EP2013469A1 - High pressure fuel pump - Google Patents
High pressure fuel pumpInfo
- Publication number
- EP2013469A1 EP2013469A1 EP07728147A EP07728147A EP2013469A1 EP 2013469 A1 EP2013469 A1 EP 2013469A1 EP 07728147 A EP07728147 A EP 07728147A EP 07728147 A EP07728147 A EP 07728147A EP 2013469 A1 EP2013469 A1 EP 2013469A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure
- valve
- fuel pump
- valve seat
- pressure fuel
- 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
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other 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
- F02M63/0012—Valves
- F02M63/0031—Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
- F02M63/0033—Lift valves, i.e. having a valve member that moves perpendicularly to the plane of the valve seat
- F02M63/0036—Lift valves, i.e. having a valve member that moves perpendicularly to the plane of the valve seat with spherical or partly spherical shaped valve member ends
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other 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
- F02M63/0012—Valves
- F02M63/0031—Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
- F02M63/005—Pressure relief valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other 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
- F02M63/02—Fuel-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
- F02M63/0225—Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other 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
- F02M63/02—Fuel-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
- F02M63/0225—Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
- F02M63/023—Means for varying pressure in common rails
- F02M63/0235—Means for varying pressure in common rails by bleeding fuel pressure
- F02M63/0245—Means for varying pressure in common rails by bleeding fuel pressure between the high pressure pump and the common rail
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/02—Stopping, starting, unloading or idling control
- F04B49/03—Stopping, starting, unloading or idling control by means of valves
- F04B49/035—Bypassing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/28—Details of throttles in fuel-injection apparatus
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/31—Fuel-injection apparatus having hydraulic pressure fluctuations damping elements
Definitions
- the invention relates to a high-pressure fuel pump according to the preamble of claim 1.
- a high pressure fuel pump of the type mentioned is known from DE 10 2004 013 307 Al.
- the delivery chamber can be connected to a high-pressure outlet via a spring-loaded outlet valve.
- a pressure limiting valve is provided which has a spring-loaded valve ball as the valve element.
- the pressure relief valve opens to the pumping chamber and connects in the open state, the high-pressure outlet with the pumping chamber.
- a pressure relief valve arranged in this way has the advantage that it protects the high-pressure region against impermissibly high pressures, but at the same time does not worsen the degree of delivery of the high-pressure fuel pump, since the pressure relief valve only opens when there is a significantly lower pressure in the delivery chamber than in the high-pressure outlet.
- Object of the present invention is to provide a high pressure fuel pump of the type mentioned, which works very reliable.
- the throttle device comprises a high pressure side arranged from the pressure relief valve and separated from the pressure relief valve part with a flow restrictor, the previously used pressure relief valves can remain unchanged. This lowers the manufacturing costs.
- the separate part may be cup-shaped with a bottom portion, wherein the Flow restrictor is formed by at least one ⁇ f ⁇ hung in the bottom portion.
- Such a part can be inexpensively manufactured as Blechform- and stamped part.
- the throttle device may also include a flow restrictor, which is arranged in a valve seat body of the pressure relief valve near or immediately adjacent to the valve seat and from this high pressure side. This eliminates the handling of a separate part, which simplifies the assembly of the erfmdungshielen fuel high-pressure pump.
- the flow restrictor can be easily formed by a constriction in an inflow channel in the valve seat body.
- the free cross-sectional area of the flow restrictor should be at least approximately 0.5 times to 0.75 times the cross-sectional area of the valve seat of the pressure relief valve.
- valve element of the pressure relief valve is a spring-loaded ball in question, which can be loosely installed, which is very cost.
- the valve seat for such a ball is advantageously conical with a cone angle approximately between 30 ° and 50 °. The smaller the angle, the better the seal in the closed state of the pressure relief valve.
- a free cross-sectional area of an inflow channel immediately upstream (ie high pressure side) from the valve seat at least approximately 0.8 times to 0.95 times the cross-sectional area of the valve seat of the pressure relief valve.
- a narrow valve seat is advantageous in order to ensure good Schmutzunempfmdige the pressure relief valve can.
- the seat can be embossed particularly well during operation by such a narrow valve seat.
- a particularly advantageous embodiment of the high-pressure fuel pump according to the invention provides that a valve seat body of the pressure relief valve comprises a securing section extending in the opening direction of the valve element for the valve element, which is designed as a substantially annular collar.
- the valve element is secured in the open, so lifted from the valve seat state in the lateral direction, so that it is impossible even when dynamic pressure surges and large opening stroke that the valve element between valve seat body and a valve element acting on the valve spring is jammed.
- the reliability of the fuel high-pressure pump is improved by this measure according to the invention, since it prevents the pressure relief valve jammed in the open state and thereby a high-pressure construction of the high-pressure fuel pump is impossible.
- the securing section ultimately ensures that the valve element finds its way back safely to the valve seat even with a large stroke.
- a development for this purpose provides that the securing portion is formed on a valve seat portion of the pressure relief valve in the vicinity of the valve seat. This reduces the number of parts to be handled during assembly, which simplifies assembly. In addition, the manufacturing costs for the securing portion are reduced, since the valve seat portion of the pressure relief valve must be processed anyway.
- At least one flow channel in particular a flow pocket, is formed on the radially inner side of the securing section, preferably at least one flow channel which extends essentially over the length of the securing section.
- a flow channel introduced, for example, through a recess allows it to open
- Pressure relief valve a low-resistance flow between the valve element and the inside of the securing portion, while at the same time closely guiding the valve member by the securing portion. Through the flow channel, the fluid can easily flow past between the inside of the securing portion and the open valve element and a possibly this holding valve element holder.
- the securing portion has at least one preferably substantially extending over its length slot.
- a slot is particularly inexpensive to produce.
- the radial inner side of the securing section comprises a conical surface that widens in the direction of opening of the pressure limiting valve.
- the cone angle of the conical surface at least approximately correspond to the cone angle of the valve seat, which allows a relatively simple production.
- the cone angle of the conical surface can also be greater than the cone angle of the valve seat, which leads to a comparatively large clearance between the radial inner side of the securing section on the one hand and the valve element or valve element holder on the other hand even with a small opening stroke of the valve element.
- valve seat body has a shoulder adjacent to the valve seat and extending at least approximately radially, from which the radial inner side of the securing section extends in the opening direction of the pressure limiting valve.
- This measure can be used both in connection with the above-mentioned flow pockets or flow slots and the above-mentioned conical surface. The heel closing flow forces are avoided on the valve element in its open state.
- the pressure limiting valve may comprise a piston-like valve element holder, which acts on the valve element in the closing direction and immersed in both the closed and open pressure relief valve in the securing portion. As a result, a particularly secure guidance of the valve element is ensured.
- Figure 1 is a schematic representation of a fuel system with a high-pressure fuel pump
- FIG. 2 shows a partial section through the high-pressure fuel pump of FIG. 1 with a first embodiment of a pressure-limiting valve and a throttle device;
- Figure 3 is an enlarged detail view of a portion of the high-pressure fuel pump of Figure 2;
- Figure 4 is a detail IV of Figure 3;
- Figure 5 is a view similar to Figure 3 of a second embodiment
- Figure 6 is a view similar to Figure 5 with the pressure relief valve open;
- Figure 7 is a view similar to Figure 5 of a third embodiment
- Figure 8 is a section along the line VIII-VIII of Figure 7;
- Figure 9 is a view similar to Figure 7 of a fourth embodiment
- Figure 10 is a section along the line X-X of Figure 9;
- Figure 11 is a view similar to Figure 7 of a fifth embodiment
- Figure 12 is a view similar to Figure 7 of a sixth embodiment.
- Figure 13 is a view similar to Figure 7 of a seventh embodiment.
- a fuel system as a whole bears the reference numeral 10.
- the fuel system 10 shown only in simplified form in FIG. 1 comprises a fuel tank 12, from which a feed pump 13 conveys the fuel into a low-pressure fuel line 14.
- a high-pressure fuel pump 16 which further compresses the fuel and delivers it to a fuel rail 18, in which the fuel is stored under high pressure and which is also referred to as "rail".
- a plurality of injectors 20 are connected, which inject the fuel directly into them associated combustion chambers (not shown) of an internal combustion engine to which the fuel system 10 belongs.
- the high-pressure fuel pump 16 has a housing 22 with a low-pressure inlet 24 and a high-pressure outlet 26.
- an inlet channel 28 leads to an inlet valve 30 (not visible in FIG. 2) and on to a delivery chamber 32, which is bounded by a pump piston 34.
- An outlet passage 36 leads to the high-pressure outlet 26 via an outlet valve 38.
- the inlet valve 30 is integrated into a quantity control valve 40, by means of which the delivery space 32 can be forcibly connected to the region of the inlet passage 28 located upstream of the inlet valve 30. In this way, during a delivery stroke, fuel can be conveyed back to the low-pressure inlet 24 and the delivery rate of the high-pressure fuel pump 16 can be adjusted.
- a pressure limiting valve 42 is arranged. This is shown in greater detail in FIG. 3: It comprises a valve seat body 44 which is arranged in an overflow channel 46 leading from the high pressure outlet 26 to the delivery chamber 32 with a fastening region 48 in a press fit. Toward the delivery chamber 32, the outer diameter of the valve seat body 44 tapers toward a valve seat region 50. The outer contour of the valve seat body 44 in this area can also be referred to as bottle neck. This prevents that this valve seat portion 50 is deformed during the pressing of the valve seat body 44 in the overflow 46.
- the valve seat body 44 is penetrated by an inflow channel 52 in the longitudinal direction, which is designed as a stepped bore, the inner diameter in the valve seat portion 50 is smaller than in the mounting portion 48.
- the actual valve seat 54 for a Valve ball trained valve element 56 incorporated.
- the valve seat 54 is conical with a cone angle in the present case of approximately 30 °.
- the half cone angle is indicated in Figure 4 by an arrow with the reference numeral 58. In principle, the cone angle should be approximately between 30 ° and 50 °, with a small cone angle having advantages with respect to the seal.
- the point of contact of the valve element 56 with the valve seat 54 is linear with a diameter di.
- the diameter d 2 of the inflow channel 52 is smaller than the diameter di.
- a free cross-sectional area Fd 2 of the valve seat 54 from the high pressure port 26 and thus high pressure side arranged inflow 52 immediately adjacent to the valve element 56 at least about 0.8 times to 0.95 times as large as the cross-sectional area F. d i, which is defined by the valve seat diameter di on the valve seat 54.
- the valve element 56 is urged towards the valve seat 54 by a valve element holder 60, which in turn engages a valve spring 62.
- An immersion depth of the valve element 56 in the inflow channel 52 of the valve seat body 54 is designated T in FIG.
- a throttle device 64 is held in the overflow 46 in a press fit.
- This throttle device 64 is formed in the embodiment shown in Figures 2 to 4 as separate from the pressure relief valve 42 and cup-shaped part 65 which has a bottom portion 66 and an approximately rectangular and peripheral wall portion 68 to this.
- the part 65 may be made, for example, as sheet metal and stamped part.
- the free cross-sectional area F D i on the basis of the diameter Dl of the flow restrictor 70 is 0.6 times the cross-sectional area F d i on the basis of the diameter di of the valve seat 54 of the pressure relief valve 42.
- the high-pressure fuel pump 16 operates as follows: During a suction stroke of the pump piston 34 opens the inlet valve 30 and fuel flows from the low-pressure fuel line 14 in the delivery chamber 32. In a subsequent delivery stroke of trapped in the delivery chamber 32 fuel is compressed until finally the exhaust valve 38th opens and the fuel is pressed under high pressure in the rail 18. If there is too high a pressure in the rail 18 and thus also in the area of the high-pressure outlet 26, the valve element 56 lifts off from the valve seat 54 and against the force of the valve spring 62 due to the then prevailing pressure difference during a suction stroke of the pump piston 34. In this way, fuel can flow out of the rail 18 or the high-pressure outlet 26 via the overflow channel 46 and the pressure-limiting valve 42 into the delivery chamber 32. As a result, the rail 18 and the high-pressure outlet 26 is relieved.
- the throttle device 64 is not formed as a separate part, but integrated into the valve seat body 44 of the pressure relief valve 42, namely the high pressure side and very close or even immediately adjacent to the valve seat 54 in shape a constriction 70.
- Their free cross-sectional area F D i based on their diameter Di, in the present case is about 0.5 times the cross-sectional area Fdi of the valve seat 54 of the pressure limiting valve 42, based on the diameter di.
- the free cross section of the flow restrictor 70 is designed so that it is at an open pressure relief valve 42, ie when the valve member 56 is lifted from the valve seat 54 (see Figure 6), at most approximately the then adjusting annular opening cross-section F R corresponds, which is formed by the gap 72 between the valve element 56 and the valve seat 54. In this way it is ensured that the thus adjusting stroke H of the valve member 56 is smaller than the immersion depth T, thereby preventing that the valve element 56 between the valve seat body 44 and the valve member holder 60 can jam.
- FIG. 7 shows a portion of yet another alternative embodiment of a high-pressure fuel pump 16. This corresponds to the embodiment shown in FIGS. 5 and 6 with regard to the design of the flow restrictor 70.
- annular collar 76 extending in the opening direction (arrow 74) of the valve element 56, that is to say in the axial direction of the pressure limiting valve 42, which forms a securing section for the valve element 56, is integrally formed on the valve seat body 44 of the pressure limiting valve 42.
- the collar 76 has a radial outer side 78, with which it bears against the inside of the overflow channel 46.
- a radial inner side 80 of the collar 76 leads from a radially extending shoulder 82 to the projecting end of the collar 76.
- the shoulder 82 extends in the radial direction approximately from the valve seat 54, thus adjacent thereto.
- the valve element holder 60 is piston-like in the embodiment shown in FIG. 7, with an annular collar 84 arranged approximately in its axial center, against which the valve spring 62 is supported.
- a pin-like portion 86 of the valve element holder 60 extends from the annular collar 84, starting from the valve spring 62 limited annular space (without reference numeral), similar to the embodiments shown in Figures 3 and 5 and 6 in.
- a lying in the vicinity of the annular collar 84 region 88 of the peg-like portion 86 has an outer diameter that is only slightly smaller than the inner diameter of the valve spring 62. In this way, the valve element holder 60 is held tilt-proof on the valve spring 62.
- the holding portion 90 has a cylindrical outer contour with constant over its length diameter.
- a blind hole (without reference numeral) serves for the radial retention of the valve element 56 on the valve element holder 60.
- the outer diameter of the holding section 90 is selected so that the holding section 90 in the closed position of the pressure limiting valve 42 shown in FIG. 7 still faces the radial inner side 80 of the collar 76 has a small distance. In this way it is ensured that the holding portion 90 does not abut the collar 76 before the valve element 56 fully abuts the valve seat 54.
- the length of the collar 76 and the holding portion 90 are coordinated so that the holding portion 90 of the valve element holder 60 immersed in both the closed and open pressure relief valve 42 in the limited of the radial inner surface 80 interior of the collar 76. Also in this way is ensured by the collar 76 that even with dynamic pressure surges and thereby caused large opening strokes of the valve element 56 this out of the limited space by the collar 76 and instead can reliably find back when closing the pressure relief valve 42 into the valve seat 54 ,
- valve element 56 when the valve element 56 has lifted from the valve seat 54, to ensure a possible unimpeded outflow of the fluid to the pumping chamber 32, are distributed over the circumferential extent of the collar 76 away three flow pockets 92 on the radial inside 80 of the
- Collar 76 is formed. These extend from the shoulder 82 over the entire length of the collar 76 away to its abragendem end and have a circular-segment-shaped edge contour. This can be seen in particular from FIG.
- FIG. 11 An alternative embodiment shown in Figures 9 and 10 differs from that of Figures 7 and 8 in that instead of the flow pockets in the collar / securing portion 76 of its entire thickness penetrating slots 94 are introduced, which are also from the shoulder 82 over the entire length of the collar 76 extend to its abragendem end.
- FIG. 11 A further variant is shown in FIG. 11: In this case, the radial inner side 80 of the collar 76 is designed as a conical surface widening in the direction of opening 74 of the pressure-limiting valve 42.
- the holding portion 90 of the valve element holder 60 is similarly conical, but with a smaller cone angle than the radial inner side 80 of the collar 76.
- the cone angle can have approximately the same cone angle as the valve seat 54 (compare in particular FIG. 4), or a larger cone angle than the valve seat 54.
- valve seat 54 transitions directly into the radial inner side 80.
- a shoulder 82 which extends in the radial direction, initially adjoins the valve seat 54, and only then does the conical surface of the radial inside 80 of the collar 76 come off.
- the shoulder 82 prevents or at least reduces a force acting on the valve element 56 in the closing direction when the valve element 56 is open.
- FIG. 13 A further variant of FIG. 12 is shown in FIG. 13, in which the cone angle of the conical surface forming the radial inner side 80 of the collar 76 is comparatively steep and the holding portion 90 is cylindrical with a constant diameter.
- This variant has the advantage that the
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Fuel-Injection Apparatus (AREA)
- Safety Valves (AREA)
- Details Of Reciprocating Pumps (AREA)
Abstract
Description
Beschreibungdescription
Titel: Kraftstoff-HochdruckpumpeTitle: High-pressure fuel pump
Stand der TechnikState of the art
Die Erfindung betrifft eine Kraftstoff-Hochdruckpumpe nach dem Oberbegriff des Anspruchs 1.The invention relates to a high-pressure fuel pump according to the preamble of claim 1.
Eine Kraftstoff-Hochdruckpumpe der eingangs genannten Art ist aus der DE 10 2004 013 307 Al bekannt. Bei dieser Einzylinder-Kolbenpumpe ist der Förderraum über ein federbelastetes Auslassventil mit einem Hochdruckauslass verbindbar. Fluidisch parallel zu dem Auslassventil ist ein Druckbegrenzungsventil vorgesehen, welches als Ventilelement eine federbelastete Ventilkugel aufweist. Das Druckbegrenzungsventil öffnet zum Förderraum hin und verbindet in geöffnetem Zustand den Hochdruckauslass mit dem Förderraum. Ein solchermaßen angeordnetes Druckbegrenzungsventil hat den Vorteil, dass es den Hochdruckbereich vor unzulässig hohen Drücken schützt, gleichzeitig aber den Liefergrad der Kraftstoff-Hochdruckpumpe nicht verschlechtert, da das Druckbegrenzungsventil lediglich dann öffnet, wenn im Förderraum ein deutlich geringerer Druck als im Hochdruckauslass herrscht.A high pressure fuel pump of the type mentioned is known from DE 10 2004 013 307 Al. In this single-cylinder piston pump, the delivery chamber can be connected to a high-pressure outlet via a spring-loaded outlet valve. Fluidically parallel to the outlet valve, a pressure limiting valve is provided which has a spring-loaded valve ball as the valve element. The pressure relief valve opens to the pumping chamber and connects in the open state, the high-pressure outlet with the pumping chamber. A pressure relief valve arranged in this way has the advantage that it protects the high-pressure region against impermissibly high pressures, but at the same time does not worsen the degree of delivery of the high-pressure fuel pump, since the pressure relief valve only opens when there is a significantly lower pressure in the delivery chamber than in the high-pressure outlet.
Offenbarung der ErfindungDisclosure of the invention
Technische AufgabeTechnical task
Aufgabe der vorliegenden Erfindung ist es, eine Kraftstoff-Hochdruckpumpe der eingangs genannten Art zu schaffen, die besonders zuverlässig arbeitet.Object of the present invention is to provide a high pressure fuel pump of the type mentioned, which works very reliable.
Technische LösungTechnical solution
Diese Aufgabe wird durch eine Kraftstoff-Hochdruckpumpe mit den Merkmalen des Anspruchs 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung sind in Unteransprüchen angegeben. Ferner finden sich für die Erfindung wesentliche Merkmale in der nachfolgenden Beschreibung und der - 7 -This object is achieved by a high-pressure fuel pump with the features of claim 1. Advantageous developments of the invention are specified in subclaims. Furthermore, for the invention essential features in the following description and the - 7 -
Zeichnung. Dabei können die Merkmale auch in ganz unterschiedlichen Kombinationen für die Erfindung wesentlich sein, ohne dass hierauf jeweils explizit hingewiesen wird.Drawing. The features may also be essential for the invention in completely different combinations, without any explicit reference to this.
Vorteilhafte WirkungenAdvantageous effects
Erfindungsgemäß wurde erkannt, dass beim Öffnen des Druckbegrenzungsventils die Gefahr besteht, dass das Ventilelement durch dynamische Druckstöße so weit vom Ventilsitz abhebt, dass es aus dem Ventilsitz herausgedrückt wird und sich zwischen Ventilsitzkörper und Federteller verklemmt. Damit könnte das Druckbegrenzungsventil nicht mehr schließen, was zur Folge hätte, dass eine Pumpenförderung nicht mehr möglich wäre. All dies wird durch die erfindungsgemäße Maßnahme verhindert: Durch die Drosseleinrichtung wird der durch das Druckbegrenzungsventil maximal abströmende Mengenstrom so begrenzt, dass das Ventilelement des Druckbegrenzungsventils einen maximalen Öffhungshub nicht überschreiten kann. Die Drosseleinrichtung wirkt also quasi als hydraulische Hubbegrenzung.According to the invention, it has been recognized that when opening the pressure limiting valve, there is the danger that the valve element lifts off from the valve seat so far by dynamic pressure surges that it is forced out of the valve seat and jammed between valve seat body and spring plate. Thus, the pressure relief valve could not close, with the result that pumping would no longer be possible. All this is prevented by the measure according to the invention: By means of the throttle device, the maximum flow rate flowing through the pressure limiting valve is limited so that the valve element of the pressure limiting valve can not exceed a maximum opening stroke. The throttling device thus acts as a kind of hydraulic stroke limitation.
Erreicht wird dies durch die spezielle Abstimmung des freien Querschnitts der Drosseleinrichtung mit dem gewünschten maximalen Öffhungsquerschnitt des Druckbegrenzungsventils, der einem Hub des Ventilelements entspricht, bei dem noch sichergestellt ist, dass das Ventilelement sich nicht verklemmen kann. In den meisten Fällen dürfte dieser maximale Öffhungsquerschnitt eine Ringfläche sein. Durch die erfindungsgemäße Maßnahme wird verhindert, dass das Ventilelement bei maximalen Durchfluss durch das Druckbegrenzungsventil aus dem Ventilsitzbereich heraustaucht, und es wird gewährleistet, dass das Ventilelement beim Schließen des Druckbegrenzungsventils wieder leicht in den Ventilsitz zurückfindet. Die Drosseleinrichtung reduziert darüber hinaus das dynamische Verhalten des Druckbegrenzungsventils, was sich auch auf den Verschleiß positiv auswirkt. Druckspitzen werden nur gedämpft auf das Ventilelement übertragen.This is achieved by the special vote of the free cross section of the throttle device with the desired maximum Öffhungsquerschnitt the pressure relief valve, which corresponds to a stroke of the valve member, in which it is still ensured that the valve element can not jam. In most cases, this maximum Öffhungsquerschnitt should be an annular surface. The measure according to the invention prevents the valve element from being pushed out of the valve seat area at maximum flow through the pressure limiting valve, and it is ensured that the valve element easily returns to the valve seat when the pressure limiting valve closes. The throttle device also reduces the dynamic behavior of the pressure relief valve, which also has a positive effect on the wear. Pressure peaks are only attenuated transferred to the valve element.
Wenn die Drosseleinrichtung ein vom Druckbegrenzungsventil aus gesehen hochdruckseitig angeordnetes und vom Druckbegrenzungsventil separates Teil mit einer Strömungsdrossel umfasst, können die bisher eingesetzten Druckbegrenzungsventile unverändert bleiben. Dies senkt die Herstellkosten.If the throttle device comprises a high pressure side arranged from the pressure relief valve and separated from the pressure relief valve part with a flow restrictor, the previously used pressure relief valves can remain unchanged. This lowers the manufacturing costs.
In die gleiche Richtung zielt jene Weiterbildung, bei welcher das separate Teil im Presssitz in einem Überströmkanal eines Pumpengehäuses gehalten ist.In the same direction aims that development in which the separate part is held in a press fit in a transfer port of a pump housing.
Das separate Teil kann topfförmig ausgebildet sein mit einem Bodenabschnitt, wobei die Strömungsdrossel durch mindestens eine Öfϊhung in dem Bodenabschnitt ausgebildet ist. Ein solches Teil kann preiswert als Blechform- und Stanzteil hergestellt werden.The separate part may be cup-shaped with a bottom portion, wherein the Flow restrictor is formed by at least one Öfϊhung in the bottom portion. Such a part can be inexpensively manufactured as Blechform- and stamped part.
Bei einer vom Druckbegrenzungsventil aus gesehen hochdruckseitig angeordneten Drosseleinrich- tung ist es vorteilhaft, wenn deren freie Querschnittsfläche wenigstens in etwa das 0,6-fache bis 1,1- fache der Querschnittsfläche eines Ventilsitzes des Druckbegrenzungsventils beträgt.In the case of a throttle device arranged on the high-pressure side from the pressure-limiting valve, it is advantageous if its free cross-sectional area amounts to at least approximately 0.6 to 1.1 times the cross-sectional area of a valve seat of the pressure-limiting valve.
Alternativ oder zusätzlich zu einer vom Druckbegrenzungsventil separaten Strömungsdrossel kann die Drosseleinrichtung auch eine Strömungsdrossel umfassen, die in einem Ventilsitzkörper des Druckbegrenzungsventils nahe oder unmittelbar benachbart zum Ventilsitz und von diesem aus gesehen hochdruckseitig angeordnet ist. Damit entfällt die Handhabung eines separaten Teils, was die Montage der erfmdungsgemäßen Kraftstoff-Hochdruckpumpe vereinfacht.Alternatively or in addition to a separate from the pressure relief valve flow restrictor, the throttle device may also include a flow restrictor, which is arranged in a valve seat body of the pressure relief valve near or immediately adjacent to the valve seat and from this high pressure side. This eliminates the handling of a separate part, which simplifies the assembly of the erfmdungsgemäßen fuel high-pressure pump.
Dabei kann die Strömungsdrossel einfach durch eine Engstelle in einem Zuströmkanal im Ventilsitzkörper gebildet werden.In this case, the flow restrictor can be easily formed by a constriction in an inflow channel in the valve seat body.
Bei einer solchen Drosseleinrichtung sollte die freie Querschnittsfläche der Strömungsdrossel wenigstens in etwa das 0,5-fache bis 0,75-fache der Querschnittsfläche des Ventilsitzes des Druckbegrenzungsventils betragen. Bei einer solchen Auslegung wird eine gute Funktion des Druckbegrenzungsventils mit guter Sicherheit gegen ein Verklemmen des Ventilelements gewährleistet.In such a throttle device, the free cross-sectional area of the flow restrictor should be at least approximately 0.5 times to 0.75 times the cross-sectional area of the valve seat of the pressure relief valve. With such a design, a good function of the pressure relief valve is ensured with good security against jamming of the valve element.
Als Ventilelement des Druckbegrenzungsventils kommt eine federbeaufschlagte Kugel in Frage, welche lose verbaut werden kann, was sehr kostengünstig ist. Der Ventilsitz für eine solche Kugel ist vorteilhafterweise konisch mit einem Konuswinkel ungefähr zwischen 30° und 50°. Je geringer der Winkel ist, desto besser ist die Abdichtung in geschlossenem Zustand des Druckbegrenzungsventils.As a valve element of the pressure relief valve is a spring-loaded ball in question, which can be loosely installed, which is very cost. The valve seat for such a ball is advantageously conical with a cone angle approximately between 30 ° and 50 °. The smaller the angle, the better the seal in the closed state of the pressure relief valve.
Vorgeschlagen wird ferner, dass eine freie Querschnittsfiäche eines Zuströmkanals unmittelbar stromaufwärts (also hochdruckseitig) vom Ventilsitz (der Begriff stromaufwärts ist hier auf die Durchströmrichtung des Druckbegrenzungsventils bezogen) wenigstens in etwa das 0,8-fache bis 0,95-fache der Querschnittsfläche des Ventilsitzes des Druckbegrenzungsventils beträgt. Ein solch schmaler Ventilsitz ist vorteilhaft, um eine gute Schmutzunempfmdlichkeit des Druckbegrenzungsventils gewährleisten zu können. Ferner kann durch einen solchen schmalen Ventilsitz der Sitz selbst im Betrieb besonders gut geprägt werden. Eine besonders vorteilhafte Ausgestaltung der erfindungsgemäßen Kraftstoff-Hochdruckpumpe sieht vor, dass ein Ventilsitzkörper des Druckbegrenzungsventils einen sich in Öffnungsrichtung des Ventilelements erstreckenden Sicherungsabschnitt für das Ventilelement umfasst, der als im Wesentlichen ringförmiger Kragen ausgebildet ist. Durch diesen Sicherungsabschnitt wird das Ventilelement in geöffnetem, also vom Ventilsitz abgehobenem Zustand in seitlicher Richtung gesichert, so dass es selbst beim Auftreten dynamischer Druckstöße und großem Öffnungshub unmöglich ist, dass das Ventilelement zwischen Ventilsitzkörper und einer das Ventilelement beaufschlagenden Ventilfeder verklemmt wird. Letztlich wird durch diese erfindungsgemäße Maßnahme die Betriebssicherheit der Kraftstoff-Hochdruckpumpe verbessert, da verhindert wird, dass das Druckbegrenzungsventil in geöffnetem Zustand verklemmt und hierdurch ein Hochdruckaufbau der Kraftstoff-Hochdruckpumpe unmöglich wird. Der Sicherungsabschnitt sorgt letztlich dafür, dass das Ventilelement auch bei einem großen Hub wieder sicher zum Ventilsitz zurückfindet.It is also proposed that a free cross-sectional area of an inflow channel immediately upstream (ie high pressure side) from the valve seat (the term upstream is here based on the flow direction of the pressure relief valve) at least approximately 0.8 times to 0.95 times the cross-sectional area of the valve seat of the pressure relief valve. Such a narrow valve seat is advantageous in order to ensure good Schmutzunempfmdlichkeit the pressure relief valve can. Furthermore, the seat can be embossed particularly well during operation by such a narrow valve seat. A particularly advantageous embodiment of the high-pressure fuel pump according to the invention provides that a valve seat body of the pressure relief valve comprises a securing section extending in the opening direction of the valve element for the valve element, which is designed as a substantially annular collar. By this securing portion, the valve element is secured in the open, so lifted from the valve seat state in the lateral direction, so that it is impossible even when dynamic pressure surges and large opening stroke that the valve element between valve seat body and a valve element acting on the valve spring is jammed. Ultimately, the reliability of the fuel high-pressure pump is improved by this measure according to the invention, since it prevents the pressure relief valve jammed in the open state and thereby a high-pressure construction of the high-pressure fuel pump is impossible. The securing section ultimately ensures that the valve element finds its way back safely to the valve seat even with a large stroke.
Eine Weiterbildung hierzu sieht vor, dass der Sicherungsabschnitt an einen Ventilsitzbereich des Druckbegrenzungsventils in der Nähe von dessen Ventilsitz angeformt ist. Damit wird die Anzahl der bei der Montage handzuhabenden Teile reduziert, was die Montage vereinfacht. Darüber hinaus werden die Herstellkosten für den Sicherungsabschnitt reduziert, da der Ventilsitzbereich des Druckbegrenzungsventils ohnehin bearbeitet werden muss.A development for this purpose provides that the securing portion is formed on a valve seat portion of the pressure relief valve in the vicinity of the valve seat. This reduces the number of parts to be handled during assembly, which simplifies assembly. In addition, the manufacturing costs for the securing portion are reduced, since the valve seat portion of the pressure relief valve must be processed anyway.
Besonders vorteilhaft ist es, wenn auf der radialen Innenseite des Sicherungsabschnittes mindestens ein vorzugsweise sich im Wesentlichen über die Länge des Sicherungsabschnitts erstreckender Strömungskanal, insbesondere eine Strömungstasche ausgebildet ist. Ein solcher beispielsweise durch eine Ausnehmung eingebrachter Strömungskanal gestattet bei geöffnetemIt is particularly advantageous if at least one flow channel, in particular a flow pocket, is formed on the radially inner side of the securing section, preferably at least one flow channel which extends essentially over the length of the securing section. Such a flow channel introduced, for example, through a recess allows it to open
Druckbegrenzungsventil eine widerstandsarme Strömung zwischen dem Ventilelement und der Innenseite des Sicherungsabschnitts, bei gleichzeitig enger Führung des Ventilelements durch den Sicherungsabschnitt. Durch den Strömungskanal kann das Fluid problemlos zwischen der Innenseite des Sicherungsabschnitts und dem geöffneten Ventilelement und einem dieses eventuell haltenden Ventilelementhalter vorbeiströmen.Pressure relief valve a low-resistance flow between the valve element and the inside of the securing portion, while at the same time closely guiding the valve member by the securing portion. Through the flow channel, the fluid can easily flow past between the inside of the securing portion and the open valve element and a possibly this holding valve element holder.
In die gleiche Richtung zielt jene Ausgestaltung der erfindungsgemäßen Kraftstoff-Hochdruckpumpe, bei welcher der Sicherungsabschnitt mindestens einen sich vorzugsweise im Wesentlichen über seine Länge erstreckenden Schlitz aufweist. Ein solcher Schlitz ist besonders preiswert herstellbar. Ferner wird vorgeschlagen, dass die radiale Innenseite des Sicherungsabschnitts eine sich in Öffhungsrichtung des Druckbegrenzungsventils erweiternde Konusfläche umfasst. Damit wird bei geöffnetem Druckbegrenzungsventil jener Freiraum geschaffen, der eine widerstandsarme Strömung des Fluids zwischen Sicherungsabschnitt einerseits und Ventilelement und Ventilelementhalter andererseits ermöglicht. Dabei kann der Konuswinkel der Konusfläche wenigstens ungefähr dem Konuswinkel des Ventilsitzes entsprechen, was eine relativ einfache Herstellung ermöglicht. Der Konuswinkel der Konusfläche kann aber auch größer sein als der Konuswinkel des Ventilsitzes, was bereits bei einem kleinen Öffnungshub des Ventilelements zu einem vergleichsweise großen Freiraum zwischen der radialen Innenseite des Sicherungsabschnitts einerseits und dem Ventilelement beziehungsweise Ventilelementhalter andererseits führt.In the same direction, that embodiment of the fuel high-pressure pump according to the invention, in which the securing portion has at least one preferably substantially extending over its length slot. Such a slot is particularly inexpensive to produce. It is also proposed that the radial inner side of the securing section comprises a conical surface that widens in the direction of opening of the pressure limiting valve. Thus, with free pressure relief valve that clearance is created, which allows a low-resistance flow of the fluid between securing portion on the one hand and valve element and valve element holder on the other. In this case, the cone angle of the conical surface at least approximately correspond to the cone angle of the valve seat, which allows a relatively simple production. The cone angle of the conical surface can also be greater than the cone angle of the valve seat, which leads to a comparatively large clearance between the radial inner side of the securing section on the one hand and the valve element or valve element holder on the other hand even with a small opening stroke of the valve element.
Besonders vorteilhaft ist es ferner, wenn der Ventilsitzkörper einen zum Ventilsitz benachbarten und sich wenigstens in etwa radial erstreckenden Absatz aufweist, von dem aus sich in Öffnungsrichtung des Druckbegrenzungsventils die radiale Innenseite des Sicherungsabschnitts erstreckt. Diese Maßnahme kann sowohl im Zusammenhang mit den oben genannten Strömungstaschen oder Strömungsschlitzen als auch der oben genannten Konusfläche Verwendung finden. Durch den Absatz werden schließende Strömungskräfte auf das Ventilelement in dessen geöffnetem Zustand vermieden.It is furthermore particularly advantageous if the valve seat body has a shoulder adjacent to the valve seat and extending at least approximately radially, from which the radial inner side of the securing section extends in the opening direction of the pressure limiting valve. This measure can be used both in connection with the above-mentioned flow pockets or flow slots and the above-mentioned conical surface. The heel closing flow forces are avoided on the valve element in its open state.
Das Druckbegrenzungsventil kann einen kolbenartigen Ventilelementhalter umfassen, der das Ventilelement in Schließrichtung beaufschlagt und sowohl bei geschlossenem als auch bei geöffnetem Druckbegrenzungsventil in den Sicherungsabschnitt eintaucht. Hierdurch wird eine besonders sichere Führung des Ventilelements gewährleistet.The pressure limiting valve may comprise a piston-like valve element holder, which acts on the valve element in the closing direction and immersed in both the closed and open pressure relief valve in the securing portion. As a result, a particularly secure guidance of the valve element is ensured.
Kurze Beschreibung der ZeichnungenBrief description of the drawings
Nachfolgend werden besonders bevorzugte Ausführungsbeispiele der vorliegenden Erfindung unter Bezugnahme auf die beiliegende Zeichnung näher erläutert. In der Zeichnung zeigen:Hereinafter, particularly preferred embodiments of the present invention will be explained in more detail with reference to the accompanying drawings. In the drawing show:
Figur 1 eine schematische Darstellung eines Kraftstoffsystems mit einer Kraftstoff- Hochdruckpumpe;Figure 1 is a schematic representation of a fuel system with a high-pressure fuel pump;
Figur 2 einen teilweisen Schnitt durch die Kraftstoff-Hochdruckpumpe von Figur 1 mit einer ersten Ausführungsform eines Druckbegrenzungsventils und einer Drosseleinrichtung; Figur 3 eine vergrößerte Detaildarstellung eines Bereichs der Kraftstoff-Hochdruckpumpe von Figur 2;FIG. 2 shows a partial section through the high-pressure fuel pump of FIG. 1 with a first embodiment of a pressure-limiting valve and a throttle device; Figure 3 is an enlarged detail view of a portion of the high-pressure fuel pump of Figure 2;
Figur 4 ein Detail IV von Figur 3;Figure 4 is a detail IV of Figure 3;
Figur 5 eine Darstellung ähnlich Figur 3 einer zweiten Ausführungsform;Figure 5 is a view similar to Figure 3 of a second embodiment;
Figur 6 eine Darstellung ähnlich Figur 5 bei geöffnetem Druckbegrenzungsventil;Figure 6 is a view similar to Figure 5 with the pressure relief valve open;
Figur 7 eine Darstellung ähnlich Figur 5 einer dritten Ausführungsform;Figure 7 is a view similar to Figure 5 of a third embodiment;
Figur 8 einen Schnitt längs der Linie VIII-VIII von Figur 7;Figure 8 is a section along the line VIII-VIII of Figure 7;
Figur 9 eine Darstellung ähnlich Figur 7 einer vierten Ausführungsform;Figure 9 is a view similar to Figure 7 of a fourth embodiment;
Figur 10 einen Schnitt längs der Linie X-X von Figur 9;Figure 10 is a section along the line X-X of Figure 9;
Figur 11 eine Darstellung ähnlich Figur 7 einer fünften Ausführungsform;Figure 11 is a view similar to Figure 7 of a fifth embodiment;
Figur 12 eine Darstellung ähnlich Figur 7 einer sechsten Ausführungsform; undFigure 12 is a view similar to Figure 7 of a sixth embodiment; and
Figur 13 eine Darstellung ähnlich Figur 7 einer siebten Ausführungsform.Figure 13 is a view similar to Figure 7 of a seventh embodiment.
Ausführungsformen der ErfindungEmbodiments of the invention
In Figur 1 trägt ein Kraftstoffsystem insgesamt das Bezugszeichen 10. Das in Figur 1 nur vereinfacht dargestellte Kraftstoffsystem 10 umfasst einen Kraftstoffbehälter 12, aus dem eine Vor- förderpumpe 13 den Kraftstoff in eine Niederdruck-Kraftstoffleitung 14 fördert. Diese führt zu einer Kraftstoff-Hochdruckpumpe 16, die den Kraftstoff weiter verdichtet und in eine Kraftstoff- Sammelleitung 18 fördert, in der der Kraftstoff unter hohem Druck gespeichert ist und die auch als "Rail" bezeichnet wird. An das Rail 18 sind mehrere Injektoren 20 angeschlossen, die den Kraftstoff direkt in ihnen zugeordnete Brennräume (nicht dargestellt) einer Brennkraftmaschine einspritzen, zu der das Kraftstoffsystem 10 gehört. Wie aus Figur 2 hervorgeht, verfugt die Kraftstoff-Hochdruckpumpe 16 über ein Gehäuse 22 mit einem Niederdruckeinlass 24 und einem Hochdruckauslass 26. Vom Niederdruckeinlass 24 führt ein Einlasskanal 28 zu einem Einlassventil 30 (in Figur 2 nicht sichtbar) und weiter zu einem Förderraum 32, der von einem Pumpenkolben 34 begrenzt wird. Ein Auslasskanal 36 führt über ein Auslassventil 38 zu dem Hochdruckauslass 26. Das Einlassventil 30 ist in ein Mengensteuerventil 40 integriert, durch welches der Förderraum 32 zwangsweise mit dem stromaufwärts vom Einlassventil 30 gelegenen Bereich des Einlasskanals 28 verbunden werden kann. Auf diese Weise kann während eines Förderhubs Kraftstoff zum Niederdruckeinlass 24 zurückgefördert und hiermit die Fördermenge der Kraftstoff-Hochdruckpumpe 16 eingestellt werden.In FIG. 1, a fuel system as a whole bears the reference numeral 10. The fuel system 10 shown only in simplified form in FIG. 1 comprises a fuel tank 12, from which a feed pump 13 conveys the fuel into a low-pressure fuel line 14. This leads to a high-pressure fuel pump 16, which further compresses the fuel and delivers it to a fuel rail 18, in which the fuel is stored under high pressure and which is also referred to as "rail". To the rail 18 a plurality of injectors 20 are connected, which inject the fuel directly into them associated combustion chambers (not shown) of an internal combustion engine to which the fuel system 10 belongs. As can be seen from FIG. 2, the high-pressure fuel pump 16 has a housing 22 with a low-pressure inlet 24 and a high-pressure outlet 26. From the low-pressure inlet 24, an inlet channel 28 leads to an inlet valve 30 (not visible in FIG. 2) and on to a delivery chamber 32, which is bounded by a pump piston 34. An outlet passage 36 leads to the high-pressure outlet 26 via an outlet valve 38. The inlet valve 30 is integrated into a quantity control valve 40, by means of which the delivery space 32 can be forcibly connected to the region of the inlet passage 28 located upstream of the inlet valve 30. In this way, during a delivery stroke, fuel can be conveyed back to the low-pressure inlet 24 and the delivery rate of the high-pressure fuel pump 16 can be adjusted.
Fluidisch parallel zum Auslassventil 38 ist ein Druckbegrenzungsventil 42 angeordnet. Dieses ist stärker im Detail in Figur 3 dargestellt: Es umfasst einen Ventilsitzkörper 44, der in einem vom Hochdruckauslass 26 zum Förderraum 32 führenden Überströmkanal 46 mit einem Befestigungsbereich 48 im Presssitz angeordnet ist. Zum Förderraum 32 hin verjüngt sich der Außendurchmesser des Ventilsitzkörpers 44 zu einem Ventilsitzbereich 50 hin. Die Außenkontur des Ventilsitzkörpers 44 in diesem Bereich kann auch als flaschenhalsartig bezeichnet werden. Damit wird verhindert, dass sich dieser Ventilsitzbereich 50 beim Einpressen des Ventilsitzkörpers 44 in den Überströmkanal 46 verformt.Fluidically parallel to the outlet valve 38, a pressure limiting valve 42 is arranged. This is shown in greater detail in FIG. 3: It comprises a valve seat body 44 which is arranged in an overflow channel 46 leading from the high pressure outlet 26 to the delivery chamber 32 with a fastening region 48 in a press fit. Toward the delivery chamber 32, the outer diameter of the valve seat body 44 tapers toward a valve seat region 50. The outer contour of the valve seat body 44 in this area can also be referred to as bottle neck. This prevents that this valve seat portion 50 is deformed during the pressing of the valve seat body 44 in the overflow 46.
Der Ventilsitzkörper 44 wird von einem Zuströmkanal 52 in Längsrichtung durchsetzt, der als Stufenbohrung ausgeführt ist, deren Innendurchmesser im Ventilsitzbereich 50 kleiner ist als im Befestigungsbereich 48. Am in den Figuren 3 und 4 rechten Ende des Zuströmkanals 52 ist der eigentliche Ventilsitz 54 für ein als Ventilkugel ausgebildetes Ventilelement 56 eingearbeitet. Der Ventilsitz 54 ist konisch ausgeführt mit einem Konuswinkel vorliegend von ungefähr 30°. Der halbe Konuswinkel ist in Figur 4 durch einen Pfeil mit dem Bezugszeichen 58 angedeutet. Grundsätzlich sollte der Konuswinkel ungefähr zwischen 30° und 50° liegen, wobei ein kleiner Konuswinkel Vorteile im Hinblick auf die Abdichtung hat. Die Berührungsstelle des Ventilelements 56 mit dem Ventilsitz 54 ist linienförmig mit einem Durchmesser di. Der Durchmesser d2 des Zuströmkanals 52 ist kleiner als der Durchmesser di. Auf diese Weise ist eine freie Querschnittsfläche Fd2 des vom Ventilsitz 54 aus gesehen zum Hochdruckanschluss 26 hin und insoweit hochdruckseitig angeordneten Zuströmkanals 52 unmittelbar benachbart zum Ventilelement 56 wenigstens in etwa 0,8-fach bis 0,95-fach so groß wie die Querschnittsfläche Fdi, die durch den Ventilsitzdurchmesser di am Ventilsitz 54 definiert wird. Das Ventilelement 56 wird zum Ventilsitz 54 hin von einem Ventilelementhalter 60 beaufschlagt, an dem wiederum eine Ventilfeder 62 angreift. Eine Eintauchtiefe des Ventilelements 56 in den Zuströmkanal 52 des Ventilsitzkörpers 54 ist in Figur 3 mit T bezeichnet.The valve seat body 44 is penetrated by an inflow channel 52 in the longitudinal direction, which is designed as a stepped bore, the inner diameter in the valve seat portion 50 is smaller than in the mounting portion 48. At the right in Figures 3 and 4 end of the inflow 52, the actual valve seat 54 for a Valve ball trained valve element 56 incorporated. The valve seat 54 is conical with a cone angle in the present case of approximately 30 °. The half cone angle is indicated in Figure 4 by an arrow with the reference numeral 58. In principle, the cone angle should be approximately between 30 ° and 50 °, with a small cone angle having advantages with respect to the seal. The point of contact of the valve element 56 with the valve seat 54 is linear with a diameter di. The diameter d 2 of the inflow channel 52 is smaller than the diameter di. In this way, a free cross-sectional area Fd 2 of the valve seat 54 from the high pressure port 26 and thus high pressure side arranged inflow 52 immediately adjacent to the valve element 56 at least about 0.8 times to 0.95 times as large as the cross-sectional area F. d i, which is defined by the valve seat diameter di on the valve seat 54. The valve element 56 is urged towards the valve seat 54 by a valve element holder 60, which in turn engages a valve spring 62. An immersion depth of the valve element 56 in the inflow channel 52 of the valve seat body 54 is designated T in FIG.
Vom Druckbegrenzungsventil 42 bzw. dessen Ventilsitz 54 aus gesehen zum Hochdruckanschluss 26 hin, als auf der Hochdruckseite des Druckbegrenzungsventils 42, ist im Überströmkanal 46 eine Drosseleinrichtung 64 im Presssitz gehalten. Diese Drosseleinrichtung 64 ist bei der in den Figuren 2 bis 4 gezeigten Ausführungsform als vom Druckbegrenzungsventil 42 separates und topfförmiges Teil 65 ausgebildet, welches einen Bodenabschnitt 66 und einen zu diesem in etwa rechtwinkligen und umlaufenden Wandabschnitt 68 aufweist. Das Teil 65 kann beispielsweise als Blechform- und Stanzteil hergestellt sein. Im Bodenabschnitt 66 ist eine Öffnung 70 vorhanden, welche einen Durchmesser Di aufweist und eine Strömungsdrossel bildet. Im vorliegenden Ausführungsbeispiel beträgt die freie Querschnittsfläche FDi auf der Basis des Durchmessers Dl der Strömungsdrossel 70 das 0,6-fache der Querschnittsfläche Fdi auf der Basis des Durchmessers di des Ventilsitzes 54 des Druckbegrenzungsventils 42. Grundsätzlich denkbar sind jedoch Werte zwischen dem 0,6- fachen bis zum 1,1 -fachen.From the pressure relief valve 42 and its valve seat 54 as seen from the high pressure port 26, as on the high pressure side of the pressure relief valve 42, a throttle device 64 is held in the overflow 46 in a press fit. This throttle device 64 is formed in the embodiment shown in Figures 2 to 4 as separate from the pressure relief valve 42 and cup-shaped part 65 which has a bottom portion 66 and an approximately rectangular and peripheral wall portion 68 to this. The part 65 may be made, for example, as sheet metal and stamped part. In the bottom portion 66 there is an opening 70 which has a diameter Di and forms a flow restrictor. In the present embodiment, the free cross-sectional area F D i on the basis of the diameter Dl of the flow restrictor 70 is 0.6 times the cross-sectional area F d i on the basis of the diameter di of the valve seat 54 of the pressure relief valve 42. However, values between the 0.6 times to 1.1 times.
Die Kraftstoff-Hochdruckpumpe 16 arbeitet folgendermaßen: Bei einem Saughub des Pumpenkolbens 34 öffnet das Einlassventil 30 und Kraftstoff strömt aus der Niederdruck-Kraftstoffleitung 14 in den Förderraum 32. Bei einem anschließenden Förderhub wird der im Förderraum 32 eingeschlossene Kraftstoff komprimiert, bis schließlich das Auslassventil 38 öffnet und der Kraftstoff unter hohem Druck in das Rail 18 gepresst wird. Kommt es im Rail 18 und somit auch im Bereich des Hochdruckauslasses 26 zu einem zu hohen Druck, hebt das Ventilelement 56 aufgrund der dann herrschenden Druckdifferenz während eines Saughubs des Pumpenkolbens 34 vom Ventilsitz 54 und gegen die Kraft der Ventilfeder 62 ab. Auf diese Weise kann Kraftstoff aus dem Rail 18 beziehungsweise dem Hochdruckauslass 26 über den Überströmkanal 46 und das Druckbegrenzungsventil 42 in den Förderraum 32 strömen. Hierdurch wird das Rail 18 und der Hochdruckauslass 26 entlastet.The high-pressure fuel pump 16 operates as follows: During a suction stroke of the pump piston 34 opens the inlet valve 30 and fuel flows from the low-pressure fuel line 14 in the delivery chamber 32. In a subsequent delivery stroke of trapped in the delivery chamber 32 fuel is compressed until finally the exhaust valve 38th opens and the fuel is pressed under high pressure in the rail 18. If there is too high a pressure in the rail 18 and thus also in the area of the high-pressure outlet 26, the valve element 56 lifts off from the valve seat 54 and against the force of the valve spring 62 due to the then prevailing pressure difference during a suction stroke of the pump piston 34. In this way, fuel can flow out of the rail 18 or the high-pressure outlet 26 via the overflow channel 46 and the pressure-limiting valve 42 into the delivery chamber 32. As a result, the rail 18 and the high-pressure outlet 26 is relieved.
Eine alternative Ausführungsform ist in den Figuren 5 und 6 gezeigt. Dabei gilt hier und bei nachfolgenden Ausführungsformen, dass solche Elemente und Bereiche, die äquivalente Funktionen zu vorab beschriebenen Elementen und Bereichen aufweisen, die gleichen Bezugszeichen tragen und nicht nochmals im Detail erläutert sind. Bei der in den Figuren 5 und 6 gezeigten Ausführungsform einer Kraftstoff-Hochdruckpumpe 16 ist die Drosseleinrichtung 64 nicht als separates Teil ausgebildet, sondern in den Ventilsitzkörper 44 des Druckbegrenzungsventils 42 integriert, und zwar hochdruckseitig und sehr nahe oder sogar unmittelbar benachbart zum Ventilsitz 54 in Form einer Engstelle 70. Deren freie Querschnittsfläche FDi, bezogen auf ihren Durchmesser Di, beträgt vorliegend etwa das 0,5-fache der Querschnittsfläche Fdi des Ventilsitzes 54 des Druckbegrenzungsventils 42, auf den Durchmesser di bezogen.An alternative embodiment is shown in Figures 5 and 6. Here and in subsequent embodiments, it applies that such elements and regions which have equivalent functions to previously described elements and regions bear the same reference numerals and are not explained again in detail. In the embodiment of a fuel high pressure pump 16 shown in Figures 5 and 6, the throttle device 64 is not formed as a separate part, but integrated into the valve seat body 44 of the pressure relief valve 42, namely the high pressure side and very close or even immediately adjacent to the valve seat 54 in shape a constriction 70. Their free cross-sectional area F D i, based on their diameter Di, in the present case is about 0.5 times the cross-sectional area Fdi of the valve seat 54 of the pressure limiting valve 42, based on the diameter di.
Bei beiden Ausführungsformen entsprechend der Figuren 2 bis 4 oder 5 und 6 ist der freie Querschnitt der Strömungsdrossel 70 ausgelegt, dass er bei geöffnetem Druckbegrenzungsventil 42, also dann, wenn das Ventilelement 56 vom Ventilsitz 54 abgehoben ist (vergleiche Figur 6), höchstens in etwa dem sich dann einstellenden ringförmigen Öffnungsquerschnitt FR entspricht, der durch den Spalt 72 zwischen Ventilelement 56 und Ventilsitz 54 gebildet wird. Auf diese Weise wird sichergestellt, dass der sich auf diese Weise einstellende Hub H des Ventilelements 56 kleiner ist als die Eintauchtiefe T, wodurch verhindert wird, dass sich das Ventilelement 56 zwischen Ventilsitzkörper 44 und dem Ventilelementhalter 60 verklemmen kann.In both embodiments according to Figures 2 to 4 or 5 and 6, the free cross section of the flow restrictor 70 is designed so that it is at an open pressure relief valve 42, ie when the valve member 56 is lifted from the valve seat 54 (see Figure 6), at most approximately the then adjusting annular opening cross-section F R corresponds, which is formed by the gap 72 between the valve element 56 and the valve seat 54. In this way it is ensured that the thus adjusting stroke H of the valve member 56 is smaller than the immersion depth T, thereby preventing that the valve element 56 between the valve seat body 44 and the valve member holder 60 can jam.
Figur 7 zeigt einen Bereich einer nochmals alternativen Ausführungsform einer Kraftstoff- Hochdruckpumpe 16. Diese entspricht im Hinblick auf die Ausführung der Strömungsdrossel 70 der in den Figuren 5 und 6 gezeigten Ausführungsform. Zusätzlich ist jedoch an den Ventilsitzkörper 44 des Druckbegrenzungsventils 42 ein sich in Öffnungsrichtung (Pfeil 74) des Ventilelements 56, also in axialer Richtung des Druckbegrenzungsventils 42 erstreckender ringförmiger Kragen 76 angeformt, der einen Sicherungsabschnitt für das Ventilelement 56 bildet. Der Kragen 76 weist dabei eine radiale Außenseite 78 auf, mit der er an der Innenseite des Überströmkanals 46 anliegt. Eine radiale Innenseite 80 des Kragens 76 führt von einem sich radial erstreckenden Absatz 82 bis zum abragenden Ende des Kragens 76. Der Absatz 82 erstreckt sich dabei in radialer Richtung ausgehend ungefähr vom Ventilsitz 54, ist zu diesem also benachbart.FIG. 7 shows a portion of yet another alternative embodiment of a high-pressure fuel pump 16. This corresponds to the embodiment shown in FIGS. 5 and 6 with regard to the design of the flow restrictor 70. In addition, however, an annular collar 76 extending in the opening direction (arrow 74) of the valve element 56, that is to say in the axial direction of the pressure limiting valve 42, which forms a securing section for the valve element 56, is integrally formed on the valve seat body 44 of the pressure limiting valve 42. The collar 76 has a radial outer side 78, with which it bears against the inside of the overflow channel 46. A radial inner side 80 of the collar 76 leads from a radially extending shoulder 82 to the projecting end of the collar 76. The shoulder 82 extends in the radial direction approximately from the valve seat 54, thus adjacent thereto.
Der Ventilelementhalter 60 ist bei der in Figur 7 gezeigten Ausführungsform kolbenartig ausgebildet mit einem ungefähr in seiner axialen Mitte angeordneten Ringbund 84, an dem sich die Ventilfeder 62 abstützt. Ein zapfenartiger Abschnitt 86 des Ventilelementhalters 60 erstreckt sich vom Ringbund 84 ausgehend, ähnlich zu den in den Figuren 3 sowie 5 und 6 gezeigten Ausführungsformen, in den von der Ventilfeder 62 begrenzten Ringraum (ohne Bezugszeichen) hinein. Ein in der Nähe des Ringbundes 84 liegender Bereich 88 des zapfenartigen Abschnitts 86 hat einen Außendurchmesser, der nur unwesentlich kleiner ist als der Innendurchmesser der Ventilfeder 62. Auf diese Weise ist der Ventilelementhalter 60 verkippsicher an der Ventilfeder 62 gehalten.The valve element holder 60 is piston-like in the embodiment shown in FIG. 7, with an annular collar 84 arranged approximately in its axial center, against which the valve spring 62 is supported. A pin-like portion 86 of the valve element holder 60 extends from the annular collar 84, starting from the valve spring 62 limited annular space (without reference numeral), similar to the embodiments shown in Figures 3 and 5 and 6 in. A lying in the vicinity of the annular collar 84 region 88 of the peg-like portion 86 has an outer diameter that is only slightly smaller than the inner diameter of the valve spring 62. In this way, the valve element holder 60 is held tilt-proof on the valve spring 62.
Auf der entgegengesetzten Seite des Ringbundes 84 erstreckt sich von diesem ein Halteabschnitt 90 bis zum Ventilelement 56. Bei der in Figur 7 gezeigten Ausführungsform hat der Halteabschnitt 90 eine zylindrische Außenkontur mit über seine Länge gleichbleibendem Durchmesser. Ein Sackloch (ohne Bezugszeichen) dient zur radialen Halterung des Ventilelements 56 am Ventilelementhalter 60. Der Außendurchmesser des Halteabschnitts 90 ist so gewählt, dass der Halteabschnitt 90 in der in Figur 7 gezeigten geschlossenen Stellung des Druckbegrenzungsventils 42 gegenüber der radialen Innenseite 80 des Kragens 76 noch einen geringen Abstand aufweist. Auf diese Weise wird sichergestellt, dass der Halteabschnitt 90 nicht am Kragen 76 anstößt, bevor das Ventilelement 56 vollständig am Ventilsitz 54 anliegt.On the opposite side of the annular collar 84 extends from this a holding portion 90 to the valve member 56. In the embodiment shown in Figure 7, the holding portion 90 has a cylindrical outer contour with constant over its length diameter. A blind hole (without reference numeral) serves for the radial retention of the valve element 56 on the valve element holder 60. The outer diameter of the holding section 90 is selected so that the holding section 90 in the closed position of the pressure limiting valve 42 shown in FIG. 7 still faces the radial inner side 80 of the collar 76 has a small distance. In this way it is ensured that the holding portion 90 does not abut the collar 76 before the valve element 56 fully abuts the valve seat 54.
Die Länge des Kragens 76 und des Halteabschnitts 90 sind jedoch so aufeinander abgestimmt, dass der Halteabschnitt 90 des Ventilelementhalters 60 sowohl bei geschlossenem als auch bei geöffnetem Druckbegrenzungsventil 42 in den von der radialen Innenseite 80 begrenzten Innenraum des Kragens 76 eintaucht. Auch auf diese Weise wird durch den Kragen 76 sichergestellt, dass selbst bei dynamischen Druckstößen und hierdurch verursachten großen Öffnungshüben des Ventilelements 56 dieses aus dem durch den Kragen 76 begrenzten Raum nicht heraustreten und stattdessen zuverlässig beim Schließen des Druckbegrenzungsventils 42 wieder in den Ventilsitz 54 zurückfinden kann.However, the length of the collar 76 and the holding portion 90 are coordinated so that the holding portion 90 of the valve element holder 60 immersed in both the closed and open pressure relief valve 42 in the limited of the radial inner surface 80 interior of the collar 76. Also in this way is ensured by the collar 76 that even with dynamic pressure surges and thereby caused large opening strokes of the valve element 56 this out of the limited space by the collar 76 and instead can reliably find back when closing the pressure relief valve 42 into the valve seat 54 ,
Um dann, wenn das Ventilelement 56 vom Ventilsitz 54 abgehoben hat, eine möglichst ungehinderte Abströmung des Fluids zum Förderraum 32 hin zu gewährleisten, sind über die Umfangserstreckung des Kragens 76 hinweg verteilt drei Strömungstaschen 92 auf der radialen Innenseite 80 desIn order then, when the valve element 56 has lifted from the valve seat 54, to ensure a possible unimpeded outflow of the fluid to the pumping chamber 32, are distributed over the circumferential extent of the collar 76 away three flow pockets 92 on the radial inside 80 of the
Kragens 76 ausgebildet. Diese erstrecken sich vom Absatz 82 über die gesamte Länge des Kragens 76 hinweg bis zu dessen abragendem Ende und haben eine kreissegmentförmige Randkontur. Dies ist insbesondere aus Figur 8 ersichtlich.Collar 76 is formed. These extend from the shoulder 82 over the entire length of the collar 76 away to its abragendem end and have a circular-segment-shaped edge contour. This can be seen in particular from FIG.
Eine in den Figuren 9 und 10 gezeigte alternative Ausführungsform unterscheidet sich von jener der Figuren 7 und 8 dadurch, dass anstelle der Strömungstaschen in den Kragen/Sicherungsabschnitt 76 dessen gesamte Dicke durchsetzende Schlitze 94 eingebracht sind, die sich ebenfalls vom Absatz 82 über die gesamte Länge des Kragens 76 bis zu dessen abragendem Ende erstrecken. Eine weitere Variante zeigt Figur 11 : Bei dieser ist die radiale Innenseite 80 des Kragens 76 als sich in Öffhungsrichtung 74 des Druckbegrenzungsventils 42 erweiternde Konusfläche ausgebildet. Auch der Halteabschnitt 90 des Ventilelementhalters 60 ist ähnlich konisch ausgeführt, jedoch mit kleinerem Konuswinkel als die radiale Innenseite 80 des Kragens 76. Bei einer Öffnungsbewegung des Ventilelements 56 und des Ventilelementhalters 60 in Öffnungsrichtung 74 ergibt sich ein sich vergrößernder Abstand zwischen diesen Elementen einerseits und der radialen Innenseite 80 des Kragens 76 andererseits, durch den das Fluid zum Förderraum 32 hin abströmen kann. Der Konuswinkel kann dabei etwa den gleichen Konuswinkel wie der Ventilsitz 54 aufweisen (vergleiche insbesondere Figur 4), oder einen größeren Konuswinkel als der Ventilsitz 54.An alternative embodiment shown in Figures 9 and 10 differs from that of Figures 7 and 8 in that instead of the flow pockets in the collar / securing portion 76 of its entire thickness penetrating slots 94 are introduced, which are also from the shoulder 82 over the entire length of the collar 76 extend to its abragendem end. A further variant is shown in FIG. 11: In this case, the radial inner side 80 of the collar 76 is designed as a conical surface widening in the direction of opening 74 of the pressure-limiting valve 42. The holding portion 90 of the valve element holder 60 is similarly conical, but with a smaller cone angle than the radial inner side 80 of the collar 76. Upon an opening movement of the valve element 56 and the valve element holder 60 in the opening direction 74 results in an increasing distance between these elements on the one hand and radial inside 80 of the collar 76 on the other hand, through which the fluid can flow to the pumping chamber 32 out. The cone angle can have approximately the same cone angle as the valve seat 54 (compare in particular FIG. 4), or a larger cone angle than the valve seat 54.
Bei der in Figur 11 gezeigten Ausführungsform geht der Ventilsitz 54 unmittelbar in die radiale Innenseite 80 über. Bei der in Figur 12 gezeigten Ausführungsform dagegen schließt sich an den Ventilsitz 54 zunächst wieder ein Absatz 82 an, der sich in radialer Richtung erstreckt, und erst von diesem aus geht dann die Konusfläche der radialen Innenseite 80 des Kragens 76 ab. Auch hier wird durch den Absatz 82 eine bei geöffnetem Ventilelement 56 in Schließrichtung auf das Ventilelement 56 wirkende Kraft verhindert oder zumindest reduziert.In the embodiment shown in FIG. 11, the valve seat 54 transitions directly into the radial inner side 80. In the embodiment shown in FIG. 12, on the other hand, a shoulder 82, which extends in the radial direction, initially adjoins the valve seat 54, and only then does the conical surface of the radial inside 80 of the collar 76 come off. Here too, the shoulder 82 prevents or at least reduces a force acting on the valve element 56 in the closing direction when the valve element 56 is open.
Eine nochmalige Variante zu Figur 12 zeigt Figur 13, bei der der Konuswinkel der die radiale Innenseite 80 des Kragens 76 bildenden Konusfläche vergleichsweise steil und der Halteabschnitt 90 zylindrisch mit gleichbleibendem Durchmesser ist. Diese Variante hat den Vorteil, dass dasA further variant of FIG. 12 is shown in FIG. 13, in which the cone angle of the conical surface forming the radial inner side 80 of the collar 76 is comparatively steep and the holding portion 90 is cylindrical with a constant diameter. This variant has the advantage that the
Abströmverhalten bei geöffnetem Druckbegrenzungsventil 42 vom Öffnungshub des Ventilelements 56 weitgehend unabhängig ist. Abströmverhalten with open pressure relief valve 42 from the opening stroke of the valve element 56 is largely independent.
Claims
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP11157492A EP2333304B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
| EP11157537.9A EP2336546B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102006019049 | 2006-04-25 | ||
| DE102007016134A DE102007016134A1 (en) | 2006-04-25 | 2007-03-29 | High pressure fuel pump, has throttle arrangement provided at high pressure side of valve seat of pressure limiting valve, where cross section of arrangement is approximately equal to desired maximum opening cross section of valve |
| PCT/EP2007/053682 WO2007122127A1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
Related Child Applications (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP11157492A Division EP2333304B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
| EP11157537.9A Division EP2336546B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
| EP11157537.9 Division-Into | 2011-03-09 | ||
| EP11157492.7 Division-Into | 2011-03-09 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2013469A1 true EP2013469A1 (en) | 2009-01-14 |
| EP2013469B1 EP2013469B1 (en) | 2011-09-28 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP11157537.9A Not-in-force EP2336546B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
| EP11157492A Not-in-force EP2333304B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
| EP07728147A Active EP2013469B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
Family Applications Before (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP11157537.9A Not-in-force EP2336546B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
| EP11157492A Not-in-force EP2333304B1 (en) | 2006-04-25 | 2007-04-16 | High pressure fuel pump |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US8202065B2 (en) |
| EP (3) | EP2336546B1 (en) |
| JP (1) | JP5069288B2 (en) |
| CN (1) | CN101432518B (en) |
| DE (1) | DE102007016134A1 (en) |
| ES (2) | ES2370854T3 (en) |
| WO (1) | WO2007122127A1 (en) |
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- 2007-03-29 DE DE102007016134A patent/DE102007016134A1/en not_active Withdrawn
- 2007-04-16 EP EP11157537.9A patent/EP2336546B1/en not_active Not-in-force
- 2007-04-16 ES ES07728147T patent/ES2370854T3/en active Active
- 2007-04-16 JP JP2009507028A patent/JP5069288B2/en active Active
- 2007-04-16 US US12/298,407 patent/US8202065B2/en active Active
- 2007-04-16 WO PCT/EP2007/053682 patent/WO2007122127A1/en not_active Ceased
- 2007-04-16 CN CN2007800148079A patent/CN101432518B/en active Active
- 2007-04-16 EP EP11157492A patent/EP2333304B1/en not_active Not-in-force
- 2007-04-16 ES ES11157537.9T patent/ES2479691T3/en active Active
- 2007-04-16 EP EP07728147A patent/EP2013469B1/en active Active
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2007122127A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2336546B1 (en) | 2014-06-18 |
| CN101432518B (en) | 2012-07-11 |
| CN101432518A (en) | 2009-05-13 |
| EP2013469B1 (en) | 2011-09-28 |
| EP2333304A1 (en) | 2011-06-15 |
| ES2370854T3 (en) | 2011-12-23 |
| ES2479691T3 (en) | 2014-07-24 |
| JP2009534582A (en) | 2009-09-24 |
| DE102007016134A1 (en) | 2007-11-08 |
| JP5069288B2 (en) | 2012-11-07 |
| WO2007122127A1 (en) | 2007-11-01 |
| US20090252621A1 (en) | 2009-10-08 |
| EP2333304B1 (en) | 2012-08-22 |
| EP2336546A1 (en) | 2011-06-22 |
| US8202065B2 (en) | 2012-06-19 |
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