EP1952011B1 - Fuel injection apparatus for an internal combustion engine having direct fuel injection - Google Patents

Fuel injection apparatus for an internal combustion engine having direct fuel injection Download PDF

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Publication number
EP1952011B1
EP1952011B1 EP06807052.3A EP06807052A EP1952011B1 EP 1952011 B1 EP1952011 B1 EP 1952011B1 EP 06807052 A EP06807052 A EP 06807052A EP 1952011 B1 EP1952011 B1 EP 1952011B1
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EP
European Patent Office
Prior art keywords
pressure
valve element
fuel injection
injection device
chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
EP06807052.3A
Other languages
German (de)
French (fr)
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EP1952011A1 (en
Inventor
Andreas Rettich
Thomas Pauer
Friedrich Boecking
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Robert Bosch GmbH
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Robert Bosch GmbH
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Publication of EP1952011A1 publication Critical patent/EP1952011A1/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
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/20Closing valves mechanically, e.g. arrangements of springs or weights or permanent magnets; Damping of valve lift
    • F02M61/205Means specially adapted for varying the spring tension or assisting the spring force to close the injection-valve, e.g. with damping of valve lift
    • 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
    • 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
    • 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
    • F02M2547/001Control chambers formed by movable sleeves
    • 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 device for an internal combustion engine with direct fuel injection according to the preamble of claim 1.
  • the DE 100 24 702 A1 and DE 100 24 703 A1 each show a fuel injection device with which the fuel can be injected directly into its associated combustion chamber of an internal combustion engine.
  • a valve element is arranged in a housing, which in the region of a fuel outlet opening has a total acting in the opening direction of the valve element pressure surface.
  • a control surface acting in the closing direction is present, which delimits a control chamber.
  • a high fuel pressure is present at a region of the pressure surface acting in the opening direction and at the control surface acting in the closing direction, as is provided by a fuel rail.
  • the excess force acting in the closing direction is achieved by the pressure surface acting in the opening direction at least when the valve element is closed is smaller than the control surface acting in the closing direction.
  • the pressure applied to the control surface is lowered until the hydraulic force resultant in the opening direction on the pressure surface exceeds the forces acting in the closing direction. As a result, opening of the valve element is effected.
  • valve element In both known fuel injectors, the valve element "floats" in high fuel pressure.
  • measures are proposed with which the pressure in the control room after lowering can be raised again very quickly.
  • Object of the present invention is to develop a fuel injection device of the type mentioned so that it closes very quickly. Another object is a simplified manufacture of the device.
  • the closing of the valve element is assisted by the fact that when the valve element is open is lowered at the pressure acting in the opening direction of the pressure surface (or at least at a part thereof). This is possible, for example, by a corresponding throttling between the valve element and a housing-side valve seat region and / or by an additional valve spool section.
  • the restriction can be adjusted so that at least slightly open valve element, the force acting in the opening direction is smaller than when the valve element is closed. As a result, the closing process is supported and accelerated. The valve element is "sucked" to close the quasi to the valve seat.
  • the invention makes it possible in a special way to design the pressure surface acting in the opening direction and the control surface acting in the closing direction, each projecting onto a plane perpendicular to the direction of movement of the valve element, at least approximately the same size. This allows a low-cost production of the valve element.
  • the fuel injection device according to the invention operates with a high efficiency, since the existing in earlier devices leakage between the valve element and the housing is no longer available. A return line can be made smaller in the sequence.
  • valve element as a whole can be arranged in a high-pressure space connected to the high-pressure connection.
  • a sealing sleeve can be provided. This can be radially free, ie without guidance, so that manufacturing tolerances can be easily compensated.
  • the control of the control chamber can then be done by an existing example in the sleeve control channel.
  • the valve element is multi-part and at least two parts of the valve element are coupled to each other via a hydraulic coupler.
  • the hydraulic coupler may comprise an intermediate disc which geometrically separates a first coupling space from a second coupling space. This simplifies the production.
  • the hydraulic coupler comprises a connecting channel which connects the two coupling spaces hydraulically with each other. This allows the optimization of the coupler, for example by designing the connecting channel as a flow restrictor.
  • At least one of the parts of the valve element can be designed as an elastic pressure rod such that an opening movement of the control chamber limiting part of the valve element is time-delayed transmits to the cooperating with the valve seat part of the valve element.
  • a fuel injector carries in the figure as a whole the reference numeral 10. It comprises a housing 12, which in turn has a nozzle body 12a, a Injector body 12b, and a nozzle lock nut 12c includes.
  • a stepped recess 14 is provided in its longitudinal direction, of which in FIG. 1 Lower end fuel outlet channels 16 go out, which pass through the wall of the nozzle body 12 a.
  • a needle-like valve element 18 is arranged in the recess 14. This has an overall substantially constant diameter D.
  • the valve element 18 has a conical tip formed by a first conical annular surface 20 and a second conical end surface 22.
  • the annular surface 20 and the end surface 22 have a different conicity, so that a sealing edge 24 is formed between them. This is when the valve element 18 is closed at an opposite also conical valve seat surface 26 in FIG. 1 lower end portion of the recess 14 in the nozzle body 12a. In this way, the valve element 18 can separate the fuel discharge passages 16 from an annular high-pressure space 28 present upstream of the sealing edge 24 between the valve element 18 and the housing 12.
  • the high pressure chamber 28 extends over the entire length of the recess 14 and the valve element 18. The latter is guided in the housing 12 above all over a only a small axial length having guide portion 30, which with a complementary guide portion 32 at in FIG. 1 cooperates with the upper end of the nozzle body 12a.
  • the high-pressure chamber 28 is not interrupted by the two guide sections 30 and 32:
  • the valve element 18 In the region of the guide section 30, the valve element 18 has four flattened portions 34 distributed over its circumference, through which the corresponding guide sections 30 and 32 pass Flow channels are formed, which are also part of the high-pressure chamber 28.
  • the flats 34 are dimensioned such that a throttling of the flow, which flows through the flow channels formed, is substantially zero.
  • the recess 14 is in FIG. 1 closed at the top by a valve piece 36.
  • the valve piece 36 is attached to the injector body 12b in a manner not shown. Between the sleeve portion 38 and a slightly spaced from this annular collar 42 on the valve element 18, a spring 44 is clamped, by which the valve element 18 is acted upon very easily in the closing direction.
  • a control surface 46 is present at the in FIG. 1 upper end of the valve element 18, a control surface 46 is present. It represents a part of a boundary of a control chamber 48 formed between the sleeve portion 38 and the valve element 18.
  • the control chamber 48 Via an inlet throttle 50, the control chamber 48 is connected to the high pressure chamber 28, which in turn is connected via a channel 52 in the injector body 12 b with a high pressure port 54.
  • This in turn is connected in the operation of the fuel injection device 10 with a fuel rail ("rail"), which in FIG. 1 but not shown.
  • fuel rail fuel can be stored under very high pressure.
  • a plurality of fuel injectors may be connected.
  • An outlet throttle 56 connects the control chamber 48 further with a switching valve 58.
  • the switching valve 58 in this example has a valve ball 62, which in turn is acted upon by a valve stem 64 which in turn either hydraulically or directly via a corresponding actuator 66 is actuated.
  • fuel injector 10 is operated as follows: In an initial state, the switching valve 58 is closed.
  • the high fuel pressure (up to 1800 bar) prevailing at the high-pressure connection 54 prevails in the high-pressure space 28 and is also transmitted through the inlet throttle 50 into the control chamber 48.
  • the high pressure is also at the conical annular surface 20 in FIG. 1 lower end of the valve element 18 at.
  • the hydraulic conical annular surface 20 acting in the opening direction is smaller overall than the control surface 46 acting in the closing direction. For this reason, a force resultant in the closing direction acts altogether on the valve element 18, which ensures that the sealing edge 24 of the valve element 18 abuts against the opposite valve seat surface 26 is pressed.
  • the connection of the high-pressure chamber 28 is interrupted to the fuel outlet channels 16.
  • the switching valve 58 is opened.
  • the control chamber 48 is now connected via the outlet throttle 56 to the low pressure port 60. Since the inlet throttle 50 throttles more than the outlet throttle 56, the pressure in the control chamber 48 and consequently also the force acting on the control surface 46 and acting in the closing direction decreases Force. As soon as it falls below the hydraulic force acting on the conical annular surface 20 and acting in the opening direction (minus the force of the spring 44), the valve element 18 with the sealing edge 24 lifts away from the valve seat surface 26. Fuel now flows from the high-pressure chamber 28 to the fuel outlet channels 16.
  • the switching valve 58 In order to stop the injection of fuel by the fuel injection device 10, the switching valve 58 is closed. The connection of the control chamber 48 to the low pressure port 60 is therefore interrupted. Fuel can now flow back through the inlet throttle 50 into the control chamber 48, so that there adjusts the pressure prevailing at the high pressure port 54 and the high pressure chamber 28.
  • the fact that the valve element 18 now executes a closing movement, although the hydraulic cross-sectional area of the control surface 46 acting in the closing direction and the hydraulic cross-sectional area of the pressure surfaces 20 and 22 acting in the opening direction are the same, is related to the following: In the region of the sealing edge 24, the flow between the both annular surfaces 20 and 22 on the one hand and the opposite valve seat surface 26 on the other hand very slightly throttled.
  • the geometry of the conical annular surface 20 and the conical end surface 22, in particular the conicity of these two surfaces 20 and 22, relative to the valve seat surface 26 is selected so that over a stroke H a course of the force acting in the opening direction F is achieved, as in FIG. 2 is shown.
  • the force F 1 acting in the opening direction is smaller than the force F 0 acting in the opening direction due to throttling effects.
  • a force F 2 Only at a further increased stroke H acts in the opening direction, a force F 2 , which is significantly greater than the force F 0 .
  • valve element 18 is virtually "sucked” toward the end of the closing operation and accordingly closes quickly.
  • a force course, as in FIG. 2 is shown, in addition or reinforced by the formation of a valve spool portion (in FIG. 1 not shown), which cooperates with a corresponding housing-side section.
  • valve element 18 is in one piece as a whole.
  • a certain elasticity which causes a certain compression with closed valve element 18, which can be used to even the smallest amounts of fuel in the range of 1 mm 3 targeted and precise inject.
  • FIG. 3 A first embodiment of a fuel-one embodiment of a fuel injection device is in FIG. 3 shown.
  • the sleeve portion 38 is formed as a separate part of the valve 36. It is pushed onto the end region 40 of the valve element 18 and is acted upon by the spring 44 against the valve piece 36.
  • a further modified second embodiment shows FIG. 4 ,
  • the valve element 18 is divided into two, with a nozzle needle 68 and a control piston 70.
  • the control piston 34 is comparatively long and dimensioned so that it, as will be explained in more detail below, has a significant elasticity.
  • Nozzle needle 68 and control piston 70 are coupled to each other via a hydraulic coupler 72 comprising two hydraulic coupling chambers 74a and 74b.
  • the two coupling spaces 74a and 74b are geometrically separated from each other by a housing-side washer 76, but hydraulically connected to each other via a connecting channel 78.
  • the upper coupling space 74a is bounded radially by a sleeve 80a, the lower of a sleeve 80b.
  • the sleeves are each pressed against the intermediate disc 76 in a spring 81a and 81b, which is supported on the housing side (spring 81a) or on the nozzle needle 68 (spring 81b).
  • the control piston 70 defines with an end face 82 axially the upper coupling space 74a, the nozzle needle with an end face 84 the lower coupling space 74b.
  • the control piston 70 moves in FIG. 4 up.
  • the pressure in the upper coupling chamber 74a decreases, which transfers via the connecting channel 78 into the lower coupling space 74b and also leads there to a pressure reduction.
  • the nozzle needle 68 is quasi wound up.
  • FIG. 4 it can be seen that the control piston 70 and the nozzle needle 68 "float" in the high pressure of the above and below the washer 76 high-pressure chambers 28a and 28b.
  • corresponding passages (without reference numerals) are present in the intermediate disk 76. As a result, the sealing problem is reduced.
  • control piston 34 Due to the elasticity and length L, in particular of the control piston 34, it is possible that even very small amounts of fuel can be injected with the fuel injection device 18. This is due to the fact that the control piston initially, when the nozzle needle 68 rests against the housing-side valve seat, is elastically compressed by the high pressure in the control chamber 48. At a pressure reduction in the control chamber 48, the control piston 70 must first be lengthen to bring about the above-mentioned pressure reduction in the coupling chambers 74a and 74b.

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

Description

Stand der TechnikState of the art

Die Erfindung betrifft eine Kraftstoff-Einspritzvorrichtung für eine Brennkraftmaschine mit Kraftstoff-Direkteinspritzung nach dem Oberbegriff des Anspruchs 1.The invention relates to a fuel injection device for an internal combustion engine with direct fuel injection according to the preamble of claim 1.

Die DE 100 24 702 A1 und DE 100 24 703 A1 zeigen jeweils eine Kraftstoff-Einspritzvorrichtung, mit der der Kraftstoff direkt in einen ihr zugeordneten Brennraum einer Brennkraftmaschine eingespritzt werden kann. Hierzu ist in einem Gehäuse ein Ventilelement angeordnet, welches im Bereich einer Kraftstoff-Austrittsöffnung eine insgesamt in Öffnungsrichtung des Ventilelements wirkende Druckfläche aufweist. Am entgegengesetzten Ende des Ventilelements ist eine in Schließrichtung wirkende Steuerfläche vorhanden, welche einen Steuerraum begrenzt.The DE 100 24 702 A1 and DE 100 24 703 A1 each show a fuel injection device with which the fuel can be injected directly into its associated combustion chamber of an internal combustion engine. For this purpose, a valve element is arranged in a housing, which in the region of a fuel outlet opening has a total acting in the opening direction of the valve element pressure surface. At the opposite end of the valve element, a control surface acting in the closing direction is present, which delimits a control chamber.

Bei geschlossener Kraftstoff-Einspritzvorrichtung liegt an einem Bereich der in Öffnungsrichtung wirkenden Druckfläche und an der in Schließrichtung wirkenden Steuerfläche ein hoher Kraftstoffdruck an, wie er beispielsweise von einer Kraftstoff-Sammelleitung ("Rail") bereitgestellt wird. Der in Schließrichtung wirkende Kraftüberschuss wird erreicht, indem die in Öffnungsrichtung wirkende Druckfläche zumindest bei geschlossenem Ventilelement kleiner ist als die in Schließrichtung wirkende Steuerfläche.When the fuel injection device is closed, a high fuel pressure is present at a region of the pressure surface acting in the opening direction and at the control surface acting in the closing direction, as is provided by a fuel rail. The excess force acting in the closing direction is achieved by the pressure surface acting in the opening direction at least when the valve element is closed is smaller than the control surface acting in the closing direction.

Zum Öffnen des Ventilelements wird der an der Steuerfläche anliegende Druck abgesenkt, bis die in Öffnungsrichtung wirkende hydraulische Kraftresultierende an der Druckfläche die in Schließrichtung wirkenden Kräfte übersteigt. Hierdurch wird ein Öffnen des Ventilelements bewirkt.To open the valve element, the pressure applied to the control surface is lowered until the hydraulic force resultant in the opening direction on the pressure surface exceeds the forces acting in the closing direction. As a result, opening of the valve element is effected.

Bei beiden bekannten Kraftstoff-Einspritzvorrichtungen "schwimmt" das Ventilelement im hohen Kraftstoffdruck. Bei dem in der DE 199 24 703 A1 gezeigten Ventilelement sind darüber hinaus die in Öffnungsrichtung wirkende Druckfläche und die in Schließrichtung wirkende Steuerfläche, auf eine Ebene orthogonal zur Längsachse des Ventilelements, gleich groß. Um dennoch ein sicheres Schließen des Ventilelements gewährleisten zu können, werden Maßnahmen vorgeschlagen, mit denen der Druck im Steuerraum nach einer Absenkung wieder besonders rasch angehoben werden kann.In both known fuel injectors, the valve element "floats" in high fuel pressure. In the in the DE 199 24 703 A1 In addition, the valve element shown in the opening direction acting pressure surface and acting in the closing direction control surface, on a plane orthogonal to the longitudinal axis of the valve element, the same size. In order to still be able to ensure a safe closing of the valve element, measures are proposed with which the pressure in the control room after lowering can be raised again very quickly.

In der EP 0971118 A wird eine weitere Einspritzvorrichtung offenbart.In the EP 0971118 A another injection device is disclosed.

Aufgabe der vorliegenden Erfindung ist es, eine Kraftstoff-Einspritzvorrichtung der eingangs genannten Art so weiterzubilden, dass sie sehr schnell schließt. Eine weitere Aufgabe ist eine vereinfachte Herstellung der Vorrichtung.Object of the present invention is to develop a fuel injection device of the type mentioned so that it closes very quickly. Another object is a simplified manufacture of the device.

Diese Aufgabe wird durch eine Kraftstoff-Einspritzvorrichtung mit den Merkmalen des Anspruchs 1 gelöst. Ferner wird die Aufgabe durch ein Verfahren mit den Merkmalen des nebengeordneten Verfahrensanspruches gelöst. Vorteilhafte Weiterbildungen sind in Unteransprüchen angegeben.This object is achieved by a fuel injection device having the features of claim 1. Furthermore, the object is achieved by a method having the features of the independent method claim. Advantageous developments are specified in subclaims.

Vorteile der ErfindungAdvantages of the invention

Erfindungsgemäß wird das Schließen des Ventilelements dadurch unterstützt, dass bei geöffnetem Ventilelement der an der in Öffnungsrichtung wirkenden Druckfläche (oder zumindest an einem Teil hiervon) anliegende Druck abgesenkt wird. Dies ist beispielsweise durch eine entsprechende Drosselung zwischen dem Ventilelement und einem gehäuseseitigen Ventilsitzbereich und/oder durch einen zusätzlichen Ventilschieberabschnitt möglich.According to the invention, the closing of the valve element is assisted by the fact that when the valve element is open is lowered at the pressure acting in the opening direction of the pressure surface (or at least at a part thereof). This is possible, for example, by a corresponding throttling between the valve element and a housing-side valve seat region and / or by an additional valve spool section.

Mittels einer entsprechenden Ausformung einerseits des gehäuseseitigen Ventilsitzbereichs und andererseits eines entsprechenden Dichtbereichs am Ventilelement kann die Drosselung so eingestellt werden, dass mindestens bei etwas geöffnetem Ventilelement die in Öffnungsrichtung wirkende Kraft kleiner ist als bei geschlossenem Ventilelement. Hierdurch wird der Schließvorgang unterstützt und beschleunigt. Das Ventilelement wird zum Schließen quasi an den Ventilsitz "angesaugt".By means of a corresponding shaping on the one hand of the housing-side valve seat portion and on the other hand a corresponding sealing region on the valve element, the restriction can be adjusted so that at least slightly open valve element, the force acting in the opening direction is smaller than when the valve element is closed. As a result, the closing process is supported and accelerated. The valve element is "sucked" to close the quasi to the valve seat.

Die Erfindung ermöglicht es in besonderer Weise, die in Öffnungsrichtung wirkende Druckfläche und die in Schließrichtung wirkende Steuerfläche, jeweils auf eine Ebene senkrecht zur Bewegungsrichtung des Ventilelements projiziert, wenigstens in etwa gleich groß auszugestalten. Dies gestattet eine preiswerte Fertigung des Ventilelements.The invention makes it possible in a special way to design the pressure surface acting in the opening direction and the control surface acting in the closing direction, each projecting onto a plane perpendicular to the direction of movement of the valve element, at least approximately the same size. This allows a low-cost production of the valve element.

Vorgeschlagen wird auch, in allen zwischen Steuerraum und Druckraum liegenden Räumen, die das Ventilelement umgeben, im Betrieb wenigstens zeitweise und wenigstens in etwa der am Hochdruckanschluss herrschende hohe Kraftstoffdruck herrscht. Dies kann beispielsweise dadurch realisiert werden, dass die Ausnehmung, in der das Ventilelement insgesamt aufgenommen ist, mit dem Hochdruckanschluss verbunden ist. Ein Niederdruckbereich ist demzufolge nicht mehr vorhanden ("druckausgeglichenes" Ventil). Somit kann keine Leckage zwischen dem Hoch- und einem solchen Niederdruckbereich auftreten, so dass auch die entsprechende Abdichtung und eine hierfür erforderliche Leckageleitung entfallen können.It is also proposed, in all lying between the control chamber and pressure chamber spaces surrounding the valve element, during operation at least temporarily and at least approximately prevails at the high pressure connection prevailing high fuel pressure. This can be realized, for example, in that the recess in which the valve element is accommodated in its entirety is connected to the high-pressure connection. A low pressure area is therefore no longer available ("pressure balanced" valve). Thus, no leakage between the high and such Low pressure area occur, so that the corresponding seal and a leaking line required for this purpose can be omitted.

Dies gestattet einen einfacheren Aufbau der Kraftstoff-Einspritzvorrichtung mit insgesamt weniger Teilen, was zum einen die Montage erleichtert und zum anderen eine kleinere Bauweise ermöglicht. Darüber hinaus arbeitet die erfindungsgemäße Kraftstoff-Einspritzvorrichtung mit einem hohen Wirkungsgrad, da die bei früheren Vorrichtungen vorhandene Leckage zwischen Ventilelement und Gehäuse nicht mehr vorhanden ist. Eine Rücklaufleitung kann in der Folge kleiner ausgelegt werden.This allows a simpler structure of the fuel injection device with fewer parts, which on the one hand facilitates the assembly and on the other hand allows a smaller design. In addition, the fuel injection device according to the invention operates with a high efficiency, since the existing in earlier devices leakage between the valve element and the housing is no longer available. A return line can be made smaller in the sequence.

Dadurch, dass eine Abdichtung zwischen der in Öffnungsrichtung wirkenden Druckfläche und der in Schließrichtung wirkenden Steuerfläche nicht mehr im bisherigen Sinne erforderlich ist, kann das Ventilelement insgesamt in einem mit dem Hochdruckanschluss verbundenen Hochdruckraum angeordnet sein. Um eine Druckabsenkung im Steuerraum dennoch erreichen zu können, kann dann einfach eine Dichthülse vorgesehen sein. Diese kann radial frei, also ohne Führung, sein, so dass Fertigungstoleranzen einfach ausgeglichen werden können. Die Ansteuerung des Steuerraums kann dann durch einen beispielsweise in der Hülse vorhandenen Steuerkanal erfolgen.Due to the fact that sealing between the pressure surface acting in the opening direction and the control surface acting in the closing direction is no longer required in the previous sense, the valve element as a whole can be arranged in a high-pressure space connected to the high-pressure connection. In order to still be able to achieve a pressure reduction in the control room, then simply a sealing sleeve can be provided. This can be radially free, ie without guidance, so that manufacturing tolerances can be easily compensated. The control of the control chamber can then be done by an existing example in the sleeve control channel.

Um mit der erfindungsgemäßen Kraftstoff-Einspritzvorrichtung auch Kleinstmengen im Bereich,von 1 mm3 einspritzen zu können, wird eine "Stauchung" des Ventilelements durch eine entsprechende Längenbeziehungsweise Materialauswahl des Ventilelements eingestellt. Alle vorangegangenen Maßnahmen ermöglichen einen Betrieb der Kraftstoff-Einspritzvorrichtung auch bei sehr hohen Drücken von bis zu 1800 bar.In order to be able to inject very small amounts in the range of 1 mm 3 with the fuel injection device according to the invention, a "compression" of the valve element is adjusted by a corresponding Längenbeziehungsweise material selection of the valve element. All previous measures allow operation of the fuel injector even at very high pressures of up to 1800 bar.

Erfindungsgemäß ist das Ventilelement mehrteilig und mindestens zwei Teile des Ventilelements über einen hydraulischen Koppler miteinander gekoppelt sind. Hierdurch wird die Freiheit bei der Auslegung der Kraftstoff-Einspritzvorrichtung erheblich erhöht. Auch die Herstellung der Vorrichtung wird vereinfacht.According to the invention, the valve element is multi-part and at least two parts of the valve element are coupled to each other via a hydraulic coupler. As a result, the freedom in the design of the fuel injection device is considerably increased. The manufacture of the device is simplified.

In Weiterbildung hierzu wird vorgeschlagen, dass die beiden Teile des Ventilelements im hydraulischen Koppler dann, wenn das Ventilelement am Ventilsitz anliegt, voneinander beabstandet sind. Hierdurch wird eine direkte mechanische Kopplung der beiden Teile und somit ein mögliches Prellen verhindert.In a further development, it is proposed that the two parts of the valve element in the hydraulic coupler, when the valve element rests against the valve seat, are spaced from each other. As a result, a direct mechanical coupling of the two parts and thus a possible bouncing is prevented.

Dabei kann der hydraulische Koppler eine Zwischenscheibe umfassen, die einen ersten Koppelraum von einem zweiten Koppelraum geometrisch trennt. Dies vereinfacht die Herstellung.In this case, the hydraulic coupler may comprise an intermediate disc which geometrically separates a first coupling space from a second coupling space. This simplifies the production.

Möglich ist, dass der hydraulische Koppler einen die beiden Koppelräume hydraulisch miteinander verbindenden Verbindungskanal umfasst. Dies gestattet die Optimierung des Kopplers, beispielsweise durch Ausgestaltung des Verbindungskanals als Strömungsdrossel.It is possible that the hydraulic coupler comprises a connecting channel which connects the two coupling spaces hydraulically with each other. This allows the optimization of the coupler, for example by designing the connecting channel as a flow restrictor.

Mindestens eines der Teile des Ventilelements kann als elastische Druckstange derart ausgebildet sein, dass eine Öffnungsbewegung des den Steuerraum begrenzenden Teils des Ventilelements sich zeitverzögert auf den mit dem Ventilsitz zusammenarbeitenden Teil des Ventilelements überträgt. Auf diese Weise können trotz des Einsatzes eine preiswerten Magnetventils zur Steuerung des Drucks im Steuerraum auch sehr kurze Öffnungszeiten und damit die Fähigkeit, auch Kleinstmengen einspritzen zu können, realisiert werden.At least one of the parts of the valve element can be designed as an elastic pressure rod such that an opening movement of the control chamber limiting part of the valve element is time-delayed transmits to the cooperating with the valve seat part of the valve element. In this way, despite the use of a cheap solenoid valve to control the pressure in the control room and very short opening times and thus the Ability to inject even very small quantities can be realized.

Zeichnungdrawing Nachfolgend werden besonders bevorzugteThe following are particularly preferred

Ausführungsbeispiele der vorliegenden Erfindung unter Bezugnahme auf die beiliegende Zeichnung näher erläutert. In der Zeichnung zeigen:

Figur 1
einen teilweisen Schnitt durch einen Bereich einer einer Kraftstoff-Einspritzvorrichtung, die nicht Teil der Erfindung ist;
Figur 2
ein Diagramm, in dem ein Verlauf einer in Öffnungsrichtung wirkenden Kraft über dem Hub eines Ventilelements der Kraftstoff-Einspritzvorrichtung von Figur 1 aufgetragen ist;
Figur 3
einen teilweisen Schnitt durch einen Bereich einer ersten Ausführungsform einer Kraftstoff-Einspritzvorrichtung; und
Figur 4
eine Darstellung ähnlich zu Figur 1 einer zweiten Ausführungsform einer Kraftstoff-Einspritzvorrichtung.
Embodiments of the present invention with reference to the accompanying drawings explained in more detail. In the drawing show:
FIG. 1
a partial section through a portion of a fuel injection device, which is not part of the invention;
FIG. 2
a diagram in which a curve of an opening force acting on the stroke of a valve element of the fuel injection device of FIG. 1 is applied;
FIG. 3
a partial section through a portion of a first embodiment of a fuel injection device; and
FIG. 4
a representation similar to FIG. 1 a second embodiment of a fuel injection device.

Beschreibung der AusführungsbeispieleDescription of the embodiments

Eine Kraftstoff-Einspritzvorrichtung trägt in Figur insgesamt das Bezugszeichen 10. Sie umfasst ein Gehäuse 12, welches wiederum einen Düsenkörper 12a, einen Injektorkörper 12b, und eine Düsenspannmutter 12c umfasst. In dem Gehäuse 12 ist in seiner Längsrichtung eine gestufte Ausnehmung 14 vorhanden, von deren in Figur 1 unterem Ende Kraftstoff-Austrittskanäle 16 ausgehen, die die Wand des Düsenkörpers 12a durchsetzen.A fuel injector carries in the figure as a whole the reference numeral 10. It comprises a housing 12, which in turn has a nozzle body 12a, a Injector body 12b, and a nozzle lock nut 12c includes. In the housing 12, a stepped recess 14 is provided in its longitudinal direction, of which in FIG. 1 Lower end fuel outlet channels 16 go out, which pass through the wall of the nozzle body 12 a.

In der Ausnehmung 14 ist ein nadelartiges Ventilelement 18 angeordnet. Dieses weist einen insgesamt im Wesentlichen konstanten Durchmesser D auf. An seinem in Figur 1 unteren Ende weist das Ventilelement 18 eine konische Spitze auf, die durch eine erste konische Ringfläche 20 und eine zweite konische Endfläche 22 gebildet wird. Die Ringfläche 20 und die Endfläche 22 haben eine unterschiedliche Konizität, so dass zwischen ihnen eine Dichtkante 24 gebildet ist. Diese liegt bei geschlossenem Ventilelement 18 an einer gegenüberliegenden ebenfalls konischen Ventilsitzfläche 26 im in Figur 1 unteren Endbereich der Ausnehmung 14 im Düsenkörper 12a an. Auf diese Weise kann das Ventilelement 18 die Kraftstoff-Austrittskanäle 16 von einem stromaufwärts von der Dichtkante 24 zwischen dem Ventilelement 18 und dem Gehäuse 12 vorhandenen ringförmigen Hochdruckraum 28 trennen.In the recess 14, a needle-like valve element 18 is arranged. This has an overall substantially constant diameter D. At his in FIG. 1 lower end, the valve element 18 has a conical tip formed by a first conical annular surface 20 and a second conical end surface 22. The annular surface 20 and the end surface 22 have a different conicity, so that a sealing edge 24 is formed between them. This is when the valve element 18 is closed at an opposite also conical valve seat surface 26 in FIG. 1 lower end portion of the recess 14 in the nozzle body 12a. In this way, the valve element 18 can separate the fuel discharge passages 16 from an annular high-pressure space 28 present upstream of the sealing edge 24 between the valve element 18 and the housing 12.

Der Hochdruckraum 28 erstreckt sich über die gesamte Länge der Ausnehmung 14 bzw. des Ventilelements 18. Letzteres wird im Gehäuse 12 vor allem über einen eine nur geringe axiale Länge aufweisenden Führungsabschnitt 30 geführt, welcher mit einem komplementären Führungsabschnitt 32 am in Figur 1 oberen Ende des Düsenkörpers 12a zusammenarbeitet. Der Hochdruckraum 28 wird durch die beiden Führungsabschnitte 30 und 32 jedoch nicht unterbrochen: Im Bereich des Führungsabschnitts 30 weist das Ventilelement 18 nämlich vier über seinen Umfang verteilt angeordnete Abflachungen 34 auf, durch die entsprechende den Führungsabschnitt 30 beziehungsweise 32 durchquerende Strömungskanäle gebildet werden, welche ebenfalls Teil des Hochdruckraums 28 sind. Die Abflachungen 34 sind dabei so dimensioniert, dass eine Drosselung der Strömung, die durch die gebildeten Strömungskanäle hindurch strömt, im Wesentlichen Null ist.The high pressure chamber 28 extends over the entire length of the recess 14 and the valve element 18. The latter is guided in the housing 12 above all over a only a small axial length having guide portion 30, which with a complementary guide portion 32 at in FIG. 1 cooperates with the upper end of the nozzle body 12a. However, the high-pressure chamber 28 is not interrupted by the two guide sections 30 and 32: In the region of the guide section 30, the valve element 18 has four flattened portions 34 distributed over its circumference, through which the corresponding guide sections 30 and 32 pass Flow channels are formed, which are also part of the high-pressure chamber 28. The flats 34 are dimensioned such that a throttling of the flow, which flows through the flow channels formed, is substantially zero.

Die Ausnehmung 14 wird in Figur 1 nach oben hin durch ein Ventilstück 36 verschlossen. Dieses ragt mit einem Hülsenabschnitt 38 ein Stück weit in die Ausnehmung 14 hinein, so dass in dem Hülsenabschnitt 38 ein von den Kraftstoff-Austrittskanälen 60 entgegengesetzter Endbereich 40 des Ventilelements 18 axial verschieblich, jedoch weitgehend fluiddicht aufgenommen ist. Das Ventilstück 36 ist auf nicht näher dargestellte Art und Weise am Injektorkörper 12b befestigt. Zwischen dem Hülsenabschnitt 38 und einem von diesem etwas beabstandeten Ringbund 42 am Ventilelement 18 ist eine Feder 44 verspannt, durch die das Ventilelement 18 ganz leicht in Schließrichtung beaufschlagt wird.The recess 14 is in FIG. 1 closed at the top by a valve piece 36. This protrudes with a sleeve portion 38 a little way into the recess 14, so that in the sleeve portion 38 a of the fuel outlet channels 60 opposite end portion 40 of the valve element 18 is axially displaceable, but largely fluid-tight. The valve piece 36 is attached to the injector body 12b in a manner not shown. Between the sleeve portion 38 and a slightly spaced from this annular collar 42 on the valve element 18, a spring 44 is clamped, by which the valve element 18 is acted upon very easily in the closing direction.

Am in Figur 1 oberen Ende des Ventilelements 18 ist eine Steuerfläche 46 vorhanden. Sie stellt einen Teil einer Begrenzung eines Steuerraums 48 dar, der zwischen dem Hülsenabschnitt 38 und dem Ventilelement 18 gebildet wird. Über eine Zulaufdrossel 50 ist der Steuerraum 48 mit dem Hochdruckraum 28 verbunden, der wiederum über einen Kanal 52 im Injektorkörper 12b mit einem Hochdruckanschluss 54 verbunden ist. Dieser wiederum ist im Betrieb der Kraftstoff-Einspritzvorrichtung 10 mit einer Kraftstoff-Sammelleitung ("Rail") verbunden, die in Figur 1 jedoch nicht dargestellt ist. In einer solchen Kraftstoff-Sammelleitung kann Kraftstoff unter sehr hohem Druck gespeichert werden. An die Kraftstoff-Sammelleitung können mehrere Kraftstoff-Einspritzvorrichtungen angeschlossen sein.At the in FIG. 1 upper end of the valve element 18, a control surface 46 is present. It represents a part of a boundary of a control chamber 48 formed between the sleeve portion 38 and the valve element 18. Via an inlet throttle 50, the control chamber 48 is connected to the high pressure chamber 28, which in turn is connected via a channel 52 in the injector body 12 b with a high pressure port 54. This in turn is connected in the operation of the fuel injection device 10 with a fuel rail ("rail"), which in FIG. 1 but not shown. In such a fuel rail fuel can be stored under very high pressure. To the fuel rail, a plurality of fuel injectors may be connected.

Eine Ablaufdrossel 56 verbindet den Steuerraum 48 ferner mit einem Schaltventil 58. Dieses verbindet den Steuerraum 48 in geöffnetem Zustand mit einem Niederdruckanschluss 60. Hierzu verfügt das Schaltventil 58 in diesem Bespiel über eine Ventilkugel 62, die wiederum von einem Ventilstößel 64 beaufschlagt wird, der wiederum entweder hydraulisch oder direkt über einen entsprechenden Aktor 66 betätigt wird.An outlet throttle 56 connects the control chamber 48 further with a switching valve 58. This connects the control chamber 48 in the open state with a low pressure port 60. For this purpose, the switching valve 58 in this example has a valve ball 62, which in turn is acted upon by a valve stem 64 which in turn either hydraulically or directly via a corresponding actuator 66 is actuated.

Die in Figur 1 gezeigte Kraftstoff-Einspritzvorrichtung 10 wird folgendermaßen betrieben: In einem Ausgangszustand ist das Schaltventil 58 geschlossen. Der am Hochdruckanschluss 54 anliegende hohe Kraftstoffdruck (bis zu 1800 bar) herrscht im Hochdruckraum 28 und wird durch die Zulaufdrossel 50 auch in den Steuerraum 48 übertragen. Der hohe Druck liegt auch an der konischen Ringfläche 20 am in Figur 1 unteren Ende des Ventilelements 18 an. Die in Öffnungsrichtung wirkende hydraulische konische Ringfläche 20 ist jedoch insgesamt kleiner als die in Schließrichtung wirkende Steuerfläche 46. Aus diesem Grund wirkt insgesamt auf das Ventilelement 18 eine in Schließrichtung wirkende Kraftresultierende, welche dafür sorgt, dass die Dichtkante 24 des Ventilelements 18 gegen die gegenüberliegende Ventilsitzfläche 26 gedrückt wird. Somit ist die Verbindung des Hochdruckraums 28 zu den Kraftstoff-Austrittskanälen 16 unterbrochen.In the FIG. 1 shown fuel injector 10 is operated as follows: In an initial state, the switching valve 58 is closed. The high fuel pressure (up to 1800 bar) prevailing at the high-pressure connection 54 prevails in the high-pressure space 28 and is also transmitted through the inlet throttle 50 into the control chamber 48. The high pressure is also at the conical annular surface 20 in FIG. 1 lower end of the valve element 18 at. However, the hydraulic conical annular surface 20 acting in the opening direction is smaller overall than the control surface 46 acting in the closing direction. For this reason, a force resultant in the closing direction acts altogether on the valve element 18, which ensures that the sealing edge 24 of the valve element 18 abuts against the opposite valve seat surface 26 is pressed. Thus, the connection of the high-pressure chamber 28 is interrupted to the fuel outlet channels 16.

Damit Kraftstoff von der Kraftstoff-Einspritzvorrichtung 10 abgegeben werden kann, wird das Schaltventil 58 geöffnet. Der Steuerraum 48 ist nun über die Ablaufdrossel 56 mit dem Niederdruckanschluss 60 verbunden. Da die Zulaufdrossel 50 stärker drosselt als die Ablaufdrossel 56, sinkt der Druck im Steuerraum 48 und in der Folge auch die an der Steuerfläche 46 angreifende und in Schließrichtung wirkende Kraft. Sobald diese unter die an der konischen Ringfläche 20 angreifende und in Öffnungsrichtung wirkende hydraulische Kraft (abzüglich der Kraft der Feder 44) absinkt, hebt das Ventilelement 18 mit der Dichtkante 24 von der Ventilsitzfläche 26 ab. Kraftstoff strömt nun vom Hochdruckraum 28 zu den Kraftstoff-Austrittskanälen 16.In order for fuel to be delivered from the fuel injector 10, the switching valve 58 is opened. The control chamber 48 is now connected via the outlet throttle 56 to the low pressure port 60. Since the inlet throttle 50 throttles more than the outlet throttle 56, the pressure in the control chamber 48 and consequently also the force acting on the control surface 46 and acting in the closing direction decreases Force. As soon as it falls below the hydraulic force acting on the conical annular surface 20 and acting in the opening direction (minus the force of the spring 44), the valve element 18 with the sealing edge 24 lifts away from the valve seat surface 26. Fuel now flows from the high-pressure chamber 28 to the fuel outlet channels 16.

Nun wirkt zusätzlich auch an der konischen Endfläche 22 ein hydraulischer Druck, der an dieser konischen Endfläche 22 eine zusätzliche in Öffnungsrichtung wirkende Kraft erzeugt (zum Verlauf der Kraft im Verhältnis zum Hub wird weiter unten im Zusammenhang mit Figur 2 noch ausführlich Stellung genommen). Hierdurch wird das Öffnen des Ventilelements 18 beschleunigt. Die konische Ringfläche 20 und die konische Endfläche 22 bilden also insgesamt eine in Öffnungsrichtung wirkende Druckfläche, deren hydraulisch wirksame Querschnittsfläche gleich der hydraulisch wirksamen Querschnittsfläche der Steuerfläche 46 ist.In addition, a hydraulic pressure also acts on the conical end face 22, which generates an additional force acting in the opening direction on this conical end face 22 (the course of the force in relation to the stroke will be described below) FIG. 2 still commented in detail). As a result, the opening of the valve element 18 is accelerated. The conical annular surface 20 and the conical end surface 22 thus form a total acting in the opening direction of the pressure surface whose hydraulically effective cross-sectional area is equal to the hydraulically effective cross-sectional area of the control surface 46.

Um die Einspritzung von Kraftstoff durch die Kraftstoff-Einspritzvorrichtung 10 zu beenden, wird das Schaltventil 58 geschlossen. Die Verbindung des Steuerraums 48 zum Niederdruckanschluss 60 ist daher unterbrochen. Kraftstoff kann nun durch die Zulaufdrossel 50 wieder in den Steuerraum 48 nachströmen, so dass sich dort der am Hochdruckanschluss 54 und im Hochdruckraum 28 herrschende Druck einstellt. Dass das Ventilelement 18 nun eine Schließbewegung ausführt, obwohl die in Schließrichtung wirkende hydraulische Querschnittsfläche der Steuerfläche 46 und die in Öffnungsrichtung wirkende hydraulische Querschnittsfläche der Druckflächen 20 und 22 gleich groß sind, hängt mit Folgendem zusammen: Im Bereich der Dichtkante 24 wird die Strömung zwischen den beiden Ringflächen 20 und 22 einerseits und der gegenüberliegenden Ventilsitzfläche 26 andererseits ganz leicht gedrosselt.In order to stop the injection of fuel by the fuel injection device 10, the switching valve 58 is closed. The connection of the control chamber 48 to the low pressure port 60 is therefore interrupted. Fuel can now flow back through the inlet throttle 50 into the control chamber 48, so that there adjusts the pressure prevailing at the high pressure port 54 and the high pressure chamber 28. The fact that the valve element 18 now executes a closing movement, although the hydraulic cross-sectional area of the control surface 46 acting in the closing direction and the hydraulic cross-sectional area of the pressure surfaces 20 and 22 acting in the opening direction are the same, is related to the following: In the region of the sealing edge 24, the flow between the both annular surfaces 20 and 22 on the one hand and the opposite valve seat surface 26 on the other hand very slightly throttled.

Damit liegt zumindest an einem Bereich der konischen Endfläche 22 ein Druck an, der kleiner ist als der Druck im Hochdruckraum 28. Dies hängt auch mit dem Abströmen des Kraftstoffs durch die Kraftstoff-Austrittskanäle 16 zusammen.This is at least at a portion of the conical end surface 22 to a pressure which is smaller than the pressure in the high-pressure chamber 28. This is also related to the outflow of the fuel through the fuel outlet channels 16.

Trotz eines insgesamt im Hochdruckraum 28 und im Steuerraum 48 gleichen Drucks und trotz gleicher in Schließrichtung und in Öffnungsrichtung wirkender hydraulisch wirksamer Querschnittsflächen ist also die in der Summe an der konischen Ringfläche 20 und der konischen Endfläche 22 in Öffnungsrichtung wirkende Kraft kleiner als die an der Steuerfläche 46 in Schließrichtung wirkende Kraft. Die am Ventilelement 18 insgesamt angreifende Kraftresultierende wirkt also in Schließrichtung, was zu einer Schließbewegung des Ventilelements 18 führt.Despite a total in the high-pressure chamber 28 and the control chamber 48 same pressure and despite acting in the same direction in the closing direction and opening direction hydraulically effective cross-sectional areas so the sum acting on the conical annular surface 20 and the conical end surface 22 in the opening direction force is smaller than that on the control surface 46 force acting in the closing direction. The total resultant force acting on the valve element 18 thus acts in the closing direction, which leads to a closing movement of the valve element 18.

Die Geometrie der konischen Ringfläche 20 und der konischen Endfläche 22, insbesondere die Konizität dieser beiden Flächen 20 und 22, relativ zur Ventilsitzfläche 26 ist so gewählt, dass über einen Hub H ein Verlauf der in Öffnungsrichtung wirkenden Kraft F erzielt wird, wie er in Figur 2 dargestellt ist. Aus dieser erkennt man, dass die in Öffnungsrichtung wirkende Kraft beim Hub H = 0 (also bei mit der Dichtkante 24 an der Ventilsitzfläche 26 anliegendem Ventilelement 18) einen Wert F0 hat. Bei etwas geöffnetem Ventilelement 18, also ungefähr bei einem Hub H1, ist auf Grund von Drosseleffekten die in Öffnungsrichtung wirkende Kraft F1 kleiner als die bei geschlossenem Ventilelement 18 in Öffnungsrichtung wirkende Kraft F0. Erst bei einem nochmals vergrößerten Hub H wirkt in Öffnungsrichtung eine Kraft F2, die deutlich größer ist als die Kraft F0.The geometry of the conical annular surface 20 and the conical end surface 22, in particular the conicity of these two surfaces 20 and 22, relative to the valve seat surface 26 is selected so that over a stroke H a course of the force acting in the opening direction F is achieved, as in FIG. 2 is shown. It can be seen from this that the force acting in the opening direction has a value F 0 at the stroke H = 0 (ie when the valve element 18 is in contact with the valve seat surface 26 with the sealing edge 24). When the valve element 18 is slightly open, ie approximately at a stroke H 1 , the force F 1 acting in the opening direction is smaller than the force F 0 acting in the opening direction due to throttling effects. Only at a further increased stroke H acts in the opening direction, a force F 2 , which is significantly greater than the force F 0 .

Dies bedeutet im Umkehrschluss während des gerade beschriebenen Schließvorgangs, dass das Ventilelement 18 gegen Ende des Schließvorgangs quasi "angesaugt" wird und entsprechend schnell schließt. Ein Kraftverlauf, wie er in Figur 2 dargestellt ist, kann zusätzlich oder verstärkt auch durch die Ausbildung eines Ventilschieberabschnitts (in Figur 1 nicht gezeigt) herbeigeführt werden, der mit einem entsprechenden gehäuseseitigen Abschnitt zusammenarbeitet.This means, conversely, during the closing process just described, that the valve element 18 is virtually "sucked" toward the end of the closing operation and accordingly closes quickly. A force course, as in FIG. 2 is shown, in addition or reinforced by the formation of a valve spool portion (in FIG. 1 not shown), which cooperates with a corresponding housing-side section.

Es versteht sich, dass für ein sicheres Öffnen der Druck im Steuerraum 48 so weit abgesenkt werden muss, dass die an der Steuerfläche 46 in Schließrichtung wirkende Kraft zuzüglich der Kraft der Feder 44 kleiner ist als die Kraft F1.It is understood that must be lowered so far for a safe opening of the pressure in the control chamber 48 such that the force acting on the control surface 46 in the closing direction plus the force of the spring 44 is smaller than the force f1.

Man erkennt aus Figur 1, dass das Ventilelement 18 insgesamt einstückig ist. Durch eine entsprechende Material- und Geometriewahl wird zwischen der Dichtkante 24 einerseits und dem Steuerraum 48 eine bestimmte Federelastizität eingestellt, die bei geschlossenem Ventilelement 18 eine gewisse Stauchung verursacht, welche dazu genutzt werden kann, auch kleinste Kraftstoffmengen im Bereich von 1 mm3 gezielt und präzise einzuspritzen.One recognizes FIG. 1 in that the valve element 18 is in one piece as a whole. By an appropriate choice of material and geometry is set between the sealing edge 24 on the one hand and the control chamber 48, a certain elasticity, which causes a certain compression with closed valve element 18, which can be used to even the smallest amounts of fuel in the range of 1 mm 3 targeted and precise inject.

Eine erste Ausführungsform einer Kraftstoff-Eine Ausführungsform einer Kraftstoff-Einspritzvorrichtung ist in Figur 3 gezeigt. Dabei tragen hier und nachfolgend solche Elemente und Bereiche, die bereits im Zusammenhang mit Figur 4 erläutert wurden, die gleichen Bezugszeichen. Sie sind nicht nochmals im Detail erläutert. Bei der in Figur 3 gezeigten Kraftstoff-Einspritzvorrichtung 10 ist der Hülsenabschnitt 38 als vom Ventilstück 36 separates Teil ausgebildet. Er ist auf den Endbereich 40 des Ventilelements 18 aufgeschoben und wird von der Feder 44 gegen das Ventilstück 36 beaufschlagt.A first embodiment of a fuel-one embodiment of a fuel injection device is in FIG. 3 shown. Here and below bear such elements and areas already in connection with FIG. 4 have been explained, the same reference numerals. They are not explained again in detail. At the in FIG. 3 shown fuel injector 10, the sleeve portion 38 is formed as a separate part of the valve 36. It is pushed onto the end region 40 of the valve element 18 and is acted upon by the spring 44 against the valve piece 36.

In radialer Richtung ist der Hülsenabschnitt 38 nicht gehalten. Die Führung des Ventilelements 18 erfolgt somit ausschließlich durch den Führungsabschnitt 30 am Ventilelement 18 und den Führungsabschnitt 32 am Düsenkörper 12a. Hierdurch wird eine leichtgängige Bewegung des Ventilelements 18 trotz gewisser Fertigungstoleranzen gewährleistet. Auch die Abdichtung des Steuerraums 48 wird hierdurch verbessert.In the radial direction of the sleeve portion 38 is not held. The guidance of the valve element 18 thus takes place exclusively through the guide section 30 on the valve element 18 and the guide section 32 on the nozzle body 12a. As a result, a smooth movement of the valve element 18 is ensured despite certain manufacturing tolerances. The sealing of the control chamber 48 is thereby improved.

Es versteht sich, dass unter dem Begriff der hydraulisch wirksamen Querschnittsfläche einerseits der Druckfläche 20, 22 und andererseits der Steuerfläche 46 die Fläche der konischen Ringfläche 20, der konischen Endfläche 22, und der Steuerfläche 46 gemeint ist, die auf eine senkrecht zur Bewegungsrichtung des Ventilelements 18 liegende Ebene projiziert ist. Da der Durchmesser des Ventilelements 18 konstant ist (Wert D), sind diese hydraulisch wirksamen Querschnittsflächen identisch.It is understood that by the term of the hydraulically effective cross-sectional area on the one hand the pressure surface 20, 22 and on the other hand the control surface 46 the area of the conical annular surface 20, the conical end surface 22, and the control surface 46 is meant, which is perpendicular to the direction of movement of the valve element 18 lying level is projected. Since the diameter of the valve element 18 is constant (value D), these hydraulically effective cross-sectional areas are identical.

Eine nochmals geänderte zweite Ausführungsform zeigt Figur 4. In dieser ist das Ventilelement 18 zweigeteilt, mit einer Düsennadel 68 und einem Steuerkolben 70. Der Steuerkolben 34 ist vergleichsweise lang und so dimensioniert, dass er, wie weiter unten noch genauer erläutert ist, eine deutliche Elastizität besitzt. Düsennadel 68 und Steuerkolben 70 sind über einen hydraulischen Koppler 72 miteinander gekoppelt, der zwei hydraulische Koppelräume 74a und 74b umfasst. Die beiden Koppelräume 74a und 74b sind durch eine gehäuseseitige Zwischenscheibe 76 geometrisch voneinander getrennt, über einen Verbindungskanal 78 aber hydraulisch miteinander verbunden.A further modified second embodiment shows FIG. 4 , In this, the valve element 18 is divided into two, with a nozzle needle 68 and a control piston 70. The control piston 34 is comparatively long and dimensioned so that it, as will be explained in more detail below, has a significant elasticity. Nozzle needle 68 and control piston 70 are coupled to each other via a hydraulic coupler 72 comprising two hydraulic coupling chambers 74a and 74b. The two coupling spaces 74a and 74b are geometrically separated from each other by a housing-side washer 76, but hydraulically connected to each other via a connecting channel 78.

Der obere Koppelraum 74a wird radial von einer Hülse 80a, der untere von einer Hülse 80b begrenzt. Die Hülsen werden jeweils in einer Feder 81a und 81b, die sich gehäuseseitig (Feder 81a) bzw. an der Düsennadel 68 (Feder 81b) abstützt, gegen die Zwischenscheibe 76 gedrückt. Der Steuerkolben 70 begrenzt mit einer Endfläche 82 axial den oberen Koppelraum 74a, die Düsennadel mit einer Endfläche 84 den unteren Koppelraum 74b.The upper coupling space 74a is bounded radially by a sleeve 80a, the lower of a sleeve 80b. The sleeves are each pressed against the intermediate disc 76 in a spring 81a and 81b, which is supported on the housing side (spring 81a) or on the nozzle needle 68 (spring 81b). The control piston 70 defines with an end face 82 axially the upper coupling space 74a, the nozzle needle with an end face 84 the lower coupling space 74b.

Wird der Druck im Steuerraum 60 durch eine Ansteuerung des Aktors 66 (hier ein Magnetaktor) gesenkt, bewegt sich der Steuerkolben 70 in Figur 4 nach oben. Hierdurch sinkt der Druck im oberen Koppelraum 74a, was sich über den Verbindungskanal 78 in den unteren Koppelraum 74b überträgt und auch dort zu einer Druckabsenkung führt. In der Folge wird die Düsennadel 68 quasi aufgezogen.If the pressure in the control chamber 60 is lowered by triggering the actuator 66 (here a solenoid actuator), the control piston 70 moves in FIG. 4 up. As a result, the pressure in the upper coupling chamber 74a decreases, which transfers via the connecting channel 78 into the lower coupling space 74b and also leads there to a pressure reduction. As a result, the nozzle needle 68 is quasi wound up.

Aus Figur 4 erkennt man, dass der Steuerkolben 70 und die Düsennadel 68 im Hochdruck der oberhalb und unterhalb der Zwischenscheibe 76 liegenden Hochdruckräume 28a und 28b "schwimmen". Hierzu sind in der Zwischenscheibe 76 entsprechende Durchlässe (ohne Bezugszeichen) vorhanden. Hierdurch wird die Abdichtungsproblematik reduziert.Out FIG. 4 it can be seen that the control piston 70 and the nozzle needle 68 "float" in the high pressure of the above and below the washer 76 high-pressure chambers 28a and 28b. For this purpose, corresponding passages (without reference numerals) are present in the intermediate disk 76. As a result, the sealing problem is reduced.

Durch die Elastizität und Länge L vor allem des Steuerkolbens 34 wird es ermöglicht, dass mit der Kraftstoff-Einspritzvorrichtung 18 auch sehr kleine Kraftstoffmengen eingespritzt werden können. Dies dadurch, dass der Steuerkolben zunächst, wenn die Düsennadel 68 am gehäuseseitigen Ventilsitz anliegt, durch den hohen Druck im Steuerraum 48 elastisch zusammengedrückt wird. Bei einer Druckabsenkung im Steuerraum 48 muss sich der Steuerkolben 70 erst längen, um die oben genannte Druckabsenkung in den Koppelräumen 74a und 74b herbeizuführen.Due to the elasticity and length L, in particular of the control piston 34, it is possible that even very small amounts of fuel can be injected with the fuel injection device 18. This is due to the fact that the control piston initially, when the nozzle needle 68 rests against the housing-side valve seat, is elastically compressed by the high pressure in the control chamber 48. At a pressure reduction in the control chamber 48, the control piston 70 must first be lengthen to bring about the above-mentioned pressure reduction in the coupling chambers 74a and 74b.

Bei der Ausführungsform nach Figur 4 können durch eine entsprechende Auswahl der Verhältnisse des Durchmesser D1 der Endfläche 84 der Düsennadel 68 zum Durchmesser D2 der Endfläche 82 des Steuerkolbens 70 (Übersetzung) und des Durchmessers D2 zum Durchmesser D3 der Steuerfläche 46 (Druckstufe) die Kraftverhältnisse auf einfache Weise und doch präzise eingestellt werden.In the embodiment according to FIG. 4 For example, by a corresponding selection of the ratios of the diameter D1 of the end face 84 of the nozzle needle 68 to the diameter D2 of the end surface 82 of the control piston 70 (translation) and the diameter D2 to the diameter D3 of the control surface 46 (pressure stage), the force ratios can be adjusted in a simple and yet precise manner become.

Claims (9)

  1. Fuel injection device (10) for an internal combustion engine with direct fuel injection, having a housing (12), having a valve element (18) which is arranged in the housing (12) and which has a hydraulic pressure surface (20, 22) which acts in an opening direction, which hydraulic pressure surface delimits a high-pressure chamber (28a, 28b) which is connected to a high-pressure port (54), and having a hydraulic control surface (46) which acts in a closing direction and which delimits a control chamber (48) in which a variable control pressure prevails during operation, wherein the closed valve element (18) bears, by way of a conical tip, against a valve seat surface (26) and thus separates fuel outlet ducts (16) from the high-pressure chamber (28a, 28b), and wherein the valve element (18), in an open position (H1) or an open position range, interacts in a throttling manner with a housing region (26) such that a pressure which is lower than the pressure in the high-pressure chamber (28a, 28b) acts at least on one part of the pressure surface (20, 22), characterized in that the valve element (18) is of multi-part form (68, 70) and at least two parts (68, 70) of the valve element (18) are coupled to one another via a hydraulic coupler (72).
  2. Fuel injection device (10) according to Claim 1, characterized in that, when the valve element (18) is open, the hydraulically acting pressure surface (20, 22) and the hydraulically acting control surface (46) are, when projected in each case onto a plane perpendicular to the direction of movement of the valve element (18), of at least approximately the same size.
  3. Fuel injection device (10) according to one of the preceding claims, characterized in that, during operation, at least approximately the high fuel pressure prevailing at the high-pressure port (54) at least intermittently prevails in spaces (28a, 28b) which are situated between the control chamber (48) and high-pressure chamber (28a, 28b) and which surround the valve element (18).
  4. Fuel injection device (10) according to one of the preceding claims, characterized in that the valve element (18) has a valve slide portion which, at least intermittently, in particular during closing, interacts in a throttling manner with a housing-side region (12) in such a way that the pressure acting at least on one part of the pressure surface (20, 22) falls below the pressure in the high-pressure chamber (28a, 28b).
  5. Fuel injection device (10) according to one of the preceding claims, characterized in that the control chamber (48) is fluidically separated from the high-pressure chamber (28a, 28b) by a sleeve portion (38) which is not guided radially by the housing (12).
  6. Fuel injection device (10) according to one of the preceding claims, characterized in that the valve element (18) has a guide portion (30) on which it is guided (32) in the housing (12) so as to permit a passage of fluid.
  7. Fuel injection device (10) according to Claim 1, characterized in that the two parts (68, 70) of the valve element (18) in the hydraulic coupler (72) are spaced apart from one another when the valve element (18) bears against the valve seat (26).
  8. Fuel injection device (10) according to Claim 7, characterized in that the hydraulic coupler (72) comprises an intermediate disc (76) which geometrically separates a first coupling chamber (74a) from a second coupling chamber (74b).
  9. Fuel injection device (10) according to Claim 8, characterized in that the hydraulic coupler (72) comprises a connecting duct (78) which hydraulically connects the two coupling chambers (74a, 74b) to one another.
EP06807052.3A 2005-11-15 2006-10-06 Fuel injection apparatus for an internal combustion engine having direct fuel injection Ceased EP1952011B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102005054385 2005-11-15
DE102006012078A DE102006012078A1 (en) 2005-11-15 2006-03-16 Fuel injection device for an internal combustion engine with direct fuel injection
PCT/EP2006/067156 WO2007057252A1 (en) 2005-11-15 2006-10-06 Fuel injection apparatus for an internal combustion engine having direct fuel injection

Publications (2)

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EP1952011A1 EP1952011A1 (en) 2008-08-06
EP1952011B1 true EP1952011B1 (en) 2013-07-24

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EP06807052.3A Ceased EP1952011B1 (en) 2005-11-15 2006-10-06 Fuel injection apparatus for an internal combustion engine having direct fuel injection

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EP (1) EP1952011B1 (en)
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WO (1) WO2007057252A1 (en)

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DE102007043540A1 (en) * 2007-09-12 2009-05-07 Robert Bosch Gmbh Leak-free fuel injector with long nozzle needle
DE102008001425A1 (en) 2008-04-28 2009-10-29 Robert Bosch Gmbh Fuel injector
DE102008001601A1 (en) 2008-05-06 2009-11-12 Robert Bosch Gmbh Fuel injector and manufacturing process
DE102008001907A1 (en) * 2008-05-21 2009-11-26 Robert Bosch Gmbh Fuel injector
DE102008042154A1 (en) 2008-09-17 2010-03-18 Robert Bosch Gmbh Fuel injector
DE102009028993A1 (en) 2009-08-28 2011-03-03 Robert Bosch Gmbh fuel injector
DE102015211672A1 (en) 2015-06-24 2016-12-29 Robert Bosch Gmbh Fuel injector

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DE10100392C1 (en) * 2001-01-05 2002-06-13 Bosch Gmbh Robert Fluid control valve for IC engine fuel injection has setting piston and operating piston received in adjacent bores in valve body
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DE10352736A1 (en) * 2003-11-12 2005-07-07 Robert Bosch Gmbh Fuel injector with direct needle injection

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DE102006012078A1 (en) 2007-05-16
EP1952011A1 (en) 2008-08-06

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