WO2018141335A1 - Fuel injector for an internal combustion engine - Google Patents

Fuel injector for an internal combustion engine Download PDF

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Publication number
WO2018141335A1
WO2018141335A1 PCT/DE2018/100069 DE2018100069W WO2018141335A1 WO 2018141335 A1 WO2018141335 A1 WO 2018141335A1 DE 2018100069 W DE2018100069 W DE 2018100069W WO 2018141335 A1 WO2018141335 A1 WO 2018141335A1
Authority
WO
WIPO (PCT)
Prior art keywords
guide bore
fuel injection
anchor rod
injection injector
injector according
Prior art date
Application number
PCT/DE2018/100069
Other languages
German (de)
French (fr)
Inventor
Hans-Joachim Koch
Frank Grässler
Original Assignee
L'orange Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by L'orange Gmbh filed Critical L'orange Gmbh
Publication of WO2018141335A1 publication Critical patent/WO2018141335A1/en

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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
    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0664Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
    • F02M51/0671Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type
    • 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
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0033Lift valves, i.e. having a valve member that moves perpendicularly to the plane of the valve seat
    • F02M63/0036Lift valves, i.e. having a valve member that moves perpendicularly to the plane of the valve seat with spherical or partly spherical shaped valve member ends
    • 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
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0043Two-way valves
    • 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
    • F02M63/0012Valves
    • F02M63/007Details not provided for in, or of interest apart from, the apparatus of the groups F02M63/0014 - F02M63/0059
    • 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
    • F02M2200/04Fuel-injection apparatus having means for avoiding effect of cavitation, e.g. erosion
    • 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
    • F02M2200/28Details of throttles in fuel-injection apparatus
    • 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
    • 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
    • F02M2547/00Special features for fuel-injection valves actuated by fluid pressure
    • F02M2547/003Valve inserts containing control chamber and valve piston

Definitions

  • the invention relates to a fuel injection injector for an internal combustion engine with a pilot valve for controlling the lifting movement of a nozzle needle according to the preamble of claim 1.
  • a fuel injection injector known from DE 10 2011 051 903 A1 has a pilot valve with an anchor rod which is lifted when the pilot valve is actuated by electromagnetic means, whereupon a nozzle needle of the fuel injection injector is lifted out of its sealing seat and fuel exits.
  • the anchor rod is guided axially displaceably in a guide bore in a pilot valve housing.
  • the guide bore is adjoined by a transitional space of larger diameter, which is bounded by a control chamber bushing with a throttle channel introduced therein.
  • the anchor rod acts on a closing body in a closed position, which closes the throttle channel in the control chamber socket.
  • the anchor rod is raised, and it can fuel that is under a high pressure, flow from a control chamber in the control chamber via the throttle passage in the transition space. This proportion of fuel, the one
  • Tax leakage forms can be removed via leakage bores from the transitional space.
  • the invention has for its object to design a fuel injection injector reliable with simple design measures.
  • the fuel injection injector according to the invention with which fuel is injected into the cylinders of an internal combustion engine, has a pilot valve for controlling the lifting movement of a nozzle needle, which is lifted from its sealing seat to carry out the injection process, whereupon fuel exits via an injection nozzle of the injection injector can.
  • the pilot valve has an armature with an anchor rod, wherein the armature can be preferably raised by electromagnetic means for the injection process.
  • the anchor rod is guided in a guide bore in a pilot valve housing and can be adjusted axially in relation to the longitudinal axis of the fuel injection injector including the nozzle needle and anchor rod in the guide bore.
  • the anchor rod is preferably subjected to a force of a spring element, against the spring force of the anchor rod is raised in electromagnetic actuation.
  • an electromagnetic actuator is preferably integrated into the housing of the pilot valve, is energized in the armature of the pilot valve is raised.
  • the guide bore in which the anchor rod is axially guided, adjacent to a transition space, which is preferably also in the pilot valve housing and which is limited on the armature rod opposite side of a control chamber socket.
  • Transition space is advantageously in the edge region of the pilot valve housing.
  • Control chamber socket is a throttle channel introduced, which in particular runs axially and connects a control chamber within the control chamber socket with the transition space.
  • Throttling channel is to be closed by an adjustable closing body of the
  • Anchor rod can be acted upon in the closed position. With the lifting of the anchor rod upon actuation of the pilot valve against the force of a force acting on the anchor rod
  • Fluid communication between the control room and the transition space is created and fuel that is under high pressure, can flow from the control room in the transition space. Then, the nozzle needle is lifted from its sealing seat and can leak fuel through the injector.
  • Transition space flows, forms a control leakage, which is preferably derived via a discharge channel to the low pressure side of the fuel injection injector.
  • a control leakage which is preferably derived via a discharge channel to the low pressure side of the fuel injection injector.
  • an axially adjustable transmission member is arranged in the transition space in the transmission path to the closing body, which closes the guide bore when the throttle channel is open in the control chamber.
  • the anchor rod is in the non-actuated state, in which the armature rod is subjected to force by the force of the spring element in the sealing position, the
  • Locking body adjusted in the closed position for closing the throttle channel, so that no fuel can flow from the control chamber via the throttle channel in the transition space.
  • the transfer member is in this position, although no longer in his
  • Control chamber socket is closed by the closing body, no tax leakage in the
  • the transmission member is in the transmission path from the anchor rod to the
  • Closing body which closes the throttle channel in the control chamber socket in the closed position.
  • the transmission member advantageously connects axially to the anchor rod.
  • Closing forces, which are exerted by the spring element on the anchor rod are passed from the anchor rod via the transmission member to the closing body, which is thereby acted upon in the closed position for closing the throttle channel.
  • the transmission member is as a separate from the
  • Anchor rod executed component formed adjacent to the front side of the anchor rod. There is advantageously no firm connection between the anchor rod and the
  • the transmission member is acted upon by the end face of the anchor rod in the direction of the closing position of the closing body.
  • the transmission member is adjusted by the pressure of the control leakage, which flows into the transition space in the guide bore closing position, so that the control leakage is prevented from flowing into the guide bore.
  • the transmission member is either integral with the transmission member
  • Anchor rod formed or formed separately from the anchor rod, but firmly with the Anchor rod connected.
  • the transmission member is adjusted at pronounceaktuiertm pilot valve by the spring element in the same manner as the anchor rod in the direction of the closed position of the closing body. With the actuation of the pilot valve, the anchor rod is lifted against the force of the spring element, as well as the transmission member, which is integral with the anchor rod or firmly connected to the anchor rod. In addition, the pressure of the control leakage, which flows into the transfer space, acts on the
  • Transmission member and acts on this in the direction of closing the guide bore.
  • the transfer member is open throttle channel on the mouth opening of the guide bore in the transitional space.
  • the transition space in the radial direction - radially to the longitudinal axis of the fuel injection injector - has a greater extent than the guide bore, so that the
  • Mouth opening of the guide bore is bounded by an edge which is part of the inner wall of the transitional space.
  • the transmission member has a
  • Mouth opening of the guide hole limiting edge rests.
  • This design can be easily realized in a constructive manner and makes it possible to close the mouth opening of the guide bore through the transmission member when the anchor rod of the pilot valve is raised, so that no control leakage can propagate axially into the guide bore.
  • the support collar has a
  • the outer diameter of the annular bead for example, at least approximately
  • Outer diameter of the support collar correspond.
  • the outer diameter of the support collar is at least 30% larger than the outer diameter of the transmission member on the control chamber bushing facing side. This difference in size in the
  • Outer diameter ensures that the transfer member is a sufficiently large
  • the control leakage surface provides so that the control leakage entering the transitional space effectively pressurizes the transmission member in the direction of closing the guide bore.
  • the transmission member on the side facing the anchor rod on a pin which preferably projects into the guide bore in all positions of the anchor rod.
  • the transmission member is safely and precisely out in the axial direction between the closed position for closing the guide bore and the open position.
  • the axial length of the pin is for example at least 30% of the total axial length of
  • the pin of the transmission member may optionally have an at least slightly larger diameter than the control chamber bushing facing portion of the
  • FIG. 1 shows a longitudinal section through a fuel injection injector for an internal combustion engine in the region of a pilot valve, via a transmission member a closing body in a
  • Fig. 2 is an enlarged view of the region of the transmission member.
  • the fuel injection injector 1 in a pilot valve housing 2 has a pilot valve 3, which has an armature 4 and a fixed armature 4 connected anchor rod 5 which is axially displaceable in a guide bore 6 in the pilot valve housing 2 - relative to the longitudinal axis 8 of the fuel injection injector 1 - is stored.
  • the pilot valve 3 is formed electromagnetically aktuierbar, wherein in the case of actuation of the armature 4 with the firmly connected anchor rod 5 against the force of a
  • Spring element 7 which forms a pilot valve spring, is pulled upwards.
  • the actuation is carried out by means of an electromagnetic actuator, which is integrated in the pilot valve housing 2 of the fuel injection injector 1 and during its energization of the armature 4 of the
  • Pilot valve 3 is raised.
  • armature 4 and anchor rod 5 are pressed by the force of the spring element 7 down in the direction of a closed position in which a throttle channel 10 is closed flow-tight in a control chamber socket 9.
  • the anchor rod 5 acts on a transmission member 12, which is located on the front side of the
  • Anchor rod 5 is against a closing body 11 in the form of a closing ball, which in a recess on the facing end face of the control chamber 9 in the area of
  • the control chamber 9 is located in a high-pressure chamber 13 which is formed in a nozzle body 14, which adjoins the pilot valve housing 2.
  • the pilot valve housing 2 and the nozzle body 14 are connected to each other via a clamping nut 15.
  • the fuel flows via a high pressure supply line 16 into the high pressure chamber 13 and passes from this into a control chamber within the control chamber 9, wherein the control chamber with the
  • Throttle channel 10 communicates and is connected via the throttle channel 10 with a transitional space 17 which connects axially to the guide bore 6 and at the
  • Nozzle body 14 facing edge side of the pilot valve housing 2 is located.
  • Transmission member 12 is for the most part arranged in the transitional space 17.
  • the transitional space 17 is connected to a discharge channel for discharging fuel, which in the
  • Transition space 17 flows. About the discharge channel takes place a derivative of the fuel from the transitional space 17 to the low pressure side.
  • Transition space 17 can flow. Then a nozzle needle is lifted from its sealing seat and can leak fuel through an injection nozzle.
  • the transmission member 12 has on the armature rod 5 side facing a pin 19 which projects into the guide bore 6. Between the pin 18 and the main body of the transmission member 12 is a support collar 19, the outer diameter is greater than the inner diameter of the guide bore 6 and 5 raised anchor rod 5 closes the mouth opening of the guide bore 6 in the transitional space 17.
  • Main body 20 of the transmission member 12 is opposite to the pin 18 and is located within the transition space 17. At the top of the main body 20 has the
  • the pin 18 protrudes into the guide bore 6 in all positions of the anchor rod 5.
  • the diameter of the pin 18 is slightly larger than the diameter of the main body 20.
  • the axial length of the pin 18 is for example at least 30% of the axial
  • Main body 20 and for example at least 20% of the total axial length below
  • the receptacle 21 may either one-piece component of the transmission member 12 or formed separately from the transmission member 12, but be connected to the transmission member 12.
  • the edge defining the mouth opening of the guide bore 6, which is part of the inner wall of the transitional space 17, is formed as a raised annular bead 22 (FIG. 2).
  • This annular bead 22 of the support collar 19 of the transfer member 12 is raised
  • Anchor rod 5 sealingly and thereby prevents a transfer of fuel, which flows with raised anchor rod 5 and raised closing body 11 via the throttle channel 10 in the transitional space 17, in the guide bore 6 into it.
  • This fuel which forms a control leak, can thus not spread axially from the transition space 17 into the guide bore 6 when the anchor rod 5 is raised, so that a deposit formation on the inner wall of the guide bore 6 or the outer jacket of the anchor rod 5 is prevented.
  • the transmission member 12 is lifted by the pressure of the inflowing into the transitional space 17 fuel from the sealing or closing position, so that the Support collar 19 sealingly pressed against the annular bead 22.
  • the lifting anchor rod 5 is carried out by actuation of the pilot valve. 3
  • the anchor rod 5 is pressed by the force of the spring element 7 back down, whereupon the anchor rod 5 and the closing body 11 are pressed into its closed position, in which the throttle channel 10 is closed flow-tight.

Abstract

The invention relates to a fuel injector for an internal combustion engine comprising a pilot valve for controlling the stroke motion of a nozzle needle, an armature rod of the pilot valve being guided in a guide bore, which a transition space adjoins. In the transition space, an axially movable transmission element is arranged, which closes the guide bore in defined states of the armature rod.

Description

BESCHREIBUNG  DESCRIPTION
Kraftstoff-Einspritzinjektor für eine Brennkraftmaschine Fuel injection injector for an internal combustion engine
Die Erfindung bezieht sich auf einen Kraftstoff-Einspritzinjektor für eine Brennkraftmaschine mit einem Pilotventil zur Steuerung der Hubbewegung einer Düsennadel nach dem Oberbegriff des Anspruches 1. The invention relates to a fuel injection injector for an internal combustion engine with a pilot valve for controlling the lifting movement of a nozzle needle according to the preamble of claim 1.
Ein aus der DE 10 2011 051 903 AI bekannter Kraftstoff-Einspritzinjektor weist ein Pilotventil mit einer Ankerstange auf, die bei elektromagnetischer Betätigung des Pilotventils angehoben wird, woraufhin eine Düsennadel des Kraftstoff-Einspritzinjektors aus ihrem Dichtsitz angehoben wird und Kraftstoff austritt. Die Ankerstange ist in einer Führungsbohrung in einem Pilotventilgehäuse axial verschieblich geführt. An die Führungsbohrung schließt sich ein Übergangsraum größeren Durchmessers an, der von einer Steuerraumbuchse mit einem darin eingebrachten Drosselkanal begrenzt ist. Die Ankerstange beaufschlagt einen Schließkörper in eine Schließposition, der den Drosselkanal in der Steuerraumbuchse verschließt. Bei einer elektromagnetischen Betätigung wird die Ankerstange angehoben, und es kann Kraftstoff, der unter einem hohen Druck steht, aus einem Steuerraum in der Steuerraumbuchse über den Drosselkanal in den Übergangsraum strömen. Dieser Anteil des Kraftstoffs, der eine A fuel injection injector known from DE 10 2011 051 903 A1 has a pilot valve with an anchor rod which is lifted when the pilot valve is actuated by electromagnetic means, whereupon a nozzle needle of the fuel injection injector is lifted out of its sealing seat and fuel exits. The anchor rod is guided axially displaceably in a guide bore in a pilot valve housing. The guide bore is adjoined by a transitional space of larger diameter, which is bounded by a control chamber bushing with a throttle channel introduced therein. The anchor rod acts on a closing body in a closed position, which closes the throttle channel in the control chamber socket. In an electromagnetic operation, the anchor rod is raised, and it can fuel that is under a high pressure, flow from a control chamber in the control chamber via the throttle passage in the transition space. This proportion of fuel, the one
Steuerleckage bildet, kann über Leckagebohrungen aus dem Übergangsraum abgeführt werden. Der Erfindung liegt die Aufgabe zugrunde, mit einfachen konstruktiven Maßnahmen einen Kraftstoff-Einspritzinjektor betriebssicher auszubilden. Tax leakage forms can be removed via leakage bores from the transitional space. The invention has for its object to design a fuel injection injector reliable with simple design measures.
Diese Aufgabe wird erfindungsgemäß mit den Merkmalen des Anspruches 1 gelöst. Die Unteransprüche geben zweckmäßige Weiterbildungen an. This object is achieved with the features of claim 1. The dependent claims indicate expedient developments.
Der erfindungsgemäße Kraftstoff-Einspritzinjektor, mit dem Kraftstoff in die Zylinder einer Brennkraftmaschine eingespritzt wird, weist ein Pilotventil zur Steuerung der Hubbewegung einer Düsennadel auf, die zur Durchführung des Einspritzvorganges aus ihrem Dichtsitz angehoben wird, woraufhin Kraftstoff über eine Einspritzdüse des Einspritzinjektors austreten kann. Das Pilotventil weist einen Anker mit einer Ankerstange auf, wobei der Anker vorzugsweise auf elektromagnetischem Weg für den Einspritzvorgang angehoben werden kann. Die Ankerstange ist in einer Führungsbohrung in einem Pilotventilgehäuse geführt und kann axial - bezogen auf die Längsachse des Kraftstoff-Einspritzinjektors einschließlich Düsennadel und Ankerstange - in der Führungsbohrung verstellt werden. Die Ankerstange ist vorzugsweise von einem Federelement kraftbeaufschlagt, gegen dessen Federkraft die Ankerstange bei elektromagnetischer Aktuierung angehoben wird. Zur Aktuierung ist vorzugsweise ein elektromagnetischer Aktor in das Gehäuse des Pilotventils integriert, bei dessen Bestromung der Anker des Pilotventils angehoben wird. The fuel injection injector according to the invention, with which fuel is injected into the cylinders of an internal combustion engine, has a pilot valve for controlling the lifting movement of a nozzle needle, which is lifted from its sealing seat to carry out the injection process, whereupon fuel exits via an injection nozzle of the injection injector can. The pilot valve has an armature with an anchor rod, wherein the armature can be preferably raised by electromagnetic means for the injection process. The anchor rod is guided in a guide bore in a pilot valve housing and can be adjusted axially in relation to the longitudinal axis of the fuel injection injector including the nozzle needle and anchor rod in the guide bore. The anchor rod is preferably subjected to a force of a spring element, against the spring force of the anchor rod is raised in electromagnetic actuation. To actuate an electromagnetic actuator is preferably integrated into the housing of the pilot valve, is energized in the armature of the pilot valve is raised.
Die Führungsbohrung, in der die Ankerstange axial geführt ist, grenzt an einen Übergangsraum an, der sich vorzugsweise ebenfalls in dem Pilotventilgehäuse befindet und der auf der der Ankerstange gegenüberliegenden Seite von einer Steuerraumbuchse begrenzt ist. Der The guide bore, in which the anchor rod is axially guided, adjacent to a transition space, which is preferably also in the pilot valve housing and which is limited on the armature rod opposite side of a control chamber socket. Of the
Übergangsraum liegt vorteilhafterweise in Randbereich des Pilotventilgehäuses. In die Transition space is advantageously in the edge region of the pilot valve housing. In the
Steuerraumbuchse ist ein Drosselkanal eingebracht, der insbesondere axial verläuft und einen Steuerraum innerhalb der Steuerraumbuchse mit dem Übergangsraum verbindet. Der Control chamber socket is a throttle channel introduced, which in particular runs axially and connects a control chamber within the control chamber socket with the transition space. Of the
Drosselkanal ist von einem verstellbaren Schließkörper zu verschließen, der von der Throttling channel is to be closed by an adjustable closing body of the
Ankerstange in die Schließposition beaufschlagbar ist. Mit dem Anheben der Ankerstange bei Aktuierung des Pilotventils gegen die Kraft eines auf die Ankerstange wirkenden Anchor rod can be acted upon in the closed position. With the lifting of the anchor rod upon actuation of the pilot valve against the force of a force acting on the anchor rod
Federelementes gibt der Schließkörper den Drosselkanal frei, wodurch eine Spring element, the closing body releases the throttle channel, whereby a
Strömungsverbindung zwischen dem Steuerraum und dem Übergangsraum geschaffen wird und Kraftstoff, der unter Hochdruck steht, aus dem Steuerraum in den Übergangsraum strömen kann. Daraufhin wird die Düsennadel aus ihrem Dichtsitz angehoben und kann Kraftstoff über die Einspritzdüse austreten.  Fluid communication between the control room and the transition space is created and fuel that is under high pressure, can flow from the control room in the transition space. Then, the nozzle needle is lifted from its sealing seat and can leak fuel through the injector.
Der Kraftstoff, der während des Anhebens der Ankerstange aus dem Steuerraum in den The fuel, which during the raising of the anchor rod from the control room in the
Übergangsraum strömt, bildet eine Steuerleckage, die vorzugsweise über einen Ableitungskanal zur Niederdruckseite des Kraftstoff-Einspritzinjektors abgeleitet wird. Um zu vermeiden, dass insbesondere während der Dauer des Einspritzvorgangs der Leckagekraftstoff sich in den Ringspalt zwischen der Führungsbohrung und der Ankerstange axial ausbreitet und aufgrund der verhältnismäßig hohen Temperatur und des Drucks einen Belag an der Innenwand der Transition space flows, forms a control leakage, which is preferably derived via a discharge channel to the low pressure side of the fuel injection injector. In order to avoid that, especially during the duration of the injection process, the leakage fuel axially propagates into the annular gap between the guide bore and the anchor rod and due to the relatively high temperature and pressure, a coating on the inner wall of the
Führungsbohrung bzw. dem Außenmantel der Ankerstange bildet, ist in dem Übergangsraum im Übertragungsweg zum Schließkörper ein axial verstellbares Übertragungsglied angeordnet, das bei geöffnetem Drosselkanal in der Steuerraumbuchse die Führungsbohrung verschließt. Damit ist gewährleistet, dass der unter hohem Druck stehende Leckagekraftstoff, der während des Anhebens der Ankerstange in den Übergangsraum strömt, sich nicht in die Führungsbohrung hinein ausbreiten kann, so dass eine Belagsbildung an der Innenwand der Führungsbohrung bzw. dem Außenmantel der Ankerstange zuverlässig verhindert wird. Forming guide bore or the outer jacket of the anchor rod, an axially adjustable transmission member is arranged in the transition space in the transmission path to the closing body, which closes the guide bore when the throttle channel is open in the control chamber. In order to ensures that the high pressure leakage fuel that flows during the lifting of the anchor rod in the transition space can not propagate into the guide bore, so that a deposit on the inner wall of the guide bore and the outer jacket of the anchor rod is reliably prevented.
Befindet sich dagegen die Ankerstange im nicht-aktuierten Zustand, in welchem die Ankerstange durch die Kraft des Federelementes in die Dichtposition kraftbeaufschlagt ist, wird der If, on the other hand, the anchor rod is in the non-actuated state, in which the armature rod is subjected to force by the force of the spring element in the sealing position, the
Schließkörper in die Schließposition zum Verschließen des Drosselkanals verstellt, so dass kein Kraftstoff vom Steuerraum über den Drosselkanal in den Übergangsraum strömen kann. Das Übertragungsglied befindet sich in dieser Position zwar nicht mehr in seiner die Locking body adjusted in the closed position for closing the throttle channel, so that no fuel can flow from the control chamber via the throttle channel in the transition space. The transfer member is in this position, although no longer in his
Führungsbohrung verschließenden Stellung; da jedoch der Drosselkanal in der Guide bore closing position; However, since the throttle channel in the
Steuerraumbuchse vom Schließkörper verschlossen ist, kann keine Steuerleckage in den Control chamber socket is closed by the closing body, no tax leakage in the
Übergangsraum und weiter in die Führungsbohrung strömen. Das Übertragungsglied befindet sich im Übertragungsweg von der Ankerstange zu dem Transition space and continue to flow into the guide hole. The transmission member is in the transmission path from the anchor rod to the
Schließkörper, der in der Schließposition den Drosselkanal in der Steuerraumbuchse verschließt. Das Übertragungsglied schließt sich vorteilhafterweise axial an die Ankerstange an. Die  Closing body which closes the throttle channel in the control chamber socket in the closed position. The transmission member advantageously connects axially to the anchor rod. The
Schließkräfte, die von dem Federelement auf die Ankerstange ausgeübt werden, werden von der Ankerstange über das Übertragungsglied auf den Schließkörper geleitet, der hierdurch in die Schließposition zum Verschließen des Drosselkanals beaufschlagt wird. Closing forces, which are exerted by the spring element on the anchor rod are passed from the anchor rod via the transmission member to the closing body, which is thereby acted upon in the closed position for closing the throttle channel.
Gemäß einer vorteilhaften Ausführung ist das Übertragungsglied als ein separat von der According to an advantageous embodiment, the transmission member is as a separate from the
Ankerstange ausgeführtes Bauteil ausgebildet, das an die Stirnseite der Ankerstange angrenzt. Es besteht vorteilhafterweise keine feste Verbindung zwischen der Ankerstange und dem Anchor rod executed component formed adjacent to the front side of the anchor rod. There is advantageously no firm connection between the anchor rod and the
Übertragungsglied. Das Übertragungsglied wird von der Stirnseite der Ankerstange in Richtung der Schließposition des Schließkörpers beaufschlagt. Beim Anheben der Ankerstange und dem Öffnen des Drosselkanals wird das Übertragungsglied vom Druck der Steuerleckage, die in den Übergangsraum einströmt, in die die Führungsbohrung verschließende Position verstellt, so dass die Steuerleckage daran gehindert ist, in die Führungsbohrung einzuströmen. Die Ableitung der Steuerleckage aus dem Übergangsraum erfolgt über den Ableitungskanal in Richtung der Niederdruckseite des Kraftstoffes. Transmission member. The transmission member is acted upon by the end face of the anchor rod in the direction of the closing position of the closing body. When lifting the armature rod and the opening of the throttle channel, the transmission member is adjusted by the pressure of the control leakage, which flows into the transition space in the guide bore closing position, so that the control leakage is prevented from flowing into the guide bore. The derivation of the tax leakage from the transition space via the discharge channel in the direction of the low pressure side of the fuel.
In einer alternativen Ausführung ist das Übertragungsglied entweder einteilig mit der In an alternative embodiment, the transmission member is either integral with the
Ankerstange ausgebildet oder separat von der Ankerstange ausgebildet, jedoch fest mit der Ankerstange verbunden. In dieser Ausführung wird das Übertragungsglied bei nicht-aktuiertem Pilotventil durch das Federelement in gleicher Weise wie die Ankerstange in Richtung der Schließposition des Schließkörpers verstellt. Mit dem Aktuieren des Pilotventils wird die Ankerstange gegen die Kraft des Federelementes angehoben, ebenso das Übertragungsglied, das einteilig mit der Ankerstange ausgeführt oder fest mit der Ankerstange verbunden ist. Zusätzlich wirkt der Druck der Steuerleckage, die in den Übertragungsraum einströmt, auf das Anchor rod formed or formed separately from the anchor rod, but firmly with the Anchor rod connected. In this embodiment, the transmission member is adjusted at nichtaktuiertem pilot valve by the spring element in the same manner as the anchor rod in the direction of the closed position of the closing body. With the actuation of the pilot valve, the anchor rod is lifted against the force of the spring element, as well as the transmission member, which is integral with the anchor rod or firmly connected to the anchor rod. In addition, the pressure of the control leakage, which flows into the transfer space, acts on the
Übertragungsglied und beaufschlagt dieses in Richtung des Verschließens der Führungsbohrung. Transmission member and acts on this in the direction of closing the guide bore.
Gemäß einer vorteilhaften Ausführung liegt das Übertragungsglied bei geöffnetem Drosselkanal auf der Mündungsöffnung der Führungsbohrung in den Übergangsraum auf. Vorteilhafterweise besitzt der Übergangsraum in Radialrichtung - radial zur Längsachse des Kraftstoff- Einspritzinjektors - eine größere Erstreckung als die Führungsbohrung, so dass die According to an advantageous embodiment, the transfer member is open throttle channel on the mouth opening of the guide bore in the transitional space. Advantageously, the transition space in the radial direction - radially to the longitudinal axis of the fuel injection injector - has a greater extent than the guide bore, so that the
Mündungsöffnung der Führungsbohrung von einem Rand begrenzt ist, der Teil der Innenwand des Übergangsraums ist. Mouth opening of the guide bore is bounded by an edge which is part of the inner wall of the transitional space.
Gemäß einer weiteren vorteilhaften Ausführung weist das Übertragungsglied einen According to a further advantageous embodiment, the transmission member has a
Auflagekragen auf, der in der Schließposition des Übertragungsglieds auf dem die Support collar, which in the closed position of the transfer member on the
Mündungsöffnung der Führungsbohrung begrenzenden Rand aufliegt. Diese Ausführung lässt sich in konstruktiver Weise einfach realisieren und erlaubt es, bei angehobener Ankerstange des Pilotventils die Mündungsöffnung der Führungsbohrung durch das Übertragungsglied zu verschließen, so dass sich keine Steuerleckage axial in die Führungsbohrung ausbreiten kann. Mouth opening of the guide hole limiting edge rests. This design can be easily realized in a constructive manner and makes it possible to close the mouth opening of the guide bore through the transmission member when the anchor rod of the pilot valve is raised, so that no control leakage can propagate axially into the guide bore.
Gemäß einer weiteren vorteilhaften Ausführung besitzt der Auflagekragen einen According to a further advantageous embodiment, the support collar has a
Außendurchmesser, der den Innendurchmesser der Führungsbohrung um mindestens 20 % übersteigt. Mit diesem Größenverhältnis ist sichergestellt, dass das Übertragungsglied bei angehobener Ankerstange die Führungsbohrung sicher verschließt. Outer diameter exceeding the inner diameter of the pilot hole by at least 20%. With this size ratio, it is ensured that the transmission member securely closes the guide bore when the anchor rod is raised.
Gemäß einer weiteren zweckmäßigen Ausführung ist der die Mündungsöffnung der According to a further advantageous embodiment of the mouth opening of the
Führungsbohrung begrenzende Rand als eine erhöhte Ringwulst ausgebildet, auf der der Guide bore limiting edge formed as an elevated annular bead on which the
Auflagekragen des Übertragungsglieds zum Verschließen der Führungsbohrung aufliegt. Der Außendurchmesser der Ringwulst kann beispielsweise zumindest annähernd dem Support collar of the transfer member for closing the guide bore rests. The outer diameter of the annular bead, for example, at least approximately
Außendurchmesser des Auflagekragens entsprechen. Gemäß noch einer weiteren vorteilhaften Ausführung ist der Außendurchmesser des Auflagekragens mindestens um 30 % größer als der Außendurchmesser des Übertragungsglieds auf der der Steuerraumbuchse zugewandten Seite. Dieser Größenunterschied im Outer diameter of the support collar correspond. According to yet another advantageous embodiment, the outer diameter of the support collar is at least 30% larger than the outer diameter of the transmission member on the control chamber bushing facing side. This difference in size in the
Außendurchmesser stellt sicher, dass das Übertragungsglied eine ausreichend große Outer diameter ensures that the transfer member is a sufficiently large
Angriffsfläche für die Steuerleckage bietet, so dass die in den Übergangsraum eintretende Steuerleckage das Übertragungsglied effektiv mit Druck in Richtung des Schließens der Führungsbohrung beaufschlagt. The control leakage surface provides so that the control leakage entering the transitional space effectively pressurizes the transmission member in the direction of closing the guide bore.
Gemäß noch einer weiteren zweckmäßigen Ausführung weist das Übertragungsglied auf der der Ankerstange zugewandten Seite einen Zapfen auf, der vorzugsweise in allen Stellungen der Ankerstange in die Führungsbohrung hineinragt. Über den Zapfen in der Führungsbohrung ist das Übertragungsglied sicher und präzise in Achsrichtung zwischen der Schließposition zum Verschließen der Führungsbohrung und der Öffnungsposition geführt. Die axiale Länge des Zapfens beträgt beispielsweise mindestens 30 % der axialen Gesamtlänge des According to yet another expedient embodiment, the transmission member on the side facing the anchor rod on a pin, which preferably projects into the guide bore in all positions of the anchor rod. About the pin in the guide bore, the transmission member is safely and precisely out in the axial direction between the closed position for closing the guide bore and the open position. The axial length of the pin is for example at least 30% of the total axial length of
Übertragungsgliedes, um die gewünschte sichere Führung zu gewährleisten. Transfer link to ensure the desired secure guidance.
Der Zapfen des Übertragungsglieds kann gegebenenfalls einen zumindest geringfügig größeren Durchmesser aufweisen als der der Steuerraumbuchse zugewandte Abschnitt des The pin of the transmission member may optionally have an at least slightly larger diameter than the control chamber bushing facing portion of the
Übertragungsglieds. Transmitting member.
Weitere Vorteile und zweckmäßige Ausführungen sind den weiteren Ansprüchen, der Further advantages and expedient embodiments are the further claims, the
Figurenbeschreibung und den Zeichnungen zu entnehmen. Es zeigen: Figures description and the drawings can be seen. Show it:
Fig. 1 einen Längsschnitt durch einen Kraftstoff-Einspritzinjektor für eine Brennkraftmaschine im Bereich eines Pilotventils, das über ein Übertragungsglied einen Schließkörper in eine1 shows a longitudinal section through a fuel injection injector for an internal combustion engine in the region of a pilot valve, via a transmission member a closing body in a
Schließposition beaufschlagt, in der ein Drosselkanal in einer Steuerraumbuchse verschlossen ist, Acted upon closing position in which a throttle channel is closed in a control chamber socket,
Fig. 2 eine vergrößerte Darstellung aus dem Bereich des Übertragungsglieds. Fig. 2 is an enlarged view of the region of the transmission member.
In den Figuren sind gleiche Bauteile mit gleichen Bezugszeichen versehen. In the figures, the same components are provided with the same reference numerals.
Wie Fig. 1 in Verbindung mit Fig. 2 zu entnehmen, weist der Kraftstoff-Einspritzinjektor 1 in einem Pilotventilgehäuse 2 ein Pilotventil 3 auf, das einen Anker 4 und eine fest mit dem Anker 4 verbundene Ankerstange 5 umfasst, welche in einer Führungsbohrung 6 im Pilotventilgehäuse 2 axial verschieblich - bezogen auf die Längsachse 8 des Kraftstoff-Einspritzinjektors 1 - gelagert ist. Das Pilotventil 3 ist elektromagnetisch aktuierbar ausgebildet, wobei im Falle einer Aktuierung der Anker 4 mit der fest verbundenen Ankerstange 5 gegen die Kraft eines As can be seen from FIG. 1 in conjunction with FIG. 2, the fuel injection injector 1 in a pilot valve housing 2 has a pilot valve 3, which has an armature 4 and a fixed armature 4 connected anchor rod 5 which is axially displaceable in a guide bore 6 in the pilot valve housing 2 - relative to the longitudinal axis 8 of the fuel injection injector 1 - is stored. The pilot valve 3 is formed electromagnetically aktuierbar, wherein in the case of actuation of the armature 4 with the firmly connected anchor rod 5 against the force of a
Federelementes 7, die eine Pilotventilfeder bildet, nach oben gezogen wird. Die Aktuierung wird mittels eines elektromagnetischen Aktors durchgeführt, der in das Pilotventilgehäuse 2 des Kraftstoff-Einspritzinjektors 1 integriert ist und bei dessen Bestromung der Anker 4 des Spring element 7, which forms a pilot valve spring, is pulled upwards. The actuation is carried out by means of an electromagnetic actuator, which is integrated in the pilot valve housing 2 of the fuel injection injector 1 and during its energization of the armature 4 of the
Pilotventils 3 angehoben wird. Im nicht-aktuierten Zustand werden Anker 4 und Ankerstange 5 durch die Kraft des Federelementes 7 nach unten in Richtung einer Schließposition gedrückt, in der ein Drosselkanal 10 in einer Steuerraumbuchse 9 strömungsdicht verschlossen ist. Hierbei beaufschlagt die Ankerstange 5 ein Übertragungsglied 12, das sich an der Stirnseite der Pilot valve 3 is raised. In the non-actuated state armature 4 and anchor rod 5 are pressed by the force of the spring element 7 down in the direction of a closed position in which a throttle channel 10 is closed flow-tight in a control chamber socket 9. Here, the anchor rod 5 acts on a transmission member 12, which is located on the front side of the
Ankerstange 5 befindet, gegen einen Schließkörper 11 in Form einer Schließkugel, die in einer Vertiefung an der zugewandten Stirnseite der Steuerraumbuchse 9 im Bereich der Anchor rod 5 is against a closing body 11 in the form of a closing ball, which in a recess on the facing end face of the control chamber 9 in the area of
Mündungsöffnung des Drosselkanals 10 sitzt. Der Drosselkanal 10 in der Steuerraumbuchse 9 ist somit bei nicht-aktuiertem Pilotventil 3 von dem Schließkörper 11 strömungsdicht verschlossen. Bei aktuiertem Pilotventil 3 befindet sich dagegen die Ankerstange 5 in der angehobenen Öffnungsposition. Mouth opening of the throttle channel 10 is seated. The throttle channel 10 in the control chamber 9 is thus closed flow-tight with non-actuated pilot valve 3 of the closing body 11. When actuated pilot valve 3, however, the anchor rod 5 is in the raised open position.
Die Steuerraumbuchse 9 liegt in einem Hochdruckraum 13, der in einem Düsenkörper 14 gebildet ist, welcher sich an das Pilotventilgehäuse 2 anschließt. Das Pilotventilgehäuse 2 und der Düsenkörper 14 sind über eine Spannmutter 15 miteinander verbunden. Der Kraftstoff strömt über eine Hochdruckversorgungsleitung 16 in den Hochdruckraum 13 und gelangt von diesem in einen Steuerraum innerhalb der Steuerraumbuchse 9, wobei der Steuerraum mit dem The control chamber 9 is located in a high-pressure chamber 13 which is formed in a nozzle body 14, which adjoins the pilot valve housing 2. The pilot valve housing 2 and the nozzle body 14 are connected to each other via a clamping nut 15. The fuel flows via a high pressure supply line 16 into the high pressure chamber 13 and passes from this into a control chamber within the control chamber 9, wherein the control chamber with the
Drosselkanal 10 kommuniziert und über den Drosselkanal 10 mit einem Übergangsraum 17 verbunden ist, der sich axial an die Führungsbohrung 6 anschließt und sich an der dem Throttle channel 10 communicates and is connected via the throttle channel 10 with a transitional space 17 which connects axially to the guide bore 6 and at the
Düsenkörper 14 zugewandten Randseite des Pilotventilgehäuses 2 befindet. Das Nozzle body 14 facing edge side of the pilot valve housing 2 is located. The
Übertragungsglied 12 ist größtenteils im Übergangsraum 17 angeordnet. Der Übergangsraum 17 ist mit einem Ableitungskanal zum Ableiten von Kraftstoff verbunden, der in den Transmission member 12 is for the most part arranged in the transitional space 17. The transitional space 17 is connected to a discharge channel for discharging fuel, which in the
Übergangsraum 17 einströmt. Über den Ableitungskanal erfolgt eine Ableitung des Kraftstoffes vom Übergangsraum 17 zur Niederdruckseite. Transition space 17 flows. About the discharge channel takes place a derivative of the fuel from the transitional space 17 to the low pressure side.
Mit dem Anheben der Ankerstange 5 bei Aktuierung des Pilotventils 3 gegen die Kraft des auf die Ankerstange 5 wirkenden Federelementes 7 gibt der Schließkörper 11 den Drosselkanal 10 frei, wodurch eine Strömungs Verbindung zwischen dem Steuerraum und dem Übergangsraum 17 geschaffen wird und Kraftstoff, der unter Hochdruck steht, aus dem Steuerraum in den With the lifting of the anchor rod 5 upon actuation of the pilot valve 3 against the force of the spring rod 7 acting on the anchor rod 5, the closing body 11 releases the throttle channel 10, whereby a flow connection between the control chamber and the transitional space 17th is created and fuel, which is under high pressure, from the control room in the
Übergangsraum 17 strömen kann. Daraufhin wird eine Düsennadel aus ihrem Dichtsitz angehoben und kann Kraftstoff über eine Einspritzdüse austreten. Das Übertragungsglied 12 weist auf der der Ankerstange 5 zugewandten Seite einen Zapfen 19 auf, der in die Führungsbohrung 6 hineinragt. Zwischen dem Zapfen 18 und dem Hauptkörper des Übertragungsglieds 12 befindet sich ein Auflagekragen 19, dessen Außendurchmesser größer ist als der Innendurchmesser der Führungsbohrung 6 und bei angehobener Ankerstange 5 die Mündungsöffnung der Führungsbohrung 6 in den Übergangsraum 17 verschließt. Der Transition space 17 can flow. Then a nozzle needle is lifted from its sealing seat and can leak fuel through an injection nozzle. The transmission member 12 has on the armature rod 5 side facing a pin 19 which projects into the guide bore 6. Between the pin 18 and the main body of the transmission member 12 is a support collar 19, the outer diameter is greater than the inner diameter of the guide bore 6 and 5 raised anchor rod 5 closes the mouth opening of the guide bore 6 in the transitional space 17. Of the
Hauptkörper 20 des Übertragungsglieds 12 liegt dem Zapfen 18 gegenüber und befindet sich innerhalb des Übergangsraums 17. An der Spitze des Hauptkörpers 20 weist das Main body 20 of the transmission member 12 is opposite to the pin 18 and is located within the transition space 17. At the top of the main body 20 has the
Übertragungsglied 12 auf der der Steuerraumbuchse 9 zugewandten Seite eine Aufnahme 21 zur Aufnahme des kugelförmigen Schließkörpers 11 auf. Der Zapfen 18 ragt in allen Positionen der Ankerstange 5 in die Führungsbohrung 6 hinein. Der Durchmesser des Zapfens 18 ist geringfügig größer als der Durchmesser des Hauptkörpers 20. Die axiale Länge des Zapfens 18 beträgt beispielsweise mindestens 30 % der axialen Transfer member 12 on the control chamber socket 9 side facing a receptacle 21 for receiving the spherical closing body 11. The pin 18 protrudes into the guide bore 6 in all positions of the anchor rod 5. The diameter of the pin 18 is slightly larger than the diameter of the main body 20. The axial length of the pin 18 is for example at least 30% of the axial
Gesamtlänge des Übertragungsgliedes, bezogen auf Zapfen 18, Auflagekragen 19 und Total length of the transfer member, based on pin 18, support collar 19 and
Hauptkörper 20, und beispielsweise mindestens 20 % der axialen Gesamtlänge unter Main body 20, and for example at least 20% of the total axial length below
Einbeziehung der Aufnahme 21. Die Aufnahme 21 kann entweder einteiliger Bestandteil des Übertragungsglieds 12 oder separat vom Übertragungsglied 12 ausgebildet, jedoch mit dem Übertragungsglied 12 verbunden sein. Inclusion of the receptacle 21. The receptacle 21 may either one-piece component of the transmission member 12 or formed separately from the transmission member 12, but be connected to the transmission member 12.
Der die Mündungsöffnung der Führungsbohrung 6 begrenzende Rand, der Teil der Innenwand des Übergangsraums 17 ist, ist als eine erhöhte Ringwulst 22 ausgebildet (Fig. 2). Auf dieser Ringwulst 22 liegt der Auflagekragen 19 des Übertragungsgliedes 12 bei angehobener The edge defining the mouth opening of the guide bore 6, which is part of the inner wall of the transitional space 17, is formed as a raised annular bead 22 (FIG. 2). On this annular bead 22 of the support collar 19 of the transfer member 12 is raised
Ankerstange 5 dichtend an und verhindert hierdurch einen Übertritt von Kraftstoff, der bei angehobener Ankerstange 5 und angehobenem Schließkörper 11 über den Drosselkanal 10 in den Übergangsraum 17 strömt, in die Führungsbohrung 6 hinein. Dieser Kraftstoff, der eine Steuerleckage bildet, kann sich somit bei angehobener Ankerstange 5 nicht vom Übergangsraum 17 axial in die Führungsbohrung 6 ausbreiten, so dass eine Belagsbildung an der Innenwand der Führungsbohrung 6 bzw. dem Außenmantel der Ankerstange 5 verhindert wird. Bei angehobener Ankerstange 5 wird das Übertragungsglied 12 durch den Druck des in den Übergangsraum 17 einströmenden Kraftstoffes aus der Dicht- bzw. Schließposition angehoben, so dass der Auflagekragen 19 dichtend gegen die Ringwulst 22 gedrückt wird. Die Anhebung Ankerstange 5 erfolgt durch Aktuierung des Pilotventils 3. Anchor rod 5 sealingly and thereby prevents a transfer of fuel, which flows with raised anchor rod 5 and raised closing body 11 via the throttle channel 10 in the transitional space 17, in the guide bore 6 into it. This fuel, which forms a control leak, can thus not spread axially from the transition space 17 into the guide bore 6 when the anchor rod 5 is raised, so that a deposit formation on the inner wall of the guide bore 6 or the outer jacket of the anchor rod 5 is prevented. When the anchor rod 5 is raised, the transmission member 12 is lifted by the pressure of the inflowing into the transitional space 17 fuel from the sealing or closing position, so that the Support collar 19 sealingly pressed against the annular bead 22. The lifting anchor rod 5 is carried out by actuation of the pilot valve. 3
Sobald die Aktuierung beendet ist, wird die Ankerstange 5 durch die Kraft des Federelementes 7 wieder nach unten gedrückt, woraufhin über die Ankerstange 5 und der Schließkörper 11 in seine Schließstellung gepresst werden, in der der Drosselkanal 10 strömungsdicht verschlossen ist. Once the actuation is completed, the anchor rod 5 is pressed by the force of the spring element 7 back down, whereupon the anchor rod 5 and the closing body 11 are pressed into its closed position, in which the throttle channel 10 is closed flow-tight.

Claims

PATENTANSPRÜCHE
1. Kraftstoff-Einspritzinjektor für eine Brennkraftmaschine, mit einem Pilotventil (3) zur1. Fuel injection injector for an internal combustion engine, with a pilot valve (3) for
Steuerung der Hubbewegung einer Düsennadel, wobei eine Ankerstange (5) des Pilotventils (3) in einer Führungsbohrung (6) in einem Pilotventilgehäuse (2) geführt ist, an die sich ein Controlling the lifting movement of a nozzle needle, wherein an anchor rod (5) of the pilot valve (3) in a guide bore (6) in a pilot valve housing (2) is guided, to which a
Übergangsraum (17) anschließt, der von einer Steuerraumbuchse (9) mit einem Drosselkanal (10) begrenzt ist, wobei die Ankerstange (5) einen verstellbaren Schließkörper (11) beaufschlagt, der in einer Schließposition den Drosselkanal (10) in der Steuerraumbuchse (9) verschließt, dadurch gekennzeichnet, dass in dem Übergangsraum (17) im Übertragungsweg zum Transitional space (17) connects, which is bounded by a control chamber bushing (9) with a throttle channel (10), wherein the anchor rod (5) acts on an adjustable closing body (11) in a closed position, the throttle channel (10) in the control chamber socket (9 ), characterized in that in the transition space (17) in the transmission path to
Schließkörper (11) ein axial verstellbares Übertragungsglied (12) angeordnet ist, das bei geöffnetem Steuerraumbuchsen-Drosselkanal (10) die Führungsbohrung (6) verschließt. Closing body (11) an axially adjustable transmission member (12) is arranged, which closes the guide bore (6) when the control chamber bushing throttle channel (10) is open.
2. Kraftstoff-Einspritzinjektor nach Anspruch 1, 2. Fuel injection injector according to claim 1,
dadurch gekennzeichnet, dass das Übertragungsglied (12) bei geöffnetem Steuerraumbuchsen- Drosselkanal auf der Mündungsöffnung der Führungsbohrung (6) in den Übergangsraum (17) aufliegt. characterized in that the transfer member (12) rests with open Steuerraumbuchsen- throttle channel on the mouth opening of the guide bore (6) in the transition space (17).
3. Kraftstoff-Einspritzinjektor nach Anspruch 2, 3. Fuel injection injector according to claim 2,
dadurch gekennzeichnet, dass das Übertragungsglied (12) einen Auflagekragen (19) aufweist, der in Schließposition des Übertragungsglieds (12) auf dem die Mündungsöffnung der characterized in that the transfer member (12) has a support collar (19) in the closed position of the transfer member (12) on which the mouth of the
Führungsbohrung (6) begrenzenden Rand aufliegt. Guide bore (6) limiting edge rests.
4. Kraftstoff-Einspritzinjektor nach Anspruch 3, 4. Fuel injection injector according to claim 3,
dadurch gekennzeichnet, dass der Außendurchmesser des Auflagekragens (19) mindestens um 20 % größer ist als der Innendurchmesser der Führungsbohrung (6). characterized in that the outer diameter of the support collar (19) is at least 20% larger than the inner diameter of the guide bore (6).
5. Kraftstoff-Einspritzinjektor nach Anspruch 3 oder 4, 5. Fuel injection injector according to claim 3 or 4,
dadurch gekennzeichnet, dass der Außendurchmesser des Auflagekragens (19) mindestens um 30 % größer ist als der Außendurchmesser des Übertragungsglieds (12) auf der der characterized in that the outer diameter of the support collar (19) is at least 30% greater than the outer diameter of the transfer member (12) on the
Steuerraumbuchse (9) zugewandten Seite. Control chamber socket (9) facing side.
6. Kraftstoff-Einspritzinjektor nach einem der Ansprüche 1 bis 5, 6. Fuel injection injector according to one of claims 1 to 5,
dadurch gekennzeichnet, dass das Übertragungsglied (12) einen in die Führungsbohrung (6) ganz oder teilweise hineinragenden Zapfen (18) aufweist. characterized in that the transmission member (12) in the guide bore (6) wholly or partially projecting pin (18).
7. Kraftstoff-Einspritzinjektor nach Anspruch 6, 7. Fuel injection injector according to claim 6,
dadurch gekennzeichnet, dass die axiale Länge des in die Führungsbohrung (6) hineinragenden Abschnitts des Zapfens (18) mindestens 30 % der axialen Gesamtlänge des Übertragungsglieds (12) beträgt. characterized in that the axial length of the into the guide bore (6) projecting portion of the pin (18) is at least 30% of the total axial length of the transfer member (12).
8. Kraftstoff-Einspritzinjektor nach einem der Ansprüche 1 bis 7, 8. Fuel injection injector according to one of claims 1 to 7,
dadurch gekennzeichnet, dass der die Mündungsöffnung der Führungsbohrung (6) characterized in that the mouth opening of the guide bore (6)
begrenzende Rand als erhöhte Ringwulst (22) ausgebildet ist. limiting edge is formed as a raised annular bead (22).
9. Kraftstoff-Einspritzinjektor nach einem der Ansprüche 1 bis 8, 9. Fuel injection injector according to one of claims 1 to 8,
dadurch gekennzeichnet, dass das Übertragungsglied (12) separat von der Ankerstange (5) ausgebildet ist und an die Stirnseite der Ankerstange (5) angrenzt. characterized in that the transmission member (12) is formed separately from the anchor rod (5) and adjacent to the end face of the anchor rod (5).
10. Kraftstoff-Einspritzinjektor nach einem der Ansprüche 1 bis 9, 10. Fuel injection injector according to one of claims 1 to 9,
dadurch gekennzeichnet, dass der Übergangsraum (17) mit einem Ableitungskanal zum Ableiten von Kraftstoff verbunden ist. characterized in that the transitional space (17) is connected to a discharge channel for draining fuel.
PCT/DE2018/100069 2017-02-01 2018-01-29 Fuel injector for an internal combustion engine WO2018141335A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017101999.5 2017-02-01
DE102017101999.5A DE102017101999A1 (en) 2017-02-01 2017-02-01 Fuel injection injector for an internal combustion engine

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002053904A1 (en) * 2001-01-05 2002-07-11 Robert Bosch Gmbh Injection valve
DE10139622A1 (en) * 2001-03-29 2002-10-02 Bosch Gmbh Robert Fuel injection valve has nozzle body with arrangement corresponding to holding tool for holding nozzle body in defined position with respect to holding body during assembly
DE10121340A1 (en) * 2001-05-02 2002-11-14 Bosch Gmbh Robert Common rail injector for internal combustion engine fuel injection system has casing and intermediate plate bounding control chamber implemented in one piece with inlet and outlet choke
DE10250720A1 (en) * 2002-10-31 2004-05-13 Robert Bosch Gmbh Injector
EP1870594A1 (en) * 2006-06-21 2007-12-26 Denso Corporation Fuel injection valve
DE102007056913A1 (en) * 2007-11-26 2009-05-28 Robert Bosch Gmbh Injector for fuel with ball valve
DE102011051903A1 (en) 2011-07-18 2012-10-31 L'orange Gmbh Fuel injector has axially segmented housing structure with high- and low-side power supply connections, where hub-adjustable nozzle needle is accommodated in axial bore which is connected to high pressure side supply terminal
EP3115592A2 (en) * 2015-07-08 2017-01-11 Robert Bosch Gmbh A control valve for fuel injector and a fuel injector

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002053904A1 (en) * 2001-01-05 2002-07-11 Robert Bosch Gmbh Injection valve
DE10139622A1 (en) * 2001-03-29 2002-10-02 Bosch Gmbh Robert Fuel injection valve has nozzle body with arrangement corresponding to holding tool for holding nozzle body in defined position with respect to holding body during assembly
DE10121340A1 (en) * 2001-05-02 2002-11-14 Bosch Gmbh Robert Common rail injector for internal combustion engine fuel injection system has casing and intermediate plate bounding control chamber implemented in one piece with inlet and outlet choke
DE10250720A1 (en) * 2002-10-31 2004-05-13 Robert Bosch Gmbh Injector
EP1870594A1 (en) * 2006-06-21 2007-12-26 Denso Corporation Fuel injection valve
DE102007056913A1 (en) * 2007-11-26 2009-05-28 Robert Bosch Gmbh Injector for fuel with ball valve
DE102011051903A1 (en) 2011-07-18 2012-10-31 L'orange Gmbh Fuel injector has axially segmented housing structure with high- and low-side power supply connections, where hub-adjustable nozzle needle is accommodated in axial bore which is connected to high pressure side supply terminal
EP3115592A2 (en) * 2015-07-08 2017-01-11 Robert Bosch Gmbh A control valve for fuel injector and a fuel injector

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