EP2496822B1 - Injection nozzle for a leakless fuel injector - Google Patents

Injection nozzle for a leakless fuel injector Download PDF

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Publication number
EP2496822B1
EP2496822B1 EP10763670.6A EP10763670A EP2496822B1 EP 2496822 B1 EP2496822 B1 EP 2496822B1 EP 10763670 A EP10763670 A EP 10763670A EP 2496822 B1 EP2496822 B1 EP 2496822B1
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EP
European Patent Office
Prior art keywords
valve needle
cutout
valve
recess
flow
Prior art date
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EP10763670.6A
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German (de)
French (fr)
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EP2496822A1 (en
Inventor
Katja Grothe
Wilhelm Christ
Klaus-Peter Gansert
Thilo Kreher
Frank Ulrich Rueckert
Gerhard Suenderhauf
Fridolin Zeck
Marcus Schilling
Kerstin Kling
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Robert Bosch GmbH
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Robert Bosch GmbH
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Publication of EP2496822A1 publication Critical patent/EP2496822A1/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
    • 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
    • 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
    • F02M61/12Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/168Assembling; Disassembling; Manufacturing; Adjusting

Definitions

  • the invention relates to a method for producing a valve needle of a fuel injector according to the preamble of claim 1.
  • Such a fuel injector is from the DE 10 2007 032 741 A1 known.
  • the fuel injector described in this document is leak-free designed for high injection pressures by dispensing with a low-pressure stage.
  • only small forces are available for closing the valve needle, which reduces the ability to inject small quantities of fuel.
  • This disadvantage is difficult to compensate, for example, by the use of correspondingly fast switching control valves, which is expensive and expensive. Therefore, in the subject of this document, a permanent and constant closing force is generated on the valve needle by a sharp-edged gap choke is formed between the valve needle and the valve body in the pressure chamber.
  • the gap choke is formed by a separately incorporated into the valve needle collar having a sharp edge at its outer edge, so that between the edge of the collar and the valve body the sharp-edged circumferential and thus an annular gap forming gap choke is formed.
  • the federal government may also have lateral poles.
  • a relief bore in the form of a closing throttle may also be provided, such a bore being incorporated in a separate component in the form of a throttle plate.
  • a throttle plate is due to the separate component an increased construction cost.
  • the invention is based on the object to provide a fuel injector in which one of the closing operation of the valve needle is optimized by an improved over the prior art closing throttle.
  • the recess has a longitudinal extent, which has at least the simple maximum recess depth based on the number of all recesses.
  • the longitudinal extension of the recess has twice the maximum recess depth based on the number of all recesses.
  • the longitudinal extent refers to the axial length of the recess along the valve needle, while the recess depth refers to the (changing) distance of the recess to the valve body.
  • the at least one recess is circular arc-shaped. This embodiment offers advantages in the case of recess grinding.
  • an upper bevel, the recess and the flow recess in the flow direction of the fuel are arranged in alignment with each other in the valve needle guide region.
  • turbulence in the flow of the fuel can be avoided.
  • an annular gap can connect to the recess or else the flow recess directly follows the recess in the collar.
  • the rotationally symmetrical intermediate region is basically without a hydraulic or mechanical function, but possibly offers advantages in the machining of the nozzle needle.
  • This advantage can be achieved in a further embodiment of the invention without the rotationally symmetrical intermediate region when a transition region is arranged between the recess and the flow gap recess, wherein the transition region has the same contour as the recess.
  • This is advantageously achieved in that the recess and a gap area in front of the recess and the Strömungsspaltaus supraung are made in a grinding operation. In this case, then, the transition region can be made in a second grinding cycle by a simple reaction of the grinding tool.
  • a particular advantage is that the valve needle does not have to be re-clamped for this second sanding cycle.
  • valve needles 1 and valve body 2 of a fuel injector shown in detail in the figures are designed in particular for use in self-igniting internal combustion engines with a common rail injection system.
  • the fuel injector is suitable for precisely controlling even small fuel injection quantities which have to be metered as part of a pilot injection in order to achieve low emission values.
  • the various embodiments all relate to a closing throttle, which is intended to ensure a stable closing of the valve needle 1 in fuel injectors without pressure stage. Through the closing throttle, a higher hydraulic pressure is built up than the closing throttle during the closing process of the valve needle 1 above the closing throttle, which supports and accelerates the closing process.
  • Fig.1 shows a valve needle 1, which is guided in a valve body 2 longitudinally displaceable.
  • the valve body 2 has one with a valve needle tip 3 ( FIG. 2 ) cooperating with the needle seat, which cooperates with at least one injection opening, can be introduced through the fuel in a combustion chamber of an associated cylinder-piston unit of the internal combustion engine.
  • the fuel taken from the rail of the common-rail injection system under high pressure (up to 3,000 bar) is supplied to the at least one injection opening controlled by a pressure space in the form of a gap formation between the nozzle needle 1 and the valve body 2.
  • the control normally takes an unillustrated and acting on a valve ball actuator module, wherein the valve ball with a in a Holding body of the actuator module incorporated valve seat cooperates.
  • the valve seat is connected via a connecting line to a control chamber, which in turn is flow-connected to the rail via an inlet throttle.
  • the control chamber is arranged opposite to the valve needle tip 3 at the end of the valve needle 1 in the valve body 2 cooperating with the holding body.
  • the valve ball lifts from the valve seat and acting on the control room side end face of the valve needle 1 hydraulic pressure in the control chamber is lowered by discharge of fuel through the connecting line and further via a subsequent to the valve seat discharge line in the holding body.
  • valve needle 1 In this switching state, the valve needle 1 is moved from the approximately approaching under rail pressure at a pressure shoulder 14 of the valve needle 1 fuel against the force of a valve needle spring 4 in the direction of the holding body and the valve needle tip 3 lifts from the needle seat. The fuel is then injected into the combustion chamber, the at least one injection port. If the actuator module is moved into its second switching position, the valve ball is moved onto the valve seat and fuel flowing into the control chamber through the inlet throttle from the rail increases the hydraulic pressure in the control chamber. The valve needle tip 3 is pressed back onto the needle seat. The injection process is thus terminated.
  • annular gap 5 is formed in an upper valve needle side region as part of the gap formation or the pressure chamber, in which - as stated - the standing under rail pressure fuel flows.
  • the valve body 2 is formed so that it forms a guide 6, in which the valve needle 1 with an upper valve needle guide portion 11 is guided exactly.
  • an upper bevel 7 is incorporated in the valve needle 1 and the upper valve needle guide portion 11, which extends to a circumferential sealing collar 8 of the valve needle 1.
  • the collar 8 is part of the upper (or below explained below) Ventilnadet Adjusts Schemes 11 and acts at all positions that can take the longitudinally displaceable valve needle 1, always together with the guide 6, while the upper section 7 always protrudes into the annular gap 5.
  • a segment-shaped recess 9 is ground in extension to the upper section 7.
  • upper sections 7 and recessed in the collar 8 recesses 9 may be arranged distributed.
  • a rotationally symmetrical region 10 incorporated in the valve needle 11 follows in the form of a recess.
  • At this rotationally symmetrical region 10 includes another cooperating with the guide 6 lower valve needle guide portion 11, in which at least one flow recess 12 is incorporated.
  • the flow recess 12 is designed such that the fuel passes along the flow recess 12 without throttling losses in an annular space 13, which in turn is connected to the needle seat.
  • the annular space 13 is created by a production of the valve needle 1 with a relation to the valve needle guide portion 11 of reduced diameter. As a result, the pressure shoulder 14 is formed.
  • FIG. 2 shows the according to FIG. 1 designed nozzle needle 1 in a perspective view, the control room end, however, is not shown.
  • FIG. 3 shows a variant of the valve needle 1, wherein the recess 9a is aligned at an angle to the longitudinal axis of the valve needle 1 in the valve guide portion 11.
  • the recess 9a extends up to the rotationally symmetrical region 10 and can be configured such that the recess 9a itself forms the closing throttle.
  • the closing throttle may be formed by a throttle point 17 in the collar 8a of the recess 9a.
  • the particular advantage of this transition region 15 is that this as in the FIGS. 9 and 10 shown, easily in two consecutive grinding operations, without re-tightening the valve needle 1 can be made.
  • a grinding tool 16 has in the FIGS. 9 and 10 shown contour on and in a first grinding cycle according to FIG. 9 the upper bevel 7 is ground above or in the drawing to the left of the recess 9, the recess 9 itself and the flow recess 12 in the valve needle guide region 11 into the valve needle 1.
  • the upper section 7 is ground deeper than the flow recess 12 in the valve needle 1.
  • the transition region 15 is shown in a raw state. However, it is also provided within the scope of the invention to loop the transition region 15 completely into the valve needle 1 during the second grinding cycle.

Description

Technisches GebietTechnical area

Die Erfindung betrifft ein Verfahren zur Herstellung einer Ventilnadel eines Kraftstoffinjektor nach dem Oberbegriff des Anspruchs 1.The invention relates to a method for producing a valve needle of a fuel injector according to the preamble of claim 1.

Stand der TechnikState of the art

Ein derartiger Kraftstoffinjektor ist aus der DE 10 2007 032 741 A1 bekannt. Der in diesem Dokument beschriebene Kraftstoffinjektor ist leckagefrei für hohe Einspritzdrücke ausgeführt, indem auf eine Niederdruckstufe verzichtet wird. Damit stehen für das Schließen der Ventilnadel jedoch nur geringe Kräfte zur Verfügung, was die Fähigkeit zur Einspritzung kleiner Kraftstoffmengen vermindert. Dieser Nachteil lässt sich nur schwer kompensieren, beispielsweise durch die Verwendung von entsprechend schnell schaltenden Steuerventilen, was jedoch teuer und aufwendig ist. Daher wird beim Gegenstand dieses Dokuments eine permanente und konstante Schließkraft auf die Ventilnadel erzeugt, indem zwischen der Ventilnadel und dem Ventikörper in dem Druckraum eine scharfkantige Spaltdrossel ausgebildet ist. Die Spaltdrossel ist durch einen separat in die Ventilnadel eingearbeiteten Bund ausgebildet, der an seinem äußeren Rand eine scharfe Kante aufweist, so dass zwischen der Kante des Bundes und dem Ventilkörper die scharfkantige umlaufende und somit einen Ringspalt bildende Spaltdrossel gebildet ist. Zusätzlich kann der Bund darüber hinaus seitliche Anschliffe aufweisen.Such a fuel injector is from the DE 10 2007 032 741 A1 known. The fuel injector described in this document is leak-free designed for high injection pressures by dispensing with a low-pressure stage. However, only small forces are available for closing the valve needle, which reduces the ability to inject small quantities of fuel. This disadvantage is difficult to compensate, for example, by the use of correspondingly fast switching control valves, which is expensive and expensive. Therefore, in the subject of this document, a permanent and constant closing force is generated on the valve needle by a sharp-edged gap choke is formed between the valve needle and the valve body in the pressure chamber. The gap choke is formed by a separately incorporated into the valve needle collar having a sharp edge at its outer edge, so that between the edge of the collar and the valve body the sharp-edged circumferential and thus an annular gap forming gap choke is formed. In addition, the federal government may also have lateral poles.

Alternativ zu der zuvor beschriebenen Ausgestaltung kann auch eine Entlastungsbohrung in Form einer Schließdrossel vorgesehen werden, wobei eine solche Bohrung in einem separaten Bauteil in Form einer Drosselplatte eingearbeitet wird. Eine solche Drosselplatte stellt aufgrund des separaten Bauteils einen erhöhten Bauaufwand dar.As an alternative to the embodiment described above, a relief bore in the form of a closing throttle may also be provided, such a bore being incorporated in a separate component in the form of a throttle plate. Such a throttle plate is due to the separate component an increased construction cost.

Ein weiterer Kraftstoffinjektor mit einem an einem Ringbund der Ventilnadel gebildeten Drosselkanal ist aus WO 02/48536 A bekannt.Another fuel injector with a throttle channel formed on a collar of the valve needle is off WO 02/48536 A known.

Der Erfindung liegt die Aufgabe zu Grunde, einen Kraftstoffinjektor bereitzustellen, bei dem ein der Schließvorgang der Ventilnadel durch eine gegenüber dem Stand der Technik verbesserte Schließdrossel optimiert ist.The invention is based on the object to provide a fuel injector in which one of the closing operation of the valve needle is optimized by an improved over the prior art closing throttle.

Offenbarung der ErfindungDisclosure of the invention

Diese Aufgabe wird durch das beanspruchte Herstellungsverfahren gelöst. Dadurch ist zunächst einmal die Herstellung vereinfacht, da die Schließdrossel nicht mehr in einen separat zu erzeugenden Bund einzuarbeiten ist. Der Kragen ist als Bestandteil des Ventilführungsbereichs dichtend in dem Ventilkörper geführt und nur durch die Aussparung strömt eine genau definierte Kraftstoffmenge. Die Strömungsmenge und damit das Schließverhalten ist durch diese Ausgestaltung gegenüber dem Stand der Technik verbessert beziehungsweise präzisiert.This object is achieved by the claimed manufacturing method. As a result, first of all the production is simplified, since the closing throttle is no longer incorporated into a separately produced federal government. The collar is guided as a part of the valve guide portion sealing in the valve body and only through the recess flows a well-defined amount of fuel. The flow rate and thus the closing behavior is improved or specified by this embodiment over the prior art.

Vorteile der ErfindungAdvantages of the invention

In Weiterbildung der Erfindung weist die Aussparung eine Längserstreckung auf, die zumindest der einfachen maximalen Aussparungstiefe bezogen auf die Anzahl aller Aussparungen aufweist. In einer besonders vorteilhaften Ausgestaltung weist die Längserstreckung der Aussparung die zweifache maximale Aussparungstiefe bezogen auf die Anzahl aller Aussparungen aus. Die Längserstreckung bezeichnet die axiale Länge der Aussparung entlang der Ventilnadel, während die Aussparungstiefe den (sich ändernden) Abstand der Aussparung zu dem Ventilkörper bezeichnet. Diese geometrische Ausgestaltung definiert den Druckabfall des Kraftstoffs entlang der Schließdrossel und beeinflusst somit das Schließverhalten der Ventilnadel. Dabei hat es sich als vorteilhafte erwiesen, insgesamt drei Aussparungen auf dem Umfang der Ventilnadel verteilt anzuordnen.In development of the invention, the recess has a longitudinal extent, which has at least the simple maximum recess depth based on the number of all recesses. In a particularly advantageous embodiment, the longitudinal extension of the recess has twice the maximum recess depth based on the number of all recesses. The longitudinal extent refers to the axial length of the recess along the valve needle, while the recess depth refers to the (changing) distance of the recess to the valve body. These geometric design defines the pressure drop of the fuel along the closing throttle and thus influences the closing behavior of the valve needle. It has proven to be advantageous to arrange a total of three recesses distributed on the circumference of the valve needle.

In Weiterbildung der Erfindung ist die zumindest eine Aussparung kreisbogenförmig ausgebildet. Diese Ausgestaltung bietet beim Einstichschleifen Vorteile.In a further development of the invention, the at least one recess is circular arc-shaped. This embodiment offers advantages in the case of recess grinding.

Nach der Erfindung sind ein oberer Anschliff, die Aussparung und die Strömungsaussparung in Strömungsrichtung des Kraftstoffs fluchtend zueinander in den Ventilnadelführungsbereich angeordnet. Durch diese Ausgestaltung werden Verwirbelungen im Strömungsverlauf des Kraftstoffs vermieden. Dabei kann an die Aussparung ein Ringspalt anschließen oder aber die Strömungsaussparung folgt unmittelbar an die Aussparung in dem Kragen an. Der rotationssymmetrische Zwischenbereich ist im Grunde ohne eine hydraulische oder mechanische Funktion, bietet aber ggf. Vorteile bei der Bearbeitung der Düsennadel.According to the invention, an upper bevel, the recess and the flow recess in the flow direction of the fuel are arranged in alignment with each other in the valve needle guide region. By this configuration, turbulence in the flow of the fuel can be avoided. In this case, an annular gap can connect to the recess or else the flow recess directly follows the recess in the collar. The rotationally symmetrical intermediate region is basically without a hydraulic or mechanical function, but possibly offers advantages in the machining of the nozzle needle.

Dieser Vorteil kann in weiterer Ausgestaltung der Erfindung auch ohne den rotationssymmetrischen Zwischenbereich erzielt werden, wenn zwischen der Aussparung und der Strömungsspaltausnehmung ein Übergangsbereich angeordnet ist, wobei der Übergangsbereich die gleiche Kontur wie die Aussparung aufweist. Dies wird vorteilhaft dadurch erreicht, dass die Aussparung und ein Spaltbereich vor der Aussparung sowie die Strömungsspaltausnehmung in einem Schleifvorgang gefertigt werden. Dabei kann dann der Übergangsbereich in einen zweiten Schleifgang durch ein einfaches Umsetzen des Schleifwerkzeugs gefertigt werden. Ein besonderer Vorteil ist es, dass für diesen zweiten Schleifgang die Ventilnadel nicht umgespannt werden muss.This advantage can be achieved in a further embodiment of the invention without the rotationally symmetrical intermediate region when a transition region is arranged between the recess and the flow gap recess, wherein the transition region has the same contour as the recess. This is advantageously achieved in that the recess and a gap area in front of the recess and the Strömungsspaltausnehmung are made in a grinding operation. In this case, then, the transition region can be made in a second grinding cycle by a simple reaction of the grinding tool. A particular advantage is that the valve needle does not have to be re-clamped for this second sanding cycle.

Es zeigen:

Fig.1
eine Schnittdarstellung einer in einem Ventilkörper längs verschiebbar angeordneten Ventilnadel mit einer segmentförmigen Aussparung an einem umlaufenden dichtenden Kragen,
Fig.2
eine Ansicht der Ventilnadel gemäß Fig.1,
Fig.3
eine Detailansicht einer Ventilnadel, bei der die segmentförmige Aussparung in einem Winkel zur Längsachse der Ventilnadel angeordnet ist,
Fig.4
eine Detailansicht einer Ventilnadel, bei der die segmentförmige Aussparung in einen Flächenanschliff integriert ist,
Fig.5
eine Ansicht einer Ventilnadel mit einer Aussparung in dem Kragen, die fluchtend zu einer dem Kragen unter Einschluss eines rotationssymetrischen Bereichs nachfolgenden Strömungsaussparung in der Nadelführung der Ventilnadel angeordnet ist,
Fig.6
eine Schnittdarstellung durch die Ventilnadel und den Ventilkörper gemäß Fig.5,
Fig.7
eine Detailansicht einer Ventilnadel mit einer Aussparung in dem Kragen, die fluchtend zu einer nachfolgenden Strömungsaussparung in der Nadelführung der Ventilnadel angeordnet ist,
Fig.8
eine Schnittdarstellung durch die Ventilnadel und den Ventilkörper gemäß Fig.5,
Fig.9
Position eines Schleifwerkzeugs bei einem ersten Schleifschritt zur Herstellung einer Ventilnadel gemäß Fig.7 und
Fig.10
Position eines Schleifwerkzeugs bei einem zweiten Schleifschritt zur Herstellung einer Ventilnadel gemäß Fig.7.
Show it:
Fig.1
a sectional view of a longitudinally displaceably arranged in a valve body valve needle with a segment-shaped recess on a circumferential sealing collar,
Fig.2
a view of the valve needle according to Fig.1 .
Figure 3
a detailed view of a valve needle, wherein the segment-shaped recess is arranged at an angle to the longitudinal axis of the valve needle,
Figure 4
a detailed view of a valve needle, in which the segment-shaped recess is integrated in a Flächenanschliff,
Figure 5
a view of a valve needle with a recess in the collar, which is arranged in alignment with a collar following the inclusion of a rotationally symmetric region flow recess in the needle guide of the valve needle,
Figure 6
a sectional view through the valve needle and the valve body according to Figure 5 .
Figure 7
a detailed view of a valve needle with a recess in the collar, which is arranged in alignment with a subsequent flow recess in the needle guide of the valve needle,
Figure 8
a sectional view through the valve needle and the valve body according to Figure 5 .
Figure 9
Position of a grinding tool in a first grinding step for producing a valve needle according to Figure 7 and
Figure 10
Position of a grinding tool in a second grinding step for producing a valve needle according to Figure 7 ,

Ausführungsform der ErfindungEmbodiment of the invention

Die in den Figuren ausschnittsweise dargestellten Ventilnadeln 1 und Ventilkörper 2 eines Kraftstoffinjektors sind insbesondere zur Verwendung bei selbstzündenden Brennkraftmaschinen mit einem Common-Rail-Einspritzsystem ausgestaltet. Dabei ist der Kraftstoffinjektor geeignet, auch kleine Kraftstoffeinspritzmengen, die im Rahmen einer Voreinspritzung zur Erreichung niedriger Emissionswerte dosiert werden müssen, präzise zu steuern. Die verschiedenen Ausgestaltungen betreffen alle eine Schließdrossel, die bei Kraftstoffinjektoren ohne Druckstufe ein stabiles Schließen der Ventilnadel 1 gewährleisten soll. Durch die Schließdrossel wird beim Schließvorgang der Ventilnadel 1 oberhalb der Schließdrossel ein höherer hydraulischer Druck als unterhalb der Schließdrossel aufgebaut, der den Schließvorgang unterstützt und beschleunigt.The valve needles 1 and valve body 2 of a fuel injector shown in detail in the figures are designed in particular for use in self-igniting internal combustion engines with a common rail injection system. In this case, the fuel injector is suitable for precisely controlling even small fuel injection quantities which have to be metered as part of a pilot injection in order to achieve low emission values. The various embodiments all relate to a closing throttle, which is intended to ensure a stable closing of the valve needle 1 in fuel injectors without pressure stage. Through the closing throttle, a higher hydraulic pressure is built up than the closing throttle during the closing process of the valve needle 1 above the closing throttle, which supports and accelerates the closing process.

Fig.1 zeigt eine Ventilnadel 1, die in einem Ventilkörper 2 längsverschiebbar geführt ist. Der Ventilkörper 2 weist eine mit einer Ventilnadelspitze 3 (Figur 2) zusammenwirkenden Nadelsitz auf, der mit zumindest einer Einspritzöffnung, durch den Kraftstoff in einem Brennraum einer zugehörigen Zylinder-Kolben-Einheit der Brennkraftmaschine eingebracht werden kann, zusammenwirkt. Der dem Rail des Common-Rail-Einspritzsystems unter hohem Druck (bis zu 3.000 bar) entnommene Kraftstoff wird der zumindest einen Einspritzöffnung durch einen Druckraum in Form einer Spaltausbildung zwischen der Düsennadel 1 und dem Ventilkörper 2 gesteuert zugeführt. Fig.1 shows a valve needle 1, which is guided in a valve body 2 longitudinally displaceable. The valve body 2 has one with a valve needle tip 3 ( FIG. 2 ) cooperating with the needle seat, which cooperates with at least one injection opening, can be introduced through the fuel in a combustion chamber of an associated cylinder-piston unit of the internal combustion engine. The fuel taken from the rail of the common-rail injection system under high pressure (up to 3,000 bar) is supplied to the at least one injection opening controlled by a pressure space in the form of a gap formation between the nozzle needle 1 and the valve body 2.

Die Steuerung übernimmt normalerweise ein nicht dargestelltes und auf eine Ventilkugel einwirkendes Aktormodul, wobei die Ventilkugel mit einem in einem Haltekörper des Aktormoduls eingearbeiteten Ventilsitz zusammenwirkt. Der Ventilsitz ist über eine Verbindungsleitung mit einem Steuerraum, der seinerseits über eine Zulaufdrossel mit dem Rail strömungsverbunden ist, verschaltet. Der Steuerraum ist gegenüberliegend zu der Ventilnadelspitze 3 endseitig der Ventilnadel 1 in dem Ventilkörper 2 zusammenwirkend mit dem Haltekörper angeordnet. In einer Schaltstellung des Aktormoduls hebt die Ventilkugel von dem Ventilsitz ab und der auf die steuerraumseitige Stirnfläche der Ventilnadel 1 wirkende hydraulische Druck in dem Steuerraum wird durch Abführung von Kraftstoff durch die Verbindungsleitung und weiter über eine an den Ventilsitz anschließende Abführleitung in dem Haltekörper abgesenkt. In diesem Schaltzustand wird die Ventilnadel 1 von dem weiterhin angenähert unter Raildruck an einer Druckschulter 14 der Ventilnadel 1 anstehenden Kraftstoff gegen die Kraft einer Ventilnadelfeder 4 in Richtung zu dem Haltekörper bewegt und die Ventilnadelspitze 3 hebt von dem Nadelsitz ab. Der Kraftstoff wird dann die zumindest eine Einspritzöffnung in den Brennraum eingespritzt. Wird das Aktormodul in seine zweite Schaltposition bewegt, wird die Ventilkugel auf den Ventilsitz bewegt und in den Steuerraum durch die Zulaufdrossel aus dem Rail einströmender Kraftstoff erhöht den hydraulischen Druck in dem Steuerraum. Die Ventilnadelspitze 3 wird wieder auf den Nadelsitz gedrückt. Der Einspritzvorgang wird somit beendet.The control normally takes an unillustrated and acting on a valve ball actuator module, wherein the valve ball with a in a Holding body of the actuator module incorporated valve seat cooperates. The valve seat is connected via a connecting line to a control chamber, which in turn is flow-connected to the rail via an inlet throttle. The control chamber is arranged opposite to the valve needle tip 3 at the end of the valve needle 1 in the valve body 2 cooperating with the holding body. In a switching position of the actuator module, the valve ball lifts from the valve seat and acting on the control room side end face of the valve needle 1 hydraulic pressure in the control chamber is lowered by discharge of fuel through the connecting line and further via a subsequent to the valve seat discharge line in the holding body. In this switching state, the valve needle 1 is moved from the approximately approaching under rail pressure at a pressure shoulder 14 of the valve needle 1 fuel against the force of a valve needle spring 4 in the direction of the holding body and the valve needle tip 3 lifts from the needle seat. The fuel is then injected into the combustion chamber, the at least one injection port. If the actuator module is moved into its second switching position, the valve ball is moved onto the valve seat and fuel flowing into the control chamber through the inlet throttle from the rail increases the hydraulic pressure in the control chamber. The valve needle tip 3 is pressed back onto the needle seat. The injection process is thus terminated.

Zwischen dem Ventilkörper 2 und der Ventilnadel 1 ist in einem oberen ventilnadelfederseitigen Bereich ein Ringspalt 5 als Teil der Spaltausbildung beziehungsweise des Druckraums gebildet, in den - wie ausgeführt - der unter Raildruck stehende Kraftstoff einströmt. Anschließend an den Ringspalt 5 ist der Ventilkörper 2 so ausgebildet, dass er eine Führung 6 bildet, in dem die Ventilnadel 1 mit einem oberen Ventilnadelführungsbereich 11 exakt geführt ist. In Höhe des Übergangsbereichs zwischen dem Ringspalt 5 und der Führung 6 ist in die Ventilnadel 1 beziehungsweise den oberen Ventilnadelführungsbereich 11 ein oberer Anschliff 7 eingearbeitet, der sich bis zu einem umlaufenden dichtenden Kragen 8 der Ventilnadel 1 erstreckt. Der Kragen 8 ist Bestandteil des oberen (oder des nachfolgend erläuterten unteren) Ventilnadetführungsbereichs 11. und wirkt bei allen Positionen, die die längsverschiebbare Ventilnadel 1 einnehmen kann, immer mit der Führung 6 zusammen, während der obere Anschliff 7 immer in den Ringsspalt 5 hineinragt. In den Kragen 8 ist in Verlängerung zu dem oberen Anschliff 7 eine segmentförmige Aussparung 9 eingeschliffen. Am Umfang der Ventilnadel 1 können mehrere, beispielsweise drei, obere Anschliffe 7 und in die Kragen 8 eingelassene Aussparungen 9 verteilt angeordnet sein. Anschließend an die zumindest eine Aussparung 9 folgt ein in die Ventilnadel 11 eingearbeiteter rotationsymmetrischer Bereich 10 in Form einer Ausnehmung. An diesen rotationssymmetrischen Bereich 10 schließt ein weiterer mit der Führung 6 zusammenwirkender unterer Ventilnadelführungsbereich 11 an, in den zumindest eine Strömungsaussparung 12 eingearbeitet ist. Die Strömungsaussparung 12 ist so ausgestaltet, dass der Kraftstoff entlang der Strömungsaussparung 12 ohne Drosselverluste in einen Ringraum 13 gelangt, der wiederum mit dem Nadelsitz verschaltet ist. Der Ringraum 13 ist durch eine Fertigung der Ventilnadel 1 mit einem gegenüber dem Ventilnadelführungsbereich 11 verringertem Durchmesser geschaffen. Dadurch wird die Druckschulter 14 gebildet.Between the valve body 2 and the valve needle 1, an annular gap 5 is formed in an upper valve needle side region as part of the gap formation or the pressure chamber, in which - as stated - the standing under rail pressure fuel flows. Subsequent to the annular gap 5, the valve body 2 is formed so that it forms a guide 6, in which the valve needle 1 with an upper valve needle guide portion 11 is guided exactly. At the level of the transition region between the annular gap 5 and the guide 6, an upper bevel 7 is incorporated in the valve needle 1 and the upper valve needle guide portion 11, which extends to a circumferential sealing collar 8 of the valve needle 1. The collar 8 is part of the upper (or below explained below) Ventilnadetführungsbereichs 11 and acts at all positions that can take the longitudinally displaceable valve needle 1, always together with the guide 6, while the upper section 7 always protrudes into the annular gap 5. In the collar 8 a segment-shaped recess 9 is ground in extension to the upper section 7. On the circumference of the valve needle 1 can more, for example three, upper sections 7 and recessed in the collar 8 recesses 9 may be arranged distributed. Subsequent to the at least one recess 9, a rotationally symmetrical region 10 incorporated in the valve needle 11 follows in the form of a recess. At this rotationally symmetrical region 10 includes another cooperating with the guide 6 lower valve needle guide portion 11, in which at least one flow recess 12 is incorporated. The flow recess 12 is designed such that the fuel passes along the flow recess 12 without throttling losses in an annular space 13, which in turn is connected to the needle seat. The annular space 13 is created by a production of the valve needle 1 with a relation to the valve needle guide portion 11 of reduced diameter. As a result, the pressure shoulder 14 is formed.

Figur 2 zeigt die gemäß Figur 1 ausgestaltete Düsennadel 1 in einer perspektivischen Ansicht, wobei das steuerraumseitige Ende allerdings nicht dargestellt ist. FIG. 2 shows the according to FIG. 1 designed nozzle needle 1 in a perspective view, the control room end, however, is not shown.

Figur 3 zeigt eine Variante der Ventilnadel 1, bei dem die Aussparung 9a unter einem Winkel zu der Längsachse der Ventilnadel 1 in dem Ventilführungsbereich 11 ausgerichtet ist. Die Aussparung 9a reicht bis zu dem rotationssymmetrischen Bereich 10 und kann so ausgestaltet sein, dass die Aussparung 9a selber die Schließdrossel bildet. Alternativ kann wie in Figur 3 dargestellt, die Schließdrossel durch eine Drosselstelle 17 in dem Kragen 8a der Aussparung 9a gebildet sein. FIG. 3 shows a variant of the valve needle 1, wherein the recess 9a is aligned at an angle to the longitudinal axis of the valve needle 1 in the valve guide portion 11. The recess 9a extends up to the rotationally symmetrical region 10 and can be configured such that the recess 9a itself forms the closing throttle. Alternatively, as in FIG. 3 illustrated, the closing throttle may be formed by a throttle point 17 in the collar 8a of the recess 9a.

Bei der Variante gemäß Figur 4 ist in die vorhandene Strömungsaussparung 12 in dem Ventilführungsbereich 11 der Ventilnadel 1 die Schließdrossel in Form einer Drosselstelle 17a ähnlich zu Figur 3 eingelassen beziehungsweise eingearbeitet.In the variant according to FIG. 4 is in the existing flow recess 12 in the valve guide portion 11 of the valve needle 1, the closing throttle in the form of a throttle point 17a similar to FIG. 3 embedded or incorporated.

Bei der Konfiguration gemäß den Figuren 5 und 6 sind der obere Anschliff 7, die in den Kragen 8 eingelassene Aussparung 9 und die Strömungsaussparung 12 in Strömungsrichtung des Kraftstoffs fluchtend zueinander angeordnet. Zwischen der Aussparung 9 und der Strömungsaussparung 12 ist wiederum ein rotationssymmetrischer Bereich 10 in die Ventilnadel 1 eingearbeitet. Diese Anordnung ist hinsichtlich einer verwirbelungsfreien Strömung des Kraftstoffs vorteilhaft.In the configuration according to the FIGS. 5 and 6 are the upper section 7, the recessed into the collar 8 recess 9 and the flow recess 12 in the flow direction of the fuel arranged in alignment with each other. Between the recess 9 and the flow recess 12, in turn, a rotationally symmetrical region 10 is incorporated into the valve needle 1. This arrangement is advantageous in terms of a turbulence-free flow of the fuel.

Hiervon unterscheidet sich die Ausgestaltung gemäß den Figuren 7 und 8 dadurch, dass hier kein rotationssymmetrischer Bereich 10 zwischen der in den Kragen 8 eingelassenen Aussparung 9 und der Strömungsaussparung 12 vorgesehen ist. Stattdessen ist hier ein Übergangsbereich 15 zwischen der Aussparung 9 und der Strömungsaussparung 12 angeordnet. Der besondere Vorteil dieses Übergangsbereichs 15 ist, dass dieser wie in den Figuren 9 und 10 dargestellt, einfach in zwei aufeinanderfolgenden Schleifvorgängen, ohne ein Umspannen der Ventilnadel 1 gefertigt werden kann.This differs from the embodiment according to the FIGS. 7 and 8 in that here no rotationally symmetrical region 10 is provided between the recessed recess 8 in the collar 8 and the flow recess 12. Instead, here is a transition region 15 between the recess 9 and the flow recess 12 is arranged. The particular advantage of this transition region 15 is that this as in the FIGS. 9 and 10 shown, easily in two consecutive grinding operations, without re-tightening the valve needle 1 can be made.

Ein Schleifwerkzeug 16 weist die in den Figuren 9 und 10 dargestellte Kontur auf und in einem ersten Schleifgang gemäß Figur 9 wird der obere Anschliff 7 oberhalb beziehungsweise in der Zeichnung links von der Aussparung 9, die Aussparung 9 selber und die Strömungsaussparung 12 in dem Ventilnadelführungsbereich 11 in die Ventilnadel 1 eingeschliffen. Von besonderer Bedeutung ist hierbei, dass der obere Anschliff 7 tiefer als die Strömungsaussparung 12 in die Ventilnadel 1 eingeschliffen wird. Weiterhin ist der Übergangsbereich 15 in einem Rohzustand dargestellt. Es ist aber im Rahmen der Erfindung auch vorgesehen, den Übergangsbereich 15 vollständig bei dem zweiten Schleifgang in die Ventilnadel 1 einzuschleifen.A grinding tool 16 has in the FIGS. 9 and 10 shown contour on and in a first grinding cycle according to FIG. 9 the upper bevel 7 is ground above or in the drawing to the left of the recess 9, the recess 9 itself and the flow recess 12 in the valve needle guide region 11 into the valve needle 1. Of particular importance here is that the upper section 7 is ground deeper than the flow recess 12 in the valve needle 1. Furthermore, the transition region 15 is shown in a raw state. However, it is also provided within the scope of the invention to loop the transition region 15 completely into the valve needle 1 during the second grinding cycle.

In einem zweiten Schleifgang gemäß Figur 10 wird durch ein Versetzen des Schleifwerkzeugs 16 nach rechts der Übergangsbereich 15 in die Ventilnadel 1 eingeschliffen. Dabei berührt nur der Teil des Schleifwerkzeugs 16 die Ventihnadel 1, der diesem Übergangsbereich 15 schleift.In a second grinding cycle according to FIG. 10 is traversed by a displacement of the grinding tool 16 to the right of the transition region 15 in the valve needle 1. In this case, only the part of the grinding tool 16 touches the Ventihnadel 1, which grinds this transition region 15.

Claims (4)

  1. Method for producing a valve needle (1) which has a valve needle tip for interacting with a valve seat of a valve body (2) and, by means of the interaction of the valve needle (1) with the valve seat, permits or shuts off a flow of fuel to at least one injection opening, wherein, on the valve needle (1), there is formed an encircling, sealing collar (8, 8a) with at least one segment-shaped cutout (9, 9a) on the encircling sealing collar (8, 8a) for forming a closing throttle, and wherein the collar (8, 8a) is a constituent part of a valve-guiding region (11), and wherein an upper ground portion (7), the cutout (9, 9a) and a flow cutout (12) are arranged, in the flow direction of the fuel, in alignment in the valve needle guiding region (11), and a transition region (15) is arranged between the cutout (9, 9a) and the flow cutout (12), and the transition region (15) has the same contour as the cutout (9, 9a), characterized by the following method steps:
    - grinding the cutout (9, 9a), the upper ground portion (7) in front of the cutout (9, 9a) and the flow cutout (12) in one grinding process by means of a grinding tool (16),
    - grinding the transition region (15) by relocating the grinding tool (16).
  2. Method according to Claim 1, characterized in that the cutout (9, 9a) has a longitudinal extent which amounts to at least one times the maximum cutout depth as viewed across the number of all cutouts (9, 9a).
  3. Method according to one of the preceding claims, characterized in that the cutout (9, 9a) is formed in the shape of an arc of a circle.
  4. Method according to one of Claims 1 to 3, characterized in that the upper ground portion (7) is ground into the valve needle (1) to a greater depth than the flow cutout (12).
EP10763670.6A 2009-11-06 2010-09-30 Injection nozzle for a leakless fuel injector Active EP2496822B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE200910046452 DE102009046452A1 (en) 2009-11-06 2009-11-06 Injector for a leak-free fuel injector
PCT/EP2010/064560 WO2011054608A1 (en) 2009-11-06 2010-09-30 Injection nozzle for a leakless fuel injector

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EP2496822A1 EP2496822A1 (en) 2012-09-12
EP2496822B1 true EP2496822B1 (en) 2014-04-16

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EP (1) EP2496822B1 (en)
DE (1) DE102009046452A1 (en)
WO (1) WO2011054608A1 (en)

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* Cited by examiner, † Cited by third party
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DE102011077464A1 (en) * 2011-06-14 2012-12-20 Robert Bosch Gmbh Fuel injector for an internal combustion engine
DE102013219568A1 (en) * 2013-09-27 2015-04-02 Robert Bosch Gmbh Fuel injection valve and a method for its production

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DE10062959A1 (en) * 2000-12-16 2002-06-20 Bosch Gmbh Robert Fuel injection valve for internal combustion engines
DE10346075B4 (en) * 2003-10-04 2014-05-08 Robert Bosch Gmbh Method for producing a fuel injection valve and fuel injection valve produced by this method
EP1851427B1 (en) * 2005-02-22 2011-05-11 Continental Automotive Systems US, Inc. Common rail injector with active needle closing device
DE102005046665A1 (en) * 2005-09-29 2007-04-05 Robert Bosch Gmbh Fuel injection valve for e.g. self-ignition internal combustion engine, has inclined groove formed at valve seat near guide section of inner needle, such that tangential force is exerted on needle during flow of fuel
DE102006036447A1 (en) * 2006-08-04 2008-02-07 Robert Bosch Gmbh Injector for a fuel injection system
DE102007032741A1 (en) 2007-07-13 2009-01-15 Robert Bosch Gmbh Fuel injection valve for internal combustion engines
DE102008001425A1 (en) * 2008-04-28 2009-10-29 Robert Bosch Gmbh Fuel injector

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WO2011054608A1 (en) 2011-05-12
DE102009046452A1 (en) 2011-05-12

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