EP1433949A2 - Système d'alimentation de carburant pour l'alimentation de carburant et pompe à jet correspondante - Google Patents
Système d'alimentation de carburant pour l'alimentation de carburant et pompe à jet correspondante Download PDFInfo
- Publication number
- EP1433949A2 EP1433949A2 EP03029136A EP03029136A EP1433949A2 EP 1433949 A2 EP1433949 A2 EP 1433949A2 EP 03029136 A EP03029136 A EP 03029136A EP 03029136 A EP03029136 A EP 03029136A EP 1433949 A2 EP1433949 A2 EP 1433949A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- fuel
- jet pump
- suction jet
- opening
- tank
- 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
Images
Classifications
-
- 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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/02—Feeding by means of suction apparatus, e.g. by air flow through carburettors
- F02M37/025—Feeding by means of a liquid fuel-driven jet pump
-
- 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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M37/10—Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
Definitions
- the present invention relates to a fuel delivery system for the supply of fuel from the Fuel tank to the motor vehicle engine with one of Fuel tank up to an injection system of the motor vehicle engine or up to this self-reaching Fuel supply line, one the excess fuel fuel return line returning to the fuel tank and at least one high pressure fuel pump to deliver fuel from the fuel tank to the engine or the injection system, according to the generic term of claim 1, and a suction jet pump for this, after the preamble of claim 8, as well as a suitable one Method according to the preamble of claim 15.
- cooling circuits such as one on the underbody of the motor vehicle arranged, additional lamella fuel cooler, by means of which the excess returned from the motor Fuel can be cooled specifically before this is returned to the fuel tank.
- a thermal switch valve is required to the cooler switch out of the fuel return flow or into to be able to switch it in, depending on the heating of the Fuel and depending on the outside temperature, because too low Heating of the fuel, for example in the branch area, and when the outside temperature is too low or too cold hypothermia of the fuel can be avoided should.
- the fuel temperature should not fall below 3 ° C if possible should.
- Fuel tank a fuel reservoir is used.
- the Fuel reservoir with a defined volume provides sure that even when the fuel tank is empty always sufficient fuel for the supply to the high-pressure fuel pump is available so this does not run dry or even draws air.
- a suction jet pump interposed that by means of a Venturi nozzle and one of these downstream suction jet pump opening fuel from the Sucks the fuel tank and into the intermediate storage or promotes the fuel reservoir.
- the thermal switch the task the temperature of the returned, heated fuel to monitor and if necessary to a predetermined Cool down limit.
- This temperature limit the fuel is determined among other things according to the material properties of the high pressure fuel pump and the material properties of those in the fuel supply system installed parts.
- the thermal switch the function to determine whether the of the High pressure fuel pump or from the injection system recirculated fuel either to the tank or in the Intermediate reservoir or fuel reservoir located in the tank can be fed directly, or whether the reverse flow via the finned cooler.
- the thermal switch is designed so that under normal operating conditions the fuel flowing back through the radiator or heat exchanger is cooled.
- the object of the present invention is therefore while avoiding the above disadvantages Fuel supply system for the supply of fuel to propose from the fuel tank to the automobile engine, that is much simpler. In particular, should on the additional thermal switch and the additional one Coolers or heat exchangers can be dispensed with entirely.
- a fuel supply system for the supply of fuel from the fuel tank to the motor vehicle engine with one from the fuel tank to the motor vehicle engine or to an injection system of the motor vehicle engine reaching fuel supply line, one return the excess fuel to the fuel tank Fuel return line and at least a fuel pressure pump to deliver the fuel provided from the fuel tank to the motor vehicle engine, in the in the fuel tank between the fuel return line and the fuel supply line a fuel buffer to maintain sufficient Amount of fuel for the fuel pressure pump, and a Suction jet pump for supplying the fuel buffer with fuel from the fuel return line and the tank is arranged, the first time Fuel supply line at least one opening into the tank and fuel branching and before the suction jet pump or the nozzle arrangement arranged opening such has only a portion of the returned fuel the suction jet pump for supplying the fuel buffer flows.
- the relative proportion of that pumped by the suction jet pump Fuel from the tank against which the suction jet pump continuous recirculated and to the Fuel passed on to intermediate storage increased significantly becomes.
- the fuel supply system according to the invention uses this the capacity of the tank and / or Tanks to absorb the heat of the returned fuel and give it to the environment in the sense of a heat exchanger.
- the opening with respect to the suction jet pump which comprises a nozzle arrangement comprising a Venturi nozzle and a catching nozzle, a suction jet opening being introduced between the two nozzles, is arranged such that the opening lies opposite the Venturi nozzle ,
- the fuel partial flow that can be traced back by the engine or by the injection system is divided into two partial flows, one of which can be fed to the Venturi nozzle of the suction jet pump, and of which the other fuel partial flow can be returned to the fuel tank in such a way that a kinetic energy is used to generate a Swirling of the fuel in the fuel tank can be forced to mix with the returned fuel.
- the invention not only makes it possible only drastically reduced the number of necessary components , but also the time clearly required for the assembly of the motor vehicle reduced, sources of error during assembly eliminated and thus the total costs are significantly reduced. In addition, the risk of damage to an im State of the art arranged on the motor vehicle underbody Finned cooler or the like.
- the fuel is a diesel fuel.
- the fuel supply system of the present invention discussed above works particularly well with diesel fuels heating problems occurring outstanding and at the same time cost-effective to control. Nevertheless this is not exclusively on diesel fuels limited, but can also apply to everyone else Fuel systems find application where one Heating of the fuel, for example, due to the Use of high pressure pumps can be determined.
- the injection system is a common rail injection system. On this way can take advantage of the present invention to the most modern variant of diesel fuel engines be transmitted.
- the opening into two parts of the returned, heated fuel flow compared to the Venturi nozzle in the rear wall or in the housing of the suction jet pump is arranged.
- This offers the advantage of one particularly compact design of the suction jet pump according to the invention. It is also ensured that the im Fuel sump at a point as low as possible Suction jet pump arranged with fuel tanks is relatively safe from running dry, at the same time over has the opening for dividing the volume flow, so that the branched volume flow in turn in the area of a the lowest possible point in the fuel tank can be returned. It also starts from there a good swirling and mixing of the whole Fuel tank content achievable.
- the cross section of the opening is variable or with a constant opening cross-section of the opening a valve is arranged downstream of it, for variation the volume of the partial fuel flow returned in the fuel tank.
- a valve is arranged downstream of it, for variation the volume of the partial fuel flow returned in the fuel tank.
- variable opening or a control unit is assigned to the valve, by means of which can actively regulate the volume flow.
- variable opening or the valve integrated directly into the control loop of the engine management and addressed by it as needed, so that about the assigned control unit of each Operating state according to the desired opening cross-section or valve position can be set.
- the fuel return line from the opening in front of the suction jet pump the fuel tank is extended into it. So that the volume flow of the heated in the fuel tank Fuel in the most suitable place in the Fuel tank are guided so that the desired optimal Mixing and swirling of the heated returned fuel and cool in the fuel tank fuel under consideration the special geometrical conditions of each Tank variant can be selected.
- the suction jet pump be pressure controlled is. This in turn can quickly turn to the applicable boundary conditions of the respective operating state Be taken into account and by the Suction jet pump amount of fuel supplied to the fuel reservoir adapted to or corresponding to the corresponding need can be set. It also prevents the partial flow of recirculated fuel that should flow through the Venturi nozzle, whose throughput exceeds and to a defect of the suction jet pump or too could cause malfunction.
- a suction jet pump in particular for a fuel supply system discussed above proposed with a suction jet pump inlet downstream Venturi nozzle, one in the direction of flow suction jet pump opening downstream of the Venturi nozzle, a further subordinate catch nozzle, which in a suction jet pump outlet opens, the suction jet pump inlet a connection for a fuel return section and the suction jet pump outlet either opens into the fuel reservoir or a connection for a fuel transfer line section.
- the Suction jet pump according to the invention provided that the Opening for volume flow distribution opposite the Venturi nozzle is arranged in the rear wall of the suction jet pump. Furthermore, it is provided that the cross section of the Opening variable or with constant opening cross-section a valve is arranged downstream of the opening, so that a variation of the volume of the recycled into the fuel tank Partial current is possible. Furthermore is provided that the variable opening or the valve a control unit is assigned to regulate the volume flow. Last but not least, it is provided that the fuel return line from the arranged in front of the suction jet pump Opening out into the fuel tank is extended. Finally, it is envisaged that the Suction jet pump is pressure controlled. With that, too already above on the fuel supply system according to the invention discussed benefits in synergistic Way achieved.
- the suction jet pump according to the invention is proposed that to form the opening for the volume flow division a small one in the back wall of the suction jet pump Hole is drilled.
- the hole forming the opening in the The rear wall is at the same height and central to rearward extension of the axis of symmetry of the suction jet pump or the Venturi nozzle.
- the opening or that Hole is preferably 1.5 mm in diameter. This corresponds to the diameter in the present embodiment the Venturi nozzle and thus leads to a division of the return flow into two partial flows of approx. 50 each %.
- the degree of division depends on the most diverse Requirements or factors. Determining factors are, for example, the consumption of the motor vehicle engine, the total amount of fuel to be pumped, the minimum and maximum throughput of the high pressure pump as well the cooling or temperature requirement etc.
- the distribution of the recirculated, heated fuel volume flow in two partial flows means that half of the Return flow remains in the suction jet pump and to Intake of fresh, cool fuel from the fuel tank can be used so that this fresh Fuel along with the proportionate heated recirculated Fuel supplied to the fuel reservoir can be. The other part of the returned fuel is delivered directly to the tank. In this way the proportion of fresher and cooler fuel increases at the to be pumped into the fuel reservoir Amount of fuel, so that the desired temperature limits are easily compliant.
- the ratio of the mixing can not only statically using a hole, but also flexibly adjusted by a regulated or controllable valve become.
- a regulated or controllable valve For. B. targeted for different Load conditions of the motor vehicle engine or the motor vehicle high pressure pump different mixing ratios can be set, creating a defined Temperature band, if not a constant temperature level, can be regulated, which subsequently the Temperature load of the high pressure pump significantly reduced or with appropriate temperature control in the for High pressure pump optimizes the optimal temperature range, and resulting in less wear and tear and thus lower fuel consumption can be achieved become.
- Another advantageous aspect of the invention is that optimized by the above Position of the hole a particularly intensive mixing of the fuel emerging from the opening the remaining fuel tank content can be done. This is related among other things to the fact that the so positioned Always open below the normal fuel level is in the tank. Furthermore, the branched off through the opening Partial flow mainly due to the aligned position of the Opening relative to the venturi opening with a relative high pressure, which is a reaction the accelerated flow rate of the fuel through the venturi opening. hereby the branched partial flow flows with a comparatively high speed in the in the fuel tank yet fresh fuel. This causes an extreme Swirling of the heated recirculated fuel in the fuel tank and thereby intensifies the Mixing, so disproportionate local heating be avoided.
- the present invention leads among other things as a result of the replacement of comparatively extremely expensive components and a considerable Simplification of the fuel supply system, which at Savings in large series not to be underestimated multi-digit range.
- the advantages of the present discussed above Invention is therefore a) one if possible easy compliance with all temperature limits of the Fuel system and the engine, b) a cost reduction by eliminating a cooler, especially one Finned cooler and the associated thermal switch, c) ensuring quality for life No additional components due to minor changes of a series part, namely the suction jet pump, and d) compliance with strict crash requirements, such as for example the new so-called "pile test", because on risky positioning of a diesel cooler on Underbody can be dispensed with entirely.
- Fig. 1 is a schematic simplified representation an exemplary embodiment of an inventive Fuel supply system 1 shown.
- Fuel 4 is stored in a fuel tank 2.
- Fuel buffer in the fuel tank 2 6 arranged in which a certain subset Fuel 8 is kept ready.
- a fuel supply line 10 a high-pressure fuel pump 12, which the fuel 4th or 8 from the fuel tank 2 or the fuel buffer 6 under appropriate pressure one here Injection system, not shown, or a common rail injection system a motor 14 supplies. From the engine 14 unused, excess fuel by means of a fuel return line 16 into the fuel tank 2 or returned to the intermediate fuel store 6.
- the symbolizes schematically in a kind of looped fuel return line 16 which due to the high complexity of a Motor vehicle's complex wiring, which at the same time forms a kind of additional "cooling loop" 18, which additionally a structurally simple beyond the invention Variant for another cooling capacity offers without use any additional, fault-prone components to have to.
- the with the fuel return line 16 to Fuel tank 2 returned fuel is in the range a suction jet pump not shown here divided into two partial fuel streams 20 and 22.
- the a partial fuel flow 20 of the recirculated, warmed up Fuel is released directly into the fuel tank 2, so that he is there with the one inside cooler fuel 4 can mix and cool.
- the other, second sub-stream 22 is not specified in detail shown suction jet pump with suction of fresh Fuel 4, here schematically simplified by the supplied Stream 24 symbolized as a mixed Fuel flow 26 fed to the fuel buffer 6.
- the branch of the fuel return line 16 recirculated fuel flow in two partial streams 20 and 22 is by means of one in Fig. 1st symbolically represented with an X variable opening or a valve 28 regulated. Sucking in fresh Fuel occurs via the partial flow 24 supplied with the help of another here in Fig. 1 X Venturi nozzle 30 shown symbolically.
- FIG. 2 is an exemplary longitudinal section an embodiment of a component shown, which includes the suction jet pump 40 according to the invention.
- the suction jet pump 40 has a Venturi nozzle 30 which in the flow or delivery direction X a suction jet pump inlet 42 is subordinate. Between the suction jet pump inlet 42 and the downstream Venturi nozzle 30 is in the embodiment shown here a suction jet pump 40 according to the invention in addition Fuel strainer 44.
- the Venturi nozzle 30 is exemplary in FIG. 2 biased by a spring 46 so that this is pressure-controlled and the maximum permitted venturi throughput possibly briefly exceeding volume flows can cushion.
- the Venturi nozzle 30 is in the flow direction X a suction jet pump suction opening 48 subordinate, in the variant shown here in Area of the coil spring 46 comes to rest, through which fresh fuel 4 from the not shown here Fuel tank can be sucked. Furthermore is in the flow direction X of the Venturi nozzle 30 and the suction jet pump suction opening 48 a so-called Subsequent catch nozzle 50.
- the capture nozzle 50 bundles the two partial streams fed to it and flows in principle in a kind of suction jet pump outlet 52.
- the suction jet pump inlet 42 has a substantially perpendicular to the flow direction X oriented connection flange 54 for a fuel return line or a fuel return section such line.
- the suction jet pump outlet 52 can directly into a fuel buffer not shown here open out, or a connecting flange 58 for a fuel transfer line section, not shown exhibit. It is also conceivable the suction jet pump outlet 52 with the connection 58 or these surrounding components directly with the no closer to connect the fuel buffer shown or to integrate into its wall.
- the one containing the suction jet pump according to the invention Component 40 also has one in front of the Venturi nozzle 30 arranged opening 60, for example in the rear wall 62 of the suction jet pump 40 may be arranged can.
- opening 60 is a through the fuel supply line connection 54 feedable, from the motor recirculated fuel flow 17 into two partial flows 20 and 22 divided.
- One partial flow 22 is in the knee or kink deflected and in the flow direction X of the Venturi nozzle 30 fed.
- the other partial stream 22 is also deflected in the knee or kink and opposite of the flow direction X of the opening 60, through which he flows through and in the ones not shown Fuel tank is transferred.
- Fig. 2 by means of a dash-dotted line Circle and the reference symbol "A" indicated cutout is shown schematically in Fig. 3 in an enlarged view.
- the partial fuel flow 20 flows through the opening 60 in the rear wall 62 of the suction jet pump 40 is arranged in the here also not closer shown fuel tank 2 back. This can be done if necessary a line extension can be provided, by means of which the partial flow 20 to a particularly suitable one Point in the fuel tank 2 can be performed.
- the other partial flow 22 flows through Kink 66 seen from the suction jet pump opening 42 and the downstream sieve 44, then in the flow direction X of the no longer shown here Venturi nozzle 30 to be supplied.
- the opening 60 is in the variant shown here is designed as a hole. This hole can z. B. a diameter of 1.5 mm.
- the opening 60 can also be a variable opening be designed with an adjustable cross section or a downstream valve, not shown here exhibit.
- Fig. 4 is the in schematically 2 and 3 shown suction jet pump component 40 in represented another variant.
- the suction jet pump component 40 is in a wall 70 of the fuel buffer 6 integrated.
- the fuel buffer 6 for its part is within one of his outer dimensions not shown fuel tanks 2, so that the suction jet pump ax 40 in its Floor area or lower area on one if possible low point comes. Accordingly, the Opening 60 of the suction jet pump 40, which at the rear Wall 62 is arranged in the fuel tank 2.
- the suction jet pump outlet which cannot be seen here, opens in an analogous manner directly in the fuel buffer 6.
- Fuel return flow 17 opens from above via the connection flange 54 into the suction jet pump 40.
- This known fuel supply system 101 has one Fuel tank 102 on. In the fuel tank 102 Fuel 104 included. The fuel tank 102 has also a fuel buffer 106, in the stocked Proportional fuel 108 is included. A Fuel supply line 110 leads to a high pressure pump 112, which supplies the fuel to an engine 114. Excess fuel is drained through a fuel return line 116 the fuel buffer 106 or returned to the fuel tank 102.
- Fuel supply system 101 is in one in FIG complex embodiment shown. That about the Fuel return line 116 to the fuel tank 2 or Fuel volume 106 fuel volume to be returned, which is heated by the high pressure pump 112 has passed through a thermal switch 180, which determines the temperature of the returned fuel.
- the fuel return line also leads 116 by a cooler 182, for example as Lamella cooler or the like can be formed. Such a finned cooler can, for example, on the underbody of a motor vehicle, so that these for example, excess heat from the airstream can derive.
- the one cooled down by the cooler 182 Fuel is on the further line section 184 of the fuel return line 116 in turn passed through the thermal switch 180 to the now cooled down temperature of the fuel to be able to determine before this the fuel buffer 106 is supplied.
- the invention discussed above provides for the first time a fuel supply system that is in advantageously as in the prior art additional cooler and felt extremely disadvantageous Thermal switch as well as other components for cooling the excess heated by the high pressure pump Can do without fuel. Furthermore, a suitable one for this Suction jet pump specified and a particularly suitable Methods of supplying fuel are discussed.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2002160473 DE10260473A1 (de) | 2002-12-21 | 2002-12-21 | Kraftstoffzufuhrsystem für die Zufuhr von Kraftstoff sowie Saugstrahlpumpe hierfür |
DE10260473 | 2002-12-21 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1433949A2 true EP1433949A2 (fr) | 2004-06-30 |
EP1433949A3 EP1433949A3 (fr) | 2006-04-12 |
EP1433949B1 EP1433949B1 (fr) | 2012-02-15 |
Family
ID=32404155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20030029136 Expired - Fee Related EP1433949B1 (fr) | 2002-12-21 | 2003-12-18 | Système d'alimentation de carburant pour l'alimentation de carburant et pompe à jet correspondante |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1433949B1 (fr) |
DE (1) | DE10260473A1 (fr) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005001277A1 (fr) * | 2003-06-30 | 2005-01-06 | Robert Bosch Gmbh | Dispositif pour acheminer du carburant contenu dans un reservoir a un moteur a combustion interne |
WO2005001278A1 (fr) * | 2003-06-30 | 2005-01-06 | Robert Bosch Gmbh | Dispositif pour acheminer du carburant contenu dans un reservoir a un moteur a combustion interne |
WO2012150059A1 (fr) * | 2011-05-04 | 2012-11-08 | Robert Bosch Gmbh | Pompe à jet pour l'alimentation en carburant |
FR2992695A1 (fr) * | 2012-06-27 | 2014-01-03 | Bosch Gmbh Robert | Pompe a jet integrant un module de filtre |
WO2015172917A1 (fr) * | 2014-05-14 | 2015-11-19 | Robert Bosch Gmbh | Dispositif d'alimentation en carburant destiné à un véhicule automobile |
EP3591212A1 (fr) * | 2018-07-02 | 2020-01-08 | Delphi Technologies IP Limited | Système de carburant comportant une pompe à jet |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4834132A (en) * | 1986-09-25 | 1989-05-30 | Nissan Motor Company, Limited | Fuel transfer apparatus |
US4860714A (en) * | 1986-08-20 | 1989-08-29 | Whitehead Engineered Products, Inc. | In-tank fuel pump assembly for fuel-injected engines |
JPH02173352A (ja) * | 1988-12-26 | 1990-07-04 | Horie Kinzoku Kogyo Kk | 燃料ポンプユニット |
US5564397A (en) * | 1994-07-28 | 1996-10-15 | Robert Bosch Gmbh | Device for delivering fuel from a fuel tank to the internal combustion engine of a motor vehicle |
US6098600A (en) * | 1997-12-02 | 2000-08-08 | Denso Corporation | Fuel supply system |
-
2002
- 2002-12-21 DE DE2002160473 patent/DE10260473A1/de not_active Withdrawn
-
2003
- 2003-12-18 EP EP20030029136 patent/EP1433949B1/fr not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4860714A (en) * | 1986-08-20 | 1989-08-29 | Whitehead Engineered Products, Inc. | In-tank fuel pump assembly for fuel-injected engines |
US4834132A (en) * | 1986-09-25 | 1989-05-30 | Nissan Motor Company, Limited | Fuel transfer apparatus |
JPH02173352A (ja) * | 1988-12-26 | 1990-07-04 | Horie Kinzoku Kogyo Kk | 燃料ポンプユニット |
US5564397A (en) * | 1994-07-28 | 1996-10-15 | Robert Bosch Gmbh | Device for delivering fuel from a fuel tank to the internal combustion engine of a motor vehicle |
US6098600A (en) * | 1997-12-02 | 2000-08-08 | Denso Corporation | Fuel supply system |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN Bd. 014, Nr. 436 (M-1027), 18. September 1990 (1990-09-18) & JP 02 173352 A (HORIE KINZOKU KOGYO KK), 4. Juli 1990 (1990-07-04) * |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005001277A1 (fr) * | 2003-06-30 | 2005-01-06 | Robert Bosch Gmbh | Dispositif pour acheminer du carburant contenu dans un reservoir a un moteur a combustion interne |
WO2005001278A1 (fr) * | 2003-06-30 | 2005-01-06 | Robert Bosch Gmbh | Dispositif pour acheminer du carburant contenu dans un reservoir a un moteur a combustion interne |
US7281524B2 (en) | 2003-06-30 | 2007-10-16 | Robert Bosch Gmbh | Device for delivering fuel from a reservoir to an internal combustion engine |
WO2012150059A1 (fr) * | 2011-05-04 | 2012-11-08 | Robert Bosch Gmbh | Pompe à jet pour l'alimentation en carburant |
US9546670B2 (en) | 2011-05-04 | 2017-01-17 | Robert Bosch Gmbh | Jet pump for delivering fuel |
FR2992695A1 (fr) * | 2012-06-27 | 2014-01-03 | Bosch Gmbh Robert | Pompe a jet integrant un module de filtre |
WO2015172917A1 (fr) * | 2014-05-14 | 2015-11-19 | Robert Bosch Gmbh | Dispositif d'alimentation en carburant destiné à un véhicule automobile |
EP3591212A1 (fr) * | 2018-07-02 | 2020-01-08 | Delphi Technologies IP Limited | Système de carburant comportant une pompe à jet |
Also Published As
Publication number | Publication date |
---|---|
DE10260473A1 (de) | 2004-07-15 |
EP1433949A3 (fr) | 2006-04-12 |
EP1433949B1 (fr) | 2012-02-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1964775B1 (fr) | Dispositif de mélange pour installation de climatisation d'avion | |
DE102006015730A1 (de) | Kraftstoffzuführsystem für einen Verbrennungsmotor | |
DE102020202570A1 (de) | Reinigungsvorrichtung | |
EP1306548A2 (fr) | Dispositif d'injection de carburant dont le réglage du débit est amélioré | |
DE102005006405A1 (de) | Kraftstoffübertragungseinrichtung | |
DE102020202571A1 (de) | Reinigungsvorrichtung | |
DE19954695A1 (de) | Kraftstoffeinspritzsystem | |
EP1977099B1 (fr) | Système d'alimentation d'une charge en carburant gazeux et procédé associé | |
DE102015220976A1 (de) | Brennkraftmaschine | |
DE102010034434A1 (de) | Dieselkraftstoffpumpenmodul mit einer Umleitung für ausgeflockten Kraftstoff | |
DE10003748A1 (de) | Kraftstoffversorgungssystem für Brennkraftmaschinen mit verbesserter Befüllung der Kraftstoffleitung | |
EP1433949A2 (fr) | Système d'alimentation de carburant pour l'alimentation de carburant et pompe à jet correspondante | |
DE102020208704A1 (de) | Brennstoffzellensystem | |
EP1124055B1 (fr) | Système d'alimentation en carburant pour moteur à combustion | |
EP3470714A1 (fr) | Soupape de réglage d'un flux de fluide de refroidissement destiné au refroidissement des pistons | |
DE102004056295B4 (de) | Ölversorgungsvorrichtung für ein Flugzeugtriebwerk | |
WO2022194770A1 (fr) | Dispositif de refroidissement de profilés et ligne de refroidissement pour un dispositif de refroidissement de profilés | |
DE102012020321A1 (de) | Kraftstoffversorgungseinrichtung | |
DE10335698A1 (de) | Kraftstoffversorgungsanlage einer Brennkraftmaschine sowie Betriebsverfahren hierfür | |
DE102017003105A1 (de) | Verfahren und Vorrichtung zum Kühlen eines Bauteils | |
DE102010019449A1 (de) | Kraftstoffsystem sowie mit diesem Kraftstoffsystem ausgestattetes Fahrzeug | |
DE102017010286A1 (de) | Ausdehnungsbehälter für das Kühlsystem eines flüssigkeitsgekühlten Verbrennungsmotors | |
DE102008042607B4 (de) | Kraftstoffkühler für den Niederdruckteil eines Speichereinspritzsystems einer Brennkraftmaschine | |
DE102018208656B4 (de) | Wassereinspritzsystem für einen Verbrennungsmotor sowie Kraftfahrzeug mit einem solchen | |
DE102019124341B4 (de) | Kraftstoffleistenbaugruppe |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
|
17P | Request for examination filed |
Effective date: 20061009 |
|
AKX | Designation fees paid |
Designated state(s): DE FR GB |
|
17Q | First examination report despatched |
Effective date: 20080131 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC. |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS LLC |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 50314213 Country of ref document: DE Effective date: 20120412 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20121116 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 50314213 Country of ref document: DE Effective date: 20121116 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20151216 Year of fee payment: 13 Ref country code: DE Payment date: 20151215 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20151110 Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50314213 Country of ref document: DE |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20161218 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20170831 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170102 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161218 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170701 |