EP1117920A1 - Common rail injector - Google Patents

Common rail injector

Info

Publication number
EP1117920A1
EP1117920A1 EP00958210A EP00958210A EP1117920A1 EP 1117920 A1 EP1117920 A1 EP 1117920A1 EP 00958210 A EP00958210 A EP 00958210A EP 00958210 A EP00958210 A EP 00958210A EP 1117920 A1 EP1117920 A1 EP 1117920A1
Authority
EP
European Patent Office
Prior art keywords
nozzle
chamber
common rail
nozzle needle
spring
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.)
Granted
Application number
EP00958210A
Other languages
German (de)
French (fr)
Other versions
EP1117920B1 (en
Inventor
Dieter Kienzler
Patrick Mattes
Wolfgang Stoecklein
Friedrich Boecking
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
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Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Priority to EP06123003A priority Critical patent/EP1772618B1/en
Publication of EP1117920A1 publication Critical patent/EP1117920A1/en
Application granted granted Critical
Publication of EP1117920B1 publication Critical patent/EP1117920B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/042The valves being provided with fuel passages
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
    • F02M47/027Electrically actuated valves draining the chamber to release the closing pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/16Sealing of fuel injection apparatus 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
    • F02M2200/28Details of throttles in fuel-injection apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • 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
    • F02M2547/006Springs assisting hydraulic closing force
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type
    • F02M61/12Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for valve bodies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/168Assembling; Disassembling; Manufacturing; Adjusting

Definitions

  • control chamber is delimited by a sleeve which can be displaced under sealing action at the end of the nozzle needle remote from the combustion chamber and is held in contact with the injector housing with the aid of the nozzle spring.
  • the sleeve provides the advantage that the control chamber and the nozzle spring chamber can be combined at the end of the nozzle needle remote from the combustion chamber, without the volume of the control chamber depending on the installation space of the nozzle spring. Therefore it is possible to use a nozzle spring with a high
  • the injection time and the injection time can be precisely defined.
  • the control room can be made very small, which leads to a quick response of the injector according to the invention.
  • the nozzle needle diameter In order to achieve higher nozzle needle speeds, which is particularly important when closing the needle, the nozzle needle diameter must be reduced. A needle diameter of less than 3.5 mm is necessary for a closing speed of 1 m / sec with an acceptable control quantity. This is technically very complex and therefore expensive. According to the present invention, the
  • Nozzle needle diameter can be chosen freely and is not dependent on the dimensions of the nozzle spring.
  • the length can be considerably reduced compared to conventional nozzle needles, which contributes to an exact stroke stop.
  • a special embodiment of the invention is characterized in that a biting edge is formed on the surface of the sleeve which is in contact with the injector housing. It is thereby achieved that the control chamber formed in the interior of the sleeve surrounding nozzle spring chamber remains separate.
  • Another special embodiment of the invention is characterized in that the inner diameter of the sleeve is less than or equal to a guide diameter on the nozzle needle.
  • the inner diameter of the sleeve and the corresponding outer diameter on the nozzle needle can be made much smaller than in conventional injectors.
  • a further special embodiment of the invention is characterized in that the fuel supply is connected to the pressure chamber via the nozzle spring chamber and that the nozzle needle is guided between the nozzle spring chamber and the pressure chamber.
  • a further special embodiment of the invention is characterized in that at least one flat surface is formed on the nozzle needle between the nozzle spring chamber and the pressure chamber, which fuel can pass from the nozzle spring chamber into the pressure chamber.
  • This type of construction offers advantages in particular with regard to high-pressure strength.
  • Further special embodiments of the invention are characterized in that the inlet throttle is integrated in the nozzle needle, the sleeve or the injector housing. The inlet throttle serves to prevent pressure surges during operation.
  • a further special embodiment of the invention is characterized in that the sleeve has a collar at its combustion chamber end.
  • the collar forms a first abutment for the nozzle spring.
  • Another particular embodiment of the invention is characterized in that a step is formed on the nozzle needle, which step forms a stop for a spring plate.
  • the spring plate forms a second abutment for the nozzle spring.
  • Another special embodiment of the invention is characterized in that a circumferential groove is recessed in the nozzle needle, in which a retaining ring is supported, which forms a stop for a spring plate.
  • the outer diameter of the nozzle needle in the control chamber and the guide diameter of the nozzle needle between the nozzle spring chamber and the pressure chamber can be the same size. This is in manufacturing, e.g. by
  • Another special embodiment of the invention is characterized in that the retaining ring is in two parts and is fixed in the assembled state by the spring plate. This prevents the spring plate from loosening in operation in a simple manner.
  • nozzle needle stroke is defined by the distance between the sleeve and the spring plate is.
  • This purely mechanical nozzle needle stroke end stop provides the advantage that the nozzle needle stroke is exactly reproducible. This can reliably shaped ground 'of the injection process. So-called hydraulic gluing is avoided.
  • Stop for the spring plate or between the nozzle spring and the abutments for the nozzle spring are arranged. The closing behavior of the injector can thereby be improved.
  • Another special embodiment of the invention is characterized in that the nozzle needle stroke is defined by the distance between the end surface of the nozzle needle remote from the combustion chamber and the injector housing.
  • This embodiment has the advantage that it is particularly easy to implement in terms of production technology.
  • a further special embodiment of the invention is characterized in that recesses are provided in the end surface of the nozzle needle remote from the combustion chamber and / or in the opposite surface of the injector housing, the dimensions of which are adapted to the volume of the control chamber.
  • Figure 1 shows a first embodiment in longitudinal section through the injector with a bore between the nozzle spring chamber and the pressure chamber.
  • Figure 2 shows a second embodiment in longitudinal section through the injector with a flattening on the nozzle needle between the nozzle spring chamber and the pressure chamber.
  • FIG 3 shows a further exemplary embodiment in a longitudinal section through the injector, the inlet throttle being integrated in the nozzle needle or in the injector housing;
  • Fig. 5 shows a variant of the embodiment shown in Fig. 4 with a two-part
  • Fig. 6 is a sectional view taken along the line VI-VI in Fig. 5;
  • FIG. 7 shows a further embodiment in longitudinal section through the injector with spacer elements for setting the nozzle needle stroke and the nozzle spring pretensioning force
  • FIG. 8 shows a further exemplary embodiment in longitudinal section through the injector with cross grooves in the end face of the nozzle needle remote from the combustion chamber;
  • the control chamber 30 is connected to the nozzle spring chamber 20 via an inlet throttle 31.
  • the control chamber 30 is connected to a relief chamber (not shown) via an outlet throttle 32.
  • connection of the control chamber 30 to the relief chamber depends on the position of a control valve member 33.
  • the injector shown in Fig. 1 works as follows
  • High-pressure fuel reaches the nozzle spring chamber 20 via the fuel inlet 21. From there, the high-pressure fuel reaches the control chamber 30 via the inlet throttle 31 and the pressure chamber 24 via the bore 23.
  • the diameter ratios are selected in a known manner that the nozzle needle 8 is due to the high pressure in the control chamber 30 with its tip 9 in contact with the nozzle needle seat.
  • the control valve member 33 opens, the control chamber 30 is relieved of pressure and the nozzle needle tip 9 lifts off its seat.
  • High-pressure fuel is then injected into the combustion chamber of the internal combustion engine through the spray holes 10 and 11 until the control valve member 33 closes again. This then has the consequence that the pressure in the control chamber 30 rises again and the nozzle needle 8 is pressed with its tip 9 again against the associated nozzle needle seat.
  • the second exemplary embodiment shown in FIG. 2 largely corresponds to the first illustrated in FIG. 1 o rH
  • two grooves 55 and 56 are arranged crosswise in the end face 54 of the nozzle needle 8.
  • a purely mechanical stop of the needle nozzle is thereby achieved. If the dimensions of the grooves 54 and 55 are adapted to the injector, this can become a "semi-hydraulic stop".
  • the breakthrough cross section remaining at the stop is chosen to be just large enough to prevent the nozzle needle 8 from oscillating, but to reduce the amount of control at the end stop as much as possible.
  • a throttle bore 58 is arranged in the end face 54 of the nozzle needle 8 parallel to the longitudinal axis of the nozzle needle 8.
  • Throttle bore 58 opens into a bore 59 which extends transversely to the longitudinal axis of the nozzle needle 8.
  • the bore 59 is a blind bore which is open towards the end of the nozzle needle 8 which is distant from the combustion chamber and is frustoconical.
  • a groove 61 is cut out in the opposite surface 62 of the valve body 3 instead of in the end face 54 of the nozzle needle 8 remote from the combustion chamber.
  • the groove 61 has the same function as the grooves 54 and 55 in the embodiment shown in FIGS. 8 and 9.

Landscapes

  • 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)
  • Manufacturing & Machinery (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Platform Screen Doors And Railroad Systems (AREA)
  • Seats For Vehicles (AREA)

Abstract

The injector has an injector housing (1) with a fuel feed connected to a central high pressure fuel reservoir and an internal pressure chamber. A reciprocally movable nozzle needle movable axially against a spring force is raised from as eat if the pressure in the pressure chamber exceeds that in a control chamber connected via a feed choke to the fuel feed. The control chamber (30) is bounded by a sleeve (28) that can be moved into contact with the injector housing under the sealing effect of the end of the needle (8) remote from the combustion chamber and with the aid of the nozzle spring (19).

Description

über eine Zulaufdrossel mit dem Kraftstoffzulauf verbunden ist, dadurch gelöst, dass der Steuerraum von einer Hülse begrenzt ist, die unter Dichtwirkung an dem brennraumfemen Ende der Düsennadel verschiebbar ist und mit Hilfe der Düsenfeder in Anlage an das Injektorgehäuse gehalten wird. Die Hülse liefert den Vorteil, dass der Steuerraum und der Düsenfederraum am brennraumfemen Ende der Düsennadel kombiniert werden können, ohne dass das Volumen des Steuerraums von dem Bauraum der Düsenfeder abhängt . Deshalb ist es möglich, eine Düsenfeder mit einer hohenIs connected via an inlet throttle to the fuel inlet, in that the control chamber is delimited by a sleeve which can be displaced under sealing action at the end of the nozzle needle remote from the combustion chamber and is held in contact with the injector housing with the aid of the nozzle spring. The sleeve provides the advantage that the control chamber and the nozzle spring chamber can be combined at the end of the nozzle needle remote from the combustion chamber, without the volume of the control chamber depending on the installation space of the nozzle spring. Therefore it is possible to use a nozzle spring with a high
Federsteifigkeit einzubauen, die ein gutes Schließen der Düsennadel gewährleistet. Dadurch können die Einspritzzeit und der Einspritzzeitpunkt exakt festgelegt werden. Außerdem kann der Steuerraum sehr klein ausgeführt werden, was zu einem schnellen Ansprechverhalten des erfindungsgemäßen Injektors führt. Weiterhin besteht ein Zusammenhang zwischen der maximal erreichbaren Dusennadelgeschwindigkeit und dem Düsennadeldurchmesser. Um zu höheren Düsennadelgeschwindigkeiten zu kommen, was besonders beim Nadelschließen wichtig ist, muss der Düsennadeldurchmesser reduziert werden. Für eine Schließgeschwindigkeit von 1 m/sec ist bei einer akzeptablen Steuermenge ein Nadeldurchmesser von unter 3 , 5 mm nötig. Das ist technisch sehr aufwendig und daher teuer. Gemäß der vorliegenden Erfindung kann derInstall spring stiffness that ensures good closing of the nozzle needle. In this way, the injection time and the injection time can be precisely defined. In addition, the control room can be made very small, which leads to a quick response of the injector according to the invention. There is also a relationship between the maximum achievable nozzle needle speed and the nozzle needle diameter. In order to achieve higher nozzle needle speeds, which is particularly important when closing the needle, the nozzle needle diameter must be reduced. A needle diameter of less than 3.5 mm is necessary for a closing speed of 1 m / sec with an acceptable control quantity. This is technically very complex and therefore expensive. According to the present invention, the
Düsennadeldurchmesser frei gewählt werden und ist nicht abhängig von den Abmessungen der Düsenfeder. Im Vergleich zu herkömmlichen Düsennadeln kann die Länge erheblich reduziert werden, was zu einem exakten Hubanschlag beiträgt.Nozzle needle diameter can be chosen freely and is not dependent on the dimensions of the nozzle spring. The length can be considerably reduced compared to conventional nozzle needles, which contributes to an exact stroke stop.
Eine besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass an der Fläche der Hülse, die sich in Anlage an dem Injektorgehäuse befindet, eine Beißkante ausgebildet ist. Dadurch wird erreicht, dass der im Inneren der Hülse ausgebildete Steuerraum von dem die Hülse umgebenden Düsenfederraum getrennt bleibt.A special embodiment of the invention is characterized in that a biting edge is formed on the surface of the sleeve which is in contact with the injector housing. It is thereby achieved that the control chamber formed in the interior of the sleeve surrounding nozzle spring chamber remains separate.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Innendurchmesser der Hülse kleiner als oder gleich einem Führungsdurchmesser an der Düsennadel ist. Je kleiner das Steuerraumvolumen gewählt werden kann, desto reaktionsfreudiger ist der Injektor. Gemäß der vorliegenden Erfindung können der Innendurchmesser der Hülse und der entsprechende Außendurchmesser an der Düsennadel viel kleiner ausgeführt werden als bei herkömmlichen Injektoren.Another special embodiment of the invention is characterized in that the inner diameter of the sleeve is less than or equal to a guide diameter on the nozzle needle. The smaller the control room volume can be selected, the more responsive the injector is. According to the present invention, the inner diameter of the sleeve and the corresponding outer diameter on the nozzle needle can be made much smaller than in conventional injectors.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Kraftstoffzulauf über den Düsenfederraum mit dem Druckraum in Verbindung steht und dass die Düsennadel zwischen dem Düsenfederraum und dem Druckraum geführt ist. Das liefert den Vorteil, dass der Düsennadelführung keine Dichtfunktion mehr zukommt. Damit werden die Anforderungen an die Qualität der Führung geringer, was zu Einsparungen in der Fertigung führt. Weil auf beiden Seiten der Führung der gleiche Druck herrscht, tritt keine Führungsleckage mehr auf.A further special embodiment of the invention is characterized in that the fuel supply is connected to the pressure chamber via the nozzle spring chamber and that the nozzle needle is guided between the nozzle spring chamber and the pressure chamber. This provides the advantage that the nozzle needle guide no longer has a sealing function. This reduces the demands on the quality of the management, which leads to savings in production. Because there is the same pressure on both sides of the guide, there is no longer any guide leakage.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Düsenfederraum über eineAnother special embodiment of the invention is characterized in that the nozzle spring chamber has a
Bohrung mit dem Druckraum in Verbindung steht. Dadurch kann der komplette Umfang der Düsennadel zu Führungszwecken benutzt werden.Bore communicates with the pressure chamber. As a result, the entire circumference of the nozzle needle can be used for guidance purposes.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass an der Düsennadel zwischen dem Düsenfederraum und dem Druckraum mindestens eine ebene Fläche ausgebildet ist, an der vorbei Kraftstoff von dem Düsenfederraum in den Druckraum gelangen kann. Diese Ausführungsart bietet insbesondere in Bezug auf die Hochdruckfestigkeit Vorteile. Weitere besondere Ausführungsarten der Erfindung sind dadurch gekennzeichnet, dass die Zulaufdrossel in die Düsennadel, die Hülse oder das Injektorgehäuse integriert ist. Die Zulaufdrossel dient dazu, Druckstöße im Betrieb zu verhindern.A further special embodiment of the invention is characterized in that at least one flat surface is formed on the nozzle needle between the nozzle spring chamber and the pressure chamber, which fuel can pass from the nozzle spring chamber into the pressure chamber. This type of construction offers advantages in particular with regard to high-pressure strength. Further special embodiments of the invention are characterized in that the inlet throttle is integrated in the nozzle needle, the sleeve or the injector housing. The inlet throttle serves to prevent pressure surges during operation.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass die Hülse an ihrem brennraumfe en Ende einen Bund aufweist. Der Bund bildet ein erstes Widerlager für die Düsenfeder.A further special embodiment of the invention is characterized in that the sleeve has a collar at its combustion chamber end. The collar forms a first abutment for the nozzle spring.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass an der Düsennadel eine Stufe ausgebildet ist, die einen Anschlag für einen Federteller bildet. Der Federteller bildet ein zweites Widerlager für die Düsenfeder.Another particular embodiment of the invention is characterized in that a step is formed on the nozzle needle, which step forms a stop for a spring plate. The spring plate forms a second abutment for the nozzle spring.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass in der Düsennadel eine Umfangsnut ausgespart ist, in der sich ein Haltering abstützt, der einen Anschlag für einen Federteller bildet. Bei dieser Ausführungsart können der Außendurchmesser der Düsennadel im Steuerraum und der Führungsdurchmesser der Düsennadel zwischen dem Düsenfederraum und dem Druckraum gleich groß sein. Das ist bei der Fertigung, z.B. durchAnother special embodiment of the invention is characterized in that a circumferential groove is recessed in the nozzle needle, in which a retaining ring is supported, which forms a stop for a spring plate. In this embodiment, the outer diameter of the nozzle needle in the control chamber and the guide diameter of the nozzle needle between the nozzle spring chamber and the pressure chamber can be the same size. This is in manufacturing, e.g. by
Läppen, von Vorteil.Lapping is an advantage.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Haltering zweiteilig ist und in zusammengebautem Zustand durch den Federteller fixiert wird. Dadurch wird in einfacher Art und Weise ein Lösen des Federtellers im Betrieb verhindert.Another special embodiment of the invention is characterized in that the retaining ring is in two parts and is fixed in the assembled state by the spring plate. This prevents the spring plate from loosening in operation in a simple manner.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Düsennadelhub durch den Abstand zwischen der Hülse und dem Federteller definiert ist . Dieser rein mechanische Düselnadelhubendanschlag liefert den Vorteil, dass der Düsennadelhub exakt reproduzierbar ist. Dadurch kann der Einspritzverlauf zuverlässig geformt' erden. Ein sogenanntes hydraulisches Kleben wird vermieden.Another special embodiment of the invention is characterized in that the nozzle needle stroke is defined by the distance between the sleeve and the spring plate is. This purely mechanical nozzle needle stroke end stop provides the advantage that the nozzle needle stroke is exactly reproducible. This can reliably shaped ground 'of the injection process. So-called hydraulic gluing is avoided.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Düsennadelhub und die Düsenfedervorspannung mit Hilfe von Distanzelementen einstellbar sind, die zwischen dem Federteller und demAnother special embodiment of the invention is characterized in that the nozzle needle stroke and the nozzle spring preload can be adjusted with the aid of spacer elements which are located between the spring plate and the
Anschlag für den Federteller bzw. zwischen der Düsenfeder und den Widerlagern für die Düsenfeder angeordnet sind. Dadurch kann das Schließverhalten des Injektors verbessert werden.Stop for the spring plate or between the nozzle spring and the abutments for the nozzle spring are arranged. The closing behavior of the injector can thereby be improved.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass der Düsennadelhub durch den Abstand zwischen der brennraumfemen Stirnfläche der Düsennadel und dem Injektorgehäuse definiert ist. Diese Ausführungsart hat den Vorteil, dass sie fertigungstechnisch besonders einfach zu realisieren ist.Another special embodiment of the invention is characterized in that the nozzle needle stroke is defined by the distance between the end surface of the nozzle needle remote from the combustion chamber and the injector housing. This embodiment has the advantage that it is particularly easy to implement in terms of production technology.
Eine weitere besondere Ausführungsart der Erfindung ist dadurch gekennzeichnet, dass in der brennraumfemen Stirnfläche der Düsennadel und/oder in der gegenüberliegenden Fläche des Injektorgehäuses Ausnehmungen vorgesehen sind, deren Abmessungen an das Volumen des Steuerraums angepasst sind. Um im Betrieb des Injektors ein möglichst lineares Mengenkennfeld zu erzielen, ist es sinnvoll, den Düsennadelhubanschlag nicht rein hydraulisch auszuführen. Bei einem rein hydraulischen Düsennadelhubanschlag kann es vorkommen, dass die Düsennadel in der geöffneten Stellung auf einem Druckpolster "schwebt" . Das kann zu Schwingungen der Düsennadel führen. Die Schwingungen wiederum ergeben nichtlineare Mengenkennfeider . Da es sich hierbei um eine oA further special embodiment of the invention is characterized in that recesses are provided in the end surface of the nozzle needle remote from the combustion chamber and / or in the opposite surface of the injector housing, the dimensions of which are adapted to the volume of the control chamber. In order to achieve a quantity map that is as linear as possible during operation of the injector, it makes sense not to carry out the nozzle needle stroke stop purely hydraulically. In the case of a purely hydraulic nozzle needle stroke stop, it can happen that the nozzle needle "floats" on a pressure cushion in the open position. This can cause the nozzle needle to vibrate. The vibrations in turn result in non-linear quantity indicators. Since this is a O
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Fig. 1 ein erstes Ausführungsbeispiel im Längsschnitt durch den Injektor mit einer Bohrung zwischen dem Düsenfederraum und dem Druckraum;Figure 1 shows a first embodiment in longitudinal section through the injector with a bore between the nozzle spring chamber and the pressure chamber.
Fig. 2 ein zweites Ausführungsbeispiel im Längsschnitt durch den Injektor mit einer Abflachung an der Düsennadel zwischen dem Düsenfederraum und dem Druckraum;Figure 2 shows a second embodiment in longitudinal section through the injector with a flattening on the nozzle needle between the nozzle spring chamber and the pressure chamber.
Fig. 3 ein weiteres Ausführungsbeispiel im Längsschnitt durch den Injektor, wobei die Zulaufdrossel in die Düsennadel oder in das Injektorgehäuse integriert ist;3 shows a further exemplary embodiment in a longitudinal section through the injector, the inlet throttle being integrated in the nozzle needle or in the injector housing;
Fig. 4 ein weiteres Ausführungsbeispiel im Längsschnitt durch den Injektor, wobei der Führungsdurchmesser gleich dem Steuerdurchmesser ist;4 shows a further embodiment in longitudinal section through the injector, the guide diameter being equal to the control diameter;
Fig. 5 eine Variante des in Fig. 4 dargestellten Ausführungsbeispiels mit einem zweiteiligenFig. 5 shows a variant of the embodiment shown in Fig. 4 with a two-part
Haltering;Retaining ring;
Fig. 6 die Ansicht eines Schnitts entlang der Linie VI- VI in Fig. 5;Fig. 6 is a sectional view taken along the line VI-VI in Fig. 5;
Fig. 7 ein weiteres Ausführungsbeispiel im Längsschnitt durch den Injektor mit Distanzelementen zur Einstellung des Düsennadelhubs und der Düsenfedervorspannkraft;7 shows a further embodiment in longitudinal section through the injector with spacer elements for setting the nozzle needle stroke and the nozzle spring pretensioning force;
Fig. 8 ein weiteres Ausführungsbeispiel im Längsschnitt durch den Injektor mit Kreuznuten in der brennraumfemen Stirnfläche der Düsennadel;8 shows a further exemplary embodiment in longitudinal section through the injector with cross grooves in the end face of the nozzle needle remote from the combustion chamber;
Fig. 9 die brennraumferne Stirnfläche der Düsennadel ausFig. 9 from the combustion chamber end face of the nozzle needle
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Beißkante 29 gegen den Ventilkörper 3 gedrückt. Dadurch wird ein im Inneren der Hülse 28 vorgesehener Steuerraum 30, der durch die brennraumferne Stirnfläche der Düsennadel 8 begrenzt ist, gegenüber dem Düsenfederraum 20 abgedichtet .Biting edge 29 pressed against the valve body 3. As a result, a control chamber 30 which is provided in the interior of the sleeve 28 and is delimited by the end face of the nozzle needle 8 remote from the combustion chamber is sealed off from the nozzle spring chamber 20.
Der Steuerraum 30 ist über eine Zulaufdrossel 31 mit dem Düsenfederraum 20 verbunden. Außerdem steht der Steuerraum 30 über eine Ablaufdrossel 32 mit einem (nicht dargestellten) Entlastungsraum in Verbindung. DieThe control chamber 30 is connected to the nozzle spring chamber 20 via an inlet throttle 31. In addition, the control chamber 30 is connected to a relief chamber (not shown) via an outlet throttle 32. The
Verbindung des Steuerraums 30 mit dem Entlastungsraum hängt von der Stellung eines Steuerventilgliedes 33 ab.Connection of the control chamber 30 to the relief chamber depends on the position of a control valve member 33.
Der in Fig. 1 dargestellte Injektor funktioniert wie folgtThe injector shown in Fig. 1 works as follows
Über den Kraftstoffzulauf 21 gelangt mit Hochdruck beaufschlagter Kraftstoff in den Düsenfederraum 20. Von dort gelangt der mit Hochdruck beaufschlagte Kraftstoff einerseits über die Zulaufdrossel 31 in den Steuerraum 30 und andererseits über die Bohrung 23 in den Druckraum 24. Die Durchmesserverhältnisse sind in bekannter Weise so gewählt, dass sich die Düsennadel 8 infolge des Hochdruckes in dem Steuerraum 30 mit ihrer Spitze 9 in Anlage an dem Düsennadelsitz befindet. Wenn das Steuerventilglied 33 öffnet, wird der Steuerraum 30 druckentlastet, und die Düsennadelspitze 9 hebt von ihrem Sitz ab. Dann wird so lange mit Hochdruck beaufschlagter Kraftstoff durch die Spritzlöcher 10 und 11 in den Brennraum der Brennkraftmaschine eingespritzt, bis das Steuerventilglied 33 wieder schließt. Das hat dann zur Folge, dass der Druck in dem Steuerraum 30 wieder ansteigt und die Düsennadel 8 mit ihrer Spitze 9 wieder gegen den zugehörigen Düsennadelsitz gedrückt wird.High-pressure fuel reaches the nozzle spring chamber 20 via the fuel inlet 21. From there, the high-pressure fuel reaches the control chamber 30 via the inlet throttle 31 and the pressure chamber 24 via the bore 23. The diameter ratios are selected in a known manner that the nozzle needle 8 is due to the high pressure in the control chamber 30 with its tip 9 in contact with the nozzle needle seat. When the control valve member 33 opens, the control chamber 30 is relieved of pressure and the nozzle needle tip 9 lifts off its seat. High-pressure fuel is then injected into the combustion chamber of the internal combustion engine through the spray holes 10 and 11 until the control valve member 33 closes again. This then has the consequence that the pressure in the control chamber 30 rises again and the nozzle needle 8 is pressed with its tip 9 again against the associated nozzle needle seat.
Das in Fig. 2 dargestellte zweite Ausführungsbeispiel entspricht weitestgehend dem in Fig. 1 dargestellten ersten o rHThe second exemplary embodiment shown in FIG. 2 largely corresponds to the first illustrated in FIG. 1 o rH
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Bei dem in den Fig. 8 und 9 dargestellten Ausführungsbeispiel sind in der Stirnfläche 54 der Düsennadel 8 zwei Nuten 55 und 56 kreuzweise angeordnet. Dadurch wird ein rein mechanischer Anschlag der Nadeldüse realisiert. Wenn die Abmessungen der Nuten 54 und 55 an den Injektor angepasst werden, kann daraus ein "halbhydraulischer Anschlag" werden. Der beim Anschlag verbleibende Durchbruchsquerschnitt wird gerade so groß gewählt, dass eine Schwingung der Düsennadel 8 zwar vermieden, die Steuermenge beim Endanschlag jedoch so weit wie möglich abgesenkt wird.In the embodiment shown in FIGS. 8 and 9, two grooves 55 and 56 are arranged crosswise in the end face 54 of the nozzle needle 8. A purely mechanical stop of the needle nozzle is thereby achieved. If the dimensions of the grooves 54 and 55 are adapted to the injector, this can become a "semi-hydraulic stop". The breakthrough cross section remaining at the stop is chosen to be just large enough to prevent the nozzle needle 8 from oscillating, but to reduce the amount of control at the end stop as much as possible.
Bei dem in Fig. 10 dargestellten Ausführungsbeispiel ist in der Stirnfläche 54 der Düsennadel 8 eine Drosselbohrung 58 parallel zur Längsachse der Düsennadel 8 angeordnet. DieIn the embodiment shown in FIG. 10, a throttle bore 58 is arranged in the end face 54 of the nozzle needle 8 parallel to the longitudinal axis of the nozzle needle 8. The
Drosselbohrung 58 mündet in eine Bohrung 59, die sich quer zur Längsachse der Düsennadel 8 erstreckt. Bei der Bohrung 59 handelt es sich um eine Sackbohrung, die zu dem brennraumfemen, kegelstumpfartigen Ende der Düsennadel 8 hin geöffnet ist. Dieses Ausführungsbeispiel hat denThrottle bore 58 opens into a bore 59 which extends transversely to the longitudinal axis of the nozzle needle 8. The bore 59 is a blind bore which is open towards the end of the nozzle needle 8 which is distant from the combustion chamber and is frustoconical. This embodiment has the
Vorteil, dass es unempfindlich gegen mechanisches Einlaufen ist.Advantage that it is insensitive to mechanical break-in.
Bei dem in Fig. 11 dargestellten Ausführungsbeispiel ist eine Nut 61 anstatt in der brennraumfemen Stirnfläche 54 der Düsennadel 8 in der gegenüberliegenden Fläche 62 des Ventilkörpers 3 ausgespart. Die Nut 61 hat die gleiche Funktion wie die Nuten 54 und 55 bei dem in den Fig. 8 und 9 dargestellten Ausführungsbeispiel. In the exemplary embodiment shown in FIG. 11, a groove 61 is cut out in the opposite surface 62 of the valve body 3 instead of in the end face 54 of the nozzle needle 8 remote from the combustion chamber. The groove 61 has the same function as the grooves 54 and 55 in the embodiment shown in FIGS. 8 and 9.

Claims

Ansprüche Expectations
1. Common-Rail-Injektor zur Einspritzung von Kraftstoff in einem Common-Rail-Einstpritzsystem einer Brennkraftmaschine, der ein Injektorgehäuse (1) mit einem KraftstoffZulauf (21) aufweist, der mit einem zentralen Kraftstoffhochdruckspeicher außerhalb des Injektorgehäuses (1) und mit einem Druckraum (24) innerhalb des1. Common rail injector for the injection of fuel in a common rail injection system of an internal combustion engine, which has an injector housing (1) with a fuel inlet (21), which has a central high-pressure fuel reservoir outside the injector housing (1) and with a pressure chamber (24) within the
Injektorgehäuses (1) in Verbindung steht, aus dem mit Hochdruck beaufschlagter Kraftstoff in Abhängigkeit von der Stellung eines Steuerventils (33) eingespritzt wird, das dafür sorgt, dass eine in einer Längsbohrung (6) des Injektors axial gegen die Vorspannkraft einer DüsenfederIs connected to the injector housing (1), from which high-pressure fuel is injected depending on the position of a control valve (33), which ensures that a longitudinal bore (6) of the injector axially against the biasing force of a nozzle spring
(19), die in einem Düsenfederraum (20) aufgenommen ist, hin und her bewegbare Düsennadel (8) von einem Sitz abhebt, wenn der Druck in dem Druckraum (24) größer als der Druck in einem Steuerraum (30) ist, der über eine Zulaufdrossel (31, 38, 39) mit dem Kraftstoffzulauf verbunden ist, dadurch gekennzeichnet, dass der Steuerraum (30) von einer Hülse (28) begrenzt ist, die unter Dichtwirkung an dem brennraumfemen Ende der Düsennadel (8) verschiebbar ist und mit Hilfe der Düsenfeder (19) in Anlage an das Injektorgehäuse (1) gehalten wird.(19), which is accommodated in a nozzle spring chamber (20), lifts the reciprocating nozzle needle (8) from a seat when the pressure in the pressure chamber (24) is greater than the pressure in a control chamber (30) which is above An inlet throttle (31, 38, 39) is connected to the fuel inlet, characterized in that the control chamber (30) is delimited by a sleeve (28) which can be displaced under the sealing effect on the end of the nozzle needle (8) remote from the combustion chamber and with the aid the nozzle spring (19) is held in contact with the injector housing (1).
2. Common-Rail-Injektor nach Anspruch 1, dadurch gekennzeichnet, dass an der Fläche der Hülse (28) , die sich in Anlage an dem Injektorgehäuse (1) befindet, eine Beißkante (29) ausgebildet ist. 2. Common rail injector according to claim 1, characterized in that a biting edge (29) is formed on the surface of the sleeve (28) which is in contact with the injector housing (1).
3. Common-Rail-Injektor nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Innendurchmesser (d3) der Hülse (28) kleiner als oder gleich einem Führungsdurchmesser (d2) an der Düsennadel (8) ist.3. Common rail injector according to one of the preceding claims, characterized in that the inner diameter (d 3 ) of the sleeve (28) is less than or equal to a guide diameter (d 2 ) on the nozzle needle (8).
4. Common-Rail-Injektor nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der4. Common rail injector according to one of the preceding claims, characterized in that the
Kraftstoffzulauf (21) über den Düsenfederraum (20) mit dem Druckraum (24) in Verbindung steht, und dass die Düsennadel (8) zwischen dem Düsenfederraum (20) und dem Druckraum (24) geführt ist.Fuel inlet (21) is connected to the pressure chamber (24) via the nozzle spring chamber (20), and that the nozzle needle (8) is guided between the nozzle spring chamber (20) and the pressure chamber (24).
5. Common-Rail-Injektor nach Anspruch 4, dadurch gekennzeichnet, dass der Düsenfederraum (20) über eine5. Common rail injector according to claim 4, characterized in that the nozzle spring chamber (20) via a
Bohrung (23) mit dem Druckraum (24) in Verbindung steht.Bore (23) communicates with the pressure chamber (24).
6. Common-Rail-Injektor nach Anspruch 4, dadurch gekennzeichnet, dass an der Düsennadel (8) zwischen dem Düsenfederraum (20) und dem Druckraun (24) mindestens eine ebene Fläche (36) ausgebildet ist, an der vorbei Kraftstoff von dem Düsenfederraum (20) in den Druckraum (24) gelangen kann.6. Common rail injector according to claim 4, characterized in that on the nozzle needle (8) between the nozzle spring chamber (20) and the pressure chamber (24) at least one flat surface (36) is formed, past the fuel from the nozzle spring chamber (20) can get into the pressure chamber (24).
7. Common-Rail-Injektor nach einem der vorhergehenden7. Common rail injector according to one of the preceding
Ansprüche, dadurch gekennzeichnet, dass die Zulaufdrossel (31, 38, 39) in die Hülse (28) , die Düsennadel (8) oder das Injektorgehäuse (1) integriert ist.Claims, characterized in that the inlet throttle (31, 38, 39) is integrated in the sleeve (28), the nozzle needle (8) or the injector housing (1).
8. Common-Rail-Injektor nach einem der vorhergehenden8. Common rail injector according to one of the preceding
Ansprüche, dadurch gekennzeichnet, dass die Hülse (28) an ihrem brennraumfemen Ende einen Bund (29) aufweist.Claims, characterized in that the sleeve (28) has a collar (29) at its end remote from the combustion chamber.
9. Common-Rail-Injektor nach einem der vorhergehendne Ansprüche, dadurch gekennzeichnet, dass an der Düsennadel (8) eine Stufe ausgebildet ist, die einen Anschlag für einen Federteller (26) bildet.9. Common rail injector according to one of the preceding claims, characterized in that a step is formed on the nozzle needle (8), which has a stop for forms a spring plate (26).
10. Common-Rail-Injektor nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass in der Düsennadel (8) eine Umfangsnut ausgespart ist, in der sich ein Haltering (42,10. Common rail injector according to one of claims 1 to 8, characterized in that in the nozzle needle (8) a circumferential groove is recessed in which a retaining ring (42,
46) abstützt, der einen Anschlag für einen Federteller (26) bildet.46) which forms a stop for a spring plate (26).
11. Common-Rail-Injektor nach Anspruch 10, dadurch gekennzeichnet, dass der Haltering (46) zweiteilig ist und in zusammengebautem Zustand durch den Federteller (26) fixiert wird.11. Common rail injector according to claim 10, characterized in that the retaining ring (46) is in two parts and is fixed in the assembled state by the spring plate (26).
12. Common-Rail-Injektor nach einem der Ansprüche 9 bis 11, dadurch gekennzeichnet, dass der Düsennadelhub (H2) durch den Abstand zwischen der Hülse (28) und dem Federteller (26) definiert ist.12. Common rail injector according to one of claims 9 to 11, characterized in that the nozzle needle stroke (H 2 ) is defined by the distance between the sleeve (28) and the spring plate (26).
13. Common-Rail-Injektor nach einem der Ansprüche 9 bis 12, dadurch gekennzeichnet, dass der Düsennadelhub (H2) und die Düsenfedervorspannung mit Hilfe von Distanzelementen (50, 51) einstellbar sind, die zwischen dem Federteller (26) und dem Anschlag für den Federteller bzw. zwischen der Düsenfeder (19) und den Widerlagern für die Düsenfeder (19) angeordnet sind.13. Common rail injector according to one of claims 9 to 12, characterized in that the nozzle needle stroke (H 2 ) and the nozzle spring preload are adjustable with the aid of spacer elements (50, 51) which are between the spring plate (26) and the stop are arranged for the spring plate or between the nozzle spring (19) and the abutments for the nozzle spring (19).
14. Common-Rail-Injektor nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Düsennadelhub14. Common rail injector according to one of the preceding claims, characterized in that the nozzle needle stroke
(H durch den Abstand zwischen der brennraumfe en Stirnfläche (54) der Düsennadel (8) und dem Injektorgehäuse(H by the distance between the end face (54) of the nozzle needle (8) and the injector housing
(1) definiert ist.(1) is defined.
15. Common-Rail-Injektor nach Anspruch 14, dadurch gekennzeichnet, dass in der brennraumfemen Stirnfläche (54) der Düsennadel (8) und/oder in der gegenüberliegenden Fläche (62) des Injektorgehäuses (1) Ausnehmungen (55, 56; 61) vorgesehen sind, deren Abmessungen an das Volumen des Steuerraums (30) angepasst sind.15. Common rail injector according to claim 14, characterized in that in the combustion chamber-remote end face (54) of the nozzle needle (8) and / or in the opposite surface (62) of the injector housing (1) recesses (55, 56; 61) are provided, the dimensions of which are adapted to the volume of the control chamber (30).
16. Common-Rail-Injektor nach Anspruch 14, dadurch gekennzeichnet, dass in der brennraumfemen Stirnfläche16. Common rail injector according to claim 14, characterized in that in the combustion chamber remote end face
(54) der Düsennadel (8) mindestens eine axiale Bohrung (58) vorgesehen ist, die mit mindestens einer radialen Bohrung(54) of the nozzle needle (8) at least one axial bore (58) is provided, which has at least one radial bore
(59) in der Düsennadel (8) in Verbindung steht. (59) in the nozzle needle (8) is connected.
EP00958210A 1999-08-04 2000-08-02 Common rail injector Expired - Lifetime EP1117920B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP06123003A EP1772618B1 (en) 1999-08-04 2000-08-02 Common rail injector

Applications Claiming Priority (3)

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DE19936668 1999-08-04
DE19936668A DE19936668A1 (en) 1999-08-04 1999-08-04 Common rail injector
PCT/DE2000/002580 WO2001011222A1 (en) 1999-08-04 2000-08-02 Common rail injector

Related Child Applications (1)

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EP1117920A1 true EP1117920A1 (en) 2001-07-25
EP1117920B1 EP1117920B1 (en) 2007-02-28

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EP (2) EP1772618B1 (en)
JP (1) JP4746230B2 (en)
KR (1) KR20010075570A (en)
AT (2) ATE413526T1 (en)
CZ (1) CZ20011135A3 (en)
DE (3) DE19936668A1 (en)
WO (1) WO2001011222A1 (en)

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WO2001011222A1 (en) 2001-02-15
CZ20011135A3 (en) 2002-01-16
DE50014113D1 (en) 2007-04-12
US6705551B1 (en) 2004-03-16
EP1772618B1 (en) 2008-11-05
KR20010075570A (en) 2001-08-09
ATE355455T1 (en) 2006-03-15
JP4746230B2 (en) 2011-08-10
ATE413526T1 (en) 2008-11-15
DE19936668A1 (en) 2001-02-22
EP1772618A1 (en) 2007-04-11
JP2003506622A (en) 2003-02-18
DE50015444D1 (en) 2008-12-18
EP1117920B1 (en) 2007-02-28

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