, the invention will be explained in more detail below.

Die einzige Figur zeigt einen Schnitt durch den erfindungsgemäß vorgeschlagenen Kraftstoffinjektor mit mehrteilig ausgebildetem, nadelförmigen Einspritzventilglied und einer hydraulischen Übersetzungsanordnung über deren Übersetzerräume Steuerräume die jeweils den inneren bzw. den äußeren Nadelteil des mehrteilig ausgebildeten Einspritzventiles zugeordnet sind, druckentlastbar oder druckbeaufschlagbar sind.The single FIGURE shows a section through the present invention proposed fuel injector with multi-part trained, needle-shaped injection valve member and a hydraulic transmission arrangement on the booster chambers control spaces which are respectively associated with the inner and the outer needle portion of the multipart injection valve, pressure relieving or druckbeaufschlagbar.

Ausführungsvariantevariant

Der in der Zeichnung dargestellt Kraftstoffinjektor 1 umfasst einen Injektorkörper 2 und einen Düsenkörper 3. Der Injektorkörper 2 und der Düsenkörper 3 liegen in montiertem Zustand an einer Stoßfuge 4 aneinander an. Der Kraftstoff strömt über einen in der Zeichnung nicht dargestellten Hochdruckspeicherraum (Common-Rail) eines Hochdruckspeichereinspritzsystemes über einen Kraftstoffzulauf 5 dem Injektorkörper 2 zu. Im oberen Bereich des Injektorkörpers 2 ist ein Aktor 6 aufgenommen, welchem eine hydraulische Übersetzungseinrichtung 9 zugeordnet ist. Vom Kraftstoffzulauf 5 zweigt im Injektorkörper 2 eine Hochdruckzuleitung 7 ab, über welche der unter hohem Druck stehende, dem Injektorkörper 2 zuströmende Kraftstoff, in einen Düsenraum 8 einströmt. Der Düsenraum 8 befindet sich im Düsenkörper 3 und umschließt ein mehrteilig ausgebildetes Einspritzventilglied 21, welches im Düsenkörper 3 in vertikale Richtung bewegbar aufgenommen ist.The fuel injector 1 shown in the drawing comprises an injector body 2 and a nozzle body 3. The injector body 2 and the nozzle body 3 are in the assembled state at a butt joint 4 to each other. The fuel flows through a high-pressure accumulator injection system, not shown in the drawing (common rail), to the injector body 2 via a fuel inlet 5. In the upper region of the injector body 2, an actuator 6 is accommodated, to which a hydraulic transmission device 9 is assigned. From the fuel inlet 5, a high-pressure feed line 7 branches off in the injector body 2, via which the high-pressure fuel flowing to the injector body 2 flows into a nozzle chamber 8. The nozzle chamber 8 is located in the nozzle body 3 and encloses a multi-part injection valve member 21, which is movably received in the nozzle body 3 in the vertical direction.

Die hydraulische Übersetzungseinrichtung 9 umfasst einen Übersetzerkolben 10. Der Übersetzerkolben 10 weist eine erste Stirnfläche 11 auf, die dem Aktor 6 gegenüberliegt. Eine zweite Stirnfläche 12 des Übersetzerkolbens 10 begrenzt einen ersten Übersetzerraum 13 der hydraulischen Übersetzungseinrichtung 9. An dem Übersetzerkolben 10 befindet sich ein Übersetzerkolbenfortsatz 14, der im Vergleich zum Durchmesser des Übersetzerkolbens 10 in einen geringeren Durchmesser ausgebildet ist. Eine Stirnseite 15 des Übersetzerkolbenfortsatzes 14 ragt in einen zweiten Übersetzerraum 17 hinein. Vom zweiten Übersetzerraum 17 aus erstreckt sich ein Kanal 16, der in einen ersten Steuerraum 19 mündet. Parallel zum Kanal 16 verläuft eine Überströmleitung 18, über welche der erste Übersetzerraum 13 und ein zweiter Steuerraum 20 miteinander hydraulisch in Verbindung stehen.The hydraulic transmission device 9 comprises a booster piston 10. The booster piston 10 has a first end face 11, which is opposite to the actuator 6. A second end face 12 of the booster piston 10 defines a first booster chamber 13 of the hydraulic transmission device 9. On the booster piston 10 is a booster piston extension 14, which is formed in a smaller diameter compared to the diameter of the booster piston 10. An end face 15 of the translator piston extension 14 projects into a second translator chamber 17. From the second booster chamber 17 from a channel 16 which opens into a first control chamber 19 extends. Parallel to the channel 16 extends an overflow 18, via which the first booster chamber 13 and a second control chamber 20 communicate with each other hydraulically.

Das mehrteilig ausgebildete, nadelförmige Einspritzventilglied 21 weist ein äußeres Nadelteil 22 sowie ein in diesem bewegbar angeordnetes inneres Nadelteil 23 auf. Das innere Nadelteil 23 wird durch den ersten Steuerraum 19 beaufschlagt, der mit dem zweiten Übersetzerraum 17 der hydraulischen Übersetzungsanordnung in Verbindung steht, während das äußere Nadelteil 22 über den zweiten Steuerraum 20, der über die Überströmleitung 18 mit dem ersten Übersetzerraum 13 in Verbindung steht, betätigt wird. Das äußere Nadelteil 22 weist eine den zweiten Steuerraum 20 begrenzende steuerraumseitige Stirnfläche 24 auf sowie eine erste Druckstufe 25 auf der Außenseite und eine weitere, zweite Druckstufe 26, die an der Innenseite des äußeren Nadelteiles 22 ausgebildet ist. Zwischen dem äußeren Nadelteil 22 und dem inneren Nadelteil 23 ist ein Druckraum 29 ausgebildet, der durch eine am inneren Nadelteil 23 ausgebildete Ringfläche 27 begrenzt wird. Die Beaufschlagung des innen liegenden Druckraumes 29 erfolgt über Druckraumzuläufe 30, welche die Wand des äußeren Nadelteiles 22 durchsetzen. Durch die Druckraumzuläufe 30 ist ein Überströmen von Kraftstoff welcher unter hohem Druck in den Düsenraum 8 einströmt, in den innen liegenden Druckraum 29 zwischen dem äußeren Nadelteil 22 und dem inneren Nadelteil 23 gewährleistet.The multi-part needle-shaped injection valve member 21 has an outer needle part 22 and an inner needle part 23 arranged movably in this needle part. The inner needle part 23 is acted upon by the first control chamber 19, which is in communication with the second booster chamber 17 of the hydraulic transmission arrangement, while the outer needle part 22 via the second control chamber 20 which communicates via the overflow 18 with the first booster chamber 13, is pressed. The outer needle part 22 has a second control chamber 20 limiting control-space-side end face 24 and a first pressure step 25 on the outside and a further, second pressure step 26, which is formed on the inside of the outer needle member 22. Between the outer needle part 22 and the inner needle part 23, a pressure chamber 29 is formed, which is bounded by an annular part 27 formed on the inner needle part 23. The application of the internal pressure chamber 29 via pressure chamber inlets 30, which pass through the wall of the outer needle member 22. Through the pressure chamber inlets 30 is an overflow of fuel which flows under high pressure into the nozzle chamber 8, guaranteed in the inner pressure chamber 29 between the outer needle member 22 and the inner needle member 23.

Am brennraumseitigen Ende des äußeren Nadelteiles 22 ist an dessen Außenumfang ein Sitz 31 ausgebildet, der einen ersten Sitzdurchmesser 32 aufweist. Die im ersten Sitzdurchmesser 32 ausgebildete Sitzkante wirkt mit der Wand des Düsenkörpers 3 zusammen. An dem inneren Nadelteil 23, welches im äußeren Nadelteil 22 des mehrteilig ausgebildeten Einspritzventilgliedes 21 geführt ist, ist ein ebenfalls mit der Wand des Düsenkörpers zusammenwirkender zweiter Sitz 33 ausgebildet. Der Sitzdurchmesser des Sitzes 33 des inneren Nadelteiles 23 ist in einem zweiten Sitzdurchmesser 34 (d1) ausgebildet, der erheblich geringer als der erste Sitzdurchmesser 32 des äußeren Nadelteiles 22 ist. Im in der Zeichnung dargestellten geschlossenen Zustand des mehrteilig ausgebildeten Einspritzventilgliedes 21 sind erste Einspritzöffnungen 35 durch den geschlossenen Sitz 31 des äußeren Nadelteiles 22 von einem Ringspalt 41 getrennt, in welchen über den Düsenraum 8 unter hohem Druck stehender Kraftstoff ansteht. Durch den in der Zeichnung ebenfalls in seinem geschlossenen Zustand dargestellten Sitz 33 des inneren Nadelteiles 23 sind zweite Einspritzöffnungen 36 ebenfalls gegen den im Ringspalt 41 anstehenden, unter hohem Druck stehenden Kraftstoff verschlossen. Im in der Zeichnung dargestellten geschlossenen Zustand des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes 21, bildet sich zwischen dem Sitz 31 des äußeren Nadelteiles 22 und dem Sitz 33 des inneren Nadelteiles 23 ein keilförmiger Ringraum 42 aus. Der Brennraum, in welchen bei geöffneten mehrteilig ausgebildetem Einspritzventilglied 21 Kraftstoff entweder über die ersten Einspritzöffnungen 35 oder über die geöffneten ersten und zweiten Einspritzöffnungen 35, 36 eingespritzt wird, ist mit Bezugszeichen 43 gekennzeichnet.At the combustion chamber end of the outer needle part 22, a seat 31 is formed on the outer circumference, which has a first seat diameter 32. The seat edge formed in the first seat diameter 32 interacts with the wall of the nozzle body 3. On the inner needle part 23, which is guided in the outer needle part 22 of the multi-part injection valve member 21, a cooperating with the wall of the nozzle body second seat 33 is formed. The seat diameter of the seat 33 of the inner needle member 23 is formed in a second seat diameter 34 (d 1 ) which is considerably smaller than the first seat diameter 32 of the outer needle member 22. In the illustrated in the drawing, the closed state of the multi-part injection valve member 21, first injection ports 35 are separated by the closed seat 31 of the outer needle member 22 of an annular gap 41, in which over the nozzle chamber 8 is under high pressure fuel. By means of the seat 33 of the inner needle part 23, which is also shown in its closed state in the drawing, second injection openings 36 are likewise closed against the fuel which is present in the annular gap 41 and is under high pressure. In the illustrated in the drawing closed state of the multi-part needle-shaped injection valve member 21, 23 forms a wedge-shaped annular space 42 between the seat 31 of the outer needle member 22 and the seat 33 of the inner needle member. The combustion chamber, in which fuel is injected either via the first injection openings 35 or via the opened first and second injection openings 35, 36 when the multi-part injection valve member 21 is open, is identified by reference number 43.

Das äußere Nadelteil 22 des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes 21 ist in einer Führungslänge 37 im Düsenkörper 3 aufgenommen, während das innere Nadelteil 23 in einer Führungslänge 38, die sich zwischen den Druckraumzuläufen 30 des äußeren Nadelteiles 23 und dessen Sitz 31 in diesen Körper 3 erstreckt, begrenzt ist. Auch wenn in der Zeichnung nicht detailliert dargestellt, kann das äußere Nadelteil 22 im Düsenkörper 3 auch in mehreren beispielsweise um 120° zueinander versetzt ausgebildeten Führungsflächen geführt sein.The outer needle part 22 of the multi-part, needle-shaped injection valve member 21 is received in a guide length 37 in the nozzle body 3, while the inner needle member 23 in a guide length 38 extending between the Druckraumzuläufen 30 of the outer needle member 23 and its seat 31 in this body 3 , is limited. Although not shown in detail in the drawing, the outer needle member 22 may be performed in the nozzle body 3 in a plurality of, for example, 120 ° offset from each other formed guide surfaces.

Das innere Nadelteil 23 des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes 21 weist im Bereich oberhalb des innen liegenden Druckraumes 29 einen zweiten Durchmesser 39 (d2) auf, welcher den zweiten Sitzdurchmesser 34 (d1) übersteigt, d. h. d2 > d1.The inner needle part 23 of the multi-part, needle-shaped injection valve member 21 has a second diameter 39 (d 2 ) in the region above the inner pressure chamber 29, which exceeds the second seat diameter 34 (d 1 ), ie d 2 > d 1 .

Aufgrund des Durchmesserverhältnisses von d1 : d2 mit d1 < d2 öffnet der innere Nadelteil 23 des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes 21 später als dessen äußerer Nadelteil 22. Die durch die Durchmesserdifferenz d2 - d1 erzeugte Druckstufe 28 am inneren Nadelteil 23, an dessen brennraumseitiger Spitze liegend, weist eine im Vergleich zu den Druckstufen 25, 26 erheblich niedrigere hydraulisch wirksame Fläche auf.Due to the diameter ratio of d 1 : d 2 with d 1 <d 2 opens the inner needle portion 23 of the multi-part, needle-shaped injection valve member 21 later than the outer needle portion 22. The generated by the diameter difference d 2 - d 1 pressure stage 28 on the inner needle portion 23rd , Lying on the combustion chamber side tip, has a compared to the pressure levels 25, 26 significantly lower hydraulically effective area.

Die Funktionsweise des erfindungsgemäß vorgeschlagenen Kraftstoffinjektors 1 gemäß der Zeichnung stellt sich wie folgt dar:The operation of the inventively proposed fuel injector 1 according to the drawing is as follows:

Im in der Zeichnung dargestellten Schließzustand des mehrteiligen Einspritzventilgliedes 21 ist der Aktor 6 bestromt und ausgefahren. Aufgrund der Bestromung des Aktors 6, der bevorzugt als Piezoaktor ausgebildet ist, längen sich dessen Piezokristalle, die in Form eines Stapels übereinander liegend angeordnet sind und beaufschlagen demzufolge den Übersetzerkolben 10. Dessen zweite Stirnfläche 12 fährt in den ersten Übersetzerraum 13 ein. Durch die zweite Stirnfläche 12 des Übersetzerkolbens 10 ist auch der Übersetzerkolbenfortsatz 14 in den zweiten Übersetzerraum 17 der hydraulischen Übersetzeranordnung 9 eingefahren. Der erste Übersetzerraum 13 und der zweite Übersetzerraum 17 werden über die Führungsleckagen zwischen dem äußeren Nadelteil 22 und dem Düsenkörper 3, der Führungsleckage zwischen dem inneren Nadelteil 23 und dem Injektorkörper 2 sowie über die Führungsleckage zwischen dem Übersetzerkolben 10 und dem Kraftstoffzulauf 5 befüllt.In the closed state of the multi-part injection valve member 21 shown in the drawing, the actuator 6 is energized and extended. Due to the energization of the actuator 6, which is preferably designed as a piezoelectric actuator, its piezocrystals length, which are arranged one above the other in the form of a stack and thus act on the booster piston 10. Its second end face 12 moves into the first booster room 13 a. By the second end face 12 of the booster piston 10 and the booster piston extension 14 is retracted into the second booster chamber 17 of the hydraulic booster assembly 9. The first booster chamber 13 and the second booster chamber 17 are filled via the guide leaks between the outer needle part 22 and the nozzle body 3, the guide leak between the inner needle part 23 and the injector body 2 and the guide leakage between the booster piston 10 and the fuel inlet 5.

Aufgrund der Druckbeaufschlagung des ersten Übersetzerraumes 13 und des zweiten Übersetzerraumes 17 sind auch der das innere Nadelteil 23 beaufschlagende erste Steuerraum 19 sowie der das äußere Nadelteil 22 beaufschlagende zweite Steuerraum 20 druckbeaufschlagt, so dass das innere Nadelteil 23 und das äußere Nadelteil 22 in ihre die Sitze 31 bzw. 33 verschließenden Positionen gestellt sind.Due to the pressurization of the first booster chamber 13 and the second booster chamber 17 and the inner needle part 23 acted upon first control chamber 19 and the outer needle member 22 acted upon second control chamber 20 are pressurized, so that the inner needle member 23 and the outer needle member 22 in their seats 31 or 33 closing positions are provided.

Da gleichzeitig über die Hochdruckzuleitung 7 unter hohem Druck stehender Kraftstoff im Düsenraum 8 ansteht, und damit auch in dem mit diesem verbundenen, den äußeren Nadelteil 22 umgebenden Ringspalt 41, gelangt der Kraftstoff nur bis zum verschlossenen Sitz 31 des äußeren Nadelteiles 22 und kann nicht in den Brennraum 43 eingespritzt werden.Since at the same time high-pressure fuel in the nozzle chamber 8 is present via the high pressure supply line 7, and thus in the connected thereto, the outer needle part 22 surrounding annular gap 41, the fuel passes only to the closed seat 31 of the outer needle member 22 and can not the combustion chamber 43 are injected.

Wird die Bestromung des Aktors 6 aufgehoben, geht die Längung der Piezokristalle zurück und der Übersetzerkolben 10 samt Übersetzerkolbenfortsatz 14 bewegt sich in vertikale Richtung nach oben. Der Hubweg des Übersetzerkolbens 10 bzw. des Übersetzerkolbenfortsatzes 14 liegt im Bereich zwischen 40 und 160µm.If the energization of the actuator 6 is canceled, the elongation of the piezoelectric crystals goes back and the booster piston 10, including the translator piston extension 14, moves in the vertical direction upwards. The stroke of the booster piston 10 and the booster piston extension 14 is in the range between 40 and 160 .mu.m.

Demzufolge werden auch der erste Steuerraum 19, welcher das innere Nadelteil 23 beaufschlagt sowie der zweite Steuerraum 20, der die steuerraumseitige Stirnfläche 24 des äußeren Nadelteiles 22 beaufschlagt, druckentlastet. Aufgrund des hohen Kraftstoffdruckes, der im Düsenraum 8 anliegt, öffnet das äußere Nadelteil 22 früher, da an diesem eine außen liegende erste Druckstufe 25 und eine innen liegende zweite Druckstufe 26 oberhalb des innen liegenden Druckraumes 29 ausgebildet sind. Demzufolge fährt zu Beginn der Aufhebung der Bestromung des Aktors 6 die steuerraumseitige Stirnfläche 24 des äußeren Nadelteiles 22 in den zweiten Steuerraum 20 ein, wodurch der Sitz 31 des äußeren Nadelteiles 22 geöffnet wird. Dadurch gelangt der Ringraum 42 in Verbindung mit dem Ringspalt 41, in welchem unter hohem Druck stehender Kraftstoff ansteht. Der unter hohem Druck stehende Kraftstoff kann über die ersten Einspritzöffnungen 35 während einer ersten Phase des Einspritzvorganges in den Brennraum 43 eingespritzt werden.Accordingly, the first control chamber 19, which acts on the inner needle part 23 and the second control chamber 20, which acts on the control-chamber-side end face 24 of the outer needle member 22, pressure relieved. Due to the high fuel pressure, which rests in the nozzle chamber 8, the outer needle part 22 opens sooner, since at this an outer first pressure stage 25 and an inner second pressure stage 26 are formed above the inner pressure chamber 29. Accordingly, at the beginning of the cancellation of the energization of the actuator 6 moves the control room-side end face 24 of the outer needle part 22 in the second control chamber 20, whereby the seat 31 of the outer needle member 22 is opened. As a result, the annular space 42 comes into communication with the annular gap 41, in which high-pressure fuel is present. The high-pressure fuel can be injected into the combustion chamber 43 via the first injection openings 35 during a first phase of the injection process.

Während der ersten Phase des Einspritzvorganges bleibt hingegen der innere Nadelteil 23 des mehrteilig ausgebildeten, nadelförmigen Einspritzventilgliedes 21 in seiner Schließstellung, d. h. der Sitz 33 des inneren Nadelteiles 23 bleibt geschlossen. Im weiteren Verlauf des Einspritzvorganges öffnet das innere Nadelteil 23 des mehrteilig ausgebildeten Einspritzventilgliedes 21, da die an diesem ausgebildete Druckstufe 28 sehr klein ausgebildet ist.During the first phase of the injection process, however, the inner needle portion 23 of the multipart, needle-shaped injection valve member 21 remains in its closed position, d. H. the seat 33 of the inner needle part 23 remains closed. In the course of the injection process, the inner needle part 23 of the multi-part injection valve member 21 opens, since the pressure stage 28 formed thereon is very small.

Im weiteren Verlauf des Einspritzvorganges strömt über die Druckraumzuläufe 30 unter hohem Druck stehender Kraftstoff in den innen liegenden Druckraum 29 zwischen dem äußeren Nadelteil 22 und dem inneren Nadelteil 23 ein. Der in den innen liegenden Druckraum 29 einströmende Kraftstoff steht an der Ringfläche 27 des inneren Nadelteiles 23 an und beaufschlagt diese weiterhin in Schließrichtung. Während der vertikalen Auffahrbewegung des äußeren Nadelteiles 22, tritt der Ringspalt 41 mit dem Ringraum 42 in Verbindung. Infolgedessen wird ein in Öffnungsrichtung wirksame hydraulische Kraft an der Druckstufe 28 am brennraumseitigen Ende des inneren Nadelteiles 23 wirksam, welche dieses in Öffnungsrichtung bewegt. Dadurch wird auch der zweite Sitz 33 des inneren Nadelteiles 23 geöffnet und Kraftstoff strömt über den nunmehr geöffneten zweiten Sitz 33 den zweiten Einspritzöffnungen 36 zu. Bei gleichzeitig geöffnetem inneren Nadelteil 23 und äußerem Nadelteil 22 strömt aus dem Düsenraum 8 über den Ringspalt 41 Kraftstoff über beide Einspritzöffnungen 35, 36 in den Brennraum 43 ein. Der Durchmesser des inneren Nadelteiles 23, d.h. der erste Durchmesser 39 liegt im Bereich zwischen 1,5 und 2,5 mm, während der Durchmesser des zweiten Steuerraumes 20 zwischen 3,5 und 5,6 mm liegen kann, je nach Ausführung des Kraftstoffinjektors.In the further course of the injection process, high-pressure fuel flows into the inner pressure space 29 between the outer needle part 22 and the inner needle part 23 via the pressure chamber inlets 30. The fuel flowing into the interior pressure chamber 29 is in contact with the annular surface 27 of the inner needle part 23 and continues to act on it in the closing direction. During the vertical movement of the outer needle part 22, the annular gap 41 enters the annular space 42 in connection. As a result, an effective in the opening direction hydraulic force at the pressure stage 28 at the combustion chamber end of the inner needle member 23 is effective, which moves this in the opening direction. As a result, the second seat 33 of the inner needle part 23 is also opened and fuel flows via the now opened second seat 33 to the second injection openings 36. When the inner needle part 23 and the outer needle part 22 are open at the same time, fuel flows from the nozzle chamber 8 via the annular gap 41 via both injection openings 35, 36 into the combustion chamber 43. The diameter of the inner needle part 23, i. the first diameter 39 is in the range between 1.5 and 2.5 mm, while the diameter of the second control chamber 20 may be between 3.5 and 5.6 mm, depending on the design of the fuel injector.

Bei Bestromung des Piezoaktors 6, welcher in den Kraftstoffzulauf 5 vom in der Zeichnung nicht dargestellten Hochdruckspeicher angeordnet ist, dehnt sich dessen Piezokristallstapel aus, so dass der Übersetzerkolben 10 samt Übersetzerkolbenfortsatz 14 eine in Richtung des Brennraumes 43 wirkende Schließbewegung ausführt. Dadurch werden die in dem ersten Übersetzerraum 13 sowie im zweiten Übersetzerraum 17 enthaltenen Kraftstoffvolumina komprimiert und über den Kanal 16 bzw. die Überströmleitung 18 die Steuerräume 19 bzw. 20 druckbeaufschlagt. Da die die Steuerräume 19 bzw. 20 begrenzenden, hydraulisch wirksamen Flächen, d. h. die obere Stirnseite des inneren Nadelteiles 23 und steuerraumseitige Stirnfläche 24 des äußeren Nadelteiles 22 hydraulisch wirksamen Flächen der Druckstufen 25, 26 des äußeren Nadelteiles 22 sowie die in Öffnungsrichtung wirksame hydraulische Fläche π(d2 2- d1 2)/4 der Druckstufe 28 am brennraumseitigen Ende des inneren Nadelteiles 23 übersteigen, werden beide Nadelteile 22, 23 des mehrteilig ausgebildeten Einspritzventilgliedes 21 wieder in ihre Schließstellung gestellt.When current flows through the piezoelectric actuator 6, which is arranged in the fuel inlet 5 from the high-pressure accumulator not shown in the drawing, its piezocrystal stack expands, so that the booster piston 10 together with the translating piston extension 14 executes a closing movement acting in the direction of the combustion chamber 43. As a result, the fuel volumes contained in the first booster chamber 13 and in the second booster chamber 17 are compressed and the control chambers 19 and 20 are pressurized via the channel 16 and the overflow line 18, respectively. Since the control spaces 19 and 20 delimiting, hydraulically effective surfaces, ie the upper end face of the inner needle member 23 and Control chamber-side end face 24 of the outer needle member 22 hydraulically effective surfaces of the compression stages 25, 26 of the outer needle member 22 and the effective in the opening direction hydraulic surface π (d 2 2 - d 1 2 ) / 4 of the pressure stage 28 at the combustion chamber end of the inner needle member 23 exceed Both needle parts 22, 23 of the multi-part injection valve member 21 are again placed in their closed position.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Kraftstoffinjektorfuel injector
22
Injektorkörperinjector
33
Düsenkörpernozzle body
44
Stoßfugebutt joint
55
KraftstoffzulaufFuel supply
66
Piezoaktorpiezo actuator
77
HochdruckzuleitungHigh pressure supply line
88th
Düsenraumnozzle chamber
99
hydraulische Übersetzeranordnunghydraulic translator assembly
1010
ÜbersetzerkolbenBooster piston
1111
erste Stirnflächefirst end face
1212
zweite Stirnflächesecond end face
1313
erster Übersetzerraumfirst translator room
1414
ÜbersetzerkolbenfortsatzIntensifier piston extension
1515
Stirnseite Übersetzerkolben FortsatzEnd of the translator piston extension
1616
Kanalchannel
1717
zweiter Übersetzerraumsecond translator room
1818
Überströmleitungoverflow
1919
erster Steuerraumfirst control room
2020
zweiter Steuerraumsecond control room
2121
mehrteiliges Einspritzventilgliedmulti-part injection valve member
2222
äußeres Nadelteilouter needle part
2323
inneres Nadelteilinner needle part
2424
steuerraumseitige Stirnfläche von 22control room-side end face of 22
2525
erste Druckstufe von 22first pressure level of 22
2626
zweite Druckstufe von 22second pressure level of 22
2727
Ringfläche inneres Nadelteil 23Ring surface inner needle part 23
2828
Druckstufe inneres Nadelteil 23Pressure stage inner needle part 23
2929
innen liegender Druckrauminside pressure room
3030
DruckraumzulaufPressure chamber inlet
3131
Sitz äußeres NadelteilSeat outer needle part
3232
erster Sitzdurchmesserfirst seat diameter
3333
Sitz inneres NadelteilSeat inner needle part
3434
zweiter Sitzdurchmessersecond seat diameter
3535
erste Einspritzöffnungenfirst injection openings
3636
zweite Einspritzöffnungensecond injection openings
3737
Führungslänge äußeres Nadelteil 22Guide length outer needle part 22
3838
Führungslänge inneres Nadelteil 23Guide length inner needle part 23
3939
erster Durchmesser inneres Nadelteil 23first diameter inner needle part 23
4141
Ringspaltannular gap
4242
Ringraumannulus
4343
Brennraumcombustion chamber

Claims (10)

  1. Fuel injector (1) for a common rail injection system for injecting fuel into a combustion chamber (43) of an internal combustion engine, having an injector body (2) and a nozzle body (3), in which an injection valve member (21) of multiple-part configuration is accommodated, and having a piezoelectric actuator (6), behind which a hydraulic transmitter arrangement (9) is connected, the injection valve member (21) of multiple-part configuration being assigned control spaces (19, 20) for its actuation, characterized in that the hydraulic transmitter arrangement (9) which is actuated by the piezoelectric actuator (6) has transmitter spaces (13, 17) which are connected hydraulically in each case directly to the control spaces (19, 20) which actuate needle parts (22, 23) of the injection valve member (21).
  2. Fuel injector according to Claim 1, characterized in that the first transmitter space (13) is connected via a channel (16) to the second control space (20) for the outer needle part (22) and the second transmitter space (17) is connected to the first control space (19) for the inner needle part (23).
  3. Fuel injector according to Claim 1, characterized in that a pressure space (29) which can be filled by a nozzle space (8) which surrounds the injection valve member (21) of multiple-part configuration is formed between the needle parts (22, 23) which are guided into one another of the injection valve member of multiple-part configuration.
  4. Fuel injector according to Claim 1, characterized in that a first and a second compression stage (25, 26) which act in the opening direction are formed on the outer needle part (22) of the injection valve member (21) of multiple-part configuration.
  5. Fuel injector according to Claims 3 and 4, characterized in that the second compression stage (26) is formed in the pressure space (29).
  6. Fuel injector according to Claim 1, characterized in that a compression stage (28) is formed on the inner needle part (23) at the combustion-chamber-side end, the hydraulic surface area of which compression stage (28) which acts in the opening direction of the inner needle part (23) is smaller than the hydraulically active surfaces areas of the first and second compression stages (25, 26) of the outer needle part (23).
  7. Fuel injector according to Claim 1, characterized in that those surface areas of the compression stages (25, 26) of the outer needle part (22) which act hydraulically in the opening direction exceed the hydraulically acting surface area (28) n (d2 2 - d1 2) /4 at the combustion-chamber-side end of the inner needle part (23).
  8. Fuel injector according to Claim 1, characterized in that a first seat (31) is formed on the outer needle part (22) and a second seat (33) is formed on the inner needle part (23), which seats (31, 33) interact with a wall of the nozzle body (3).
  9. Fuel injector according to Claim 1, characterized in that the piezoelectric actuator (6) is integrated into the fuel feed line (5).
  10. Fuel injector according to Claim 1, characterized in that first injection openings (35) which can be opened or closed on the nozzle body (3) by the first seat (31) in the direction of the combustion chamber (43) and second injection openings (36) which can be opened or closed by the second seat (33) are formed.
EP04786717A 2003-10-18 2004-09-06 Fuel injector with a multipart, directly controlled injection valve element Expired - Lifetime EP1682769B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10348925A DE10348925A1 (en) 2003-10-18 2003-10-18 Fuel injector with multipart, directly controlled injection valve member
PCT/DE2004/001995 WO2005040595A1 (en) 2003-10-18 2004-09-06 Fuel injector with a multipart, directly controlled injection valve element

Publications (2)

Publication Number Publication Date
EP1682769A1 EP1682769A1 (en) 2006-07-26
EP1682769B1 true EP1682769B1 (en) 2007-09-05

Family

ID=34428498

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04786717A Expired - Lifetime EP1682769B1 (en) 2003-10-18 2004-09-06 Fuel injector with a multipart, directly controlled injection valve element

Country Status (7)

Country Link
US (1) US20070204837A1 (en)
EP (1) EP1682769B1 (en)
JP (1) JP4273153B2 (en)
KR (1) KR20060096049A (en)
AT (1) ATE372457T1 (en)
DE (2) DE10348925A1 (en)
WO (1) WO2005040595A1 (en)

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CN107940798A (en) * 2017-11-24 2018-04-20 山东理工大学 The sectionally assembled injector conversion assembly of multi-state and on-line automatic conversion equipment

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DE102005037954A1 (en) * 2005-08-11 2007-02-15 Robert Bosch Gmbh Fuel injection valve for internal combustion engines
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JP4591555B2 (en) * 2008-06-12 2010-12-01 株式会社日本自動車部品総合研究所 Fuel injection nozzle and fuel injection control device using the same
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DE102014215450B4 (en) * 2014-08-05 2016-03-31 Engineering Center Steyr Gmbh & Co. Kg Fluid injection apparatus

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Also Published As

Publication number Publication date
WO2005040595A1 (en) 2005-05-06
DE10348925A1 (en) 2005-05-12
EP1682769A1 (en) 2006-07-26
KR20060096049A (en) 2006-09-05
JP4273153B2 (en) 2009-06-03
US20070204837A1 (en) 2007-09-06
JP2007508487A (en) 2007-04-05
ATE372457T1 (en) 2007-09-15
DE502004004907D1 (en) 2007-10-18

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