EP1062423B1 - Fuel injection valve - Google Patents

Fuel injection valve Download PDF

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Publication number
EP1062423B1
EP1062423B1 EP99964369A EP99964369A EP1062423B1 EP 1062423 B1 EP1062423 B1 EP 1062423B1 EP 99964369 A EP99964369 A EP 99964369A EP 99964369 A EP99964369 A EP 99964369A EP 1062423 B1 EP1062423 B1 EP 1062423B1
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EP
European Patent Office
Prior art keywords
valve
transition region
fuel injection
upstream
sealing
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Expired - Lifetime
Application number
EP99964369A
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German (de)
French (fr)
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EP1062423A1 (en
Inventor
Christoph Buehler
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Robert Bosch GmbH
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Robert Bosch GmbH
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/44Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
    • F02M59/46Valves
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1873Valve seats or member ends having circumferential grooves or ridges, e.g. toroidal
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • 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
    • F02M2200/30Fuel-injection apparatus having mechanical parts, the movement of which is damped
    • F02M2200/304Fuel-injection apparatus having mechanical parts, the movement of which is damped using hydraulic means

Definitions

  • the invention relates to a fuel injection valve for internal combustion engines according to the preamble of the patent claim 1.
  • fuel injectors are for example from DE 195 47 423 A1 and DE 196 34 133 A1 known.
  • valves In such fuel injection valves is a piston-shaped one Valve member axially displaceable in one Drilled bore of a valve body.
  • the valve member has a conical end on the combustion chamber side Valve sealing surface with which it is conical Valve seat surface cooperates on the valve body, at the inwardly projecting end of the closed valve bore is formed.
  • the valve sealing surface on the valve member is in several, preferably two areas divided different cone angles, one Transition area between the two valve sealing surface areas is provided by a downstream side and an upstream valve sealing edge is limited.
  • the valve member is elastically equal under the valve closing force to the nozzle body.
  • the resulting one hydraulically effective seat diameter is in in this case arranged undefined in the transition area, as shown schematically in Fig. 1. Due to the inverse seat angle difference Pressure distribution at the offset from the axial direction A valve member, which the valve member back into the centric, axial position pushes back. In contrast to would look at a fuel injector without an inverse Seat angle difference set a pressure distribution, through which the valve member further from the centric, axial position would be moved.
  • the invention has for its object a fuel injection itzventil of the generic type such further that it by axial alignment of the Valve member a symmetrical spray pattern and above a defined hydraulically effective seat diameter, a high damping of the valve member and enables the lowest possible risk of cavitation.
  • the distance between the upstream valve sealing edge and the downstream valve sealing edge the transition area is chosen so that the upstream valve sealing edge of the transition area forms the hydraulically effective seat diameter.
  • the distance can be determined by test measurements and / or Bills can be determined.
  • a fuel injector shown in FIGS. 1 to 3 for internal combustion engines has a cylindrical valve body 1 on with its free lower End in a combustion chamber, not shown protrudes with fuel to be supplied to the internal combustion engine.
  • An axial blind bore 3 is provided in the valve body 1, in which a piston-shaped valve member 5 axially is slidably guided.
  • the valve member 5 instructs a conical valve sealing surface at its lower end near the combustion chamber 7 with which it is used to control a Injection cross section with a conical valve seat 9 at the combustion chamber end of the valve body 1 interacts with the closed cantilever End of the bore 3 is formed and from the injection openings 6 in the combustion chamber of the internal combustion engine out.
  • the valve sealing surface 7 is like 3, in particular, in an upper region 71 and divided into a lower area. Between the upper area 71 and the lower area 72 a transition region 73 is formed. The angle that from the difference between transition area 73 and Valve seat surface 9 results must be smaller than that Angle resulting from the difference between valve seat area 9 and the lower area 72 results (inverse Seat angle difference). Adjacent to the downstream side Area 72 are injection openings in the valve body 1 20 provided.
  • the upstream side Area 71 of the valve sealing surface has a radial, undercut-shaped recess 74. This forms a space formed by one on the valve body 1 Edge 75 is limited upstream.
  • the transition region 73 is marked by an upstream Valve sealing edge 73a and a downstream side Valve sealing edge 73b limited, which is adjacent are arranged to each other that the hydraulic effective seat diameter during a closing process the upstream valve sealing edge 73a coincides. Because of this defined hydraulically effective Seat diameter becomes a resulting radial Prevents force on the valve member, which in the Fig. 1 shown undefined hydraulic effective seat diameter 90 occurs.
  • the design of the distance between the two valve sealing edges 73a and 73b will be experimental and based determined by bills. With a maximum closing force of 1250 N, which are determined experimentally can result, for example, in a difference in diameter of approximately 0.15 mm with a geometric seat diameter of 2 mm. With this minimal transition area, i.e. with this minimal seating area is in any case guaranteed that the hydraulic effective seat diameter exactly with the valve sealing edge 73a coincides.
  • the angle that the Damping room includes, chosen so that it is larger is than the body seat angle. In this way it is created in the closed state a damping room that one Effect similar to that of a sail Pressure cushion generated when the valve member 5 is closed, that increases the damping of the valve member 5.
  • the fuel injector will close the fuel arranged in the damping space displaces and flows over between the valve member 5 and the edge 75 formed upstream gap from the damping room. The damping effect is due to the flow resistance generated by the gap generated during the closing process.
  • the upstream side Edge 75 is designed so that it in Extreme case with complete deformation of the valve member has no distance from the valve body 5. Out this damping results in a lower tip load.
  • Such a fuel injection valve also has the advantage that the bladder collapse of the cavitation bubbles preferably in the area upstream of the edge 75 takes place because the originating from the injection pump Pressure waves through edge 75 from the transition area be kept away. This does not cause damage the seating area.
  • valve holding body (not shown) tends to an opening pressure drop, whereas the valve member 5 due to the inverse seat angle difference to an increase in opening pressure tends. Opposing effects occur that partially cancel each other out. hereby the service life of the fuel injector increases.

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

Description

Stand der TechnikState of the art

Die Erfindung betrifft ein Kraftstoffeinspritzventil für Brennkraftmaschinen nach der Gattung des Patentanspruchs 1. Derartige Kraftstoffeinspritzventile sind beispielsweise aus der DE 195 47 423 A1 sowie der DE 196 34 133 A1 bekannt.The invention relates to a fuel injection valve for internal combustion engines according to the preamble of the patent claim 1. Such fuel injectors are for example from DE 195 47 423 A1 and DE 196 34 133 A1 known.

Bei derartigen Kraftstoffeinspritzventilen ist ein kolbenförmiges Ventilglied axial verschiebbar in einer Bohrung eines Ventilkörpers geführt. Das Ventilglied weist dabei an seinem brennraumseitigen Ende eine konische Ventildichtfläche auf, mit der es mit einer konischen Ventilsitzfläche am Ventilkörper zusammenwirkt, die am nach innen kragenden Ende der geschlossenen Ventilbohrung gebildet ist. Die Ventildichtfläche am Ventilglied ist in mehrere, vorzugsweise zwei Bereiche mit unterschiedlichen Kegelwinkeln unterteilt, wobei ein Übergangsbereich zwischen den beiden Ventildichtflächenbereichen vorgesehen ist, der von einer stromabwärtsseitigen und einer stromaufwärtsseitigen Ventildichtkante begrenzt wird.In such fuel injection valves is a piston-shaped one Valve member axially displaceable in one Drilled bore of a valve body. The valve member has a conical end on the combustion chamber side Valve sealing surface with which it is conical Valve seat surface cooperates on the valve body, at the inwardly projecting end of the closed valve bore is formed. The valve sealing surface on the valve member is in several, preferably two areas divided different cone angles, one Transition area between the two valve sealing surface areas is provided by a downstream side and an upstream valve sealing edge is limited.

Aufgrund der hohen Ventilschließkräfte, die besonders bei diesen Kraftstoffeinspritzventilen der "Lochdüsen-Bauart" auftreten, tritt insbesondere bei sehr geringen Hüben des Ventilglieds oder beim Vorhub bei zwei Federhaltern ein unsymmetrisches Strahlbild auf, das zur Erhöhung der Emission der Brennkraftmaschine führt. Das Ventilglied gleicht sich dabei elastisch unter der Ventilschließkraft an den Düsenkörper an. Der dabei entstehende hydraulisch wirksame Sitzdurchmesser ist in diesem Falle undefiniert in dem Übergangsbereich angeordnet, wie es in Fig. 1 schematisch dargestellt ist. Durch die inverse Sitzwinkeldifferenz stellt sich eine Druckverteilung an dem aus der Axialrichtung versetzten Ventilglied ein, welche das Ventilglied wieder in die zentrische, axiale Lage zurückdrückt. Im Gegensatz dazu würde sich bei einem Kraftstoffeinspritzventil ohne inverse Sitzwinkeldifferenz eine Druckverteilung einstellen, durch welche das Ventilglied noch weiter aus der zentrischen, axialen Lage bewegt würde.Due to the high valve closing forces, the particular with these fuel injection valves of the "perforated nozzle type" occur, especially occurs at very low Lifting the valve member or during the preliminary stroke with two spring holders an asymmetrical beam pattern that increases the emission of the internal combustion engine leads. The The valve member is elastically equal under the valve closing force to the nozzle body. The resulting one hydraulically effective seat diameter is in in this case arranged undefined in the transition area, as shown schematically in Fig. 1. Due to the inverse seat angle difference Pressure distribution at the offset from the axial direction A valve member, which the valve member back into the centric, axial position pushes back. In contrast to would look at a fuel injector without an inverse Seat angle difference set a pressure distribution, through which the valve member further from the centric, axial position would be moved.

Der Erfindung liegt die Aufgabe zugrunde, ein Kraftstoffeinspr itzventil der gattungsgemäßen Art derart weiterzubilden, daß es durch axiale Ausrichtung des Ventilglieds ein symmetrisches Strahlbild und darüber hinaus einen definierten hydraulisch wirksamen Sitzdurchmesser, eine hohe Dämpfung des Ventilglieds und eine möglichst geringe Kavitationsgefährdung ermöglicht.The invention has for its object a fuel injection itzventil of the generic type such further that it by axial alignment of the Valve member a symmetrical spray pattern and above a defined hydraulically effective seat diameter, a high damping of the valve member and enables the lowest possible risk of cavitation.

Diese Aufgabe wird bei einem Kraftstoffeinspritzventil der eingangs beschriebenen Art erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst und hat den Vorteil, daß der hydraulisch wirksame Sitzdurchmesser insbesondere bei zunehmendem Verschleiß des Kraftstoffeinspritzventils durch die an den Übergangsbereich stromaufwärts im dem Ventilglied ausgebildete radiale, hinterschnittförmige Ausnehmung und die inverse Sitzwinkeldifferenz maximal bis zu der strömaufwärtsseitigen ventildichtkante "wandern" kann. Auf diese weise wird ein präzise definierter hydraulisch wirksamer Sitzdurchmesser an der stromaufwärtsseitigen Ventildichtkante erzielt.This task is done with a fuel injector of the type described above according to the invention solved the features of claim 1 and has the advantage that the hydraulically effective seat diameter in particular with increasing wear of the fuel injector through upstream to the transition area radial, undercut-shaped in the valve member Recess and the inverse seat angle difference up to the upstream side valve sealing edge can "wander". This way a precisely defined hydraulically effective seat diameter on the upstream valve sealing edge achieved.

Der Abstand zwischen der stromaufwärtsseitigen Ventildichtkante und der stromabwärtsseitigen Ventildichtkante des Übergangsbereichs wird dabei so gewählt, daß die stromaufwärtsseitige Ventildichtkante des Übergangsbereichs den hydraulisch wirksamen Sitzdurchmesser bildet. Der Abstand kann durch versuchsmessungen und/oder Rechnungen bestimmt werden.The distance between the upstream valve sealing edge and the downstream valve sealing edge the transition area is chosen so that the upstream valve sealing edge of the transition area forms the hydraulically effective seat diameter. The distance can be determined by test measurements and / or Bills can be determined.

Zeichnungdrawing

Ein Ausführungsbeispiel des erfindungsgemäßen Kraftstoffeinspritzventils für Brennkraftmaschinen sind in der Zeichnung dargestellt und in der nachfolgenden Beschreibung näher erläutert.An embodiment of the fuel injection valve according to the invention for internal combustion engines are in shown in the drawing and in the description below explained in more detail.

In der Zeichnung zeigen:

Fig. 1
schematisch den hydraulisch wirksamen Sitzdurchmesser bei einem aus dem Stand der Technik bekannten Ventil;
Fig. 2
ein von der Erfindung Gebrauch machendes Kraftstoffeinspritzventil und
Fig. 3
eine vergrößerte Ausschnittdarstellung des in Fig. 2 dargestellten Kraftstoffeinspritzventils.
The drawing shows:
Fig. 1
schematically the hydraulically effective seat diameter in a valve known from the prior art;
Fig. 2
a fuel injector making use of the invention; and
Fig. 3
an enlarged sectional view of the fuel injector shown in Fig. 2.

Beschreibung der AusführungsbeispieleDescription of the embodiments

Ein in Fig. 1 bis Fig. 3 dargestelltes Kraftstoffeinspritzventil für Brennkraftmaschinen weist einen zylindrischen ventilkörper 1 auf, der mit seinem freien unteren Ende in einem nicht dargestellten Brennraum der mit Kraftstoff zu versorgenden Brennkraftmaschine ragt. Im Ventilkörper 1 ist eine axiale Sackbohrung 3 vorgesehen, in der ein kolbenförmiges Ventilglied 5 axial verschiebbar geführt ist. Das Ventilglied 5 weist an seinem unteren, brennraumnahen Ende eine konische Ventildichtfläche 7 auf, mit der es zur Steuerung eines Einspritzquerschnitts mit einer konischen Ventilsitzfläche 9 am brennraumseitigen Ende des Ventilkörpers 1 zusammenwirkt, die am nach innen kragenden geschlossenen Ende der Bohrung 3 gebildet ist und von der Einspritzöffnungen 6 in den Brennraum der Brennkraftmaschine ausgehen. Die ventildichtfläche 7 ist dabei wie insbesondere aus Fig. 3 hervorgeht, in einen oberen Bereich 71 und in einen unteren Bereich geteilt. zwischen dem oberen Bereich 71 und dem unteren Bereich 72 ist ein Übergangsbereich 73 ausgebildet. Der Winkel, der sich aus der Differenz zwischen Übergangsbereich 73 und Ventilsitzfläche 9 ergibt, muß kleiner sein als der Winkel, der sich aus der Differenz zwischen Ventilsitzfläche 9 und dem unteren Bereich 72 ergibt (inverse Sitzwinkeldifferenz). Benachbart zu dem stromabwärtsseitigen Bereich 72 sind in dem Ventilkörper 1 Einspritzöffnungen 20 vorgesehen. Der stromaufwärtsseitige Bereich 71 der Ventildichtfläche weist eine radiale, hinterschnittförmige Ausnehmung 74 auf. Diese bildet einen Raum, der von einer an dem Ventilkörper 1 ausgebildeten Kante 75 stromaufwärtsseitig begrenzt wird. Der Übergangsbereich 73 wird durch eine stromaufwärtsseitige Ventildichtkante 73a und eine stromabwärtsseitige Ventildichtkante 73b begrenzt, die derart benachbart zueinander angeordnet sind, daß der hydraulisch wirksame Sitzdurchmesser bei einem Schließvorgang mit der stromaufwärtsseitigen Ventildichtkante 73a zusammenfällt. Aufgrund dieses definierten hydraulisch wirksamen Sitzdurchmesser wird eine resultierende radiale Kraft auf das Ventilglied verhindert, die bei dem in Fig. 1 dargestellten undefiniert verlaufenden hydraulisch wirksamen Sitzdurchmesser 90 auftritt.A fuel injector shown in FIGS. 1 to 3 for internal combustion engines has a cylindrical valve body 1 on with its free lower End in a combustion chamber, not shown protrudes with fuel to be supplied to the internal combustion engine. An axial blind bore 3 is provided in the valve body 1, in which a piston-shaped valve member 5 axially is slidably guided. The valve member 5 instructs a conical valve sealing surface at its lower end near the combustion chamber 7 with which it is used to control a Injection cross section with a conical valve seat 9 at the combustion chamber end of the valve body 1 interacts with the closed cantilever End of the bore 3 is formed and from the injection openings 6 in the combustion chamber of the internal combustion engine out. The valve sealing surface 7 is like 3, in particular, in an upper region 71 and divided into a lower area. between the upper area 71 and the lower area 72 a transition region 73 is formed. The angle that from the difference between transition area 73 and Valve seat surface 9 results must be smaller than that Angle resulting from the difference between valve seat area 9 and the lower area 72 results (inverse Seat angle difference). Adjacent to the downstream side Area 72 are injection openings in the valve body 1 20 provided. The upstream side Area 71 of the valve sealing surface has a radial, undercut-shaped recess 74. This forms a space formed by one on the valve body 1 Edge 75 is limited upstream. The transition region 73 is marked by an upstream Valve sealing edge 73a and a downstream side Valve sealing edge 73b limited, which is adjacent are arranged to each other that the hydraulic effective seat diameter during a closing process the upstream valve sealing edge 73a coincides. Because of this defined hydraulically effective Seat diameter becomes a resulting radial Prevents force on the valve member, which in the Fig. 1 shown undefined hydraulic effective seat diameter 90 occurs.

Die Auslegung des Abstands der beiden Ventildichtkanten 73a und 73b wird experimentell und auf der Grundlage von Rechnungen ermittelt. Bei einer maximalen Schließkraft von 1250 N, die experimentell bestimmt werden kann, ergibt sich beispielsweise eine Durchmesserdifferenz von ungefähr 0,15 mm bei einem geometrischen Sitzdurchmesser von 2 mm. Bei diesem minimalen Übergangsbereich, d.h. bei dieser minimalen Sitzangleichsfläche ist auf jeden Fall gewährleistet, daß der hydraulisch wirksame Sitzdurchmesser genau mit der Ventildichtkante 73a zusammenfällt.The design of the distance between the two valve sealing edges 73a and 73b will be experimental and based determined by bills. With a maximum closing force of 1250 N, which are determined experimentally can result, for example, in a difference in diameter of approximately 0.15 mm with a geometric seat diameter of 2 mm. With this minimal transition area, i.e. with this minimal seating area is in any case guaranteed that the hydraulic effective seat diameter exactly with the valve sealing edge 73a coincides.

Durch die radiale Ausnehmung 74 im Ventilglied 5 wird ein Dämpfungsraum geschaffen, der eine sehr hohe Dämpfung des Ventilglieds 5 bei einem Schließvorgang ermöglicht. Dabei wird vorzugsweise der Winkel, der den Dämpfungsraum einschließt, so gewählt, daß er größer ist als der Körpersitzwinkel. Auf diese Weise entsteht im geschlossenen Zustand ein Dämpfungsraum, der einen Effekt ähnlich dem eines Segels hervorruft und ein Druckpolster beim Schließen des Ventilglieds 5 erzeugt, das die Dämpfung des Ventilglieds 5 verstärkt. Bei einem Schließvorgang des Kraftstoffeinspritzventils wird der in dem Dämpfungsraum angeordnete Brennstoff verdrängt und strömt über den zwischen dem Ventilglied 5 und der Kante 75 gebildeten Spalt stromaufwärtsseitig aus dem Dämpfungsraum. Der Dämpfungseffekt wird aufgrund des durch den Spalt erzeugten Strömungswiderstands beim Schließvorgang erzeugt. Die stromaufwärtsseitige Kante 75 wird dabei so ausgelegt, daß sie im Extremfall bei vollständiger Deformation des Ventilglieds keinen Abstand zum Ventilkörper 5 aufweist. Aus dieser Dämpfung resultiert eine geringere Kuppenbelastung. Through the radial recess 74 in the valve member 5 created a damping space that has a very high damping of the valve member 5 allows for a closing operation. The angle that the Damping room includes, chosen so that it is larger is than the body seat angle. In this way it is created in the closed state a damping room that one Effect similar to that of a sail Pressure cushion generated when the valve member 5 is closed, that increases the damping of the valve member 5. At a The fuel injector will close the fuel arranged in the damping space displaces and flows over between the valve member 5 and the edge 75 formed upstream gap from the damping room. The damping effect is due to the flow resistance generated by the gap generated during the closing process. The upstream side Edge 75 is designed so that it in Extreme case with complete deformation of the valve member has no distance from the valve body 5. Out this damping results in a lower tip load.

Ein derartiges Kraftstoffeinspritzventil weist ferner den Vorteil auf, daß der Blasenkollaps der Kavitationsblasen vorzugsweise im Bereich stromaufwärts der Kante 75 erfolgt, da die von der Einspritzpumpe herrührenden Druckwellen durch die Kante 75 von dem Übergangsbereich ferngehalten werden. Dadurch kommt es nicht zur Schädigung des Sitzbereichs.Such a fuel injection valve also has the advantage that the bladder collapse of the cavitation bubbles preferably in the area upstream of the edge 75 takes place because the originating from the injection pump Pressure waves through edge 75 from the transition area be kept away. This does not cause damage the seating area.

Der (nicht dargestellte) Ventilhaltekörper tendiert zu einem Öffnungsdruckabfall, wohingegen das Ventilglied 5 wegen der inversen Sitzwinkeldifferenz zu einem Öffnungsdruckanstieg tendiert. Es treten gegenläufige Effekte auf, die sich zum Teil wieder aufheben. Hierdurch steigt die Lebensdauer des Kraftstoffeinspritzventils.The valve holding body (not shown) tends to an opening pressure drop, whereas the valve member 5 due to the inverse seat angle difference to an increase in opening pressure tends. Opposing effects occur that partially cancel each other out. hereby the service life of the fuel injector increases.

Claims (2)

  1. Fuel injection valve for internal combustion engines, having a valve element (5) which can be displaced axially in a bore (3) of a valve body (1) and, at its end which faces the combustion space of the internal combustion engine, has a conical valve-sealing surface (7) with which it interacts with a conical valve seat surface (9) at that end of the bore (3) of the valve body (1) which is closed on the combustion-space side, the conical valve-sealing surface (7) on the valve element (5) being divided into two regions (71, 72) which have different cone angles and at the transition of which a transition region (73) bounded by a valve-sealing edge (73a) on the upstream side and a valve-sealing edge (73b) on the downstream side is formed, the difference of the cone angles of the transition region (73) and of the valve seat surface (9) being smaller than the difference of the cone angles of the region (72) on the downstream side and of the valve seat surface (9), characterized in that a radial recess (74) which is formed in the valve element (5) adjoins the transition region (73) upstream and is bounded by that sealing edge (73a) of the transition region (73) which is on the upstream side and by an edge (75) formed with respect to the valve body (1).
  2. Fuel injection valve according to Claim 1, characterized in that the valve-sealing edges (73a, 73b) which bound the transition region (73) are arranged so closely adjacent to each other that the valve-sealing edge (73a) on the upstream side forms a hydraulically effective seat diameter.
EP99964369A 1999-01-14 1999-11-24 Fuel injection valve Expired - Lifetime EP1062423B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19901057A DE19901057A1 (en) 1999-01-14 1999-01-14 Fuel injection valve for internal combustion engines
DE19901057 1999-01-14
PCT/DE1999/003723 WO2000042316A1 (en) 1999-01-14 1999-11-24 Fuel injection valve

Publications (2)

Publication Number Publication Date
EP1062423A1 EP1062423A1 (en) 2000-12-27
EP1062423B1 true EP1062423B1 (en) 2004-08-11

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EP99964369A Expired - Lifetime EP1062423B1 (en) 1999-01-14 1999-11-24 Fuel injection valve

Country Status (6)

Country Link
US (1) US6502554B1 (en)
EP (1) EP1062423B1 (en)
JP (1) JP4587248B2 (en)
KR (1) KR100631298B1 (en)
DE (2) DE19901057A1 (en)
WO (1) WO2000042316A1 (en)

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DE10050600A1 (en) * 2000-10-12 2002-04-25 Siemens Ag Injector for a fuel injection system
DE10105681A1 (en) * 2001-02-08 2002-08-29 Siemens Ag Fuel injection valve for an internal combustion engine
EP1522721B1 (en) 2003-10-06 2006-05-03 Delphi Technologies, Inc. Injection nozzle
DE10359302A1 (en) * 2003-12-17 2005-07-21 Robert Bosch Gmbh Valve body with multi-cone geometry at the valve seat
JP2006307678A (en) * 2005-04-26 2006-11-09 Denso Corp Fuel injection nozzle
US20070200011A1 (en) * 2006-02-28 2007-08-30 Caterpillar Inc. Fuel injector having nozzle member with annular groove
EP2969318B1 (en) * 2013-03-15 2018-07-25 Schott Corporation Glass-metal composites

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Also Published As

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JP2002535537A (en) 2002-10-22
US6502554B1 (en) 2003-01-07
KR20010041733A (en) 2001-05-25
DE59910205D1 (en) 2004-09-16
WO2000042316A1 (en) 2000-07-20
JP4587248B2 (en) 2010-11-24
KR100631298B1 (en) 2006-10-09
EP1062423A1 (en) 2000-12-27
DE19901057A1 (en) 2000-07-27

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