EP2294309B1 - Kraftstoff-injektor - Google Patents

Kraftstoff-injektor Download PDF

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Publication number
EP2294309B1
EP2294309B1 EP09765667.2A EP09765667A EP2294309B1 EP 2294309 B1 EP2294309 B1 EP 2294309B1 EP 09765667 A EP09765667 A EP 09765667A EP 2294309 B1 EP2294309 B1 EP 2294309B1
Authority
EP
European Patent Office
Prior art keywords
pressure
fuel
chamber
injector
fuel injector
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP09765667.2A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2294309A1 (de
Inventor
Matthias Burger
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 EP2294309A1 publication Critical patent/EP2294309A1/de
Application granted granted Critical
Publication of EP2294309B1 publication Critical patent/EP2294309B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • 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
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • 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
    • F02M63/02Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
    • F02M63/0225Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
    • 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
    • F02M2200/31Fuel-injection apparatus having hydraulic pressure fluctuations damping elements
    • 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
    • F02M2200/31Fuel-injection apparatus having hydraulic pressure fluctuations damping elements
    • F02M2200/315Fuel-injection apparatus having hydraulic pressure fluctuations damping elements for damping fuel pressure fluctuations
    • 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
    • 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, in particular a common rail injector, for injecting fuel into a combustion chamber of an internal combustion engine according to the preamble of claim 1.
  • the invention has for its object to propose a designed for highest injection pressures fuel injector. Preferably, this should be produced with conventional materials such as C45 steel.
  • the invention is based on the idea radially between the injector body (housing part) and one, preferably designed as injector-side rail pressure accumulator (Minirail), high-pressure space to arrange an annulus in which permanently or temporarily a lower fuel pressure than in the high pressure chamber and a higher fuel pressure than in Low pressure range of the fuel injector prevails.
  • injector-side rail pressure accumulator Minirail
  • the pressure is thus gradually reduced from radially inward to radially outward, so that critical material loads can be avoided.
  • injector body designed for well above 2000 bar fuel injectors with conventional materials, such as C45 steel can be performed, especially if the fuel pressure in the annulus does not exceed about 1800 bar. If, for example, the pressure in the high-pressure chamber of the fuel injector is at most 2000 bar, it is generally sufficient if the pressure difference between the annular space and the high-pressure space is approximately 200 bar.
  • the pressure in the annular space during operation of the fuel injector is at least half as high as the pressure in the pressure chamber so as not to burden the separation between the annulus and the high-pressure chamber overly.
  • a channel passing through the annular space in the radial direction is preferably provided, which is formed, for example, by the injector component which radially bounds the annular space.
  • the fuel injector is preferably a so-called low-leakage injector, preferably without a permanent, low-pressure stage which produces a hydraulic closing force acting on the one-part or multi-part injection valve element.
  • Such fuel injectors are preferably equipped with a long injection valve element whose axial extent preferably corresponds to at least 50%, preferably at least 60% or 70% of the axial extent of the entire fuel injector.
  • An embodiment is particularly preferred in which the high-pressure space in which the injection valve element is accommodated extends in the axial direction as far as a nozzle hole arrangement, wherein the high-pressure space can be subdivided as required into two axially adjacent space sections, between which a closing throttle is arranged.
  • the high-pressure chamber extends in the axial direction into a nozzle body which is axially adjacent to the injector body, in which case an embodiment can also be realized in which the pressure-reduced annular space formed between the injector body and the high-pressure chamber extends in the axial direction as far as into the nozzle body.
  • a series-connected throttle combination which consists of at least one annulus inlet throttle and at least one annulus flow restrictor, via the annulus inlet throttle under high pressure, in particular at least approximately under rail pressure, standing fuel can flow into the annulus.
  • Fuel can again flow out of the annular space in the direction of the low-pressure region of the fuel injector via the annular space drain throttle, the flow cross-sections of the at least one annular space inlet throttle and the at least one annular space throttle being dimensioned such that the desired pressure difference between annular space and high-pressure space is established.
  • This pressure reduction mechanism is comparable to the known control room pressure drop, as is known from servo-controlled fuel injectors.
  • the annulus pressure in comparison to the control chamber pressure has no influence on the injection behavior of the fuel injector, so that a lower accuracy requirement can be made in the production of the at least one annulus inlet throttle and the at least one annulus flow restrictor. It is particularly advantageous if the at least one annular space inlet throttle and / or the at least one annular space outlet throttle are structurally realized via a guide and / or a leak gap, as a result of which additional working steps for producing throttle bores can be saved. Of course it is also possible to perform at least one of the throttles as a throttle bore.
  • the at least one annulus drain can also be replaced or formed by a pressure relief valve to be explained later.
  • an embodiment of the fuel injector is not lowered in the pressure in the annulus during the entire operating time against the pressure in the high pressure chamber, but only at times when the pressure in the high pressure chamber exceeds a critical limit. This is usually only the case when the internal combustion engine is operated under full load.
  • an embodiment is preferred in which the pressure in the annular space is reduced or reduced compared to the pressure in the high-pressure space only when a minimum pressure, in particular of approximately 1800 bar, is exceeded.
  • At least one pressure relief valve is provided in the fuel flow direction between the annulus and the low pressure region of the fuel injector, which is preferably designed as a check valve.
  • the pressure relief valve is designed such that it acts as an annular space drain throttle in the open state, so that the desired annular space pressure defines defined. The only temporary opening of the pressure relief valve, the parasitic flow rate can be reduced to an absolute minimum.
  • the pressure relief valve comprises at least one spring, the spring force acts on an adjustable valve element.
  • the spring is particularly preferably a leaf spring and / or the valve element is a valve ball, in particular designed as a steel ball.
  • Structurally elegant is an embodiment in which the valve element is pressed by the spring onto a valve seat which is formed on an injector component which axially delimits the low-pressure region.
  • the leaf spring can be clamped axially between a valve clamping screw for securing the injector component in the injector body and the injector component.
  • the adjustable valve element of the pressure relief valve is formed by the injector component axially delimiting the low-pressure region, this injector component in this case being subjected to spring force against the injector body by means of a spring, for example an expansion sleeve or a disc spring.
  • a spring for example an expansion sleeve or a disc spring.
  • the fuel from the annulus with open pressure relief valve flows through an annular leakage gap in the low pressure region of the fuel injector, wherein the leakage gap, preferably axially, is formed between the Injektorbauteil and the injector, wherein to ensure sufficient tightness the closed pressure relief valve on the injector body and / or on the injector component preferably at least one biting edge is formed.
  • the spring of the pressure relief valve is arranged such that the bias of the spring and thus the maximum pressure of the annular space is adjustable by means of a valve clamping screw, wherein the valve clamping screw preferably an axial securing for the low pressure region of the Fuel injector in the axial direction limiting injector component.
  • Fig. 1 is a trained as a common rail injector fuel injector 1 for injecting fuel into a combustion chamber, not shown, of an internal combustion engine of a motor vehicle.
  • a high pressure pump 2 delivers fuel from a reservoir 3 into a high-pressure fuel accumulator 4 (rail).
  • this fuel especially diesel or gasoline, under high pressure, of about 2500 bar in this embodiment, stored.
  • the fuel injector 1 is connected, among other injectors, not shown, via a supply line 5.
  • This supply line 5 leads to a fuel supply connection 6 of the fuel injector 1, which leads via a supply channel 7 to a centric, serving as a minirail high-pressure chamber 8.
  • this high-pressure chamber 8 there is essentially rail pressure of about 2500 bar.
  • a fuel return port 10 is provided, to which a return line 11 is connected. Via the fuel return connection 10 and the return line 11, a control amount to be explained later as well as a leakage quantity of fuel from a low-pressure region 12 of the fuel injector 1 to the reservoir 3, which is also at low pressure of about 1 to 10 bar, flow off.
  • an injection valve element 13 which is integral in the embodiment shown is one recorded axially adjustable.
  • the injection valve element 13 is designed in several parts and consists for example of an upper control rod and a lower nozzle needle.
  • the injection valve element 13 is guided longitudinally displaceable in a guide bore 14 of a lower nozzle body 15 in the drawing plane.
  • axial channels 16 are realized on the outer circumference of the injection valve element 13 in the region of its lower guide as polished sections, via which the fuel can flow in the axial direction down to a nozzle hole arrangement 17 when the injection valve element 13 is open.
  • the nozzle body 15 is clamped by means of a union nut 18 with an injector body 19.
  • the injector body 19 forms the largest housing part of a housing 20.
  • the injection valve element 13 has at its tip 21 a closing surface 22 with which the injection valve element 13 can be brought into tight contact with an injection valve element seat 23 formed inside the nozzle body 15.
  • an injection valve element seat 23 formed inside the nozzle body 15.
  • the injection valve element 13 abuts against its injection valve element seat 23, ie is in a closed position, the fuel outlet from the nozzle hole arrangement 17 is blocked. If, on the other hand, it is lifted off its injection valve element seat 23, fuel can flow from the high-pressure chamber 8 in the axial direction via the axial channels 16 into a lower nozzle space 24 designed as an annular space and from there past the injection valve element seat 23 to the nozzle hole arrangement 17 and there substantially under high pressure (FIG. Rail pressure) standing in the combustion chamber (not shown) to be injected.
  • FOG. Rail pressure high pressure standing in the combustion chamber
  • a control chamber 28 is limited, which is supplied via an introduced into the injection valve element 13 inlet throttle 29 with fuel from the high-pressure chamber 8.
  • the control chamber 28 is connected via a axially extending in the injector component 27 drain passage 30 with outlet throttle 31 with a valve chamber 32 of a control valve 33 (servo-valve).
  • the valve chamber 32 is bounded radially on the outside by a sleeve-shaped control valve element 34.
  • the sleeve-shaped control valve element 34 is substantially pressure balanced in its closed position in the axial direction.
  • valve chamber 32 is bounded in the axial direction upwards by a pressure pin 35, which is supported axially on the injector cover 9 and is formed as a component separate from the injector component 27.
  • a co-operating with the sleeve-shaped control valve element 34 control valve seat 36 (here flat seat) is formed on the injector component 27.
  • the sleeve-shaped control valve element 34 is integrally formed with an anchor plate 37 which cooperates with an electromagnetic actuator 38. If this is energized, lifts the control valve member 34 in the axial direction of its control valve seat 36 so that fuel from the valve chamber 32 and subsequently from the control chamber 28 in the low pressure region 12 and from there via the fuel return port 10 and the return line 11 to the reservoir 3 can flow out.
  • the flow cross-sections of the inlet throttle 29, which may alternatively be embodied, for example, in the injector component 27, and the outlet throttle 31 are matched to one another such that when the control valve 33 is open, a net outflow of fuel from the control chamber 28 results. with the result that the fuel pressure in the control chamber 33 drops rapidly and thus a hydraulic opening force acts on the injection valve element 13, which lifts in sequence from its injection valve element seat 23 and the nozzle hole assembly 17 for injecting fuel into the combustion chamber releases.
  • the energization of the electromagnetic actuator 38 is interrupted. With a one end on a shoulder of the pressure pin 35 and the other end on an upper end face of the armature plate 37 supporting the control closing spring 39, the sleeve-shaped control valve member 34 is moved back to its control valve seat 36.
  • the fuel flowing in through the inlet throttle 29 causes an increase in pressure in the control chamber 28, with the result that the injection valve element 13 is moved back onto the injection valve element seat 23 assisted by a closing spring 40.
  • the closing spring 40 is arranged in the projecting into the nozzle body 15 high-pressure chamber 8 and is supported at one end on a lower end face of the Injektorbauteils 27 and the other end on a peripheral collar 41 of the injection valve element 13.
  • the axial channels 16 may be formed as throttle channels, thus reducing the pressure in the nozzle chamber 24 in comparison to the high pressure chamber 8 something.
  • the pressure is advantageously reduced by only about 100 to 200 bar, so that the nozzle chamber 24 and the high-pressure chamber 8 can be regarded as a common space.
  • annular space 42 In order to allow the injector body 19 not to be excessively stressed in pressure and subsequently made of conventional steels such as C45, see US Pat Fig. 1 shown fuel injector 1 an annular space 42 before, which is located radially between the high-pressure chamber 8 and the injector 19.
  • the annular space 42 extends in the axial direction over the largest part of the axial extent of the injector body 19 and, if necessary, can also project axially into the nozzle body 15.
  • the annular space 42 is bounded radially inwards with respect to the high-pressure chamber 8 by a tubular portion 43 of the injector component 27.
  • a stepped bore 44 is introduced for this purpose, which limits the control chamber 28 in its upper end in the drawing plane.
  • the pressure in the annular space 42 is permanently lower than in the high pressure chamber 8. Die Flow cross sections of the chokes to be explained below are adjusted so that the pressure in the annular space 42 does not exceed 1800 bar. As a result, the pressure load of the injector body 19, at least in pressure-critical Reduced areas over most of its axial extent.
  • the supply channel 7 is partially formed as a bore in a screwed to the injector body 19, sleeve-shaped connection part 60, wherein the supply channel 7 continues in the radial direction in the high-pressure chamber 8, while the annular space 42 passes through in the radial direction and is sealed against this ,
  • the injector component 22 is provided with a positive diameter jump 45 (circumferential collar) in the region of the supply channel 7, into which openings axially extending at a distance from the supply channel 7 are introduced, via which the fuel is introduced from a lower section of the annular space 42 into an upper section of the Annulus 42 can flow unhindered and preferably unthrottled.
  • FIG. 1 shown Injektorbauteil 27 does not necessarily have to be made in one piece.
  • the annular space 42 is bounded by the plate section 47 of the injector component 27, which, as mentioned above, can also be embodied as a separate component. This is pressed by a valve clamping screw 48 against an annular shoulder 49 of the injector body 19.
  • a sealing element 50 In the axial direction down the annular space 42 is bounded by a sealing element 50, which is located radially between the lower portion of the tubular portion 43 of the Injektorbauteils 27 and the injector body 19.
  • Fig. 1 further results can under high pressure of in the illustrated embodiment 2500 bar standing fuel flow in the radial direction via an annular space inlet throttle 51 into the annular space 42. From there, fuel flows via an annular component outlet throttle 52 provided in the injector component 27 into the low-pressure region 12 of the fuel injector 1.
  • the flow cross-sections of the annular space inlet throttle 51 and the annular space flow restrictor 52 are matched to one another in such a way that the pressure in the annular space 42, as explained above, a Maximum pressure of 1800 bar does not exceed, whereby the pressure load of the injector body 19 is significantly reduced.
  • the annular space inlet throttle 51 and the annular space drain throttle 52 are designed as throttle bores, with alternative manufacturing options can be realized. Since the pressure in the annular space 42 has no influence on the injection behavior of the fuel injector 1, the annular space inlet throttle 51 and the annular space drain throttle 52 can be made very small, whereby the necessary for the pressure reduction parasitic flow rate is low. On the other hand, the pressure in the annular space 42 does not react to highly dynamic pressure changes in the high-pressure space 8 serving as a minirail, but only to function-related rail pressure changes.
  • the pressure in the annular space 42 in the embodiment according to Fig. 2 not permanently reduced compared to the high-pressure chamber 8. This is due to the fact that the fuel from the annular space 42 can only temporarily flow into the low-pressure region 12 of the fuel injector 1.
  • the influx from the high-pressure chamber 8 in the annular space 42 is also at the in Fig. 2 shown embodiment via a designed as a throttle bore annular space inlet throttle 51.
  • the annular space drain throttle 52 is in the embodiment according to Fig. 2 formed by a designed as a check valve pressure relief valve 53 which is designed so that this opens only in the direction of low pressure area 12 when a minimum pressure in the annular space 42 is exceeded.
  • the overpressure valve 53 comprises a valve element 54 designed as a steel ball, which is acted upon by a spring 55 designed as a flat spring in the direction of a valve seat 56 formed on the injector component 27, more precisely on the plate section 47.
  • a spring 55 designed as a flat spring in the direction of a valve seat 56 formed on the injector component 27, more precisely on the plate section 47.
  • the underside of the valve element 54 via a channel 57 in the injector 27 is permanently in communication with the annulus volume of the annular space 42.
  • the pressure relief valve 53 is dimensioned so that the throttling action of the pressure relief valve 53 has the desired level of pressure reduction in the annular space 42 result.
  • annular space inlet throttle 51 is not formed as a throttle bore but as a leakage gap between a peripheral collar 58 of the tubular portion 43 of the injector 27 and the injector 19.
  • a further annular space inlet throttle 51 is provided between the upper positive diameter jump 45 (circumferential collar) and the injector body 19.
  • annular space drain throttle 52 no throttle channel is provided as annular space drain throttle 52.
  • This is formed by the pressure relief valve 53, via which the annular space 42 with the low pressure region 12 of the fuel injector 1 is connectable.
  • the valve element 54 is formed by the plate portion 47 of the Injektorbauteils 27. This is in the closed state of the pressure relief valve 53 on the annular shoulder 49 of the injector body 9 on.
  • the overpressure valve 53 is open, the plate section 47 is adjusted in the axial direction upward, so that an annular gap is formed axially between the plate section 47 and a biting edge 59 of the injector body 19, wherein the flow cross-section of the annular gap is adjusted so that the desired throttling is achieved.
  • the plate section 47 only lifts off from its valve seat 56 formed by the biting edge 59 on the injector body 19 when the pressure force acting on it exceeds the spring force of a spring 55 designed as a plate spring, which is supported in the axial direction upward on the valve clamping screw 48.
  • the spring 55 tends to press the plate portion 47 axially downwardly against the annular shoulder 49 of the injector body 19.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fuel-Injection Apparatus (AREA)
EP09765667.2A 2008-06-19 2009-04-22 Kraftstoff-injektor Not-in-force EP2294309B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008002527A DE102008002527A1 (de) 2008-06-19 2008-06-19 Kraftstoff-Injektor
PCT/EP2009/054814 WO2009153087A1 (de) 2008-06-19 2009-04-22 Kraftstoff-injektor

Publications (2)

Publication Number Publication Date
EP2294309A1 EP2294309A1 (de) 2011-03-16
EP2294309B1 true EP2294309B1 (de) 2014-06-11

Family

ID=40887985

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09765667.2A Not-in-force EP2294309B1 (de) 2008-06-19 2009-04-22 Kraftstoff-injektor

Country Status (6)

Country Link
EP (1) EP2294309B1 (ru)
CN (1) CN102066741B (ru)
BR (1) BRPI0914857A2 (ru)
DE (1) DE102008002527A1 (ru)
RU (1) RU2541484C2 (ru)
WO (1) WO2009153087A1 (ru)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010003202A1 (de) * 2010-03-24 2011-09-29 Robert Bosch Gmbh Common-Rail-Injektor mit druckausgeglichenem Schaltventil und zusätzlichem Speichervolumen
CH710127A1 (de) * 2014-09-17 2016-03-31 Ganser Crs Ag Brennstoffeinspritzventil für Verbrennungskraftmaschinen.
JP6384366B2 (ja) * 2015-03-09 2018-09-05 株式会社デンソー 燃料噴射装置
GB2553140B (en) * 2016-08-25 2020-04-01 Delphi Tech Ip Ltd Control valve assembly of a fuel injector
CN108513600B (zh) * 2016-12-28 2020-02-07 白保忠 一种复进式顺序阀及其顺序驱动方法
CN110848060B (zh) * 2019-10-14 2022-03-15 中国北方发动机研究所(天津) 一种电控蓄压喷油器

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6012644A (en) * 1997-04-15 2000-01-11 Sturman Industries, Inc. Fuel injector and method using two, two-way valve control valves
US5720318A (en) * 1995-05-26 1998-02-24 Caterpillar Inc. Solenoid actuated miniservo spool valve
US6047899A (en) * 1998-02-13 2000-04-11 Caterpillar Inc. Hydraulically-actuated fuel injector with abrupt end to injection features
DE10002109A1 (de) * 2000-01-19 2001-08-02 Bosch Gmbh Robert Einspritzsystem
DE102006051581A1 (de) * 2006-11-02 2008-05-08 Robert Bosch Gmbh Düsenspannkörper für Kraftstoffinjektoren
DE102007021330A1 (de) 2007-05-07 2008-11-13 Robert Bosch Gmbh Kraftstoffinjektor für eine Brennkraftmaschine mit Common-Rail-Einspritzsystem

Also Published As

Publication number Publication date
EP2294309A1 (de) 2011-03-16
BRPI0914857A2 (pt) 2020-08-18
RU2011101635A (ru) 2012-07-27
WO2009153087A1 (de) 2009-12-23
DE102008002527A1 (de) 2009-12-24
CN102066741B (zh) 2014-07-09
CN102066741A (zh) 2011-05-18
RU2541484C2 (ru) 2015-02-20

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