EP2310662A1 - Fuel injector - Google Patents

Fuel injector

Info

Publication number
EP2310662A1
EP2310662A1 EP09779562A EP09779562A EP2310662A1 EP 2310662 A1 EP2310662 A1 EP 2310662A1 EP 09779562 A EP09779562 A EP 09779562A EP 09779562 A EP09779562 A EP 09779562A EP 2310662 A1 EP2310662 A1 EP 2310662A1
Authority
EP
European Patent Office
Prior art keywords
pressure
fuel
injector
guide
injection valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP09779562A
Other languages
German (de)
French (fr)
Other versions
EP2310662B1 (en
Inventor
Matthias Burger
Hans-Christoph Magel
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 EP2310662A1 publication Critical patent/EP2310662A1/en
Application granted granted Critical
Publication of EP2310662B1 publication Critical patent/EP2310662B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
    • F02M47/027Electrically actuated valves draining the chamber to release the closing pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type
    • F02M61/12Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for valve bodies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • 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
    • F02M63/0003Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure
    • F02M63/0005Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure using valves actuated by fluid 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
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/30Fuel-injection apparatus having mechanical parts, the movement of which is damped
    • F02M2200/304Fuel-injection apparatus having mechanical parts, the movement of which is damped using hydraulic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/70Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
    • F02M2200/703Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/70Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
    • F02M2200/703Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic
    • F02M2200/704Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic with actuator and actuated element moving in different directions, e.g. in opposite directions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/70Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
    • F02M2200/703Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic
    • F02M2200/705Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic with means for filling or emptying hydraulic chamber, e.g. for compensating clearance or thermal expansion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2547/00Special features for fuel-injection valves actuated by fluid pressure
    • F02M2547/003Valve inserts containing control chamber and valve piston
    • 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
    • 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
    • F02M63/007Details not provided for in, or of interest apart from, the apparatus of the groups F02M63/0014 - F02M63/0059
    • F02M63/0078Valve member details, e.g. special shape, hollow or fuel passages in the valve member
    • F02M63/008Hollow valve members, e.g. members internally guided

Definitions

  • the invention relates to a fuel injector for injecting fuel into a combustion chamber of an internal combustion engine according to the preamble of claim 1.
  • a trained as a common rail injector fuel injector which has a two-part injection valve element, which via a control valve (servo-valve) can be controlled.
  • the two parts of the injection valve element are coupled together via a hydraulic coupler.
  • the known fuel injector is low leakage, ie executed without low pressure stage.
  • a closing throttle is introduced in a connection channel supplying fuel to a lower nozzle chamber.
  • a disadvantage of the known fuel injector is that the two parts of the injection valve element do not react as a single part, but delayed in a control of the injection valve element. This can only be compensated by very fast switching control valves, which, however, is associated with higher costs.
  • the invention is therefore based on the object to propose an alternative fuel injector, in which at least two injection valve element parts are coupled together via a low-leakage hydraulic coupler.
  • the invention is based on the idea of achieving strong compression of the two separate injector element parts coupled by means of the hydraulic coupler in that the hydraulic coupler, more precisely a coupler space of the coupler, in particular permanently, with a low pressure source, in particular a connected to an injector return low pressure region of the injector is connected. Due to the reduced pressure within the hydraulic coupler compared to the high-pressure region of the fuel injector, the injection valve element parts are permanently and substantially interconnected during operation of the fuel injector, so that from a functional point of view they can be considered as one-piece.
  • a fuel injector designed according to the concept of the invention provides that both guides are surrounded at least in sections radially outward with fuel under high pressure.
  • the at least one injector component which delimits the guide gap radially outwardly, is surrounded by high-pressure fuel in an area radially outward of the respective guide gap formed between the at least one injector component and the injection valve element, thereby expanding the guide gaps by penetrating into the guide gaps High pressure fuel is avoided.
  • a low-pressure stage is realized, which causes a force acting in the closing direction of the injection valve element hydraulic force.
  • the injection valve element switching time can be accelerated. Since the closing force generated by the low-pressure stage, hydraulic, acting on the injection valve element, closing force is rail horrin, this closing force acts not only during the injection, as in a closing throttle, but permanently.
  • an additional closing throttle which reduces the fuel pressure in the region of the injection valve element support in comparison to the fuel pressure in the region of an inlet passage of the fuel injector, is dispensed with. By providing a closing throttle, the effective injection pressure would be reduced by up to 150 bar.
  • the low-pressure stage is preferably realized by reducing the diameter of the nozzle-hole-adjacent injection valve member member (nozzle needle) as compared to the diameter of the nozzle-hole-remote injector member member in a hydraulic coupler-limiting portion (something).
  • the guide diameter of the guide facing the nozzle hole arrangement is preferably somewhat smaller than the guide diameter of the other, the hydraulic coupler axially delimiting (in particular upper) guide.
  • the hydraulic coupler is connected via a connecting channel to a low pressure region of the fuel injector.
  • the connecting channel at least approximately, throttle-free, prevails within the hydraulic coupler, at least approximately, low pressure, preferably in a pressure range between about 0 and 20 bar.
  • At least one of the two, the hydraulic coupler limiting guides is formed by a sleeve-shaped extension of a plate member, said sleeve-shaped extension, at least partially, preferably completely, radially outwardly surrounded by under high pressure fuel is. It is particularly preferred to provide a portion of the connecting channel, in particular as a radial channel, in the plate element, which connects the hydraulic coupler to the low-pressure region of the fuel injector. In the low-pressure region of the fuel injector, not only the named connection channel but also a discharge channel from a control chamber, via which fuel flows out of the control chamber in the direction of the injector return when the control valve is open, preferably discharges.
  • the plate member at least one, preferably throttle-free, axial channel is provided, can flow through the fuel with the injector element open in the axial direction of the nozzle hole arrangement. It is particularly expedient if the plate element is arranged between an (upper) injector body and a (lower) nozzle nozzle arrangement having a nozzle body, that is clamped between these housing parts. Preferably, the nozzle body is screwed by means of a union nut with an external thread of the injector body.
  • At least one of the couplers axially delimiting guides is formed by a sleeve arranged in a high-pressure chamber, in particular spring-loaded sleeve.
  • a sleeve arranged in a high-pressure chamber, in particular spring-loaded sleeve.
  • the sleeve is pressed by the spring in the axial direction against the previously explained plate element is particularly expedient.
  • this spring is at the same time the closing spring acting on an injection valve element part in the direction of the nozzle hole arrangement, which is located at one end on the sleeve and at other ends on the injection valve element part, in particular on a circumferential collar or a retaining ring of the injection valve element. element part, supports.
  • the hydraulic coupler is placed at the low pressure applied to the injector return.
  • the pressure in the hydraulic coupler is dimensioned such that it lies under the high pressure of the fuel outside the guides delimiting the hydraulic coupler but above the low pressure in the region of the injector return.
  • at least one throttle is preferably applied in the connecting channel connecting the hydraulic coupler to the low-pressure region. assigns. This is adjusted so that the pressure in the hydraulic coupler is higher than in the area of the injector return. By implementing a higher (low) pressure in the hydraulic coupler compared to the low pressure in the injector return region, the component load in the area of the hydraulic coupler is reduced.
  • the pressure in the hydraulic coupler is now load-dependent, it is preferred, in the case of providing such a throttle, to dispense with a low-pressure stage in the hydraulic coupler, so that the hydraulic coupler no longer has the function of a hydraulic Closing force to produce, but only a coupling function. Due to the slightly increased pressure in the hydraulic coupler, the already small amount of leakage, which flows through the guides into the hydraulic coupler and thus into the low-pressure area, is further reduced.
  • the throttle is designed so that the pressure in the hydraulic coupler corresponds approximately to half the rail pressure.
  • a closing throttle is preferably provided for generating a hydraulic closing force, which is dimensioned such that the pressure in the region of the tip of the injection valve element is lower, preferably by about 50 to 200 bar, than the rail pressure.
  • An embodiment in which such a closing throttle is arranged in an injector component which delimits a control chamber radially on the inside is structurally particularly elegant.
  • an inlet throttle for the control chamber and an outlet throttle from the control chamber and possibly also a filling throttle are preferred in this injector component. Throttle introduced for accelerated refilling the control chamber.
  • Fig. 1 shows a first embodiment of a fuel injector with a connected to a low pressure region of the fuel Inj ector hydraulic coupler with low pressure stage and
  • Fig. 2 shows an embodiment of a fuel injector with connected to a low pressure region of the fuel injector hydraulic coupler without low pressure stage and arranged in a connecting channel between the hydraulic coupler and the low pressure region throttle for adjusting the pressure in the hydraulic coupler.
  • Fig. 1 is designed as a common rail injector fuel Inj ector 1 for injecting fuel into a combustion chamber, not shown, of an internal combustion engine an presented a motor vehicle.
  • a high pressure pump 2 delivers fuel from a reservoir 3 in a high-pressure fuel storage 4 (Rail).
  • this fuel especially diesel or gasoline, under high pressure, stored in this embodiment about 2000 bar.
  • the fuel injector 1 is connected, among other injectors, not shown, via a supply line 5.
  • the supply line 5 opens into a supply channel 6 of the fuel injector 1, which opens into a high-pressure chamber 7 of the fuel injector 1.
  • the high-pressure chamber 7 forms a mini-rail, due to which pressure oscillations are minimized.
  • a return line 8 a low-pressure region 9 of the fuel injector 1 is connected to the reservoir 3. Via an injector return port 10 and the return line 8, a control amount to be explained later as well as a small amount of leakage of fuel from the fuel injector 1 to the reservoir 3 can flow off.
  • the fuel injector 1 has a housing 11, which has an injector body 12 into which the supply channel 6 is introduced and comprises a lower nozzle body 13. Between the injector body 12 and the nozzle body 13, a plate element 14 to be explained later is clamped, wherein the nozzle body 13 is braced against the plate element 14 by means of a union nut 15 and this in turn against the nozzle body 13.
  • the union nut 15 is screwed to an external thread of the injector body 12.
  • the head part of the housing 11 is formed by a clamping nut 16, which is screwed to the injector body 12, and which clamps a cover element 17, comprising the injector return port 10, against an electromagnet arrangement 18 of an electromagnetic actuator 19 to be explained later. which in turn rests in the axial direction on an inner shoulder 20 of the clamping nut 16.
  • a two-part injection valve element 21 is accommodated in the housing 11, more precisely in the injector body 12 and in the duplex body 13, a two-part injection valve element 21 is accommodated.
  • This comprises an upper, first part 22 (control rod) and a lower, second part 23 (nozzle needle).
  • the first and the second part 22, 23 of the injection valve element 21 are coupled to each other via a hydraulic coupler 24 to be explained later and behave like a single component.
  • the second, lower part 23 of the injection valve element 21 is guided in a guide bore 25 in the nozzle body 13.
  • axial channels 26 are formed on the outer circumference of the second part 23 in an area within the guide bore 25, through which fuel can flow from the high-pressure chamber 7 into a lower annular space 67 when the injection valve element 21 is open, in which substantially the same fuel pressure prevails as in the high-pressure space 7.
  • the axial channels 26 designed as bevels and an axial channel 66 in the plate element 14 are (at least approximately) throttle-free.
  • the fuel pressure in a gap 27 formed between the plate element 14 and the guide bore 25 also corresponds to the fuel pressure within the high-pressure space 7.
  • the closing throttle otherwise required in the prior art is used in the embodiment. Measure Fig. 1 (in contrast to the later still to be explained embodiment of FIG. 2) deliberately omitted.
  • the injection valve element 21, more precisely the second part 23, has at its tip 28 a closing surface 29 with which the injection valve element 21 can be brought into tight contact with an injection valve element seat 30 (nozzle needle seat) formed inside the nozzle body 13.
  • an injection valve element seat 30 nozzle needle seat
  • the injection valve element 21 abuts against its injection valve element seat 30, i. is in a closed position, the fuel outlet from a Düsenlochanord- tion 31 is locked. If, on the other hand, it is lifted from its injection valve element seat 30 and is in an open position, here fuel can flow from the high-pressure chamber 7 via the intermediate space 27 and the lower annular space 67 past the injection valve element seat 30 to the nozzle hole arrangement 31 and essentially there under high pressure (rail pressure) standing in the combustion chamber are injected.
  • a Steuerkam- mer 35 is limited, via a radially extending in the sleeve-shaped portion 33 inlet throttle 36 with high pressure Stagnant fuel from the high-pressure chamber 7 is supplied.
  • the control chamber 35 is connected to a valve chamber 39 of a control valve 40 (servo-valve) via a drain throttle 38 provided in an upper, plate-shaped section 37 of the injector component 34.
  • the valve chamber 39 is bounded radially outwardly by a sleeve-shaped control valve member 41, which is integral with one with the electromagnetic actuator 19 cooperating armature plate 42 is formed.
  • the sleeve-shaped control valve element 41 is pressure balanced in its closed position in the axial direction.
  • the control chamber 35 is bounded axially upward by a guide pin 43 which is axially supported on the cover member 17 and on the one hand has the task to guide the control valve member 41 during its adjustment and on the other hand to seal the valve chamber 39 in the axial direction upwards.
  • the pressure in the control chamber 35 decreases rapidly, whereby the injection valve element 21 experiences a resulting opening force and abuts in the sequence with an end-side abutment portion 45 on the ceiling of the sleeve-shaped portion 33.
  • the injection valve element 21 thus lifts off from its injection valve element seat 30, so that fuel can flow out through the nozzle hole arrangement 31.
  • the energization of the solenoid assembly 18 of the electromagnetic actuator 19 is interrupted.
  • the sleeve-shaped control valve element 41 moves back onto its control valve seat 44.
  • the fuel flowing in through the inlet throttle 36 rapidly increases the pressure in the control chamber 35, as a result of which the injection valve element 21 is supported by the Spring force of a closing spring 47, is moved back to its injection valve element seat 30, which in turn the fuel flow from the Düsenlochan- Regulation 31 is interrupted in the combustion chamber.
  • the filling of the control chamber 35 via the inlet throttle 36 is accelerated via a Ruddrossel 61 which connects the high pressure chamber 7 permanently hydraulically with the valve chamber 39. Possibly. can also be dispensed with this Feedbackrossel 61.
  • the first and second parts 22, 23 of the injection valve element 21 are hydraulically coupled together in the hydraulic coupler 24, more specifically in a coupler space 48, and behave as a single component. This is due to the fact that the hydraulic coupler 24, or the coupler chamber 48 is permanently connected via a multi-part connecting channel 49 with the arranged in the injector low-pressure region 9 of the fuel injector 1, and thus during operation of the fuel injector 1 permanently low pressure.
  • the connecting channel 49 is formed by a radial channel 50 provided in the plate element 14, an annular space 51 radially between the plate element 14 and the union nut 15 and a vertical channel 52 in the injector body 12.
  • the hydraulic coupler 24 is limited in the embodiment shown in the axial direction upward by a first guide 53 for the first part 22 of the injection valve element 21 and in the axial direction down from a second guide 54 for the second, lower part 23 of the injection valve element 21st
  • the first guide 53 comprises a first guide gap 55 (annular gap) radially between a sleeve-shaped extension 56 of the plate member 14 and a lower portion of the first part 22 of the injection valve element 21.
  • the second guide 54 comprises a second guide gap 57 (annular gap) radially between a
  • the closing spring 47 is supported at one end on the lower end face of the sleeve 58 and at the other end on a circumferential collar 59 of the second part 23 of the injection valve element 21 from the closing spring 47 spring-loaded sleeve 58 and an upper portion of the second part 23 of the injection valve element 21.
  • the guide gaps 55, 57 are comparatively fuel-tight. This is primarily attributable to the fact that the first guide 53, more precisely the sleeve-shaped extension 56, is arranged inside the high-pressure chamber 7, that is to say is surrounded radially on the outside by high-pressure fuel. As a result, the first guide gap 55 experiences no expansion radially outward due to the low leakage flowing through the first guide gap 55 into the coupler space 48.
  • the second guide 54 more precisely, the sleeve 58 is disposed within the gap 27, in which approximately the same pressure prevails as in the high-pressure chamber 7, so that the second guide gap 57 is not widened because the sleeve 58 radially outward from under high pressure Fuel is surrounded. As a result, the lever, which flows via the guides 53, 54 into the hydraulic coupler 24, is level, which continues to flow via the connecting channel 49 in the low-pressure region 9, low.
  • a low-pressure stage 60 is realized in the hydraulic coupler 24, which has a force acting in the closing direction on the injection valve element 21.
  • the low-pressure stage 60 is realized in that the diameter O 1 of the first part 21 in the region of the first guide 53 is (slightly) greater than the diameter Du of the second part 23 of the injection valve element 21 in the region of the second guide 54.
  • the injection valve element 21 should only open when the control valve 40 can already be operated non-ballistically. Without the realized low-pressure stage 60, the start of injection can be delayed only for a mechanically soft injection valve element 21 or a small drain / inlet throttle ratio. Both measures lead to disadvantages in the injector behavior: While a soft injection valve element 21 leads to a poorer multiple injection suitability, a small drain / feed throttle ratio reduces the increase in the jet force of the injection jet and generally leads to emission disadvantages.
  • a throttle 62 is integrated in the connecting channel 49, more precisely in the radial channel 50 between the hydraulic coupler 24 and the low-pressure region 9. This is designed so that approximately half the pressure prevails in the hydraulic coupler 24, more precisely in the coupler chamber 48, as in the high-pressure chamber 7 and in the intermediate space 27. This is achieved by the pressure drop across the guides 53, 54 being approximately equal to the Pressure drop at the throttle 62 corresponds.
  • the effluent via the guide gaps 55, 56 leakage amount is further reduced.
  • the component load of the plate member 14 and the sleeve 58 is reduced.
  • the diameters O 1 and Du of the first and second part 22, 23 of the injection valve element 21 in the region of the guides 53, 54 are the same size - so it became aware of the realization of a low-pressure stage in the hydraulic coupler 24 omitted, since the pressure in the hydraulic coupler 24 by the provision of the throttle 62 is load-dependent and thus fluctuates during operation, which would result in fluctuating closing forces in the event that a low pressure stage would be provided in the coupler 24.
  • the embodiment of FIG. 2 with a low pressure stage to equip for certain applications analogous to the embodiment of FIG. Due to the omission of a low-pressure stage, production-related and / or temperature-dependent guide leakage fluctuations on the guides 53, 54 do not affect the injector function.
  • the fuel injector 1 according to FIG. 2 is equipped with an additional closing throttle 63, which is introduced into the sleeve-shaped section 33 of the injector component 34.
  • This connects the high-pressure chamber 7 with an annular, additional inlet chamber 64, which surrounds the sleeve-shaped section 33 radially on the outside in comparison with FIG. 1, and which is sealed by way of an annular sealing element 65 with respect to the high-pressure space 7 serving as a minirail.
  • the closing throttle 63 is designed in the illustrated embodiment so that the pressure in the high-pressure chamber 7 is about 50-200 bar less than the rail pressure in Zulaufhoffm 64.
  • the inlet throttle 36 and the Golfdrossel 61 do not open the high-pressure chamber 7, but from the inlet chamber 64.
  • the throttle 62 can, as shown, be designed as a simple throttle bore. Due to the necessary small flow cross sections which are necessary in the throttle 62, a conventional throttle bore, however, is relatively difficult to produce for reasons of tolerance. Therefore, it is preferable to perform the throttle 62 as an annular gap throttle. This can be achieved, for example, by positioning an insert part, for example a pin, in the actual throttle bore, on which the Fuel must flow past radially outside. The advantage of such a construction is the easier manufacturability.

Abstract

The invention relates to a fuel injector (1) and, in particular, to a common-rail injector for injecting fuel into a combustion chamber of an internal combustion engine with a multi-part injection valve element (21), which can be adjusted between an open position and a closed position, wherein a first part (22 ) and a second part (23) of the injection valve element (21) are coupled to one another via a hydraulic coupler (24), which is bounded radially by a first guide (53) for the first part (22) and by a second guide (54) for the second part (23). According to the invention, at least some sections of the first and the second guide (53, 54) are surrounded at their outer radii by fuel under high pressure, and the pressure realized in the hydraulic coupler (24) is lower than the pressure radially outside the guides (53, 54).

Description

Beschreibungdescription
Titeltitle
Kraftstoff-InjektorFuel injector
Stand der TechnikState of the art
Die Erfindung betrifft einen Kraftstoff-Injektor zum Einspritzen von Kraftstoff in einen Brennraum einer Brenn- kraftmaschine gemäß dem Oberbegriff des Anspruchs 1.The invention relates to a fuel injector for injecting fuel into a combustion chamber of an internal combustion engine according to the preamble of claim 1.
Aus der DE 10 2006 008 648 Al ist ein als Common-Rail- Injektor ausgebildeter Kraftstoff-Injektor bekannt, der ein zweiteiliges Einspritzventilelement aufweist, welches über ein Steuerventil (Servo-Ventil) ansteuerbar ist. Die beiden Teile des Einspritzventilelementes sind über einen hydraulischen Koppler miteinander gekoppelt. Im Ruhezustand des Kraftstoff-Injektors herrscht im hydraulischen Koppler Raildruck. Der bekannte Kraftstoff-Injektor ist leckagearm, d.h. ohne Niederdruckstufe ausgeführt. Zum Erzielen einer ausreichenden hydraulischen Nadelschließkraft ist in einem einen unteren Düsenraum mit Kraftstoff versorgenden Verbindungskanal eine Schließdrossel eingebracht. Nachteilig bei dem bekannten Kraftstoff-Injektor ist es, dass die beiden Teile des Einspritzventilelementes nicht wie ein einziges Teil, sondern verzögert bei einer Ansteuerung des Einspritzventilelementes reagieren. Dies kann nur durch sehr schnell schaltende Steuerventile kompensiert werden, was jedoch mit höheren Kosten verbunden ist. Offenbarung der Erfindung Technische AufgabeFrom DE 10 2006 008 648 Al a trained as a common rail injector fuel injector is known, which has a two-part injection valve element, which via a control valve (servo-valve) can be controlled. The two parts of the injection valve element are coupled together via a hydraulic coupler. In the idle state of the fuel injector prevails in the hydraulic coupler rail pressure. The known fuel injector is low leakage, ie executed without low pressure stage. To achieve a sufficient hydraulic needle-closing force, a closing throttle is introduced in a connection channel supplying fuel to a lower nozzle chamber. A disadvantage of the known fuel injector is that the two parts of the injection valve element do not react as a single part, but delayed in a control of the injection valve element. This can only be compensated by very fast switching control valves, which, however, is associated with higher costs. DISCLOSURE OF THE INVENTION Technical Problem
Der Erfindung liegt daher die Aufgabe zugrunde, einen alternativen Kraftstoff-Injektor vorzuschlagen, bei dem mindestens zwei Einspritzventilelementteile über einen leckagearmen hydraulischen Koppler miteinander gekoppelt sind.The invention is therefore based on the object to propose an alternative fuel injector, in which at least two injection valve element parts are coupled together via a low-leakage hydraulic coupler.
Technische LösungTechnical solution
Diese Aufgabe wird mit einem Kraftstoff-Injektor mit den Merkmalen des Anspruchs 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung sind in den Unteransprüchen angegeben. In den Rahmen der Erfindung fallen sämtliche Kombinationen aus zumindest zwei von in der Beschreibung, den Ansprüchen und/oder den Figuren offenbarten Merkmalen.This object is achieved with a fuel injector having the features of claim 1. Advantageous developments of the invention are specified in the subclaims. All combinations of at least two features disclosed in the description, the claims and / or the figures fall within the scope of the invention.
Der Erfindung liegt der Gedanke zugrunde, eine starke Ver- pressung der beiden separaten, mittels des hydraulischen Kopplers gekoppelten (wirkverbundenen) , Einspritzventilelementteile dadurch zu erreichen, dass der hydraulische Koppler, genauer ein Kopplerraum des Kopplers, insbesondere dauerhaft, mit einer Niederdruckquelle, insbesondere einem mit einem Injektorrücklauf verbundenen Niederdruckbereich des Injektors, verbunden ist. Aufgrund des im Vergleich zum Hochdruckbereich des Kraftstoff-Injektors reduzierten Drucks innerhalb des hydraulischen Kopplers werden die Einspritzventilelementteile während des Betriebs des Kraft- Stoff-Inj ektors permanent und mit erheblichen Kräften miteinander verbunden, sodass sie aus Funktionssicht als einteilig betrachtet werden können. Dieser Effekt ist gerade bei einer Mehrfacheinspritzung von signifikantem Vorteil, da im Vergleich mit bekannten, nicht druckreduzierten hydraulischen Kopplern ein Unterdruck im hydraulischen Koppler nicht erst mit dem Einspritzventilelementhub aufgebaut werden muss. Im Vergleich zu einem einteiligen Einspritzven- tilelement wird der Vorteil erzielt, dass auf eine auf aktuelle Fertigungsabläufe abgestimmte Logistik zurückgegriffen werden kann. Darüber hinaus ist es möglich, den Düsen- nadelteil des Einspritzventilelementes aus einem anderen Material auszubilden, als den Steuerstangenteil, wodurch die Einspritzventilelementteile an spezifische Anforderungen (Steifigkeit/Festigkeit) optimal angepasst werden können. Um die durch die den hydraulischen Koppler, genauer den Kopplerraum, axial begrenzenden Führungsspalte hindurchströmende Leckagemenge zu minimieren, ist bei einem nach dem Konzept der Erfindung ausgebildeten Kraftstoff- Injektor vorgesehen, dass beide Führungen zumindest abschnittsweise radial außen mit unter Hochdruck stehendem Kraftstoff umgeben sind. Anders ausgedrückt, ist das mindestens eine die Führungsspalte radial außen begrenzenden Injektorbauteil in einem Bereich radial außerhalb des jeweiligen, zwischen dem mindestens ein Injektorbauteil und dem Einspritzventilelement ausgebildeten Führungsspalt mit unter Hochdruck stehendem Kraftstoff umgeben, wodurch eine Aufweitung der Führungsspalte durch in die Führungsspalte eindringenden, unter Hochdruck stehenden Kraftstoff vermieden wird. Noch anders ausgedrückt wird eine Aufweitung des einen oder der die Führungsspalte begrenzenden Injektorbauteil (e) dadurch minimiert, dass der Druck in den Führungsspalten zumindest näherungsweise genauso groß ist wie au- ßerhalb des/der Inj ektorbauteil (e) in einem Bereich radial außerhalb der Führungsspalte. Auf die beschriebene Weise wird besonders elegant eine starke hydraulische Kopplung zweier Einspritzventilelementteile unter Zuhilfenahme ei- nes, insbesondere wesentlich, geringeren Drucks als der Raildruck erreicht, ohne dass hierbei besonders große Leckagemengen anfallen.The invention is based on the idea of achieving strong compression of the two separate injector element parts coupled by means of the hydraulic coupler in that the hydraulic coupler, more precisely a coupler space of the coupler, in particular permanently, with a low pressure source, in particular a connected to an injector return low pressure region of the injector is connected. Due to the reduced pressure within the hydraulic coupler compared to the high-pressure region of the fuel injector, the injection valve element parts are permanently and substantially interconnected during operation of the fuel injector, so that from a functional point of view they can be considered as one-piece. This effect is of significant advantage especially with multiple injection, since, in comparison with known, not pressure-reduced hydraulic couplers, a negative pressure in the hydraulic coupler does not have to be built up with the Einspritzventilelementhub. In comparison with a one-piece injection valve element, the advantage is achieved that it is possible to fall back on a logistics adapted to current production processes. Moreover, it is possible to form the nozzle needle part of the injection valve element from a different material than the control rod part, whereby the injection valve element parts can be optimally adapted to specific requirements (stiffness / strength). In order to minimize the leakage amount flowing through the hydraulic coupler, more precisely the coupler space, axially delimiting guide gaps, a fuel injector designed according to the concept of the invention provides that both guides are surrounded at least in sections radially outward with fuel under high pressure. In other words, the at least one injector component, which delimits the guide gap radially outwardly, is surrounded by high-pressure fuel in an area radially outward of the respective guide gap formed between the at least one injector component and the injection valve element, thereby expanding the guide gaps by penetrating into the guide gaps High pressure fuel is avoided. In other words, widening of the one or more guide gaps limiting injector component (s) is minimized by the fact that the pressure in the guide gaps at least approximately the same size as outside of the Inj ektorbauteil (e) in a region radially outside the guide gaps , In the manner described, a particularly strong hydraulic coupling of two injection valve element parts with the aid of an Nes, in particular significantly, lower pressure than the rail pressure achieved, without causing particularly large leakage quantities.
In Weiterbildung der Erfindung ist mit Vorteil vorgesehen, dass innerhalb des hydraulischen Kopplers eine Niederdruckstufe realisiert ist, die eine in Schließrichtung auf das Einspritzventilelement wirkende hydraulische Kraft verursacht. Hierdurch kann die Einspritzventilelementschaltzeit beschleunigt werden. Da die von der Niederdruckstufe erzeugte, hydraulische, auf das Einspritzventilelement wirkende, Schließkraft raildruckabhängig ist, wirkt diese Schließkraft nicht erst während der Einspritzung, wie bei einer Schließdrossel, sondern permanent. Besonders bevor- zugt ist es dabei, wenn auf eine zusätzliche Schließdrossel, die den Kraftstoffdruck im Bereich der Einspritzven- tilelementstütze im Vergleich zum Kraftstoffdruck im Bereich eines Zulaufkanals des Kraftstoff-Injektors verringert, verzichtet wird. Durch das Vorsehen einer Schließ- drossel würde der effektive Einspritzdruck um etwa bis zu 150 bar reduziert. Hierauf kann aufgrund des Vorsehens einer Niederdruckstufe im hydraulischen Koppler mit Vorteil verzichtet werden. Die Niederdruckstufe wird bevorzugt dadurch realisiert, dass der Durchmesser des zur Düsenlochan- Ordnung benachbarten Einspritzventilelementteils (Düsennadel) im Vergleich zu dem Durchmesser des düsenlochfernen Einspritzventilelementteils in einem den hydraulischen Koppler begrenzenden Abschnitt (etwas) reduziert wird. Anders ausgedrückt ist der Führungsdurchmesser der der Düsen- lochanordnung zugewandten Führung bevorzugt etwas geringer als der Führungsdurchmesser der anderen, den hydraulischen Koppler axial begrenzenden (insbesondere oberen) Führung. Besonders bevorzugt ist eine Ausführungsform, bei der der hydraulische Koppler über einen Verbindungskanal an einen Niederdruckbereich des Kraftstoff-Injektors angeschlossen ist. Hierdurch kann der Druck im hydraulischen Koppler im Vergleich zum Raildruck erheblich reduziert werden. Für den Fall, dass der Verbindungskanal, zumindest näherungsweise, drosselfrei ausgebildet ist, herrscht innerhalb des hydraulischen Kopplers, zumindest näherungsweise, Niederdruck, vorzugsweise in einem Druckbereich zwischen etwa 0 und 20 bar.In a further development of the invention is advantageously provided that within the hydraulic coupler, a low-pressure stage is realized, which causes a force acting in the closing direction of the injection valve element hydraulic force. As a result, the injection valve element switching time can be accelerated. Since the closing force generated by the low-pressure stage, hydraulic, acting on the injection valve element, closing force is raildruckabhängig, this closing force acts not only during the injection, as in a closing throttle, but permanently. In this case, it is particularly preferred if an additional closing throttle, which reduces the fuel pressure in the region of the injection valve element support in comparison to the fuel pressure in the region of an inlet passage of the fuel injector, is dispensed with. By providing a closing throttle, the effective injection pressure would be reduced by up to 150 bar. This can be dispensed with advantageously due to the provision of a low-pressure stage in the hydraulic coupler. The low-pressure stage is preferably realized by reducing the diameter of the nozzle-hole-adjacent injection valve member member (nozzle needle) as compared to the diameter of the nozzle-hole-remote injector member member in a hydraulic coupler-limiting portion (something). In other words, the guide diameter of the guide facing the nozzle hole arrangement is preferably somewhat smaller than the guide diameter of the other, the hydraulic coupler axially delimiting (in particular upper) guide. Particularly preferred is an embodiment in which the hydraulic coupler is connected via a connecting channel to a low pressure region of the fuel injector. As a result, the pressure in the hydraulic coupler compared to the rail pressure can be significantly reduced. In the event that the connecting channel, at least approximately, throttle-free, prevails within the hydraulic coupler, at least approximately, low pressure, preferably in a pressure range between about 0 and 20 bar.
In Weiterbildung der Erfindung ist mit Vorteil vorgesehen, dass zumindest eine der beiden, den hydraulischen Koppler begrenzenden Führungen von einem hülsenförmigen Fortsatz eines Plattenelementes gebildet ist, wobei dieser hülsen- förmige Fortsatz, zumindest abschnittsweise, vorzugsweise vollständig, radial außen von unter Hochdruck stehendem Kraftstoff umgeben ist. Besonders bevorzugt ist es dabei, in dem Plattenelement einen Abschnitt des Verbindungska- nals, insbesondere als Radialkanal, vorzusehen, der den hydraulischen Koppler mit dem Niederdruckbereich des Kraftstoff-Injektors verbindet. Bevorzugt mündet in den Niederdruckbereich des Kraftstoff-Inj ektors nicht nur der genannte Verbindungskanal, sondern auch ein Ablaufkanal aus einer Steuerkammer, über den bei geöffnetem Steuerventil Kraftstoff aus der Steuerkammer in Richtung Injektorrücklauf abströmt .In a further development of the invention is advantageously provided that at least one of the two, the hydraulic coupler limiting guides is formed by a sleeve-shaped extension of a plate member, said sleeve-shaped extension, at least partially, preferably completely, radially outwardly surrounded by under high pressure fuel is. It is particularly preferred to provide a portion of the connecting channel, in particular as a radial channel, in the plate element, which connects the hydraulic coupler to the low-pressure region of the fuel injector. In the low-pressure region of the fuel injector, not only the named connection channel but also a discharge channel from a control chamber, via which fuel flows out of the control chamber in the direction of the injector return when the control valve is open, preferably discharges.
Besonders bevorzugt ist eine Konstruktionsvariante, bei der in dem Plattenelement mindestens ein, vorzugsweise drosselfreier, Axialkanal vorgesehen ist, durch den Kraftstoff bei geöffnetem Einspritzventilelement in axialer Richtung zur Düsenlochanordnung strömen kann. Besonders zweckmäßig ist es, wenn das Plattenelement zwischen einem (oberen) Injektorkörper und einem (unteren) eine Düsenlochanordnung aufweisenden Düsenkörper angeordnet, also zwischen diesen Gehäuseteilen verspannt ist. Bevorzugt wird dabei der Düsenkörper mittels einer Überwurfmutter mit einem Außengewinde des Injektorkörpers verschraubt.Particularly preferred is a design variant in which in the plate member at least one, preferably throttle-free, axial channel is provided, can flow through the fuel with the injector element open in the axial direction of the nozzle hole arrangement. It is particularly expedient if the plate element is arranged between an (upper) injector body and a (lower) nozzle nozzle arrangement having a nozzle body, that is clamped between these housing parts. Preferably, the nozzle body is screwed by means of a union nut with an external thread of the injector body.
Besonders bevorzugt ist eine Ausführungsform, bei der zu- mindest eine der den Koppler axial begrenzenden Führungen von einer in einem Hochdruckraum angeordneten, insbesondere federkraftbeaufschlagten, Hülse gebildet ist. Besonders zweckmäßig ist dabei eine Ausführungsform, bei der die Hülse von der Feder in axialer Richtung gegen das zuvor erläu- terte Plattenelement gepresst wird. Dabei ist eine Ausführungsform besonders bevorzugt, bei der es sich bei dieser Feder gleichzeitig um die ein Einspritzventilelementteil in Richtung der Düsenlochanordnung beaufschlagende Schließfeder handelt, die sich einenends an der Hülse und andere- nends am Einspritzventilelementteil, insbesondere an einem Umfangsbund oder einem Sicherungsring des Einspritzventil- elementteils, abstützt.Particularly preferred is an embodiment in which at least one of the couplers axially delimiting guides is formed by a sleeve arranged in a high-pressure chamber, in particular spring-loaded sleeve. An embodiment in which the sleeve is pressed by the spring in the axial direction against the previously explained plate element is particularly expedient. An embodiment is particularly preferred in which this spring is at the same time the closing spring acting on an injection valve element part in the direction of the nozzle hole arrangement, which is located at one end on the sleeve and at other ends on the injection valve element part, in particular on a circumferential collar or a retaining ring of the injection valve element. element part, supports.
Wie zuvor erläutert, ist es möglich, den hydraulischen Koppler auf den am Injektorrücklauf anliegenden Niederdruck zu legen. Es ist jedoch auch eine Ausführungsform realisierbar, bei der der Druck im hydraulischen Koppler so dimensioniert wird, dass er zwar unter dem Hochdruck des Kraftstoffs außerhalb der den hydraulischen Koppler begren- zenden Führungen, jedoch oberhalb des Niederdrucks im Bereich des Injektorrücklaufs liegt. Hierzu wird bevorzugt in dem den hydraulischen Koppler mit dem Niederdruckbereich verbindenden Verbindungskanal mindestens eine Drossel ange- ordnet. Diese ist dabei so abgestimmt, dass der Druck im hydraulischen Koppler höher ist als im Bereich des Injektorrücklaufs. Durch die Realisierung eines im Vergleich zum Niederdruck im Injektorrücklaufbereich höheren (Nie- der-) Drucks im hydraulischen Koppler wird die Bauteilbelastung im Bereich des hydraulischen Kopplers reduziert. Da aufgrund des Vorsehens der Drossel im Verbindungskanal der Druck im hydraulischen Koppler nun lastabhängig ist, ist es bevorzugt, im Fall des Vorsehens einer derartigen Drossel, auf eine Niederdruckstufe im hydraulischen Koppler zu verzichten, sodass der hydraulische Koppler nicht mehr die Funktion hat, eine hydraulische Schließkraft zu erzeugen, sondern ausschließlich eine Kopplungsfunktion. Durch den etwas erhöhten Druck im hydraulischen Koppler wird die so- wieso schon geringe Leckagemenge, die durch die Führungen in den hydraulischen Koppler und damit in den Niederdruckbereich abströmt, noch weiter reduziert. Bevorzugt ist die Drossel so ausgelegt, dass der Druck im hydraulischen Koppler etwa dem halben Raildruck entspricht.As previously explained, it is possible to place the hydraulic coupler at the low pressure applied to the injector return. However, it is also possible to implement an embodiment in which the pressure in the hydraulic coupler is dimensioned such that it lies under the high pressure of the fuel outside the guides delimiting the hydraulic coupler but above the low pressure in the region of the injector return. For this purpose, at least one throttle is preferably applied in the connecting channel connecting the hydraulic coupler to the low-pressure region. assigns. This is adjusted so that the pressure in the hydraulic coupler is higher than in the area of the injector return. By implementing a higher (low) pressure in the hydraulic coupler compared to the low pressure in the injector return region, the component load in the area of the hydraulic coupler is reduced. Since due to the provision of the throttle in the connecting channel, the pressure in the hydraulic coupler is now load-dependent, it is preferred, in the case of providing such a throttle, to dispense with a low-pressure stage in the hydraulic coupler, so that the hydraulic coupler no longer has the function of a hydraulic Closing force to produce, but only a coupling function. Due to the slightly increased pressure in the hydraulic coupler, the already small amount of leakage, which flows through the guides into the hydraulic coupler and thus into the low-pressure area, is further reduced. Preferably, the throttle is designed so that the pressure in the hydraulic coupler corresponds approximately to half the rail pressure.
Bevorzugt wird in diesem Fall zum Erzeugen einer hydraulischen Schließkraft eine Schließdrossel vorgesehen, die derart dimensioniert ist, dass der Druck im Bereich der Spitze des Einspritzventilelementes geringer ist, vorzugsweise um etwa 50 bis 200 bar, als der Raildruck.In this case, a closing throttle is preferably provided for generating a hydraulic closing force, which is dimensioned such that the pressure in the region of the tip of the injection valve element is lower, preferably by about 50 to 200 bar, than the rail pressure.
Konstruktiv besonders elegant ist eine Ausführungsform, bei der eine derartige Schließdrossel in einem Injektorbauteil angeordnet ist, das radial innen eine Steuerkammer be- grenzt. Bevorzugt sind in diesem Injektorbauteil gleichzeitig auch eine Zulaufdrossel für die Steuerkammer und eine Ablaufdrossel aus der Steuerkammer und ggf. auch eine Füll- drossel zum beschleunigten Rückbefüllen der Steuerkammer eingebracht .An embodiment in which such a closing throttle is arranged in an injector component which delimits a control chamber radially on the inside is structurally particularly elegant. At the same time, an inlet throttle for the control chamber and an outlet throttle from the control chamber and possibly also a filling throttle are preferred in this injector component. Throttle introduced for accelerated refilling the control chamber.
Kurze Beschreibung der ZeichnungenBrief description of the drawings
Weitere Vorteile, Merkmale und Einzelheiten der Erfindung ergeben sich aus der nachfolgenden Beschreibung bevorzugterFurther advantages, features and details of the invention will become apparent from the following description
Ausführungsbeispiele sowie anhand der Zeichnungen. Diese zeigen in:Embodiments and with reference to the drawings. These show in:
Fig. 1 ein erstes Ausführungsbeispiel eines Kraftstoff- Injektors mit einem an einen Niederdruckbereich des Kraftstoff-Inj ektors angeschlossenem hydraulischen Koppler mit Niederdruckstufe undFig. 1 shows a first embodiment of a fuel injector with a connected to a low pressure region of the fuel Inj ector hydraulic coupler with low pressure stage and
Fig. 2 eine Ausführungsvariante eines Kraftstoff- Injektors mit an einem Niederdruckbereich des Kraftstoff-Injektors angeschlossenem hydraulischen Koppler ohne Niederdruckstufe und mit einer in einem Verbindungskanal zwischen dem hydraulischen Koppler und dem Niederdruckbereich angeordneten Drossel zur Einstellung des Drucks im hydraulischen Koppler.Fig. 2 shows an embodiment of a fuel injector with connected to a low pressure region of the fuel injector hydraulic coupler without low pressure stage and arranged in a connecting channel between the hydraulic coupler and the low pressure region throttle for adjusting the pressure in the hydraulic coupler.
Ausführungsformen der ErfindungEmbodiments of the invention
In den Figuren sind gleiche Bauteile und Bauteile mit der gleichen Funktion mit den gleichen Bezugszeichen gekennzeichnet .In the figures, the same components and components with the same function with the same reference numerals.
In Fig. 1 ist ein als Common-Rail-Injektor ausgebildeter Kraftstoff-Inj ektor 1 zum Einspritzen von Kraftstoff in einen nicht gezeigten Brennraum einer Brennkraftmaschine ei- nes Kraftfahrzeugs dargestellt. Eine Hochdruckpumpe 2 fördert Kraftstoff aus einem Vorratsbehälter 3 in einen Kraftstoff-Hochdruckspeicher 4 (Rail) . In diesem ist Kraftstoff, insbesondere Diesel oder Benzin, unter hohem Druck, von in diesem Ausführungsbeispiel über 2000 bar, gespeichert.In Fig. 1 is designed as a common rail injector fuel Inj ector 1 for injecting fuel into a combustion chamber, not shown, of an internal combustion engine an presented a motor vehicle. A high pressure pump 2 delivers fuel from a reservoir 3 in a high-pressure fuel storage 4 (Rail). In this fuel, especially diesel or gasoline, under high pressure, stored in this embodiment about 2000 bar.
An den Kraftstoff-Hochdruckspeicher 4 ist der Kraftstoff- Injektor 1 neben anderen, nicht gezeigten Injektoren über eine Versorgungsleitung 5 angeschlossen. Die Versorgungs- leitung 5 mündet in einen Versorgungskanal 6 des Kraftstoff-Injektors 1, der in einen Hochdruckraum 7 des Kraftstoff-Injektors 1 mündet. Der Hochdruckraum 7 bildet ein Mini-Rail, aufgrund dessen Druckschwingungen minimiert werden. Mittels einer Rücklaufleitung 8 ist ein Niederdruckbe- reich 9 des Kraftstoff-Injektors 1 an den Vorratsbehälter 3 angeschlossen. Über einen Injektor-Rücklaufanschluss 10 und die Rücklaufleitung 8 kann eine später noch zu erläuternde Steuermenge sowie eine geringe Leckagemenge an Kraftstoff von dem Kraftstoff-Injektor 1 zu dem Vorratsbehälter 3 ab- fließen.To the high-pressure fuel accumulator 4, the fuel injector 1 is connected, among other injectors, not shown, via a supply line 5. The supply line 5 opens into a supply channel 6 of the fuel injector 1, which opens into a high-pressure chamber 7 of the fuel injector 1. The high-pressure chamber 7 forms a mini-rail, due to which pressure oscillations are minimized. By means of a return line 8, a low-pressure region 9 of the fuel injector 1 is connected to the reservoir 3. Via an injector return port 10 and the return line 8, a control amount to be explained later as well as a small amount of leakage of fuel from the fuel injector 1 to the reservoir 3 can flow off.
Der Kraftstoff-Injektor 1 weist ein Gehäuse 11 auf, das einen Injektorkörper 12, in den der Versorgungskanal 6 eingebracht ist und einen unteren Düsenkörper 13 umfasst. Zwi- sehen dem Injektorkörper 12 und dem Düsenkörper 13 ist ein später noch zu erläuterndes Plattenelement 14 geklemmt, wobei der Düsenkörper 13 mittels einer Überwurfmutter 15 gegen das Plattenelement 14 und dieses in der Folge gegen den Düsenkörper 13 verspannt ist. Hierzu ist die Überwurfmutter 15 mit einem Außengewinde des Injektorkörpers 12 verschraubt . Das Kopfteil des Gehäuses 11 wird gebildet von einer Spannmutter 16, die mit dem Injektorkörper 12 verschraubt ist, und die ein Deckelelement 17, aufweisend den Injektor- Rücklaufanschluss 10, gegen eine Elektromagnetanordnung 18 eines später noch zu erläuternden, elektromagnetischen Ak- tuators 19 verspannt, welcher wiederum in axialer Richtung auf einer inneren Schulter 20 der Spannmutter 16 aufliegt.The fuel injector 1 has a housing 11, which has an injector body 12 into which the supply channel 6 is introduced and comprises a lower nozzle body 13. Between the injector body 12 and the nozzle body 13, a plate element 14 to be explained later is clamped, wherein the nozzle body 13 is braced against the plate element 14 by means of a union nut 15 and this in turn against the nozzle body 13. For this purpose, the union nut 15 is screwed to an external thread of the injector body 12. The head part of the housing 11 is formed by a clamping nut 16, which is screwed to the injector body 12, and which clamps a cover element 17, comprising the injector return port 10, against an electromagnet arrangement 18 of an electromagnetic actuator 19 to be explained later. which in turn rests in the axial direction on an inner shoulder 20 of the clamping nut 16.
In dem Gehäuse 11, genauer im Injektorkörper 12 und im Du- senkörper 13, ist ein zweiteiliges Einspritzventilelement 21 aufgenommen. Dieses umfasst einen oberen, ersten Teil 22 (Steuerstange) und einen unteren, zweiten Teil 23 (Düsennadel) . Das erste und das zweite Teil 22, 23 des Einspritzventilelementes 21 sind über einen später noch zu erläu- ternden hydraulischen Koppler 24 miteinander gekoppelt und verhalten sich wie ein einziges Bauteil. Das zweite, untere Teil 23 des Einspritzventilelementes 21 ist in einer Führungsbohrung 25 im Düsenkörper 13 geführt. Hier sind am Außenumfang des zweiten Teils 23 in einem Bereich innerhalb des Führungsbohrung 25 Axialkanäle 26 ausgebildet, über die bei geöffnetem Einspritzventilelement 21 Kraftstoff aus dem Hochdruckraum 7 in einen unteren Ringraum 67 strömen kann, in dem im Wesentlichen der gleiche Kraftstoffdruck herrscht, wie im Hochdruckraum 7. Um dies zu gewährleisten, sind die als Anschliffe ausgebildeten Axialkanäle 26 sowie ein Axialkanal 66 im Plattenelement 14 (zumindest näherungsweise) drosselfrei ausgebildet. In der Folge entspricht auch der Kraftstoffdruck in einem zwischen dem Plattenelement 14 und der Führungsbohrung 25 gebildeten Zwischenraum 27 dem Kraftstoffdruck innerhalb des Hochdruckraums 7. Auf eine im Stand der Technik ansonsten notwendige Schließdrossel wird bei dem Ausführungsbeispiel ge- maß Fig. 1 (im Gegensatz zu dem später noch zu erläuternden Ausführungsbeispiel gemäß Fig. 2) bewusst verzichtet.In the housing 11, more precisely in the injector body 12 and in the duplex body 13, a two-part injection valve element 21 is accommodated. This comprises an upper, first part 22 (control rod) and a lower, second part 23 (nozzle needle). The first and the second part 22, 23 of the injection valve element 21 are coupled to each other via a hydraulic coupler 24 to be explained later and behave like a single component. The second, lower part 23 of the injection valve element 21 is guided in a guide bore 25 in the nozzle body 13. In this case, axial channels 26 are formed on the outer circumference of the second part 23 in an area within the guide bore 25, through which fuel can flow from the high-pressure chamber 7 into a lower annular space 67 when the injection valve element 21 is open, in which substantially the same fuel pressure prevails as in the high-pressure space 7. In order to ensure this, the axial channels 26 designed as bevels and an axial channel 66 in the plate element 14 are (at least approximately) throttle-free. As a result, the fuel pressure in a gap 27 formed between the plate element 14 and the guide bore 25 also corresponds to the fuel pressure within the high-pressure space 7. The closing throttle otherwise required in the prior art is used in the embodiment. Measure Fig. 1 (in contrast to the later still to be explained embodiment of FIG. 2) deliberately omitted.
Das Einspritzventilelement 21, genauer das zweite Teil 23, weist an seiner Spitze 28 eine Schließfläche 29 auf, mit der das Einspritzventilelement 21 in dichte Anlage an einen innerhalb des Düsenkörpers 13 ausgebildeten Einspritzven- tilelementsitz 30 (Düsennadelsitz) bringbar ist. Wenn das Einspritzventilelement 21 an seinem Einspritzventilelement- sitz 30 anliegt, d.h. sich in einer Schließstellung befindet, ist der Kraftstoffaustritt aus einer Düsenlochanord- nung 31 gesperrt. Ist es dagegen von seinem Einspritzven- tilelementsitz 30 abgehoben und befindet sich in einer, hier nicht-ballistischen, Öffnungsstellung kann Kraftstoff aus dem Hochdruckraum 7 über den Zwischenraum 27 und den unteren Ringraum 67 an dem Einspritzventilelementsitz 30 vorbei zur Düsenlochanordnung 31 strömen und dort im Wesentlichen unter Hochdruck (Raildruck) stehend in den Brennraum gespritzt werden.The injection valve element 21, more precisely the second part 23, has at its tip 28 a closing surface 29 with which the injection valve element 21 can be brought into tight contact with an injection valve element seat 30 (nozzle needle seat) formed inside the nozzle body 13. When the injection valve element 21 abuts against its injection valve element seat 30, i. is in a closed position, the fuel outlet from a Düsenlochanord- tion 31 is locked. If, on the other hand, it is lifted from its injection valve element seat 30 and is in an open position, here fuel can flow from the high-pressure chamber 7 via the intermediate space 27 and the lower annular space 67 past the injection valve element seat 30 to the nozzle hole arrangement 31 and essentially there under high pressure (rail pressure) standing in the combustion chamber are injected.
Von einer oberen Stirnseite 32 des ersten Teils 22 des Einspritzventilelementes 21 und einem in der Zeichnungsebene unteren hülsenförmigen Abschnitt 33 eines als Drosselbauteil ausgebildeten Injektorbauteils 34 wird eine Steuerkam- mer 35 begrenzt, die über eine radial in dem hülsenförmigen Abschnitt 33 verlaufende Zulaufdrossel 36 mit unter Hochdruck stehendem Kraftstoff aus dem Hochdruckraum 7 versorgt wird. Die Steuerkammer 35 ist über eine, in einem oberen, plattenförmigen Abschnitt 37 des Injektorbauteils 34 vorge- sehene Ablaufdrossel 38 mit einer Ventilkammer 39 eines Steuerventils 40 (Servo-Ventil) verbunden. Die Ventilkammer 39 wird radial außen von einem hülsenförmigen Steuerventilelement 41 begrenzt, das einstückig mit einer mit dem elektromagnetischen Aktuator 19 zusammenwirkenden Ankerplatte 42 ausgebildet ist. Das hülsenförmige Steuerventilelement 41 ist in seiner Schließstellung in axialer Richtung druckausgeglichen. Die Steuerkammer 35 wird axial nach oben von einem Führungsbolzen 43 begrenzt, der sich axial am Deckelelement 17 abstützt und der zum einen die Aufgabe hat, das Steuerventilelement 41 bei seiner Verstellbewegung zu führen und zum anderen die Ventilkammer 39 in axialer Richtung nach oben abzudichten. Aus der Ventilkammer 39 kann Kraftstoff in den Niederdruckbereich 9 des Kraftstoff- Injektors 1 einströmen, wenn das von dem elektromagnetischen Aktuator 19 betätigbare Steuerventilelement 41 von seinem als Flachsitz ausgebildeten und am dem plattenförmi- gen Abschnitt 37 des Injektorbauteils 34 angeordneten, Steuerventilsitz 44 abgehoben, d.h. das Steuerventil 40 geöffnet ist. Bei geöffnetem Steuerventil 40 strömt dabei ü- ber die Ablaufdrossel 38 Kraftstoff aus der Steuerkammer 35 nach. Die Durchflussquerschnitte der Zulaufdrossel 36 und der Ablaufdrossel 38 sind dabei derart aufeinander abge- stimmt, dass bei geöffnetem Steuerventil 40 ein Nettoab- fluss von Kraftstoff (Steuermenge) aus der Steuerkammer 35 über die Ventilkammer 39 in den Niederdruckbereich 9 des Kraftstoff-Inj ektors 1 und von dort aus über die Rücklaufleitung 8 in den Vorratsbehälter 3 resultiert. Hierdurch sinkt der Druck in der Steuerkammer 35 rapide ab, wodurch das Einspritzventilelement 21 eine resultierende Öffnungskraft erfährt und in der Folge mit einem stirnseitigen Anschlagabschnitt 45 an der Decke des hülsenförmigen Abschnitts 33 anschlägt. Das Einspritzventilelement 21 hebt also von seinem Einspritzventilelementsitz 30 ab, sodass Kraftstoff durch die Düsenlochanordnung 31 ausströmen kann. Zum Beenden des Einspritzvorgangs wird die Bestromung der Elektromagnetanordnung 18 des elektromagnetischen Aktuators 19 unterbrochen. Eine sich an dem Führungsbolzen 43 axial abstützende Steuerschließfeder 46 bewegt in der Folge das hülsenförmige Steuerventilelement 41 zurück auf seinen Steuerventilsitz 44. Durch den durch die Zulaufdrossel 36 nachströmenden Kraftstoff steigt der Druck in der Steuerkammer 35 rapide an, wodurch das Einspritzventilelement 21, unterstützt durch die Federkraft einer Schließfeder 47, zu- rück auf seinen Einspritzventilelementsitz 30 bewegt wird, wodurch wiederum der Kraftstofffluss aus der Düsenlochan- ordnung 31 in den Brennraum unterbrochen wird. Das Auffüllen der Steuerkammer 35 über die Zulaufdrossel 36 wird über eine Fülldrossel 61 beschleunigt, die den Hochdruckraum 7 dauerhaft hydraulisch mit der Ventilkammer 39 verbindet. Ggf. kann auch auf diese Fülldrossel 61 verzichtet werden.From an upper end face 32 of the first part 22 of the injection valve element 21 and a lower in the drawing plane sleeve-shaped portion 33 of an injector designed as a throttle component 34 a Steuerkam- mer 35 is limited, via a radially extending in the sleeve-shaped portion 33 inlet throttle 36 with high pressure Stagnant fuel from the high-pressure chamber 7 is supplied. The control chamber 35 is connected to a valve chamber 39 of a control valve 40 (servo-valve) via a drain throttle 38 provided in an upper, plate-shaped section 37 of the injector component 34. The valve chamber 39 is bounded radially outwardly by a sleeve-shaped control valve member 41, which is integral with one with the electromagnetic actuator 19 cooperating armature plate 42 is formed. The sleeve-shaped control valve element 41 is pressure balanced in its closed position in the axial direction. The control chamber 35 is bounded axially upward by a guide pin 43 which is axially supported on the cover member 17 and on the one hand has the task to guide the control valve member 41 during its adjustment and on the other hand to seal the valve chamber 39 in the axial direction upwards. From the valve chamber 39, fuel can flow into the low-pressure region 9 of the fuel injector 1 when the control valve element 41 which can be actuated by the electromagnetic actuator 19 is lifted off its control valve seat 44, which is designed as a flat seat and is arranged on the plate-shaped section 37 of the injector component 34 the control valve 40 is open. When the control valve 40 is open, fuel flows out of the control chamber 35 via the outlet throttle 38. The flow cross sections of the inlet throttle 36 and the outlet throttle 38 are matched to one another such that when the control valve 40 is open, a net outflow of fuel (control quantity) from the control chamber 35 via the valve chamber 39 into the low pressure region 9 of the fuel injector 1 and from there via the return line 8 results in the reservoir 3. As a result, the pressure in the control chamber 35 decreases rapidly, whereby the injection valve element 21 experiences a resulting opening force and abuts in the sequence with an end-side abutment portion 45 on the ceiling of the sleeve-shaped portion 33. The injection valve element 21 thus lifts off from its injection valve element seat 30, so that fuel can flow out through the nozzle hole arrangement 31. To end the injection process, the energization of the solenoid assembly 18 of the electromagnetic actuator 19 is interrupted. As a result, the sleeve-shaped control valve element 41 moves back onto its control valve seat 44. The fuel flowing in through the inlet throttle 36 rapidly increases the pressure in the control chamber 35, as a result of which the injection valve element 21 is supported by the Spring force of a closing spring 47, is moved back to its injection valve element seat 30, which in turn the fuel flow from the Düsenlochan- Regulation 31 is interrupted in the combustion chamber. The filling of the control chamber 35 via the inlet throttle 36 is accelerated via a Fülldrossel 61 which connects the high pressure chamber 7 permanently hydraulically with the valve chamber 39. Possibly. can also be dispensed with this Fülldrossel 61.
Das erste und das zweite Teil 22, 23 des Einspritzventilelementes 21 sind hydraulisch in dem hydraulischen Koppler 24, genauer in einem Kopplerraum 48, miteinander gekoppelt und verhalten sich wie ein einziges Bauteil. Dies ist darauf zurückzuführen, dass der hydraulische Koppler 24, bzw. der Kopplerraum 48 über einen mehrteiligen Verbindungskanal 49 dauerhaft mit dem im Injektorkopf angeordneten Nieder- druckbereich 9 des Kraftstoff-Injektors 1 verbunden ist, und somit während des Betriebs des Kraftstoff-Injektors 1 dauerhaft auf Niederdruck liegt. Der Verbindungskanal 49 wird gebildet von einem im Plattenelement 14 vorgesehenen Radialkanal 50, einem Ringraum 51 radial zwischen dem Plat- tenelement 14 und der Überwurfmutter 15 sowie einem senkrecht verlaufenden Kanal 52 im Injektorkörper 12. Der hydraulische Koppler 24 wird in dem gezeigten Ausführungsbeispiel in axialer Richtung nach oben begrenzt von einer ersten Führung 53 für den ersten Teil 22 des Einspritzventilelementes 21 und in axialer Richtung nach unten von einer zweiten Führung 54 für den zweiten, unteren Teil 23 des Einspritzventilelementes 21. Dabei umfasst die erste Führung 53 einen ersten Führungsspalt 55 (Ringspalt) radial zwischen einem hülsenförmigen Fortsatz 56 des Plattenelementes 14 und einem unteren Abschnitt des ersten Teils 22 des Einspritzventilelementes 21. Analog umfasst die zweite Führung 54 einen zweiten Führungsspalt 57 (Ringspalt) radial zwischen einer von der Schließfeder 47 federkraftbeaufschlagten Hülse 58 und einem oberen Abschnitt des zweiten Teils 23 des Einspritzventilelements 21. Die Schließfeder 47 stützt sich dabei einenends an der unteren Stirnseite der Hülse 58 und anderenends an einem Umfangsbund 59 des zweiten Teils 23 des Einspritzventilelements 21 ab.The first and second parts 22, 23 of the injection valve element 21 are hydraulically coupled together in the hydraulic coupler 24, more specifically in a coupler space 48, and behave as a single component. This is due to the fact that the hydraulic coupler 24, or the coupler chamber 48 is permanently connected via a multi-part connecting channel 49 with the arranged in the injector low-pressure region 9 of the fuel injector 1, and thus during operation of the fuel injector 1 permanently low pressure. The connecting channel 49 is formed by a radial channel 50 provided in the plate element 14, an annular space 51 radially between the plate element 14 and the union nut 15 and a vertical channel 52 in the injector body 12. The hydraulic coupler 24 is limited in the embodiment shown in the axial direction upward by a first guide 53 for the first part 22 of the injection valve element 21 and in the axial direction down from a second guide 54 for the second, lower part 23 of the injection valve element 21st In this case, the first guide 53 comprises a first guide gap 55 (annular gap) radially between a sleeve-shaped extension 56 of the plate member 14 and a lower portion of the first part 22 of the injection valve element 21. Analogously, the second guide 54 comprises a second guide gap 57 (annular gap) radially between a The closing spring 47 is supported at one end on the lower end face of the sleeve 58 and at the other end on a circumferential collar 59 of the second part 23 of the injection valve element 21 from the closing spring 47 spring-loaded sleeve 58 and an upper portion of the second part 23 of the injection valve element 21.
Die Führungsspalte 55, 57 sind vergleichsweise kraftstoff- dicht ausgeführt. Dies ist vor allem darauf zurückzuführen, dass die erste Führung 53, genauer der hülsenförmige Fortsatz 56 innerhalb des Hochdruckraums 7 angeordnet, also radial außen von unter Hochdruck stehendem Kraftstoff umgeben ist. Hierdurch erfährt der erste Führungsspalt 55 durch die durch den ersten Führungsspalt 55 in den Kopplerraum 48 strömende, geringe Leckage keine Aufweitung nach radial außen. Analog ist die zweite Führung 54, genauer die Hülse 58 innerhalb des Zwischenraums 27 angeordnet, in dem in etwa der gleiche Druck herrscht wie im Hochdruckraum 7, sodass auch der zweite Führungsspalt 57 nicht aufgeweitet wird, da die Hülse 58 radial außen von unter Hochdruck stehendem Kraftstoff umgeben ist. In der Folge ist die über die Führungen 53, 54 in den hydraulischen Koppler 24 strömende Le- ckagemenge, die weiter über den Verbindungskanal 49 in den Niederdruckbereich 9 strömt, gering.The guide gaps 55, 57 are comparatively fuel-tight. This is primarily attributable to the fact that the first guide 53, more precisely the sleeve-shaped extension 56, is arranged inside the high-pressure chamber 7, that is to say is surrounded radially on the outside by high-pressure fuel. As a result, the first guide gap 55 experiences no expansion radially outward due to the low leakage flowing through the first guide gap 55 into the coupler space 48. Similarly, the second guide 54, more precisely, the sleeve 58 is disposed within the gap 27, in which approximately the same pressure prevails as in the high-pressure chamber 7, so that the second guide gap 57 is not widened because the sleeve 58 radially outward from under high pressure Fuel is surrounded. As a result, the lever, which flows via the guides 53, 54 into the hydraulic coupler 24, is level, which continues to flow via the connecting channel 49 in the low-pressure region 9, low.
Bei dem Ausführungsbeispiel gemäß Fig. 1 ist im hydrauli- sehen Koppler 24 eine Niederdruckstufe 60 realisiert, die eine in Schließrichtung auf das Einspritzventilelement 21 wirkende Kraft zur Folge hat. Die Niederdruckstufe 60 ist dadurch realisiert, dass der Durchmesser O1 des ersten Teils 21 im Bereich der ersten Führung 53 (etwas) größer ist als der Durchmesser Du des zweiten Teils 23 des Einspritzventilelementes 21 im Bereich der zweiten Führung 54. Mit Hilfe der Niederdruckstufe 60 wird eine permanent wirkende, in Schließrichtung wirkende Kraft auf das Einspritzventilelement 21 erzeugt. Hierdurch wird die Summe aller schließenden, auf das Einspritzventilelement 21 wirkenden Kräfte vergrößert, was den Öffnungszeitpunkt des Einspritzventilelementes 21 verzögert. Dies ist entscheidend: Aus Toleranzgründen sollte das Einspritzventilelement 21 erst dann öffnen, wenn das Steuerventil 40 bereits nicht- ballistisch betrieben werden kann. Ohne die realisierte Niederdruckstufe 60 kann der Einspritzbeginn nur für ein mechanisch weiches Einspritzventilelement 21 oder ein kleines Ablauf-/Zulauf-Drosselverhältnis verzögert werden. Beide Maßnahmen führen zu Nachteilen im Injektorverhalten: Während ein weiches Einspritzventilelement 21 zu einer schlechteren Mehrfacheinspritzungseignung führt, reduziert ein kleines Ablauf-/Zulauf-Drosselverhältnis den Anstieg der Strahlkraft des Einspritzstrahls und führt im Allgemeinen zu Emissionsnachteilen.In the embodiment according to FIG. 1, a low-pressure stage 60 is realized in the hydraulic coupler 24, which has a force acting in the closing direction on the injection valve element 21. The low-pressure stage 60 is realized in that the diameter O 1 of the first part 21 in the region of the first guide 53 is (slightly) greater than the diameter Du of the second part 23 of the injection valve element 21 in the region of the second guide 54. With the aid of the low-pressure stage 60 a permanently acting, acting in the closing direction force is generated on the injection valve element 21. As a result, the sum of all closing forces acting on the injection valve element 21 is increased, which delays the opening time of the injection valve element 21. This is crucial: For reasons of tolerance, the injection valve element 21 should only open when the control valve 40 can already be operated non-ballistically. Without the realized low-pressure stage 60, the start of injection can be delayed only for a mechanically soft injection valve element 21 or a small drain / inlet throttle ratio. Both measures lead to disadvantages in the injector behavior: While a soft injection valve element 21 leads to a poorer multiple injection suitability, a small drain / feed throttle ratio reduces the increase in the jet force of the injection jet and generally leads to emission disadvantages.
Im Folgenden wird das Ausführungsbeispiel eines Kraftstoff- Injektors 1 gemäß Fig. 2 erläutert. Da wesentliche Funkti- ons- und Konstruktionsmerkmale mit dem in Fig. 1 gezeigten und zuvor beschriebenen Kraftstoff-Injektor 1 übereinstimmen, werden im Folgenden im Wesentlichen nur die Unterschiede zu dem zuvor gezeigten und beschriebenen Ausführungsbeispiel erläutert. Im Hinblick auf die Gemeinsamkei- ten wird auf Fig. 1 und die zugehörige Beschreibung verwiesen .In the following, the embodiment of a fuel injector 1 according to FIG. 2 will be explained. Since essential funktions- and design features with the one shown in Fig. 1 and previously described fuel injector 1, in the following essentially only the differences from the previously shown and described embodiment will be explained. With regard to the common features, reference is made to FIG. 1 and the associated description.
Im Unterschied zu dem Ausführungsbeispiel gemäß Fig. 1 ist in dem Verbindungskanal 49, genauer in dem Radialkanal 50 zwischen dem hydraulischen Koppler 24 und dem Niederdruckbereich 9, eine Drossel 62 integriert. Diese ist so ausgelegt, dass im hydraulischen Koppler 24, genauer im Kopplerraum 48, etwa der hälftige Druck vorherrscht, wie im Hochdruckraum 7 sowie im Zwischenraum 27. Dies wird dadurch er- reicht, dass der Druckabfall an den Führungen 53, 54 in etwa dem Druckabfall an der Drossel 62 entspricht. Durch den im Vergleich zu dem Ausführungsbeispiel gemäß Fig. 1 erhöhten Druck im Kopplerraum 48 wird die über die Führungsspalte 55, 56 abströmende Leckagemenge noch weiter reduziert. Darüberhinaus wird die Bauteilbelastung des Plattenelementes 14 sowie der Hülse 58 reduziert.In contrast to the embodiment according to FIG. 1, a throttle 62 is integrated in the connecting channel 49, more precisely in the radial channel 50 between the hydraulic coupler 24 and the low-pressure region 9. This is designed so that approximately half the pressure prevails in the hydraulic coupler 24, more precisely in the coupler chamber 48, as in the high-pressure chamber 7 and in the intermediate space 27. This is achieved by the pressure drop across the guides 53, 54 being approximately equal to the Pressure drop at the throttle 62 corresponds. By compared to the embodiment of FIG. 1 increased pressure in the coupler chamber 48, the effluent via the guide gaps 55, 56 leakage amount is further reduced. In addition, the component load of the plate member 14 and the sleeve 58 is reduced.
Im Gegensatz zu dem Ausführungsbeispiel gemäß Fig. 1 sind die Durchmesser O1 und Du des ersten bzw. zweiten Teils 22, 23 des Einspritzventilelementes 21 im Bereich der Führungen 53, 54 gleich groß - es wurde also bewusst auf die Realisierung einer Niederdruckstufe im hydraulischen Koppler 24 verzichtet, da der Druck im hydraulischen Koppler 24 durch das Vorsehen der Drossel 62 lastabhängig ist und somit im Betrieb schwankt, was schwankende Schließkräfte zur Folge hätte für den Fall, dass eine Niederdruckstufe im Koppler 24 vorgesehen würde. Es ist jedoch auch denkbar, das Ausführungsbeispiel gemäß Fig. 2 mit einer Niederdruckstufe analog zu dem Ausführungsbeispiel gemäß Fig. 1 für bestimmte Anwendungen auszustatten. Aufgrund des Verzichts auf eine Niederdruckstufe wirken sich fertigungstoleranzbedingte und/oder temperaturabhängige Führungsleckagenschwankungen an den Führungen 53, 54 nicht auf die Injektorfunktion aus.In contrast to the embodiment according to FIG. 1, the diameters O 1 and Du of the first and second part 22, 23 of the injection valve element 21 in the region of the guides 53, 54 are the same size - so it became aware of the realization of a low-pressure stage in the hydraulic coupler 24 omitted, since the pressure in the hydraulic coupler 24 by the provision of the throttle 62 is load-dependent and thus fluctuates during operation, which would result in fluctuating closing forces in the event that a low pressure stage would be provided in the coupler 24. However, it is also conceivable, the embodiment of FIG. 2 with a low pressure stage to equip for certain applications analogous to the embodiment of FIG. Due to the omission of a low-pressure stage, production-related and / or temperature-dependent guide leakage fluctuations on the guides 53, 54 do not affect the injector function.
Um trotz des Verzichts auf eine Niederdruckstufe eine ausreichend große hydraulische Schließkraft zu realisieren, ist der Kraftstoff-Injektor 1 gemäß Fig. 2 mit einer zu- sätzlichen Schließdrossel 63 ausgestattet, die in den hül- senförmigen Abschnitt 33 des Injektorbauteils 34 eingebracht ist. Diese verbindet den Hochdruckraum 7 mit einem im Vergleich zu Fig. 1 zusätzlichen, ringförmigen Zulaufraum 64, der den hülsenförmigen Abschnitt 33 radial außen umgibt, und der über ein ringförmiges Dichtelement 65 gegenüber dem als Minirail dienenden Hochdruckraum 7 abgedichtet ist. Dabei ist die Schließdrossel 63 im gezeigten Ausführungsbeispiel so ausgelegt, dass der Druck im Hochdruckraum 7 etwa 50-200 bar geringer ist als der Raildruck im Zulaufräum 64. Im Gegensatz zu dem Ausführungsbeispiel gemäß Fig. 1 münden die Zulaufdrossel 36 und die Fülldrossel 61 nicht aus dem Hochdruckraum 7, sondern aus dem Zulaufraum 64 aus.In order to realize a sufficiently large hydraulic closing force despite the omission of a low-pressure stage, the fuel injector 1 according to FIG. 2 is equipped with an additional closing throttle 63, which is introduced into the sleeve-shaped section 33 of the injector component 34. This connects the high-pressure chamber 7 with an annular, additional inlet chamber 64, which surrounds the sleeve-shaped section 33 radially on the outside in comparison with FIG. 1, and which is sealed by way of an annular sealing element 65 with respect to the high-pressure space 7 serving as a minirail. The closing throttle 63 is designed in the illustrated embodiment so that the pressure in the high-pressure chamber 7 is about 50-200 bar less than the rail pressure in Zulaufräum 64. In contrast to the embodiment of FIG. 1, the inlet throttle 36 and the Fülldrossel 61 do not open the high-pressure chamber 7, but from the inlet chamber 64.
Die Drossel 62 kann, wie dargestellt, als einfache Drosselbohrung ausgeführt werden. Aufgrund der notwendigen kleinen Strömungsquerschnitte die bei der Drossel 62 notwendig sind, ist eine herkömmliche Drosselbohrung jedoch aus Gründen der Toleranz vergleichsweise schwer herstellbar. Daher ist es bevorzugt die Drossel 62 als Ringspaltdrossel auszuführen. Dies kann beispielsweise dadurch realisiert werden, dass in der eigentlichen Drosselbohrung ein Einlegeteil, beispielsweise ein Stift, positioniert wird, an dem der Kraftstoff radial außen vorbeiströmen muss. Der Vorteil einer derartigen Konstruktion ist die einfachere Herstellbarkeit. The throttle 62 can, as shown, be designed as a simple throttle bore. Due to the necessary small flow cross sections which are necessary in the throttle 62, a conventional throttle bore, however, is relatively difficult to produce for reasons of tolerance. Therefore, it is preferable to perform the throttle 62 as an annular gap throttle. This can be achieved, for example, by positioning an insert part, for example a pin, in the actual throttle bore, on which the Fuel must flow past radially outside. The advantage of such a construction is the easier manufacturability.

Claims

Ansprüche claims
1. Kraftstoff-Inj ektor, insbesondere Common-Rail- Injektor, zum Einspritzen von Kraftstoff in einen Brennraum einer Brennkraftmaschine, mit einem zwischen einer Öffnungsstellung und einer Schließstellung verstellbaren, mehrteiligen Einspritzventilelement (21), wobei ein erstes Teil (22) und ein zweites Teil (23) des Einspritzventilelementes (21) über einen hydrauli- sehen Koppler (24) miteinander gekoppelt sind, der axial von einer ersten Führung (53) für das erste Teil (22) und von einer zweiten Führung (54) für das zweite Teil (23) begrenzt ist,1. fuel Inj ector, in particular common rail injector, for injecting fuel into a combustion chamber of an internal combustion engine, with an adjustable between an open position and a closed position, multi-part injection valve element (21), wherein a first part (22) and a second Part (23) of the injection valve element (21) via a hydraulic see coupler (24) are coupled together, the axially of a first guide (53) for the first part (22) and of a second guide (54) for the second part (23) is limited
dadurch gekennzeichnet,characterized,
dass die erste und die zweite Führung (53, 54) zumindest abschnittsweise radial außen mit unter Hochdruck stehendem Kraftstoff umgeben sind, und dass im hydrau- lischen Koppler (24) ein geringerer Druck realisiert ist, als radial außerhalb der Führungen (53, 54) .the first and the second guide (53, 54) are surrounded radially at least in sections with fuel under high pressure, and that a lower pressure is realized in the hydraulic coupler (24) than radially outside the guides (53, 54) ,
2. Kraftstoff-Inj ektor nach Anspruch 1, dadurch gekennzeichnet, dass im hydraulischen Koppler (24) am Einspritzventilelement (21) eine eine Schließkraft verursachende Niederdruckstufe (60) realisiert ist.2. Fuel Inj ector according to claim 1, characterized in that in the hydraulic coupler (24) on the injection valve element (21) a closing force causing low pressure stage (60) is realized.
3. Kraftstoff-Injektor nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, dass der hydraulische Koppler (24) über einen Verbindungskanal (49) an einen Niederdruckbereich (9) des Kraftstoff-Injektors (1) angeschlossen ist. 3. Fuel injector according to one of claims 1 or 2, characterized in that the hydraulic coupler (24) via a connecting channel (49) to a low pressure region (9) of the fuel injector (1) is connected.
4. Kraftstoff-Inj ektor nach Anspruch 3, dadurch gekennzeichnet, dass die erste und/oder die zweite Führung (53, 54) von einem hülsenförmigen Fortsatz (56) eines Plattenelementes (14) gebildet sind/ist, in dem abschnittsweise der Verbindungskanal (49), vorzugsweise als Radialkanal (50), eingebracht ist.4. Fuel Inj ector according to claim 3, characterized in that the first and / or the second guide (53, 54) of a sleeve-shaped extension (56) of a plate element (14) are / is formed, in the sections of the connecting channel ( 49), preferably as a radial channel (50) is introduced.
5. Kraftstoff-Injektor nach Anspruch 4, dadurch gekennzeichnet, dass in dem Plattenelement (14) mindestens ein, vorzugsweise drosselfreier, Axialkanal (66) vorgesehen ist.5. Fuel injector according to claim 4, characterized in that in the plate element (14) at least one, preferably throttle-free, axial channel (66) is provided.
6. Kraftstoff-Injektor nach einem der Ansprüche 4 oder 5, dadurch gekennzeichnet, dass das Plattenelement (14) zwischen einem Injektorkörper (12) und einem eine Düsenlochanordnung (31) aufweisenden Düsenkörper (13) angeordnet ist.6. Fuel injector according to one of claims 4 or 5, characterized in that the plate element (14) between an injector body (12) and a nozzle nozzle arrangement (31) having nozzle body (13) is arranged.
7. Kraftstoff-Injektor nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die erste und/oder die zweite Führung (53, 54) von einer in einem Hochdruckraum (7) angeordneten, insbesondere federkraftbeaufschlagten, Hülse (58) gebildet sind/ist.7. Fuel injector according to one of the preceding claims, characterized in that the first and / or the second guide (53, 54) arranged in a high-pressure chamber (7), in particular spring-loaded, sleeve (58) are / is formed.
8. Kraftstoff-Inj ektor nach einem der Ansprüche 3 bis 7, dadurch gekennzeichnet, dass in dem Verbindungskanal (49) eine Drossel (62) angeordnet ist, die derart dimensioniert ist, dass der Druck im hydraulischen Koppler (24) niedriger ist als der die Führungen (53, 54) umschließende Hochdruck und höher ist als der Druck im Niederdruckbereich (9) .8. Fuel Inj ector according to one of claims 3 to 7, characterized in that in the connecting channel (49) a throttle (62) is arranged, which is dimensioned such that the Pressure in the hydraulic coupler (24) is lower than the guide (53, 54) enclosing high pressure and higher than the pressure in the low pressure region (9).
9. Kraftstoff-Inj ektor nach Anspruch 8, dadurch gekennzeichnet, dass eine Schließdrossel (63) vorgesehen ist, die derart dimensioniert und angeordnet ist, dass der Druck im Bereich einer Spitze (28) des Einspritzventilele- mentes (21) geringer ist als der Druck in einem Kraftstoffzulaufkanal des Kraftstoff-Injektors (1) .9. Fuel Inj ector according to claim 8, characterized in that a closing throttle (63) is provided, which is dimensioned and arranged such that the pressure in the region of a tip (28) of the Einspritzventilele- Mentes (21) is less than that Pressure in a fuel inlet channel of the fuel injector (1).
10. Kraftstoff-Inj ektor nach Anspruch 9, dadurch gekennzeichnet, dass die Schließdrossel (63) in einem eine Steuerkammer (35) begrenzenden Injektorbauteil (34) angeordnet ist. 10. Fuel Inj ector according to claim 9, characterized in that the closing throttle (63) in a control chamber (35) limiting injector component (34) is arranged.
EP09779562A 2008-07-24 2009-05-27 Fuel injector Not-in-force EP2310662B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE200810040680 DE102008040680A1 (en) 2008-07-24 2008-07-24 Fuel injector
PCT/EP2009/056467 WO2010009932A1 (en) 2008-07-24 2009-05-27 Fuel injector

Publications (2)

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EP2310662A1 true EP2310662A1 (en) 2011-04-20
EP2310662B1 EP2310662B1 (en) 2013-01-02

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EP09779562A Not-in-force EP2310662B1 (en) 2008-07-24 2009-05-27 Fuel injector

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US (1) US8864054B2 (en)
EP (1) EP2310662B1 (en)
DE (1) DE102008040680A1 (en)
WO (1) WO2010009932A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009000181A1 (en) * 2009-01-13 2010-07-15 Robert Bosch Gmbh Fuel injector
DE102013225384A1 (en) 2013-12-10 2015-06-11 Robert Bosch Gmbh fuel injector
DE102014205093A1 (en) 2014-03-19 2015-09-24 Robert Bosch Gmbh fuel injector
GB201421885D0 (en) * 2014-12-09 2015-01-21 Delphi International Operations Luxembourg S.�.R.L. Fuel injector
US10006429B2 (en) * 2016-03-31 2018-06-26 GM Global Technology Operations LLC Variable-area poppet nozzle actuator
CN114060193A (en) * 2020-08-04 2022-02-18 温特图尔汽柴油公司 Fuel injection valve for large diesel engine and large diesel engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19500706C2 (en) * 1995-01-12 2003-09-25 Bosch Gmbh Robert Metering valve for dosing liquids or gases
WO2000028205A1 (en) * 1998-11-10 2000-05-18 Ganser-Hydromag Ag Fuel injection valve for internal combustion engines
DE10229418A1 (en) * 2002-06-29 2004-01-29 Robert Bosch Gmbh Device for damping the needle stroke on fuel injectors
DE10248379A1 (en) * 2002-10-17 2004-04-29 Robert Bosch Gmbh Fuel injection device for an internal combustion engine
DE102004005452B4 (en) * 2004-02-04 2014-01-09 Robert Bosch Gmbh Nozzle holder combination with direct-operated injection valve member
DE102004035313A1 (en) * 2004-07-21 2006-02-16 Robert Bosch Gmbh Fuel injector with two-stage translator
DE102005016796A1 (en) * 2005-04-12 2006-10-19 Robert Bosch Gmbh Two-stage fuel injector
DE102006008648A1 (en) 2006-02-24 2007-08-30 Robert Bosch Gmbh Fuel e.g. diesel or petrol, injecting device for internal combustion engine, has valve unit including control piston and nozzle needle that are coupled with each other by hydraulic coupler, and guiding unit guiding fluid outlet of piston
DE102007001363A1 (en) * 2007-01-09 2008-07-10 Robert Bosch Gmbh Injector for injecting fuel into combustion chambers of internal combustion engines

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2010009932A1 *

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US20110139906A1 (en) 2011-06-16
DE102008040680A1 (en) 2010-01-28
US8864054B2 (en) 2014-10-21
WO2010009932A1 (en) 2010-01-28
EP2310662B1 (en) 2013-01-02

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