EP1598551B1 - Fuel injection device - Google Patents

Fuel injection device Download PDF

Info

Publication number
EP1598551B1
EP1598551B1 EP05101652A EP05101652A EP1598551B1 EP 1598551 B1 EP1598551 B1 EP 1598551B1 EP 05101652 A EP05101652 A EP 05101652A EP 05101652 A EP05101652 A EP 05101652A EP 1598551 B1 EP1598551 B1 EP 1598551B1
Authority
EP
European Patent Office
Prior art keywords
throttle
pressure
fuel
fuel injection
injection device
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.)
Not-in-force
Application number
EP05101652A
Other languages
German (de)
French (fr)
Other versions
EP1598551A1 (en
Inventor
Hans-Christoph Magel
Dirk Vahle
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
Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP1598551A1 publication Critical patent/EP1598551A1/en
Application granted granted Critical
Publication of EP1598551B1 publication Critical patent/EP1598551B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/022Injectors structurally combined with fuel-injection pumps characterised by the pump drive
    • F02M57/025Injectors structurally combined with fuel-injection pumps characterised by the pump drive hydraulic, e.g. with pressure amplification
    • 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
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0014Valves characterised by the valve actuating means
    • F02M63/0015Valves characterised by the valve actuating means electrical, e.g. using solenoid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0014Valves characterised by the valve actuating means
    • F02M63/0028Valves characterised by the valve actuating means 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0049Combined valve units, e.g. for controlling pumping chamber and injection valve

Definitions

  • the invention relates to a device for injecting fuel into a combustion chamber of an internal combustion engine, with a fuel injector which can be acted upon by a high-pressure source with high-pressure fuel and actuated via a metering valve, through which the pressure in an injection valve member control chamber is controlled so that a Injector member for injecting fuel opens and closes.
  • a device for injecting fuel into a combustion chamber of an internal combustion engine having a fuel injector which can be acted upon by a high-pressure shaft with high-pressure fuel and actuated via a metering valve.
  • An injection valve member which is acted upon in the closing direction by a closing force, is enclosed by a pressure chamber.
  • the injection valve member associated with a independently movable damping element which defines a damping space and at least one overflow channel for connecting the damping chamber with a further hydraulic space.
  • the damping element may be formed as a damping piston, which is surrounded by the other hydraulic space.
  • a device for injecting fuel into a combustion chamber of an internal combustion engine with a fuel injector in which the injection pressure of the fuel injector is increased by means of a pressure booster by a pressure booster control chamber via a control line is depressurized and the pressure in a nozzle needle control chamber via an outlet throttle and emptied over an inlet throttle device can be filled.
  • the pressure booster control chamber and the nozzle needle control chamber are connected via a hydraulic connection.
  • the pressure booster control chamber is controlled by a first metering valve and the nozzle needle control chamber by a second metering valve.
  • the object of the invention is to provide a device for injecting fuel into a combustion chamber of an internal combustion engine having a fuel injector which can be acted upon by a high-pressure source with high-pressure fuel, in which the injection pressure is amplified by a hydraulic pressure booster in the fuel injector.
  • the device should work reliably, be simple and inexpensive to produce.
  • the object of the invention is achieved in that the nozzle needle control chamber can be emptied via an outlet throttle device and an inlet throttle device, wherein the pressure booster control chamber and the nozzle needle control chamber are connected via a hydraulic connection, wherein the hydraulic connection between the pressure booster control chamber and nozzle needle control chamber contains a second control line, wherein the nozzle needle control chamber via the outlet throttle in the second control line can be emptied and filled via the inlet throttle from the second control line, and wherein the throttle cross section of the outlet throttle is smaller than the throttle cross section of the inlet throttle.
  • the outlet throttle device allows a slow opening of the injection valve member.
  • the inlet throttle allows a fast closing of the injection valve member.
  • the slow opening of the injection valve member improves the minimum quantity capability of the fuel injection device.
  • the rapid closing of the injection valve member improves the emission values of the internal combustion engine.
  • the two separate throttle devices provide the advantage that opening and closing speed of the injection valve member are independently adjustable.
  • a preferred embodiment of the fuel injection device is characterized in that a valve element is provided, which is closed when the injection valve member control chamber is emptied, and which is open when the injection valve member control chamber is filled.
  • a further preferred exemplary embodiment of the fuel injection device is characterized in that one of the throttle devices, in particular the outlet throttle device, develops its throttling action only when the injection valve member control chamber is emptied and no throttling action develops during filling of the injection valve member control chamber, but an unimpeded passage guaranteed by fuel. As a result, the closing of the injection valve member is accelerated.
  • a further preferred embodiment of the fuel injection device is characterized in that the two throttle devices are connected in series. As a result, a simple construction is made possible, which is economically feasible in terms of manufacturing technology.
  • a further preferred exemplary embodiment of the fuel injection device is characterized in that the two throttle devices are arranged centrally with respect to the longitudinal axis of the fuel injector. This arrangement provides manufacturing advantages, since both throttle bodies can be edited in the middle.
  • a further preferred embodiment of the fuel injection device is characterized in that the outlet throttle device comprises a throttle element with a sealing edge which is biased by a spring element so that the sealing edge is pressed against an associated sealing seat when the throttle element is flowed through in the discharge direction, and so in that the sealing edge lifts off from its sealing seat when the throttle element is flowed through in the filling direction.
  • the combination of a throttle with a check valve enables a compact design with a shortened fuel injector length.
  • a further preferred embodiment of the fuel injection device is characterized in that the throttle element comprises a biased by the spring element and equipped with a throttle point having a throttle hole throttle piston whose free end forms a stroke stop for the injection valve member. This prevents the pressure in the injection valve member control chamber from falling too much after the injection valve member has been opened.
  • a further preferred embodiment of the fuel injection device is characterized in that the stroke stop of the nozzle needle is designed so that a first sealing seat and a second sealing seat are closed when the combustion chamber remote end of the nozzle needle comes to rest on the throttle piston. This prevents that when the nozzle needle is open, the pressure on the inside of a sealing sleeve in an annular space between the throttle piston and the sealing sleeve drops too much. As a result, an undesirably large deformation of the sealing sleeve can be prevented.
  • a further preferred embodiment of the fuel injection device is characterized in that the nozzle needle comes into abutment in its upper stroke stop with its end remote from the combustion chamber at a sealing edge, which is formed on an injector housing portion. This prevents that after needle opening, the pressure on the inside of a sealing sleeve drops too much, so that an undesirably large deformation of the sealing sleeve is prevented.
  • a further preferred embodiment of the fuel injection device is characterized in that the two throttle devices are connected in parallel. This arrangement provides advantages in the operation of the fuel injector.
  • a further preferred embodiment of the fuel injection device is characterized in that the outlet throttle device comprises a throttle element, which is connected in series with a check valve, that the throttle element is flowed through in one direction, in particular the filling direction, and is closed in the discharge direction.
  • This structure is manufacturing technology particularly easy to implement.
  • a further preferred embodiment of the fuel injection device is characterized in that the inlet throttle device is arranged off-center relative to the longitudinal axis of the fuel injector. As a result, the inlet throttle device can be assigned a larger pressure-loaded surface, which allows a faster closing of the injection valve member.
  • a further preferred exemplary embodiment of the fuel injection device is characterized in that the outlet throttle device is arranged centrally with respect to the longitudinal axis of the fuel injector is.
  • the central arrangement simplifies the processing of the throttle point during production.
  • the present invention relates to an injector with pressure booster or pressure booster and the control of the pressure booster via the rear space.
  • the description of the device according to the invention for damping the lifting movement of an injection valve member is based on a fuel injector with pressure booster.
  • the proposed device for damping the lifting movement in particular with regard to a reduction of its opening speed, can also be used on other fuel injection systems, such as pump-nozzle systems and pump-line-nozzle systems, distribution injection systems and also high-pressure accumulator injection systems, the fuel injector none Take pressure translation.
  • FIG. 1 is a longitudinal section through a common rail injector 1 shown, which is supplied via an only schematically indicated pressure accumulator space 2 (common rail) with fuel under high pressure.
  • a fuel supply line 3, 4 extends to a pressure booster 5, which is integrated into the fuel injector 1.
  • the pressure booster 5 is enclosed by an injector housing (not shown).
  • the injector housing includes an injector body and a nozzle body having a central guide bore. In the guide bore, a nozzle needle 10 is guided back and forth movable.
  • the nozzle needle 10 has a tip 11, on which a sealing surface is formed, which cooperates with a sealing seat, which is formed on the nozzle body.
  • a pressure chamber 15 is formed, which communicates via a connecting channel 18 with a pressure booster chamber 22 in connection.
  • the pressure booster chamber 22 is supplied with high-pressure fuel, which is further compressed in response to the pressure in a pressure booster control chamber 23.
  • one end 24 of a pressure booster piston 25 protrudes into the pressure booster chamber 22.
  • the end 24 of the pressure booster piston 25 has substantially the shape of a circular cylinder whose outer diameter is smaller than the outer diameter of the section 25 of the pressure booster piston.
  • a pressure booster spring 27 is arranged, by means of which the pressure booster piston 25 is biased in the direction of the nozzle needle 10 away.
  • the pressure booster control chamber 23 communicates via a connecting channel 29 with a 3/2-way valve 32 in connection, which in turn communicates via a connecting channel 34 and the fuel supply lines 3,4 with the high-pressure accumulator chamber 2.
  • the 3/2-way valve 32 has a port 35 to a fuel tank (not shown).
  • the pressure booster control chamber 23 via the connection channels or connecting lines 29, 34, 3 and 4 with the high-pressure fuel storage chamber 2 in connection.
  • the pressure booster chamber 22 communicates with the pressure booster control chamber 23.
  • the check valve 40 has a check ball, which is biased for example by means of a check valve spring against a check valve seat that the pressure booster chamber 22 is filled via the connecting lines 41, 29, 34, 3 and 4 from the high-pressure fuel reservoir 2 with fuel when the Pressure in the booster chamber 22 is smaller than in the high-pressure fuel chamber 2.
  • the pressure booster chamber 22 communicates via a connecting line 42 with a nozzle needle control chamber 44, which is also referred to as a damping chamber.
  • the nozzle needle control chamber 44 is bounded at the top by a portion 45 of the injector.
  • the Injektorgepurabites 45 has a central bore in which in a throttle piston 50, a first throttle 47, which is also referred to as a drain throttle, and a second throttle 48 are formed, which is also referred to as inlet throttle. Since both throttles, in particular the outlet throttle 47 with the smaller throttle cross-section, are flowed through or, when the pressure in the control chamber 41 decreases, the opening of the nozzle needle 10 takes place relatively slowly.
  • the closing of the nozzle needle 10 is effected by a pressure increase in the nozzle needle control chamber 44.
  • the pressure increase is caused by fuel flowing from the high-pressure fuel storage 2 via the supply lines 3, 4, the connecting channel 34, the pressure booster control chamber 23, the connecting channel 41, the connecting channel 42 and the inlet throttle 48 past the throttle body 61 in the nozzle needle control chamber 44.
  • the nozzle needle control chamber 44 is bounded laterally by a sealing sleeve 56, which has a biting edge 57.
  • the biting edge 57 opposite side of the sealing sleeve 56 is acted upon by a compression spring 58 which is biased between the sealing sleeve 56 and a collar 54 which is formed on the nozzle needle 10.
  • the biasing force of the spring 58 causes the biting edge 57 of the sealing sleeve 56 to abut against the injector section 45.
  • the biasing force of the spring 58 causes the tip 11 of the nozzle needle 10 to be pressed against its associated sealing seat.
  • the combustion chamber facing away from the outer edge of the collar 51 on the throttle piston 50 forms a sealing edge 61 which is pressed by the prestressed compression spring 53 against an associated sealing seat, which is provided on the Injektorgepurabites 45.
  • the Preload force of the compression spring 53 and the throttle cross section of the outlet throttle 47 are selected so that the throttle piston 50 lifts off with its sealing edge 61 of the associated seat on the Injektorgepurabites 45 when flows through the connecting line 42 and the inlet throttle 48 with high pressure fuel.
  • the high-pressure fuel raises the throttle piston 50 from the sealing edge 61 and can then flow past the outlet throttle 47 into the nozzle needle control chamber 44. As a result, a fast closing of the nozzle needle 10 is ensured.
  • the nozzle needle 10 is guided in the shaft, wherein flow channels 59, 60 are provided in the guide region, passes through the fuel from the pressure chamber 15 to the tip 11 of the nozzle needle 10.
  • the pressure chamber 15, in which the nozzle closing spring 58 is arranged, is formed in the upper nozzle region.
  • the pressure booster control chamber 23 is acted upon by the 3/2-way valve 32 with the same pressure as the pressure booster working chamber 26.
  • the connection to the return line 35 is closed.
  • the pressure booster piston 25 is pressure balanced and there is no pressure gain.
  • the nozzle needle 10 is closed.
  • the throttle piston 50 is in contact with the injector housing section 45 with the sealing edge 61.
  • the pressure booster control chamber 23 is depressurized.
  • the pressure booster control chamber 23 is decoupled from the high-pressure accumulator 2 with the aid of the 3/2-way valve 32 and is depressurized via the connecting line 29 into the return line 35.
  • the pressure in the compression chamber 22 is thereby increased according to the transmission ratio of the pressure booster 5 and forwarded to the injection nozzle.
  • the injector starts to open. Since the collar 51 of the throttle piston 50 rests against the injector housing section 45, ie the sealing seat is closed at 61, fuel must be displaced via the outlet throttle 47 and then via the inlet throttle 48 from the nozzle needle control chamber 44, which is also referred to as a damping chamber. This reduces the needle opening speed. By way of the flow rate of the outlet throttle 47, the needle opening speed can thus be set.
  • the first throttle 47 is formed in a central bore of a throttle piston 50, which has a collar 51.
  • the collar 51 of the throttle piston 50 is biased by a compression spring 53 against the tip 11 opposite end of the nozzle needle 10.
  • the pressure in the nozzle needle control chamber 44 serves to control the injection of fuel through the injection holes 12, 13.
  • the outlet throttle 47 has a smaller throttle cross-section than the inlet throttle 48. If the 3/2-way valve from the in FIG. 1 shown position is switched to its second (not shown) position, then the nozzle needle control chamber 44 via the connecting lines 42, 41, 29 and 35 in the (not shown) fuel tank emptied or relieved. When emptying or relieving the nozzle needle control chamber 44, both the first throttle 47 and the second throttle 48 are flowed through. Due to the pressure drop in the nozzle needle control chamber 44, the nozzle needle 10 lifts with its tip 11 from the associated sealing seat.
  • the pressure booster 5 remains activated and compresses the fuel in the booster chamber 22, which can also be referred to as a compression chamber.
  • the compressed fuel is forwarded to the nozzle needle 10 and injected.
  • the throttle piston 50 is also designed as a stroke stop for the nozzle needle 10.
  • the stroke stop of the nozzle needle 10 is adjustable over the height or length of the throttle piston 50, whereby a high accuracy of the Nadelhubs is achieved in the production of the injector.
  • the stroke stop of the nozzle needle 10 may be formed so that the sealing seat at 61 and another sealing seat at 62 are closed when the combustion chamber distal end of the nozzle needle 10 comes to rest on the throttle piston 50.
  • the throttle piston 50 is formed shorter than that in the FIGS. 1 and 2 illustrated embodiment.
  • FIG. 3 forms the throttle piston 50 no stroke stop for the nozzle needle 10.
  • the nozzle needle 10 comes in the in FIG. 3 illustrated embodiment in its upper stroke stop with its combustion chamber remote end 62 to a sealing edge 63 for conditioning, which is formed on the Injektorgepuruseabites 45. This prevents that after needle opening, the pressure on the inside of the sealing sleeve 56 drops too much, so that an undesirably large deformation of the sealing sleeve 56 is prevented.
  • an overshoot of the pressure in the chambers 23 and 44 via system pressure and undershooting in the chamber 15 under system pressure can be achieved for a short time in the needle closing phase.
  • a higher pressure than in the pressure chamber 15, which is also referred to as an intermediate space In this case, the sealing sleeve 56 can be released from the contact point on the throttle piston 50 and the closing pressure in the nozzle needle control chamber 44 breaks. Due to the closing spring force on the nozzle needle 10, however, this continues its closing movement. This opening of the sealing sleeve 56 can be used to achieve a flushing of the nozzle needle control chamber 44.
  • the pressure booster piston 25 is returned to its initial position by the booster spring 27, which may also be referred to as a return spring.
  • the pressure booster chamber 22 is filled via the check valve 40.
  • the throttle piston 50 is by the compression spring 53 in its closed rest position reset.
  • the connecting line 41 which may be designed, for example, as a control bore, may alternatively also be connected to the region of the pressure booster working space 26 / high-pressure reservoir 2.
  • FIG. 4 is a similar fuel injector as in FIG. 1 shown.
  • the same reference numerals are used to designate like parts. To avoid repetition, the preceding description of the FIG. 1 directed. In the following, only the differences between the two embodiments will be discussed.
  • FIG. 4 shows an embodiment with two separately formed throttle paths 71 and 73 in the nozzle needle control chamber 44.
  • a discharge throttle 72 is provided in the throttle path 71.
  • a check valve 74 and an inlet throttle 75 are provided in the throttle path 73. Due to the separately formed throttle paths 71 and 73, the volume of the nozzle needle control chamber 44 can be kept very small, whereby a vibration-reduced needle opening can be achieved.
  • the nozzle needle control chamber 44 is connected via the throttle 72 to the control line 41.
  • the nozzle needle control chamber 44 is connected to the control line 41 via the throttle 75 and the check valve 74.
  • the needle opening speed is determined by the drain throttle 72.
  • the needle closing speed can be adjusted via the inlet throttle 75.
  • FIG. 5 is a similar fuel injector as in FIG. 4 shown.
  • the same reference numerals are used to designate like parts. To avoid repetition, the preceding description of the FIG. 4 directed. In the following, only the differences between the two embodiments will be discussed.
  • FIG. 5 illustrated embodiment another design of the nozzle needle 10 is used.
  • the two inlet paths 71 and 73 which can also be referred to as throttle paths, open into a nozzle needle control chamber 80, in which a nozzle needle spring 81 is arranged.
  • a nozzle needle spring 81 By the biasing force of the nozzle needle spring 81, the nozzle needle 10 is held with its tip 11 against the associated sealing seat in abutment.
  • a pressure shoulder 83 is formed, which is arranged in a substantially annular pressure chamber 84.
  • the pressure chamber 84 is connected via a connecting line 86 to the pressure booster chamber 22 in connection.

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)
  • Fuel-Injection Apparatus (AREA)

Description

Die Erfindung betrifft eine Einrichtung zum Einspritzen von Kraftstoff in einen Brennraum einer Brennkraftmaschine, mit einem Kraftstoffinjektor, der über eine Hochdruckquelle mit unter hohem Druck stehendem Kraftstoff beaufschlagbar und über ein Zumessventil betätigbar ist, durch das der Druck in einem Einspritzventilgliedsteuerraum so steuerbar ist, dass ein Einspritzventilglied zum Einspritzen von Kraftstoff öffnet und schließt.The invention relates to a device for injecting fuel into a combustion chamber of an internal combustion engine, with a fuel injector which can be acted upon by a high-pressure source with high-pressure fuel and actuated via a metering valve, through which the pressure in an injection valve member control chamber is controlled so that a Injector member for injecting fuel opens and closes.

Stand der TechnikState of the art

Aus der deutschen Offenlegungsschrift DE 102 94 15 A1 ist eine Einrichtung zum Einspritzen von Kraftstoff in einen Brennraum einer Verbrennungskraftmaschine mit einem Kraftstoffinjektor bekannt, der über eine Hochdruckwelle mit unter hohem Druck stehendem Kraftstoff beaufschlagbar und über ein Zumessventil betätigbar ist. Ein Einspritzventilglied, das in Schließrichtung durch eine Schließkraft beaufschlagt ist, ist von einem Druckraum umschlossen. Um die Öffnungsgeschwindigkeit des Einspritzventilglieds, wie zum Beispiel einer Düsennadel, zu dämpfen, ohne dass ein schnelles Schließen des Einspritzventilglieds beeinträchtigt würde, ist dem Einspritzventilglied ein von diesem unabhängig bewegbares Dämpfungselement zugeordnet, das einen Dämpfungsraum begrenzt und mindestens einen Überströmkanal zur Verbindung des Dämpfungsraums mit einem weiteren hydraulischen Raum aufweist. Das Dämpfungselement kann als Dämpfungskolben ausgebildet sein, der von dem weiteren hydraulischen Raum umgeben ist.From the German patent application DE 102 94 15 A1 a device for injecting fuel into a combustion chamber of an internal combustion engine having a fuel injector is known, which can be acted upon by a high-pressure shaft with high-pressure fuel and actuated via a metering valve. An injection valve member, which is acted upon in the closing direction by a closing force, is enclosed by a pressure chamber. To dampen the opening speed of the injection valve member, such as a nozzle needle, without interfering with rapid closing of the injection valve member the injection valve member associated with a independently movable damping element which defines a damping space and at least one overflow channel for connecting the damping chamber with a further hydraulic space. The damping element may be formed as a damping piston, which is surrounded by the other hydraulic space.

Aus WO 2004/007974 A2 ist weiterhin eine Einrichtung zum Einspritzen von Kraftstoff in einen Brennraum einer Verbrennungskraftmaschine mit einem Kraftstoffinjektor bekannt, bei dem der Einspritzdruck des Kraftstoffinjektors mittels eines Druckverstärkers erhöht wird, indem ein Druckverstärkersteuerraum über eine Steuerleitung druckentlastet wird sowie der Druck in einem Düsennadelsteuerraum über eine Ablaufdrosseleinrichtung entleerbar und über eine Zulaufdrosseleinrichtung befüllbar ist. Der Druckverstärkersteuerraum und der Düsennadelsteuerraum sind dabei über eine hydraulische Verbindung verbunden. Bei dieser Ausführungsform wird der Druckverstärkersteuerraum von einem ersten Zumessventil und der Düsennadelsteuerraum von einem zweiten Zumessventil angesteuert.Out WO 2004/007974 A2 Furthermore, a device for injecting fuel into a combustion chamber of an internal combustion engine with a fuel injector is known, in which the injection pressure of the fuel injector is increased by means of a pressure booster by a pressure booster control chamber via a control line is depressurized and the pressure in a nozzle needle control chamber via an outlet throttle and emptied over an inlet throttle device can be filled. The pressure booster control chamber and the nozzle needle control chamber are connected via a hydraulic connection. In this embodiment, the pressure booster control chamber is controlled by a first metering valve and the nozzle needle control chamber by a second metering valve.

Aufgabe der Erfindung ist es, eine Einrichtung zum Einspritzen von Kraftstoff in einen Brennraum einer Brennkraftmaschine mit einem Kraftstoffinjektor, der über eine Hochdruckquelle mit unter hohem Druck stehendem Kraftstoff beaufschlagbar ist, zu schaffen, bei der der Einspritzdruck von einem hydraulischen Druckverstärker im Kraftstoffinjektor verstärket wird. Die Einrichtung soll zuverlässig arbeitet, einfach aufgebaut und kostengünstig herstellbar sein.The object of the invention is to provide a device for injecting fuel into a combustion chamber of an internal combustion engine having a fuel injector which can be acted upon by a high-pressure source with high-pressure fuel, in which the injection pressure is amplified by a hydraulic pressure booster in the fuel injector. The device should work reliably, be simple and inexpensive to produce.

Darstellung der ErfindungPresentation of the invention

Die Aufgabe der Erfindung wird dadurch gelöst, indem der Düsennadelsteuerraum über eine Ablaufdrosseleinrichtung entleerbar und über eine Zulaufdrosseleinrichtung befüllbar ist, wobei der Druckverstärkersteuerraum und der Düsennadelsteuerraum über eine hydraulische Verbindung verbunden sind, wobei die hydraulische Verbindung zwischen Druckverstärkersteuerraum und Düsennadelsteuerraum eine zweite Steuerleitung enthält, wobei der Düsennadelsteuerraum über die Ablaufdrosseleinrichtung in die zweite Steuerleitung entleerbar und über die Zulaufdrosseleinrichtung aus der zweiten Steuerleitung befüllbar ist, und wobei der Drosselquerschnitt der Ablaufdrosseleinrichtung kleiner ist als der Drosselquerschnitt der zulaufdrosseleinrichtung.The object of the invention is achieved in that the nozzle needle control chamber can be emptied via an outlet throttle device and an inlet throttle device, wherein the pressure booster control chamber and the nozzle needle control chamber are connected via a hydraulic connection, wherein the hydraulic connection between the pressure booster control chamber and nozzle needle control chamber contains a second control line, wherein the nozzle needle control chamber via the outlet throttle in the second control line can be emptied and filled via the inlet throttle from the second control line, and wherein the throttle cross section of the outlet throttle is smaller than the throttle cross section of the inlet throttle.

Die Ablaufdrosseleinrichtung ermöglicht ein langsames Öffnen des Einspritzventilglieds. Die Zulaufdrossel ermöglicht ein schnelles Schließen des Einspritzventilglieds. Durch das langsame Öffnen des Einspritzventilglieds wird die Kleinstmengenfähigkeit der Kraftstoffeinspritzeinrichtung verbessert. Durch das schnelle Schließen des Einspritzventilglieds werden die Emissionswerte der Brennkraftmaschine verbessert. Die beiden separaten Drosseleinrichtungen liefern den Vorteil, dass Öffnungs- und Schließgeschwindigkeit des Einspritzventilglieds unabhängig voneinander einstellbar sind.The outlet throttle device allows a slow opening of the injection valve member. The inlet throttle allows a fast closing of the injection valve member. The slow opening of the injection valve member improves the minimum quantity capability of the fuel injection device. The rapid closing of the injection valve member improves the emission values of the internal combustion engine. The two separate throttle devices provide the advantage that opening and closing speed of the injection valve member are independently adjustable.

Ein bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass ein Ventilelement vorgesehen ist, das geschlossen ist, wenn der Einspritz-ventilgliedsteuerraum entleert wird, und die geöffnet ist, wenn der Einspritzventilgliedsteuerraum befüllt wird.A preferred embodiment of the fuel injection device is characterized in that a valve element is provided, which is closed when the injection valve member control chamber is emptied, and which is open when the injection valve member control chamber is filled.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass eine der Drosseleinrichtungen, insbesondere die Ablaufdrosseleinrichtung, nur beim Entleeren des Einspritzventilgliedsteuerraums ihre Drosselwirkung entfaltet und beim Befüllen des Einspritzventilgliedsteuerraums keine Drosselwirkung entfaltet, sondern einen ungehinderten Durchtritt von Kraftstoff gewährleistet. Dadurch wird das Schließen des Einspritzventilglieds beschleunigt.A further preferred exemplary embodiment of the fuel injection device is characterized in that one of the throttle devices, in particular the outlet throttle device, develops its throttling action only when the injection valve member control chamber is emptied and no throttling action develops during filling of the injection valve member control chamber, but an unimpeded passage guaranteed by fuel. As a result, the closing of the injection valve member is accelerated.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die beiden Drosseleinrichtungen in Reihe geschaltet sind. Dadurch wird ein einfacher Aufbau ermöglicht, der fertigungstechnisch kostengünstig realisierbar ist.A further preferred embodiment of the fuel injection device is characterized in that the two throttle devices are connected in series. As a result, a simple construction is made possible, which is economically feasible in terms of manufacturing technology.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die beiden Drosseleinrichtungen, bezogen auf die Längsachse des Kraftstoffinjektors, mittig angeordnet sind. Diese Anordnung liefert fertigungstechnische Vorteile, da beide Drosselstellen mittig bearbeitet werden können.A further preferred exemplary embodiment of the fuel injection device is characterized in that the two throttle devices are arranged centrally with respect to the longitudinal axis of the fuel injector. This arrangement provides manufacturing advantages, since both throttle bodies can be edited in the middle.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die Ablaufdrosseleinrichtung, ein Drosselelement mit einer Dichtkante umfasst, das durch ein Federelement so vorgespannt ist, dass die Dichtkante gegen einen zugehörigen Dichtsitz gedrückt wird, wenn das Drosselelement in der Entleerungsrichtung durchströmt wird, und so, dass die Dichtkante von ihrem Dichtsitz abhebt, wenn das Drosselelement in der Befüllungsrichtung durchströmt wird. Durch die Kombination einer Drossel mit einem Rückschlagventil wird eine kompakte Bauform mit einer verkürzten Kraftstoffinjektorlänge ermöglicht.A further preferred embodiment of the fuel injection device is characterized in that the outlet throttle device comprises a throttle element with a sealing edge which is biased by a spring element so that the sealing edge is pressed against an associated sealing seat when the throttle element is flowed through in the discharge direction, and so in that the sealing edge lifts off from its sealing seat when the throttle element is flowed through in the filling direction. The combination of a throttle with a check valve enables a compact design with a shortened fuel injector length.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass das Drosselelement einen durch das Federelement vorgespannten und mit einem eine Drosselstelle aufweisenden Durchgangsloch ausgestatteten Drosselkolben umfasst, dessen freies Ende einen Hubanschlag für das Einspritzventilglied bildet. Dadurch wird verhindert, dass nach dem Öffnen des Einspritzventilglieds der Druck in dem Einspritzventilgliedsteuerraum zu stark absinkt.A further preferred embodiment of the fuel injection device is characterized in that the throttle element comprises a biased by the spring element and equipped with a throttle point having a throttle hole throttle piston whose free end forms a stroke stop for the injection valve member. This prevents the pressure in the injection valve member control chamber from falling too much after the injection valve member has been opened.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass der Hubanschlag der Düsennadel so ausgeführt ist, dass ein erster Dichtsitz und ein zweiter Dichtsitz geschlossen werden, wenn das brennraumferne Ende der Düsennadel an dem Drosselkolben zur Anlage kommt. Dadurch wird verhindert, dass bei offener Düsennadel der Druck an der Innenseite einer Dichthülse in einem Ringraum zwischen dem Drosselkolben und der Dichthülse zu stark absinkt. Dadurch kann eine unerwünscht große Verformung der Dichthülse verhindert werden.A further preferred embodiment of the fuel injection device is characterized in that the stroke stop of the nozzle needle is designed so that a first sealing seat and a second sealing seat are closed when the combustion chamber remote end of the nozzle needle comes to rest on the throttle piston. This prevents that when the nozzle needle is open, the pressure on the inside of a sealing sleeve in an annular space between the throttle piston and the sealing sleeve drops too much. As a result, an undesirably large deformation of the sealing sleeve can be prevented.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die Düsennadel in ihrem oberen Hubanschlag mit ihrem brennraumfernen Ende an einer Dichtkante zur Anlage kommt, die an einem Injektorgehäuseabschnitt ausgebildet ist. Dadurch wird verhindert, dass nach dem Nadelöffnen der Druck an der Innenseite einer Dichthülse zu stark absinkt, so dass eine unerwünscht große Verformung der Dichthülse verhindert wird.A further preferred embodiment of the fuel injection device is characterized in that the nozzle needle comes into abutment in its upper stroke stop with its end remote from the combustion chamber at a sealing edge, which is formed on an injector housing portion. This prevents that after needle opening, the pressure on the inside of a sealing sleeve drops too much, so that an undesirably large deformation of the sealing sleeve is prevented.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die beiden Drosseleinrichtungen parallel geschaltet sind. Diese Anordnung liefert im Betrieb des Kraftstoffinjektors Vorteile.A further preferred embodiment of the fuel injection device is characterized in that the two throttle devices are connected in parallel. This arrangement provides advantages in the operation of the fuel injector.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die Ablaufdrosseleinrichtung ein Drosselelement umfasst, das mit einem Rückschlagventil so in Reihe geschaltet ist, dass das Drosselelement nur in einer Richtung, insbesondere der Befüllungsrichtung, durchströmt wird und in der Entleerungsrichtung geschlossen ist. Dieser Aufbau ist fertigungstechnisch besonders einfach realisierbar.A further preferred embodiment of the fuel injection device is characterized in that the outlet throttle device comprises a throttle element, which is connected in series with a check valve, that the throttle element is flowed through in one direction, in particular the filling direction, and is closed in the discharge direction. This structure is manufacturing technology particularly easy to implement.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die Zulaufdrosseleinrichtung bezogen auf die Längsachse des Kraftstoffinjektors außermittig angeordnet ist. Dadurch kann der Zulaufdrosseleinrichtung eine größere druckbeaufschlagte Fläche zugeordnet werden, wodurch ein schnelleres Schließen des Einspritzventilglieds ermöglicht wird.A further preferred embodiment of the fuel injection device is characterized in that the inlet throttle device is arranged off-center relative to the longitudinal axis of the fuel injector. As a result, the inlet throttle device can be assigned a larger pressure-loaded surface, which allows a faster closing of the injection valve member.

Ein weiteres bevorzugtes Ausführungsbeispiel der Kraftstoffeinspritzeinrichtung ist dadurch gekennzeichnet, dass die Ablaufdrosseleinrichtung bezogen auf die Längsachse des Kraftstoffinjektors mittig angeordnet ist. Die mittige Anordnung vereinfacht die Bearbeitung der Drosselstelle bei der Fertigung.A further preferred exemplary embodiment of the fuel injection device is characterized in that the outlet throttle device is arranged centrally with respect to the longitudinal axis of the fuel injector is. The central arrangement simplifies the processing of the throttle point during production.

Die vorliegende Erfindung betrifft einen Injektor mit Druckübersetzer beziehungsweise Druckverstärker und die Ansteuerung des Druckverstärkers über den Rückraum.The present invention relates to an injector with pressure booster or pressure booster and the control of the pressure booster via the rear space.

Weitere Vorteile, Merkmale und Einzelheiten der Erfindung ergeben sich aus der nachfolgenden Beschreibung, in der unter Bezugnahme auf die Zeichnung verschiedene Ausführungsbeispiele im Einzelnen beschrieben sind. Dabei können die in den Ansprüchen und in der Beschreibung erwähnten Merkmale jeweils einzeln für sich oder in beliebiger Kombination erfindungswesentlich sein.Further advantages, features and details of the invention will become apparent from the following description in which, with reference to the drawings, various embodiments are described in detail. The features mentioned in the claims and in the description may each be essential to the invention individually or in any desired combination.

Zeichnungdrawing

Es zeigen:

Figur 1
ein erstes Ausführungsbeispiel der erfin- dungsgemäßen Kraftstoffeinspritzeinrich- tung im Längsschnitt durch den Kraftstof- finjektor;
Figur 2
einen vergrößerten Ausschnitt aus Figur 1;
Figur 3
eine ähnliche Ansicht wie in Figur 2 ge- mäß einem weiteren Ausführungsbeispiel;
Figur 4
eine ähnliche Darstellung wie in Figur 1 gemäß einem weiteren Ausführungsbeispiel;
Figur 5
eine ähnliche Darstellung wie in Figur 1 gemäß einem weiteren Ausführungsbeispiel;
Show it:
FIG. 1
a first embodiment of the fuel injection device according to the invention in longitudinal section through the fuel injector;
FIG. 2
an enlarged section FIG. 1 ;
FIG. 3
a similar view as in FIG. 2 according to a further embodiment;
FIG. 4
a similar representation as in FIG. 1 according to a further embodiment;
FIG. 5
a similar representation as in FIG. 1 according to a further embodiment;

Beschreibung der AusführungsbeispieleDescription of the embodiments

Die Beschreibung der erfindungsgemäßen Einrichtung zur Dämpfung der Hubbewegung eines Einspritzventilglieds erfolgt anhand eines Kraftstoffinjektors mit Druckübersetzer. Die vorgeschlagene Einrichtung zur Dämpfung der Hubbewegung, insbesondere hinsichtlich einer Verringerung von dessen Öffnungsgeschwindigkeit, lässt sich auch an anderen Kraftstoffeinspritzsystemen, wie Pumpe-Düse-Systemen als auch an Pumpe-Leitung-Düse-Systemen, Verteilereinspritzsystemen sowie auch an Hochdruckspeichereinspritzsystemen einsetzen, deren Kraftstoffinjektor keine Druckübersetzung fassen.The description of the device according to the invention for damping the lifting movement of an injection valve member is based on a fuel injector with pressure booster. The proposed device for damping the lifting movement, in particular with regard to a reduction of its opening speed, can also be used on other fuel injection systems, such as pump-nozzle systems and pump-line-nozzle systems, distribution injection systems and also high-pressure accumulator injection systems, the fuel injector none Take pressure translation.

In Figur 1 ist ein Längsschnitt durch einen Common-Rail-Injektor 1 dargestellt, der über einen nur schematisch angedeuteten Druckspeicherraum 2 (Common-Rail) mit unter hohem Druck stehendem Kraftstoff versorgt wird. Vom Innenraum des Hochdruckspeicherraums 2 erstreckt sich eine Kraftstoffzuleitung 3, 4 zu einem Druckübersetzer 5, der in den Kraftstoffinjektor 1 integriert ist. Der Druckübersetzer 5 ist von einem (nicht dargestellten) Injektorgehäuse umschlossen. Das Injektorgehäuse umfasst einen Injektorkörper und einen Düsenkörper, der eine zentrale Führungsbohrung aufweist. In der Führungsbohrung ist eine Düsennadel 10 hin und her bewegbar geführt. Die Düsennadel 10 weist eine Spitze 11 auf, an der eine Dichtfläche ausgebildet ist, die mit einem Dichtsitz zusammenwirkt, der an dem Düsenkörper ausgebildet ist. Wenn sich die Spitze 11 der Düsennadel 10 mit ihrer Dichtfläche in Anlage an dem Dichtsitz befindet, sind zwei Spritzlöcher 12, 13 in dem Düsenkörper verschlossen. Wenn die Düsennadelspitze 11 von ihrem Sitz abhebt, wird mit Hochdruck beaufschlagter Kraftstoff durch die Spritzlöcher 12, 13 in den Brennraum der Brennkraftmaschine eingespritzt.In FIG. 1 is a longitudinal section through a common rail injector 1 shown, which is supplied via an only schematically indicated pressure accumulator space 2 (common rail) with fuel under high pressure. From the interior of the high pressure accumulator 2, a fuel supply line 3, 4 extends to a pressure booster 5, which is integrated into the fuel injector 1. The pressure booster 5 is enclosed by an injector housing (not shown). The injector housing includes an injector body and a nozzle body having a central guide bore. In the guide bore, a nozzle needle 10 is guided back and forth movable. The nozzle needle 10 has a tip 11, on which a sealing surface is formed, which cooperates with a sealing seat, which is formed on the nozzle body. When the tip 11 of the nozzle needle 10 with its sealing surface is in contact with the sealing seat, two spray holes 12, 13 are closed in the nozzle body. When the nozzle needle tip 11 lifts off its seat, high pressure fuel is injected through the injection holes 12, 13 into the combustion chamber of the engine.

In dem Düsenkörper ist ein Druckraum 15 ausgebildet, der über einen Verbindungskanal 18 mit einem Druckverstärkerraum 22 in Verbindung steht. In dem Druckverstärkerraum 22 ist mit Hochdruck beaufschlagter Kraftstoff enthalten, der in Abhängigkeit von dem Druck in einem Druckverstärkersteuerraum 23 noch weiter komprimiert wird. Zu diesem Zweck ragt ein Ende 24 eines Druckverstärkerkolbens 25 in den Druckverstärkerraum 22. Das Ende 24 des Druckverstärkerkolbens 25 hat im Wesentlichen die Gestalt eines Kreiszylinders, dessen Außendurchmesser kleiner als der Außendurchmesser des Abschnitts 25 des Druckverstärkerkolbens ist. In einem Druckverstärkerarbeitsraum 26 ist eine Druckverstärkerfeder 27 angeordnet, mit deren Hilfe der Druckverstärkerkolben 25 in Richtung von der Düsennadel 10 weg vorgespannt ist.In the nozzle body, a pressure chamber 15 is formed, which communicates via a connecting channel 18 with a pressure booster chamber 22 in connection. In the pressure booster chamber 22 is supplied with high-pressure fuel, which is further compressed in response to the pressure in a pressure booster control chamber 23. For this purpose, one end 24 of a pressure booster piston 25 protrudes into the pressure booster chamber 22. The end 24 of the pressure booster piston 25 has substantially the shape of a circular cylinder whose outer diameter is smaller than the outer diameter of the section 25 of the pressure booster piston. In a pressure booster working chamber 26, a pressure booster spring 27 is arranged, by means of which the pressure booster piston 25 is biased in the direction of the nozzle needle 10 away.

Der Druckverstärkersteuerraum 23 steht über einen Verbindungskanal 29 mit einem 3/2-Wegeventil 32 in Verbindung, das wiederum über einen Verbindungskanal 34 und die Kraftstoffzuleitungen 3,4 mit dem Hochdruckspeicherraum 2 in Verbindung steht. Außerdem weist das 3/2-Wegeventil 32 einen Anschluss 35 zu einem (nicht dargestellten) Kraftstofftank auf.The pressure booster control chamber 23 communicates via a connecting channel 29 with a 3/2-way valve 32 in connection, which in turn communicates via a connecting channel 34 and the fuel supply lines 3,4 with the high-pressure accumulator chamber 2. In addition, the 3/2-way valve 32 has a port 35 to a fuel tank (not shown).

In der in Figur 1 dargestellten Stellung des 3/2-Wegeventils steht der Druckverstärkersteuerraum 23 über die Verbindungskanäle beziehungsweise Verbindungsleitungen 29, 34, 3 und 4 mit dem Kraftstoffhochdruckspeicherraum 2 in Verbindung. Über ein Rückschlagventil 40 und eine Verbindungsleitung 41 steht der Druckverstärkerraum 22 mit dem Druckverstärkersteuerraum 23 in Verbindung. Das Rückschlagventil 40, weist eine Rückschlagkugel auf, die zum Beispiel mit Hilfe einer Rückschlagventilfeder so gegen einen Rückschlagventilsitz vorgespannt ist, dass der Druckverstärkerraum 22 über die Verbindungsleitungen 41, 29, 34, 3 und 4 aus dem Kraftstoffhochdruckspeicher 2 mit Kraftstoff gefüllt wird, wenn der Druck in dem Druckverstärkerräum 22 kleiner als in dem Kraftstoffhochdruckraum 2 ist.In the in FIG. 1 shown position of the 3/2-way valve is the pressure booster control chamber 23 via the connection channels or connecting lines 29, 34, 3 and 4 with the high-pressure fuel storage chamber 2 in connection. Via a check valve 40 and a connecting line 41, the pressure booster chamber 22 communicates with the pressure booster control chamber 23. The check valve 40 has a check ball, which is biased for example by means of a check valve spring against a check valve seat that the pressure booster chamber 22 is filled via the connecting lines 41, 29, 34, 3 and 4 from the high-pressure fuel reservoir 2 with fuel when the Pressure in the booster chamber 22 is smaller than in the high-pressure fuel chamber 2.

Der Druckverstärkerraum 22 steht über eine Verbindungsleitung 42 mit einem Düsennadelsteuerraum 44 in Verbindung, der auch als Dämpfungsraum bezeichnet wird. Der Düsennadelsteuerraum 44 wird nach oben hin durch einen Abschnitt 45 des Injektorgehäuses begrenzt. Der Injektorgehäuseabschnitt 45 weist eine zentrale Bohrung auf, in der in einem Drosselkolben 50 eine erste Drossel 47, die auch als Ablaufdrossel bezeichnet wird, und eine zweite Drossel 48 ausgebildet sind, die auch als Zulaufdrossel bezeichnet wird. Da beide Drosseln, insbesondere die Ablaufdrossel 47 mit dem kleineren Drosselquerschnitt, durchströmt werden beziehungsweise wird, wenn der Druck im Steuerraum 41 sinkt, erfolgt das Öffnen der Düsennadel 10 relativ langsam. Das Schließen der Düsennadel 10 wird durch einen Druckanstieg in dem Düsennadelsteuerraum 44 bewirkt. Der Druckanstieg wird durch Kraftstoff bewirkt, der aus dem Kraftstoffhochdruckspeicher 2 über die Zuleitungen 3, 4, den Verbindungskanal 34, den Druckverstärkersteuerraum 23, den Verbindungskanal 41, den Verbindungskanal 42 und die Zulaufdrossel 48 an der Drosselstelle 61 vorbei in den Düsennadelsteuerraum 44 einströmt.The pressure booster chamber 22 communicates via a connecting line 42 with a nozzle needle control chamber 44, which is also referred to as a damping chamber. The nozzle needle control chamber 44 is bounded at the top by a portion 45 of the injector. The Injektorgehäuseabschnitt 45 has a central bore in which in a throttle piston 50, a first throttle 47, which is also referred to as a drain throttle, and a second throttle 48 are formed, which is also referred to as inlet throttle. Since both throttles, in particular the outlet throttle 47 with the smaller throttle cross-section, are flowed through or, when the pressure in the control chamber 41 decreases, the opening of the nozzle needle 10 takes place relatively slowly. The closing of the nozzle needle 10 is effected by a pressure increase in the nozzle needle control chamber 44. The pressure increase is caused by fuel flowing from the high-pressure fuel storage 2 via the supply lines 3, 4, the connecting channel 34, the pressure booster control chamber 23, the connecting channel 41, the connecting channel 42 and the inlet throttle 48 past the throttle body 61 in the nozzle needle control chamber 44.

Der Düsennadelsteuerraum 44 wird seitlich von einer Dichthülse 56 begrenzt, die eine Beißkante 57 aufweist. Die der Beißkante 57 entgegengesetzte Seite der Dichthülse 56 ist durch eine Druckfeder 58 beaufschlagt, die zwischen der Dichthülse 56 und einem Bund 54 vorgespannt ist, der an der Düsennadel 10 ausgebildet ist. Die Vorspannkraft der Feder 58 bewirkt einerseits, dass die Beißkante 57 der Dichthülse 56 an dem Injektorabschnitt 45 anliegt. Andererseits bewirkt die Vorspannkraft der Feder 58, dass die Spitze 11 der Düsennadel 10 gegen ihren zugehörigen Dichtsitz gedrückt wird.The nozzle needle control chamber 44 is bounded laterally by a sealing sleeve 56, which has a biting edge 57. The biting edge 57 opposite side of the sealing sleeve 56 is acted upon by a compression spring 58 which is biased between the sealing sleeve 56 and a collar 54 which is formed on the nozzle needle 10. On the one hand, the biasing force of the spring 58 causes the biting edge 57 of the sealing sleeve 56 to abut against the injector section 45. On the other hand, the biasing force of the spring 58 causes the tip 11 of the nozzle needle 10 to be pressed against its associated sealing seat.

Der dem Brennraum abgewandte äußere Rand des Bundes 51 an dem Drosselkolben 50 bildet eine Dichtkante 61, die durch die vorgespannte Druckfeder 53 gegen einen zugehörigen Dichtsitz gedrückt wird, der an dem Injektorgehäuseabschnitt 45 vorgesehen ist. Die Vorspannkraft der Druckfeder 53 und der Drosselquerschnitt der Ablaufdrossel 47 sind so gewählt, dass der Drosselkolben 50 mit seiner Dichtkante 61 von dem zugehörigen Sitz an dem Injektorgehäuseabschnitt 45 abhebt, wenn über die Verbindungsleitung 42 und die Zulaufdrossel 48 mit Hochdruck beaufschlagter Kraftstoff einströmt. Der mit Hochdruck beaufschlagte Kraftstoff hebt den Drosselkolben 50 aus der Dichtkante 61 und kann dann an der Ablaufdrossel 47 vorbei in den Düsennadelsteuerraum 44 einströmen. Dadurch wird ein schnelles Schließen der Düsennadel 10 gewährleistet. Beim Befüllen des Düsennadelsteuerraums 44 über den Verbindungskanal 42 entfaltet nur die Zulaufdrossel 48 ihre Drosselwirkung, nicht aber die Ablaufdrossel 47.The combustion chamber facing away from the outer edge of the collar 51 on the throttle piston 50 forms a sealing edge 61 which is pressed by the prestressed compression spring 53 against an associated sealing seat, which is provided on the Injektorgehäuseabschnitt 45. The Preload force of the compression spring 53 and the throttle cross section of the outlet throttle 47 are selected so that the throttle piston 50 lifts off with its sealing edge 61 of the associated seat on the Injektorgehäuseabschnitt 45 when flows through the connecting line 42 and the inlet throttle 48 with high pressure fuel. The high-pressure fuel raises the throttle piston 50 from the sealing edge 61 and can then flow past the outlet throttle 47 into the nozzle needle control chamber 44. As a result, a fast closing of the nozzle needle 10 is ensured. When filling the nozzle needle control chamber 44 via the connecting channel 42, only the inlet throttle 48 unfolds its throttling effect, but not the outlet throttle 47.

Die Düsennadel 10 ist im Schaft geführt, wobei im Führungsbereich Strömungskanäle 59, 60 vorgesehen sind, über die Kraftstoff aus dem Druckraum 15 zur Spitze 11 der Düsennadel 10 gelangt. Der Druckraum 15, in dem auch die Düsenschließfeder 58 angeordnet ist, ist im oberen Düsenbereich ausgebildet.The nozzle needle 10 is guided in the shaft, wherein flow channels 59, 60 are provided in the guide region, passes through the fuel from the pressure chamber 15 to the tip 11 of the nozzle needle 10. The pressure chamber 15, in which the nozzle closing spring 58 is arranged, is formed in the upper nozzle region.

Im deaktivierten Ruhezustand, der in Figur 1 dargestellt ist, ist der Druckverstärkersteuerraum 23 über das 3/2-Wegeventil 32 mit dem gleichen Druck beaufschlagt, wie der Druckverstärkerarbeitsraum 26. Die Verbindung zum Rücklauf 35 ist geschlossen. Der Druckverstärkerkolben 25 ist druckausgeglichen und es findet keine Druckverstärkung statt. Die Düsennadel 10 ist geschlossen. Der Drosselkolben 50 befindet sich mit der Dichtkante 61 in Anlage an dem Injektorgehäuseabschnitt 45.In deactivated hibernation, which is in FIG. 1 is shown, the pressure booster control chamber 23 is acted upon by the 3/2-way valve 32 with the same pressure as the pressure booster working chamber 26. The connection to the return line 35 is closed. The pressure booster piston 25 is pressure balanced and there is no pressure gain. The nozzle needle 10 is closed. The throttle piston 50 is in contact with the injector housing section 45 with the sealing edge 61.

Zur Aktivierung des Injektors wird der Druckverstärkersteuerraum 23 druckentlastet. Dazu wird der Druckverstärkersteuerraum 23 mit Hilfe des 3/2-Wegeventils 32 von dem Hochdruckspeicher 2 abgekoppelt und wird über die Verbindungsleitung 29 in den Rücklauf 35 druckentlastet. Der Druck im Kompressionsraum 22 wird dadurch entsprechend dem Übersetzungsverhältnis des Druckverstärkers 5 erhöht und zur Einspritzdüse weitergeleitet. Die Einspritzdüse beginnt zu öffnen. Da der Bund 51 des Drosselkolbens 50 an dem Injektorgehäuseabschnitt 45 anliegt, also der Dichtsitz bei 61 geschlossen ist, muss dabei Kraftstoff über die Ablaufdrossel 47 und anschließend noch über die Zulaufdrossel 48 aus dem Düsennadelsteuerraum 44, der auch als Dämpfungsraum bezeichnet wird, verdrängt werden. Dadurch wird die Nadelöffnungsgeschwindigkeit verringert. Über den Durchfluss der Ablaufdrossel 47 lässt sich somit die Nadelöffnungsgeschwindigkeit einstellen.To activate the injector, the pressure booster control chamber 23 is depressurized. For this purpose, the pressure booster control chamber 23 is decoupled from the high-pressure accumulator 2 with the aid of the 3/2-way valve 32 and is depressurized via the connecting line 29 into the return line 35. The pressure in the compression chamber 22 is thereby increased according to the transmission ratio of the pressure booster 5 and forwarded to the injection nozzle. The injector starts to open. Since the collar 51 of the throttle piston 50 rests against the injector housing section 45, ie the sealing seat is closed at 61, fuel must be displaced via the outlet throttle 47 and then via the inlet throttle 48 from the nozzle needle control chamber 44, which is also referred to as a damping chamber. This reduces the needle opening speed. By way of the flow rate of the outlet throttle 47, the needle opening speed can thus be set.

In der vergrößerten Darstellung der Figur 2 sieht man, dass die erste Drossel 47 in einer zentralen Bohrung eines Drosselkolbens 50 ausgebildet ist, der einen Bund 51 aufweist. Der Bund 51 des Drosselkolbens 50 ist durch eine Druckfeder 53 gegen das der Spitze 11 entgegengesetzte Ende der Düsennadel 10 vorgespannt. Der Druck in dem Düsennadelsteuerraum 44 dient zur Steuerung der Einspritzung von Kraftstoff durch die Spritzlöcher 12, 13. Die Ablaufdrossel 47 weist einen geringeren Drosselquerschnitt als die Zulaufdrossel 48 auf. Wenn das 3/2-Wegeventil aus der in Figur 1 dargestellten Stellung in seine zweite (nicht dargestellte) Stellung geschaltet wird, dann wird der Düsennadelsteuerraum 44 über die Verbindungsleitungen 42, 41, 29 und 35 in dem (nicht dargestellten) Kraftstofftank entleert beziehungsweise entlastet. Beim Entleeren beziehungsweise Entlasten des Düsennadelsteuerraums 44 werden sowohl die erste Drossel 47 als auch die zweite Drossel 48 durchströmt. Aufgrund des Druckabfalls in dem Düsennadelsteuerraum 44 hebt die Düsennadel 10 mit ihrer Spitze 11 von dem zugehörigen Dichtsitz ab.In the enlarged view of the FIG. 2 it can be seen that the first throttle 47 is formed in a central bore of a throttle piston 50, which has a collar 51. The collar 51 of the throttle piston 50 is biased by a compression spring 53 against the tip 11 opposite end of the nozzle needle 10. The pressure in the nozzle needle control chamber 44 serves to control the injection of fuel through the injection holes 12, 13. The outlet throttle 47 has a smaller throttle cross-section than the inlet throttle 48. If the 3/2-way valve from the in FIG. 1 shown position is switched to its second (not shown) position, then the nozzle needle control chamber 44 via the connecting lines 42, 41, 29 and 35 in the (not shown) fuel tank emptied or relieved. When emptying or relieving the nozzle needle control chamber 44, both the first throttle 47 and the second throttle 48 are flowed through. Due to the pressure drop in the nozzle needle control chamber 44, the nozzle needle 10 lifts with its tip 11 from the associated sealing seat.

Solange der Druckverstärkersteuerraum 23 druckentlastet ist, bleibt der Druckverstärker 5 aktiviert und verdichtet den Kraftstoff in dem Druckverstärkerraum 22, der auch als Kompressionsraum bezeichnet werden kann. Der verdichtete Kraftstoff wird zur Düsennadel 10 weitergeleitet und eingespritzt. Der Drosselkolben 50 ist gleichzeitig als Hubanschlag für die Düsennadel 10 ausgebildet. Dadurch wird der Hubanschlag der Düsennadel 10 über die Höhe beziehungsweise Länge des Drosselkolbens 50 einstellbar, wodurch in der Fertigung des Injektors eine hohe Genauigkeit des Nadelhubs erreicht wird. Der Hubanschlag der Düsennadel 10 kann so ausgeformt sein, dass der Dichtsitz bei 61 und ein weiterer Dichtsitz bei 62 geschlossen werden, wenn das brennraumferne Ende der Düsennadel 10 an dem Drosselkolben 50 zur Anlage kommt. Dadurch wird verhindert, dass bei offener Düsennadel 10 der Druck an der Innenseite der Dichthülse 56 in dem Ringraum zwischen dem Drosselkolben 50 und der Dichthülse 56 zu stark absinkt. Dadurch kann eine unerwünscht große Verformung der Dichthülse 56 verhindert werden.As long as the pressure booster control chamber 23 is relieved of pressure, the pressure booster 5 remains activated and compresses the fuel in the booster chamber 22, which can also be referred to as a compression chamber. The compressed fuel is forwarded to the nozzle needle 10 and injected. The throttle piston 50 is also designed as a stroke stop for the nozzle needle 10. As a result, the stroke stop of the nozzle needle 10 is adjustable over the height or length of the throttle piston 50, whereby a high accuracy of the Nadelhubs is achieved in the production of the injector. The stroke stop of the nozzle needle 10 may be formed so that the sealing seat at 61 and another sealing seat at 62 are closed when the combustion chamber distal end of the nozzle needle 10 comes to rest on the throttle piston 50. This prevents that with open nozzle needle 10, the pressure on the inside of the sealing sleeve 56 in the annular space between the throttle piston 50 and the sealing sleeve 56 drops too much. As a result, an undesirably large deformation of the sealing sleeve 56 can be prevented.

Bei dem in Figur 3 dargestellten Ausführungsbeispiel ist der Drosselkolben 50 kürzer ausgebildet als bei dem in den Figuren 1 und 2 dargestellten Ausführungsbeispiel. In Figur 3 bildet der Drosselkolben 50 keinen Hubanschlag für die Düsennadel 10. Die Düsennadel 10 kommt bei dem in Figur 3 dargestellten Ausführungsbeispiel in ihrem oberen Hubanschlag mit ihrem brennraumfernen Ende 62 an einer Dichtkante 63 zur Anlage, die an dem Injektorgehäuseabschnitt 45 ausgebildet ist. Dadurch wird verhindert, dass nach dem Nadelöffnen der Druck an der Innenseite der Dichthülse 56 zu stark absinkt, so dass eine unerwünscht große Verformung der Dichthülse 56 verhindert wird.At the in FIG. 3 illustrated embodiment, the throttle piston 50 is formed shorter than that in the FIGS. 1 and 2 illustrated embodiment. In FIG. 3 forms the throttle piston 50 no stroke stop for the nozzle needle 10. The nozzle needle 10 comes in the in FIG. 3 illustrated embodiment in its upper stroke stop with its combustion chamber remote end 62 to a sealing edge 63 for conditioning, which is formed on the Injektorgehäuseabschnitt 45. This prevents that after needle opening, the pressure on the inside of the sealing sleeve 56 drops too much, so that an undesirably large deformation of the sealing sleeve 56 is prevented.

Zum Beenden der Einspritzung wird der Druckerstärkersteuerraum 23 durch das 3/2-Wegeventil 32 von dem Rücklauf 35 getrennt und mit dem Raildruck beaufschlagt, das heißt mit dem Kraftstoffhochdruckspeicher 2 verbunden. Dadurch baut sich in dem Druckverstärkersteuerraum 23 und der Verbindungsleitung 41, die auch als Steuerleitung bezeichnet werden kann, Raildruck auf. Gleichzeitig fällt der Druck in dem Druckverstärkerraum 22 und dem Druckraum 15 auf Raildruck ab. Der Drosselkolben 50 hebt von dem Injektorgehäuseabschnitt 45 ab und gibt damit den Dichtsitz bei 61 frei. Somit kann der Kraftstoff nur durch die Zulaufdrossel 48 gedrosselt in den Düsennadelsteuerraum 44 einströmen, wodurch in dem Düsennadelsteuerraum 44 ebenfalls Raildruck aufgebaut wird. Dadurch schließt die Düsennadel 10. Zum Nadelschließen muss der Düsennadelsteuerraum 44 nicht über die kleine Drossel 47 befüllt werden, wodurch ein schnelles Nadelschließen ermöglicht wird. Die Nadelschließgeschwindigkeit lässt sich über die Zulaufdrossel 48 unabhängig von der Öffnungsgeschwindigkeit einstellen.To terminate the injection of the printer amplifier control chamber 23 is separated by the 3/2-way valve 32 from the return line 35 and acted upon by the rail pressure, that is connected to the high-pressure fuel storage 2. As a result, rail pressure builds up in the pressure booster control chamber 23 and the connecting line 41, which can also be referred to as a control line. At the same time, the pressure in the pressure booster chamber 22 and the pressure chamber 15 drops to rail pressure. The throttle piston 50 lifts off from the Injektorgehäuseabschnitt 45 and thus releases the sealing seat at 61. Thus, the fuel can only flow throttled through the inlet throttle 48 in the nozzle needle control chamber 44, whereby in the nozzle needle control chamber 44 also rail pressure is built up. This closes the nozzle needle 10. For needle closing the nozzle needle control chamber 44 does not have to be filled via the small throttle 47, allowing a fast needle closing becomes. The needle closing speed can be adjusted via the inlet throttle 48, regardless of the opening speed.

Durch eine geeignete Systemauslegung kann in der Nadelschließphase kurzzeitig ein Überschwingen des Drucks in den Räumen 23 und 44 über Systemdruck und ein Unterschwingen in dem Raum 15 unter Systemdruck erreicht werden. Dadurch wird ein schnelles Nadelschließen erreicht. In der Schließphase tritt dabei im Dämpfungsraum 44 ein höherer Druck auf als im Druckraum 15, der auch als Zwischenraum bezeichnet wird. Dabei kann sich die Dichthülse 56 von der Kontaktstelle an dem Drosselkolben 50 lösen und der Schließdruck in dem Düsennadelsteuerraum 44 bricht ein. Durch die schließende Federkraft auf die Düsennadel 10 setzt diese ihre Schließbewegung jedoch fort. Dieses Öffnen der Dichthülse 56 kann dazu benutzt werden, um eine Durchspülung des Düsennadelsteuerraums 44 zu erreichen. Dadurch wird eine Erwärmung des Kraftstoffs in dem Düsennadelsteuerraum 44 verhindert. Falls ein Öffnen der Dichthülse 56 nicht erwünscht ist, kann dies durch eine entsprechend große Federkraft der Druckfeder 58 oder durch eine zusätzliche Federkraft auf die Dichthülse 56 vermieden werden.By means of a suitable system design, an overshoot of the pressure in the chambers 23 and 44 via system pressure and undershooting in the chamber 15 under system pressure can be achieved for a short time in the needle closing phase. This achieves a quick needle closure. In the closing phase occurs in the damping chamber 44, a higher pressure than in the pressure chamber 15, which is also referred to as an intermediate space. In this case, the sealing sleeve 56 can be released from the contact point on the throttle piston 50 and the closing pressure in the nozzle needle control chamber 44 breaks. Due to the closing spring force on the nozzle needle 10, however, this continues its closing movement. This opening of the sealing sleeve 56 can be used to achieve a flushing of the nozzle needle control chamber 44. This prevents heating of the fuel in the nozzle needle control chamber 44. If opening of the sealing sleeve 56 is not desired, this can be avoided by a correspondingly large spring force of the compression spring 58 or by an additional spring force on the sealing sleeve 56.

Nach dem Druckausgleich des Systems wird der Druckverstärkerkolben 25 durch die Druckverstärkerfeder 27, die auch als Rückstellfeder bezeichnet werden kann, in seine Ausgangslage zurückgestellt. Dabei wird der Druckverstärkerraum 22 über das Rückschlagventil 40 befüllt. Der Drosselkolben 50 wird durch die Druckfeder 53 in seine geschlossene Ruhelage zurückgestellt. Die Verbindungsleitung 41, die zum Beispiel als Steuerbohrung ausgeführt sein kann, kann alternativ auch mit dem Bereich Druckverstärkerarbeitsraum 26/Hochdruckspeicherraum 2 verbunden sein.After pressure equalization of the system, the pressure booster piston 25 is returned to its initial position by the booster spring 27, which may also be referred to as a return spring. In this case, the pressure booster chamber 22 is filled via the check valve 40. The throttle piston 50 is by the compression spring 53 in its closed rest position reset. The connecting line 41, which may be designed, for example, as a control bore, may alternatively also be connected to the region of the pressure booster working space 26 / high-pressure reservoir 2.

In Figur 4 ist eine ähnliche Kraftstoffeinspritzeinrichtung wie in Figur 1 dargestellt. Zur Bezeichnung gleicher Teile werden dieselben Bezugszeichen verwendet. Um Wiederholungen zu vermeiden, wird auf die vorangegangene Beschreibung der Figur 1 verwiesen. Im Folgenden wird nur auf die Unterschiede zwischen den beiden Ausführungsbeispielen eingegangen.In FIG. 4 is a similar fuel injector as in FIG. 1 shown. The same reference numerals are used to designate like parts. To avoid repetition, the preceding description of the FIG. 1 directed. In the following, only the differences between the two embodiments will be discussed.

Figur 4 zeigt ein Ausführungsbeispiel mit zwei getrennt ausgebildeten Drosselpfaden 71 und 73 in den Düsennadelsteuerraum 44. In dem Drosselpfad 71 ist eine Ablaufdrossel 72 vorgesehen. In dem Drosselpfad 73 sind ein Rückschlagventil 74 und eine Zulaufdrossel 75 vorgesehen. Durch die getrennt ausgebildeten Drosselpfade 71 und 73 kann das Volumen des Düsennadelsteuerraums 44 sehr klein gehalten werden, wodurch eine schwingungsreduzierte Nadelöffnung erreicht werden kann. Der Düsennadelsteuerraum 44 ist über die Drossel 72 mit der Steuerleitung 41 verbunden. Außerdem ist der Düsennadelsteuerraum 44 über die Drossel 75 und das Rückschlagventil 74 mit der Steuerleitung 41 verbunden. Die Nadelöffnungsgeschwindigkeit wird durch die Ablaufdrossel 72 bestimmt. Die Nadelschließgeschwindigkeit kann über die Zulaufdrossel 75 eingestellt werden. FIG. 4 shows an embodiment with two separately formed throttle paths 71 and 73 in the nozzle needle control chamber 44. In the throttle path 71, a discharge throttle 72 is provided. In the throttle path 73, a check valve 74 and an inlet throttle 75 are provided. Due to the separately formed throttle paths 71 and 73, the volume of the nozzle needle control chamber 44 can be kept very small, whereby a vibration-reduced needle opening can be achieved. The nozzle needle control chamber 44 is connected via the throttle 72 to the control line 41. In addition, the nozzle needle control chamber 44 is connected to the control line 41 via the throttle 75 and the check valve 74. The needle opening speed is determined by the drain throttle 72. The needle closing speed can be adjusted via the inlet throttle 75.

In Figur 5 ist eine ähnliche Kraftstoffeinspritzeinrichtung wie in Figur 4 dargestellt. Zur Bezeichnung gleicher Teile werden dieselben Bezugszeichen verwendet. Um Wiederholungen zu vermeiden, wird auf die vorangegangene Beschreibung der Figur 4 verwiesen. Im Folgenden wird nur auf die Unterschiede zwischen den beiden Ausführungsbeispielen eingegangen.In FIG. 5 is a similar fuel injector as in FIG. 4 shown. The same reference numerals are used to designate like parts. To avoid repetition, the preceding description of the FIG. 4 directed. In the following, only the differences between the two embodiments will be discussed.

Bei dem in Figur 5 dargestellten Ausführungsbeispiel wird eine andere Bauform der Düsennadel 10 verwendet. Die beiden Zulaufpfade 71 und 73, die auch als Drosselpfade bezeichnet werden können, münden in einen Düsennadelsteuerraum 80, in dem eine Düsennadelfeder 81 angeordnet ist. Durch die Vorspannkraft der Düsennadelfeder 81 wird die Düsennadel 10 mit ihrer Spitze 11 gegen den zugehörigen Dichtsitz in Anlage gehalten. An der Düsennadel 10 ist eine Druckschulter 83 ausgebildet, die in einem im Wesentlichen ringförmigen Druckraum 84 angeordnet ist. Der Druckraum 84 steht über eine Verbindungsleitung 86 mit dem Druckverstärkerraum 22 in Verbindung. Wenn der Druck in dem Düsennadelsteuerraum 80 abnimmt, dann hebt die Düsennadel 10 mit ihrer Spitze 11 von dem zugehörigen Sitz ab und der mit Hochdruck beaufschlagte Kraftstoff in dem Druckraum 84 wird durch die Spritzlöcher 12, 13 in den Brennraum der Brennkraftmaschine eingespritzt.At the in FIG. 5 illustrated embodiment, another design of the nozzle needle 10 is used. The two inlet paths 71 and 73, which can also be referred to as throttle paths, open into a nozzle needle control chamber 80, in which a nozzle needle spring 81 is arranged. By the biasing force of the nozzle needle spring 81, the nozzle needle 10 is held with its tip 11 against the associated sealing seat in abutment. On the nozzle needle 10, a pressure shoulder 83 is formed, which is arranged in a substantially annular pressure chamber 84. The pressure chamber 84 is connected via a connecting line 86 to the pressure booster chamber 22 in connection. When the pressure in the nozzle needle control chamber 80 decreases, the nozzle needle 10 lifts with its tip 11 from the associated seat and the high-pressure fuel in the pressure chamber 84 is injected through the injection holes 12, 13 in the combustion chamber of the internal combustion engine.

Claims (13)

  1. Device for the injection of fuel into a combustion chamber of an internal combustion engine, having a metering valve (32) and having a fuel injector (1) which can be loaded with highly pressurized fuel via a high-pressure source (2) and can be actuated via the metering valve (32), the pressure in a first control line (29) being built up by the activation of the metering valve (32), with the result that a pressure intensifier (5) is activated by a pressure-intensifier control space (23) being relieved of pressure via the first control line (29) via a return line (35), it being possible for the pressure in a nozzle-needle control space (44) to be controlled via the metering valve (32) in such a way that a nozzle needle (10) opens and closes for the injection of fuel, it being possible for the nozzle-needle control space (44) to be emptied via an outflow throttle device (47, 72) and to be filled via an inflow throttle device (48, 75), and the pressure-intensifier control space (23) and the nozzle-needle control space (44) being connected via a hydraulic connection, characterized in that the hydraulic connection between the pressure-intensifier control space (23) and the nozzle-needle control space (44) contains a second control line (41), in that the nozzle-needle control space (44) can be emptied via the outflow throttle device into the second control line (41) and can be filled via the inflow throttle device from the second control line (41), and in that the throttle cross section of the outflow throttle device (47, 72) is smaller than the throttle cross section of the inflow throttle device (48, 75).
  2. Fuel injection device according to Claim 1, characterized in that a valve element (74) is provided which is closed when the injection valve-element control space (44) is emptied and which is open when the injection valve-element control space (44) is filled.
  3. Fuel injection device according to one of the preceding claims, characterized in that the outflow throttle device displays its throttling action only during emptying of the injection valve-element control space (44) and does not display any throttling action during filling of the injection valve-element control space (44), but rather ensures an unimpeded passage of fuel.
  4. Fuel injection device according to Claim 3, characterized in that the two throttle devices are connected in series.
  5. Fuel injection device according to Claim 3 or 4, characterized in that the two throttle devices are arranged centrally in relation to the longitudinal axis of the fuel injector (1).
  6. Fuel injection device according to one of Claims 3 to 5, characterized in that the outflow throttle device comprises a throttle element (50) with a sealing edge (61), which throttle element (50) is prestressed by a spring element (53) in such a way that the sealing edge (61) is pressed against an associated sealing seat when the throttle element (50) is flowed through in the emptying direction, and in such a way that the sealing edge (61) raises up from its sealing seat when the throttle element (50) is flowed through in the filling direction.
  7. Fuel injection device according to Claim 6, characterized in that the throttle element (50) comprises a throttling piston which is prestressed by the spring element (53), is equipped with a through hole which has a throttle point, and the free end of which forms a stroke stop for the nozzle needle (10).
  8. Fuel injection device according to Claim 7, characterized in that the stroke stop (62) of the nozzle needle (10) is configured in such a way that a sealing seat (61) and a further sealing seat (62) are closed when that end of the nozzle needle (10) which is remote from the combustion chamber comes into contact with the throttling piston (50).
  9. Fuel injection device according to one of Claims 1 to 6, characterized in that, at its upper stroke stop, the nozzle needle (10) comes into contact with its end (62) which is remote from the combustion chamber with a sealing edge (63) which is formed on an injector-housing section (45).
  10. Fuel injection device according to one of Claims 1 to 3, characterized in that the two throttle devices are connected in parallel.
  11. Fuel injection device according to Claim 10, characterized in that the inflow throttle device comprises a throttle element (75) which is connected in series to a non-return valve in such a way that the throttle element (75) is flowed through only in the filling direction and is closed in the emptying direction.
  12. Fuel injection device according to Claim 10 or 11, characterized in that the inflow throttle device is arranged eccentrically in relation to the longitudinal axis of the fuel injector (1).
  13. Fuel injection device according to one of Claims 10 to 12, characterized in that the outflow throttle device is arranged centrally in relation to the longitudinal axis of the fuel injector (1).
EP05101652A 2004-05-18 2005-03-03 Fuel injection device Not-in-force EP1598551B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004024527A DE102004024527A1 (en) 2004-05-18 2004-05-18 Fuel injection system
DE102004024527 2004-05-18

Publications (2)

Publication Number Publication Date
EP1598551A1 EP1598551A1 (en) 2005-11-23
EP1598551B1 true EP1598551B1 (en) 2011-08-24

Family

ID=34938875

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05101652A Not-in-force EP1598551B1 (en) 2004-05-18 2005-03-03 Fuel injection device

Country Status (3)

Country Link
US (1) US20050263135A1 (en)
EP (1) EP1598551B1 (en)
DE (1) DE102004024527A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004017305A1 (en) * 2004-04-08 2005-10-27 Robert Bosch Gmbh Fuel injection device for internal combustion engines with directly controllable nozzle needles
DE102004053274A1 (en) * 2004-11-04 2006-05-11 Robert Bosch Gmbh Fuel injection system
DE102005030220A1 (en) * 2005-06-29 2007-01-04 Robert Bosch Gmbh Injector with switchable pressure intensifier
DE102005058556B4 (en) * 2005-12-08 2017-04-06 Man Diesel & Turbo Se Injector of a fuel injection system
JP4519143B2 (en) * 2007-01-19 2010-08-04 株式会社デンソー Injector
US9163597B2 (en) * 2008-10-01 2015-10-20 Caterpillar Inc. High-pressure containment sleeve for nozzle assembly and fuel injector using same
DE102009000181A1 (en) * 2009-01-13 2010-07-15 Robert Bosch Gmbh Fuel injector
DE102010001170A1 (en) * 2010-01-25 2011-07-28 Robert Bosch GmbH, 70469 Injection device with reduced pressure oscillations
EP2912300B1 (en) 2012-10-25 2018-05-30 Picospray, Inc. Fuel injection system
DE102013212269A1 (en) * 2013-06-26 2014-12-31 Robert Bosch Gmbh Fuel injection valve for internal combustion engines
US10197025B2 (en) 2016-05-12 2019-02-05 Briggs & Stratton Corporation Fuel delivery injector
CN109790806B (en) 2016-07-27 2021-05-25 布里格斯斯特拉顿有限责任公司 Reciprocating pump injector
US10947940B2 (en) 2017-03-28 2021-03-16 Briggs & Stratton, Llc Fuel delivery system
WO2020077181A1 (en) 2018-10-12 2020-04-16 Briggs & Stratton Corporation Electronic fuel injection module

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2885076B2 (en) * 1994-07-08 1999-04-19 三菱自動車工業株式会社 Accumulator type fuel injection device
GB9614822D0 (en) * 1996-07-13 1996-09-04 Lucas Ind Plc Injector
IT1289795B1 (en) * 1996-12-23 1998-10-16 Elasis Sistema Ricerca Fiat IMPROVEMENTS TO AN ELECTROMAGNETICALLY OPERATED DOSING VALVE, WITH BALL SHUTTER, FOR A FUEL INJECTOR.
DE19822503C1 (en) * 1998-05-19 1999-11-25 Siemens Ag Control valve for fuel injector
US6293254B1 (en) * 2000-01-07 2001-09-25 Cummins Engine Company, Inc. Fuel injector with floating sleeve control chamber
DE10123775B4 (en) * 2001-05-16 2005-01-20 Robert Bosch Gmbh Fuel injection device for internal combustion engines, in particular common rail injector, and fuel system and internal combustion engine
DE10218904A1 (en) * 2001-05-17 2002-12-05 Bosch Gmbh Robert Fuel injection system
EP1395748B1 (en) * 2001-05-21 2005-05-18 Robert Bosch Gmbh High pressure sealing element for injectors
DE10158951A1 (en) * 2001-12-03 2003-06-12 Daimler Chrysler Ag Fuel Injection system for IC engine, operates with pressure conversion, has connection from control chamber and admission chamber to return line passing via common valve connection
DE10160263A1 (en) * 2001-12-07 2003-06-18 Bosch Gmbh Robert Fuel injection device for an internal combustion engine
DE10229419A1 (en) * 2002-06-29 2004-01-29 Robert Bosch Gmbh Pressure-translated fuel injector with rapid pressure reduction at the end of injection
GB0215490D0 (en) * 2002-07-04 2002-08-14 Delphi Tech Inc Control valve arrangement
JP4007103B2 (en) * 2002-07-11 2007-11-14 株式会社豊田中央研究所 Fuel injection device
SE523110C2 (en) 2002-07-15 2004-03-30 Stock Of Sweden Ab hydraulic System
DE10300045A1 (en) * 2003-01-03 2004-07-15 Robert Bosch Gmbh Inward opening vario nozzle
DE10335211A1 (en) * 2003-08-01 2005-02-17 Robert Bosch Gmbh Fuel injection device for an internal combustion engine
DE10346222A1 (en) * 2003-09-23 2005-04-14 Robert Bosch Gmbh Fuel injection device, especially for internal combustion engine with direct injection, has alignment arrangement that aligns sleeve part radially relative to housing recess and valve element is guided in sleeve part

Also Published As

Publication number Publication date
EP1598551A1 (en) 2005-11-23
US20050263135A1 (en) 2005-12-01
DE102004024527A1 (en) 2005-12-15

Similar Documents

Publication Publication Date Title
EP1598551B1 (en) Fuel injection device
EP1771651B1 (en) Fuel injector comprising a direct multi-stage injection valve member control system
EP1636484B1 (en) Injector for internal combustion engines
EP1654456B1 (en) Fuel injection device for an internal combustion engine
DE19742320A1 (en) Fuel injector
WO2005019637A1 (en) Fuel injection valve controlled by a pilot valve
EP1657428B1 (en) Fuel injection apparatus
DE10336327A1 (en) Injector for fuel injection systems of internal combustion engines, in particular direct injection diesel engines
EP1520100B1 (en) Device for attenuating the stroke of the needle in pressure-controlled fuel injectors
DE19919432C2 (en) Common rail injector
DE102009000181A1 (en) Fuel injector
EP1117921B1 (en) Fuel injector for a common rail fuel system
DE19939939A1 (en) Injector for a common rail injection system for internal combustion engines with a compact design
EP2743493A2 (en) Fuel injector
EP2156045B1 (en) Injector
EP1719904A1 (en) Fuel injector
DE60111164T2 (en) Fuel injection valve with piezoelectric actuator
DE3009750C2 (en) Fuel injection device for internal combustion engines
WO2004022929A1 (en) Hydraulic valve actuator for actuating a gas exchange valve
WO2005014997A1 (en) Fuel injection device for a combustion engine
EP2275666A1 (en) Fuel injector with pressure-equalised control valve
DE10147830B4 (en) fuel injector
DE102007034319A1 (en) injector
EP1377745B1 (en) Method for operating a pump-nozzle unit and a corresponding pump-nozzle unit
DE10160490B4 (en) Fuel injection device, fuel system and internal combustion engine

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR LV MK YU

17P Request for examination filed

Effective date: 20060523

AKX Designation fees paid

Designated state(s): DE ES FR IT

17Q First examination report despatched

Effective date: 20080919

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE ES FR IT

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502005011802

Country of ref document: DE

Effective date: 20111020

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20120525

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502005011802

Country of ref document: DE

Effective date: 20120525

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111205

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20150324

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20150319

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20161130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160303

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20170529

Year of fee payment: 13

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502005011802

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181002