EP1576272B1 - Non-return fuel supply system - Google Patents

Non-return fuel supply system Download PDF

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Publication number
EP1576272B1
EP1576272B1 EP03799428A EP03799428A EP1576272B1 EP 1576272 B1 EP1576272 B1 EP 1576272B1 EP 03799428 A EP03799428 A EP 03799428A EP 03799428 A EP03799428 A EP 03799428A EP 1576272 B1 EP1576272 B1 EP 1576272B1
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EP
European Patent Office
Prior art keywords
fuel
pressure
supply system
region
return
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.)
Expired - Lifetime
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EP03799428A
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German (de)
French (fr)
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EP1576272A1 (en
Inventor
Peter Schelhas
Andreas Herforth
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Robert Bosch GmbH
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Robert Bosch GmbH
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Priority claimed from DE10327562A external-priority patent/DE10327562A1/en
Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP1576272A1 publication Critical patent/EP1576272A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus 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
    • F02M37/04Feeding by means of driven pumps
    • F02M37/08Feeding by means of driven pumps electrically driven
    • F02M37/10Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
    • F02M37/106Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir the pump being installed in a sub-tank
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/3809Common rail control systems
    • F02D41/3836Controlling the fuel pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus 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
    • F02M37/02Feeding by means of suction apparatus, e.g. by air flow through carburettors
    • F02M37/025Feeding by means of a liquid fuel-driven jet pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus 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
    • F02M37/04Feeding by means of driven pumps
    • F02M37/08Feeding by means of driven pumps electrically driven
    • F02M2037/085Electric circuits therefor
    • F02M2037/087Controlling fuel pressure valve

Definitions

  • the invention is based on a non-return fuel supply system according to the preamble of claim 1.
  • a fuel supply system fuel is pumped from a fuel tank from a fuel pump via a pressure line to a fuel rail on the engine with injectors or to a gasoline or diesel high pressure pump.
  • Modern fuel supply systems have a tank installation unit inserted into the fuel tank, in which the fuel pump, a suction filter and a pot are integrated as a fuel reserve, which is filled by one or more suction jet pumps. Consequently, the suction jet pumps ensure that even when the fuel level in the fuel tank drops, the pot for providing the reserve fuel is always completely filled.
  • the suction jet pumps are arranged in the branched off from the pressure line Saugstrahlpumpentechnisch, which opens into the pot.
  • a return line branches from the fuel rail, leading back into the fuel tank.
  • the fuel quantity not required by the internal combustion engine then flows through the fuel distributor via the return line back into the fuel tank.
  • no return line from the fuel rail to provided the fuel tank is adjusted as needed by the actual fuel pressure measured by a pressure sensor, compared within a control unit with a stored in a map target fuel pressure and depending on the control difference, the speed of the fuel pump is changed.
  • a downstream of the fuel pump check valve in the pressure line ensures a seal of the pressure distribution containing the fuel rail.
  • the control function takes place as long as the internal combustion engine is operated under load and a consumption amount of fuel is called up.
  • Another type of pressure relief valve is closed during operation, so that after a phase of non-promotion and at the beginning of load operation because of the sudden onset of pressure increase over-greasing and higher pressure due to the higher leaks at the injectors higher HC emissions can occur.
  • the opening pressure in both types of pressure relief valves can not be varied during operation.
  • the solenoid valve can be included in the electronic control of the internal combustion engine, which is a control of the system pressure and the amount of fuel in allows all operating conditions of the internal combustion engine, in particular during the shift operation and at a standstill.
  • the electrically actuated solenoid valve depending on the opening duration variable opening pressures are adjustable. This is particularly advantageous for the compensation of temperature-induced pressure changes.
  • electrically actuated solenoid valves eliminates the need for constant flushing, which is why the fuel pump can be made smaller and significantly reduces the risk of contamination of the valve seat.
  • the solenoid valve is interposed between the check valve and the ejector and is driven by a central engine control unit, wherein the control of the solenoid valve in response to the pressure measured by a pressure sensor arranged in the pressure region.
  • the solenoid valve is integrated into the electronic engine control, whereby variable opening pressures can be realized.
  • the pressure range associated with injectors is preferably formed by a pressure line connecting the fuel pump to the injectors.
  • an input of the solenoid valve is connected to the pressure range and an output to the ejector.
  • the solenoid valve is de-energized closed during a standstill phase of the internal combustion engine and otherwise open, for example, during normal operation under load and energized during the coasting operation.
  • the solenoid valve is opened by signals from the engine control unit in order to keep the pressure in the pressure line constant.
  • the electronic control of the solenoid valve, in particular, the holding pressure during coasting and engine downtime can be set arbitrarily. However, this also means that the function of the engine control unit must be temporarily maintained even during the stoppage phase of the internal combustion engine.
  • the solenoid valve is formed by a 2/3 way valve, of which an input to the pressure line, a first output to the suction jet pump and a second output is connected to a pressure relief valve.
  • This 2/3 way valve is controlled by the engine control unit such that it connects the input to the second output in the de-energized state and the input to the first output when energized. Consequently, at standstill of the engine and de-energized deactivated engine control unit, the 2/3 way valve automatically, for example, by spring preload, in its de-energized position, in which the pressure line is connected to the pressure relief valve, via which then pressure is reduced. In normal load operation or coasting of the internal combustion engine, however, the 2/3 way valve is energized by the engine control unit, so that the suction jet pump is connected to the pressure line.
  • the control of the solenoid valve takes place as a function of a degree of filling of the second region the fuel reservoir forming fuel tank with fuel.
  • the pot forming the first region of the fuel reservoir and receiving the fuel pump is then arranged as a reservoir for the reserve fuel. If the solenoid valve is closed when the fill level of the fuel tank is in a range between maximum charge and a level substantially flush with an upper rim of the pot, the fuel will no longer travel past the fuel injector via the closed solenoid valve promoted in the pot. Rather, the fuel then flows to compensate for levels from the fuel tank over the edge of the pot in this.
  • the ejector With sufficient filling level of the fuel tank, the ejector can therefore be put out of operation, resulting in a significant reduction in the required by the fuel pump power, in an increase in system efficiency, in a lower electrical system load, in a lower tank heating and in a longer life of the fuel pump.
  • a further embodiment provides that the solenoid valve is formed by a switching valve, which is controlled clocked to control the driving pressure of the suction jet pump.
  • the solenoid valve may also be a proportional valve, which is controlled to control the driving pressure of the suction jet pump. In both cases, the suction jet pump can always be operated in a region of highest efficiency.
  • the solenoid valve in the sense of a multiple function not only for a particularly advantageous control of the system pressure and the amount of fuel during coasting and at a standstill but also for further energy-saving measures.
  • the generally designated 1 in Fig.1 return-free fuel supply system is used for example for fueling an internal combustion engine of a vehicle and includes as essential components held within a swirl pot 2 of a fuel tank 4 tank installation unit 6 comprising a fuel pump 8 with a suction side filter 10, based on the fuel pump 8 disposed in a pressure-side pressure line 12 check valve 14 and a fuel injector 16 in fluid communication with fuel injectors 18 or a gasoline or diesel high-pressure pump.
  • a pressure sensor 20 measures the actual pressure in the pressure line 12 and sends via a signal line 22 a corresponding signal to a control unit, which is preferably formed by a central engine control unit 24 (MOTRONIC) and in which is controlled as a function of a control difference between the actual pressure and a demand-based desired pressure via an electrical line 26, a control signal to an electronic, connected to the fuel pump 8 via electrical lines 28 fuel pump controller 30 to the pressure in the pressure line 12 via the Regulate fuel pump 8 demand-dependent.
  • MOTRONIC central engine control unit 24
  • downstream portion of the pressure line 12 branches off at a branch point 32 from a Saugstrahlpumpentechnisch 34, which branches, for example in several, preferably in two individual lines 36 branching in each branch 36 a fuel-carrying suction pump 38, wherein the individual lines 36 open into the swirl pot 2.
  • the swirl pot 2 serves on the one hand as a fuel reservoir, on the other hand it prevents that with strong lateral acceleration the fuel pump 8 can no longer suck fuel for a short time, because this centrifugal force is concentrated in a remote from the suction side portion of the fuel tank 4.
  • the suction jet pumps 38 suck fuel from the area of the fuel tank 4 located outside the swirl pot into the two individual lines 36 and ensure a constant fuel level within the swirl pot 2 in a known manner.
  • an electrically actuated solenoid valve 40 Arranged in the suction jet pump line 34 branching off from the pressure line 12 is an electrically actuated solenoid valve 40, which is controlled by the central engine control unit 24 via a control line 42, preferably as a function of the measured pressure in the pressure line 12, the temperature of the fuel, the level and / or the engine operating conditions is controlled.
  • the solenoid valve 40 is designed to open or close the cross section of the suction jet pump line 34.
  • the solenoid valve 40 is preferably closed and energized closed open.
  • the operation of the fuel supply system 1 is as follows: In load operation of the internal combustion engine, the fuel pump sucks 8 fuel from the swirl pot 2, wherein the fuel flow opens the check valve 14 under the effect of fuel pressure and a portion of the fuel flow at the branch point 32 in the Saugstrahlpumpen Koch 34th flows.
  • the engine control unit 24 energizes the solenoid valve 40, whereupon this is switched to the open position, so that the suction jet pumps 38 fuel the region of the fuel tank 4 located outside of the swirl pot 2 can suck into the swirl pot 2.
  • the other part of the fuel flow is fed to the fuel meter 18 as required depending along the pressure line 12 in order to be injected via the injection valves 16 into combustion chambers of the internal combustion engine.
  • the engine control unit 24 switches the solenoid valve 40 de-energized, whereupon it closes. Consequently, the arranged downstream of the check valve 14 portion of the pressure line 12 and the upstream of the solenoid valve 40 disposed portion of the Saugstrahlpumpen Koch 34 is sealed by the closed injectors 16, the closed solenoid valve 40 and by the closed fuel pump 8 towards the check valve 14 against the environment, the Pressure of existing in these sections amount of fuel to be kept constant. Ternperatur myself however, the holding pressure may be too high, which is detected by the pressure sensor 20 and reported to the central engine control unit 24. Then, the solenoid valve 40 is briefly switched by the engine control unit 24 by a current pulse in the open position to reduce the predetermined holding pressure.
  • a solenoid valve here a 2/3 way valve 44 is used, of which an input 46 to the pressure line 12, a first output 48 to the suction jet 38 and a second output 50 is connected to a pressure relief valve 52.
  • the 2/3 way valve 44 is controlled by the central engine control unit 24 such that it connects the input 46 to the second output 50 in the de-energized state and the input 46 to the first output 48 when energized.
  • the 2/3-way valve 44 is de-energized during a standstill phase of the internal combustion engine and otherwise energized, ie in load operation and in overrun operation.
  • the 2/3-way valve 44 automatically, for example by spring preload, in its de-energized position, in which the pressure line 12 is connected to the pressure relief valve 52, via which then pressure can be reduced.
  • the 2/3 way valve 44 is energized by the engine control unit 24, so that the suction jet pumps 38 are connected to the pressure line 12.
  • the control of the solenoid valve 40 takes place in dependence on a degree of filling of the fuel tank 4 with fuel. If the solenoid valve 40 is closed, when the filling level of the fuel tank 4 is in a range between maximum filling and a level that is substantially flush with an upper edge 54 of the swirl pot 2, the fuel is no longer beyond that through the closed solenoid valve 40 except Operation set Saugstrahlpumpen 38 from the fuel tank 4 in the swirl pot 2 promoted. Rather, the fuel then flows to level compensation from the fuel tank 4 via the edge 54 of the swirl pot 2 in this. With sufficient degree of filling of the fuel tank 4, the suction jet pumps 38 can thus be put out of operation. Further, it is possible to vary the shutdown pressure as a function of the temperature and / or of the engine operating conditions.
  • the decommissioning of the Saugstrahlpumpen 38 and the variation of the Abstelltiks can also by the 3/2-way valve 44 according to the second embodiment 2, if it is switched in the above-described, sufficient water level in the fuel tank 4 such that the input 46 is connected to the second output 50, which opens into the pressure relief valve 52. Then, the part of the suction jet pump line 34 located downstream of the 2/3-way valve 44 is shut off to a predetermined pressure level, so that the suction jet pumps 38 are no longer supplied with fuel.
  • the solenoid valves 40, 44 are preferably switching valves, they can be controlled clocked to control the motive pressure of the ejector 38.
  • the solenoid valve 40, 44 may also be a proportional valve, which is controlled to control the driving pressure of the suction jet pump. By controlling the driving pressure, the suction jet pump 38 can then always be operated in a region of highest efficiency.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

The invention relates to a non-return fuel supply system (1) for an internal combustion engine, in particular in a motor vehicle, comprising at least one fuel pump (8), by means of which the fuel may be pumped from a first region (2) of a fuel tank into a pressurised region (12), connected to a fuel distributor (18), at least one suction jet pump (38) through which fuel supplied by the fuel pump (8) along a suction jet pump line (34) flows, by means of which fuel may be supplied from a second region (4) of the fuel tank into the first region (2), at least one means (20, 24, 30), for regulating and/or controlling the pressure in the pressurised region (12) and at least one non-return valve (14), by means of which at least a part of the pressurised region (12) may be sealed off from the fuel pump (8). According to the invention, the means (20, 24, 30) for regulation and/or control of the pressure in the pressurised region contains at least one electrically operated solenoid valve (40; 44), arranged downstream of the non-return valve (14) in the suction jet pump line (34).

Description

Stand der TechnikState of the art

Die Erfindung geht aus von einem rücklauffreien Kraftstoffversorgungssystem gemäß dem Oberbegriff von Anspruch 1.The invention is based on a non-return fuel supply system according to the preamble of claim 1.

In einem Kraftstoffversorgungssystem wird Kraftstoff aus einem Kraftstoffbehälter von einer Kraftstoffpumpe über eine Druckleitung zu einem an der Brennkraftmaschine befindlichen Kraftstoffverteiler mit Einspritzventilen oder zu einer Benzin- oder Dieselhochdruckpumpe gepumpt. Moderne Kraftstoffversorgungssysteme weisen eine in den Kraftstoffbehälter eingesetzte Tankeinbaueinheit auf, in welche die Kraftstoffpumpe, ein Saugfilter und ein Topf als Kraftstoffreserve integriert ist, welcher durch eine oder mehrere Saugstrahlpumpen befüllt wird. Die Saugstrahlpumpen sorgen folglich dafür, dass auch bei abfallendem Kraftstoffpegel im Kraftstoffbehälter der Topf zur Bereitstellung des Reservekraftstoffs stets vollständig gefüllt ist. Die Saugstrahlpumpen sind in der von der Druckleitung abzweigenden Saugstrahlpumpenleitung angeordnet, welche in den Topf mündet.In a fuel supply system, fuel is pumped from a fuel tank from a fuel pump via a pressure line to a fuel rail on the engine with injectors or to a gasoline or diesel high pressure pump. Modern fuel supply systems have a tank installation unit inserted into the fuel tank, in which the fuel pump, a suction filter and a pot are integrated as a fuel reserve, which is filled by one or more suction jet pumps. Consequently, the suction jet pumps ensure that even when the fuel level in the fuel tank drops, the pot for providing the reserve fuel is always completely filled. The suction jet pumps are arranged in the branched off from the pressure line Saugstrahlpumpenleitung, which opens into the pot.

Bei manchen Kraftstoffversorgungssystemen zweigt von dem Kraftstoffverteiler eine Rücklaufleitung ab, die zurück in den Kraftstoffbehälter führt. Die von der Brennkraftmaschine nicht benötigte Kraftstoffmenge strömt dann durch den Kraftstoffverteiler über die Rücklaufleitung zurück in den Kraftstoffbehälter. Bei beispielsweise aus der DE 199 51 132 A1 bekannten rücklauffreien Kraftstoffversorgungssystemen ist dagegen keine Rücklaufleitung von dem Kraftstoffverteiler zu dem Kraftstoffbehälter vorgesehen. Vielmehr wird der Druck im Kraftstoffverteiler bedarfsgerecht geregelt, indem der Ist-Kraftstoffdruck mittels eines Drucksensors gemessen, innerhalb eines Steuergeräts mit einem in einem Kennfeld abgelegten Soll-Kraftstoffdruck verglichen und abhängig von der Regeldifferenz die Drehzahl der Kraftstoffpumpe verändert wird. Ein der Kraftstoffpumpe nachgeordnetes Rückschlagventil in der Druckleitung sorgt für eine Abdichtung des den Kraftstoffverteiler enthaltenden Druckbereichs. Die Regelfunktion erfolgt, solange die Brennkraftmaschine unter Last betrieben und eine Verbrauchsmenge an Kraftstoff abgerufen wird.In some fuel supply systems, a return line branches from the fuel rail, leading back into the fuel tank. The fuel quantity not required by the internal combustion engine then flows through the fuel distributor via the return line back into the fuel tank. In contrast, in known from DE 199 51 132 A1 return-free fuel supply systems, however, no return line from the fuel rail to provided the fuel tank. Rather, the pressure in the fuel rail is adjusted as needed by the actual fuel pressure measured by a pressure sensor, compared within a control unit with a stored in a map target fuel pressure and depending on the control difference, the speed of the fuel pump is changed. A downstream of the fuel pump check valve in the pressure line ensures a seal of the pressure distribution containing the fuel rail. The control function takes place as long as the internal combustion engine is operated under load and a consumption amount of fuel is called up.

Während Phasen, in denen die Einspritzventile geschlossen sind und die Kraftstoffpumpe keinen Kraftstoff in die Druckleitung fördert, beispielsweise bei Motorstillstand, kann bei hohen Temperaturen der Druck in der einerseits durch die geschlossenen Einspritzventile und andererseits das geschlossene Rücklaufventil dichten Druckleitung ansteigen, weshalb mechanisch betätigte Druckbegrenzungsventile oder Membrandruckregler verwendet werden siehe z.B. US 2002/0043253, um den Druck in der Druckleitung konstant zu halten. Ein Typ dieser Druckbegrenzungsventile muss im Betrieb stets von einer geringen Überströmmenge durchspült werden, was einerseits den ständigen Betrieb der Kraftstoffpumpe und folglich einen gewissen Energieverbrauch erfordert und andererseits wegen der geringen Spülmenge die Gefahr besteht, dass sich Schmutz am Ventilsitz ablagert. Ein weiterer Typ von Druckbegrenzungsventil ist im Betriebsfall geschlossen, so dass nach einer Phase der Nichtförderung und zu Beginn des Lastbetriebs wegen des dann plötzlich einsetzenden Druckanstiegs Überfettungen und aufgrund der druckbedingt höheren Leckagen an den Einspritzventilen auch höhere HC-Emissionen auftreten können. Außerdem ist der Öffnungsdruck bei beiden Typen von Druckbegrenzungsventilen während des Betriebs nicht variierbar.During phases in which the injection valves are closed and the fuel pump promotes no fuel in the pressure line, for example, engine stall, at high temperatures, the pressure in the one hand by the closed injectors and on the other hand, the closed return valve sealed pressure line rise, which is why mechanically actuated pressure relief valves or Diaphragm pressure regulator can be used see eg US 2002/0043253 to keep the pressure in the pressure line constant. A type of pressure relief valves must always be flushed during operation of a small overflow, which on the one hand requires continuous operation of the fuel pump and thus a certain energy consumption and on the other hand because of the small amount of flushing there is a risk that dirt deposits on the valve seat. Another type of pressure relief valve is closed during operation, so that after a phase of non-promotion and at the beginning of load operation because of the sudden onset of pressure increase over-greasing and higher pressure due to the higher leaks at the injectors higher HC emissions can occur. In addition, the opening pressure in both types of pressure relief valves can not be varied during operation.

Vorteile der ErfindungAdvantages of the invention

Indem die den Druck im Druckbereich regelnden und/oder steuernden Mittel wenigstens ein elektrisch betätigbares Magnetventil beinhalten, welches stromabwärts des Rückschlagventils in der Saugstrahlpumpenleitung angeordnet ist, kann das Magnetventil in die elektronische Regelung der Brennkraftmaschine einbezogen werden, was eine Regelung des Systemdrucks und der Kraftstoffmenge in allen Betriebszuständen der Brennkraftmaschine ermöglicht, insbesondere während des Schiebebetriebs und bei Stillstand. Dann sind auch im Gegensatz zu den mechanisch hydraulisch betätigten Ventilen des Stands der Technik über das elektrische betätigbare Magnetventil je nach Öffnungsdauer variable Öffnungsdrücke einstellbar. Dies ist insbesondere zum Ausgleich von temperaturbedingten Druckänderungen von Vorteil. Schließlich entfällt bei elektrisch betätigten Magnetventilen das Erfordernis der ständigen Durchspülung, weshalb die Kraftstoffpumpe kleiner dimensioniert werden kann und sich das Verschmutzungsrisiko des Ventilsitzes wesentlich reduziert.By the means controlling and / or controlling the pressure in the pressure region including at least one electrically actuated solenoid valve which is disposed downstream of the check valve in the Saugstrahlpumpenleitung, the solenoid valve can be included in the electronic control of the internal combustion engine, which is a control of the system pressure and the amount of fuel in allows all operating conditions of the internal combustion engine, in particular during the shift operation and at a standstill. Then, in contrast to the mechanically hydraulically actuated valves of the prior art via the electrically actuated solenoid valve depending on the opening duration variable opening pressures are adjustable. This is particularly advantageous for the compensation of temperature-induced pressure changes. Finally, with electrically actuated solenoid valves eliminates the need for constant flushing, which is why the fuel pump can be made smaller and significantly reduces the risk of contamination of the valve seat.

Durch die in den Unteransprüchen aufgeführten Maßnahmen sind vorteilhafte Weiterbildungen und Verbesserungen der im Patentanspruch 1 angegebenen Erfindung möglich.The measures listed in the dependent claims advantageous refinements and improvements of the patent claim 1 invention are possible.

In bevorzugter Weise ist das Magnetventil dem Rückschlagventil und der Saugstrahlpumpe zwischengeordnet und wird von einem zentralen Motorsteuergerät angesteuert, wobei die Ansteuerung des Magnetventils in Abhängigkeit des von einem im Druckbereich angeordneten Drucksensors gemessenen Drucks erfolgt.Preferably, the solenoid valve is interposed between the check valve and the ejector and is driven by a central engine control unit, wherein the control of the solenoid valve in response to the pressure measured by a pressure sensor arranged in the pressure region.

Durch diese Maßnahme ist das Magnetventil in die elektronische Motorsteuerung integriert, wodurch variable Öffnungsdrücke realisierbar sind. Der mit Einspritzventilen in Verbindung stehende Druckbereich wird vorzugsweise durch eine Druckleitung gebildet wird, welche die Kraftstoffpumpe mit den Einspritzventilen verbindet.By this measure, the solenoid valve is integrated into the electronic engine control, whereby variable opening pressures can be realized. The pressure range associated with injectors is preferably formed by a pressure line connecting the fuel pump to the injectors.

Gemäß einer ersten Ausführungsform ist ein Eingang des Magnetventils mit dem Druckbereich und ein Ausgang mit der Saugstrahlpumpe verbunden. Insbesondere ist das Magnetventil während einer Stillstandsphase der Brennkraftmaschine unbestromt geschlossen und ansonsten, beispielsweise während des normalen Betriebs unter Last und während des Schiebebetriebs bestromt geöffnet. Im Falle eines beispielsweise temperaturbedingten Druckanstiegs während der Stillstandsphase wird das Magnetventil durch Signale des Motorsteuergeräts geöffnet, um den Druck in der Druckleitung konstant zu halten. Durch die elektronische Regelung des Magnetventils kann insbesondere der Haltedruck bei Schiebebetrieb und bei Motorstillstand beliebig festgelegt werden. Dies bedeutet aber auch, dass die Funktion des Motorsteuergeräts temporär auch während der Stillstandsphase der Brennkraftmaschine aufrecht erhalten werden muss.According to a first embodiment, an input of the solenoid valve is connected to the pressure range and an output to the ejector. In particular, the solenoid valve is de-energized closed during a standstill phase of the internal combustion engine and otherwise open, for example, during normal operation under load and energized during the coasting operation. In the case of, for example, a temperature-induced increase in pressure during the standstill phase, the solenoid valve is opened by signals from the engine control unit in order to keep the pressure in the pressure line constant. The electronic control of the solenoid valve, in particular, the holding pressure during coasting and engine downtime can be set arbitrarily. However, this also means that the function of the engine control unit must be temporarily maintained even during the stoppage phase of the internal combustion engine.

Hierauf kann bei einer zweiten Ausführungsform verzichtet werden, bei welcher das Magnetventil durch ein 2/3 Wegeventil gebildet wird, von welchem ein Eingang mit der Druckleitung, ein erster Ausgang mit der Saugstrahlpumpe und ein zweiter Ausgang mit einem Druckbegrenzungsventil verbunden ist. Dieses 2/3 Wegeventil wird vom Motorsteuergerät derart angesteuert ist, dass es in stromlosem Zustand den Eingang mit dem zweiten Ausgang und in bestromtem Zustand den Eingang mit dem ersten Ausgang verbindet. Folglich schaltet bei Stillstand der Brennkraftmaschine und stromlos deaktiviertem Motorsteuergerät das 2/3 Wegeventil automatisch, beispielsweise durch Federvorspannung, in seine stromlose Stellung, in welcher die Druckleitung mit dem Druckbegrenzungsventil verbunden ist, über welches dann Überdruck abgebaut wird. Im normalen Lastbetrieb oder im Schiebebetrieb der Brennkraftmaschine wird das 2/3 Wegeventil hingegen vom Motorsteuergerät bestromt, so dass die Saugstrahlpumpe an die Druckleitung angeschlossen ist.This can be omitted in a second embodiment, in which the solenoid valve is formed by a 2/3 way valve, of which an input to the pressure line, a first output to the suction jet pump and a second output is connected to a pressure relief valve. This 2/3 way valve is controlled by the engine control unit such that it connects the input to the second output in the de-energized state and the input to the first output when energized. Consequently, at standstill of the engine and de-energized deactivated engine control unit, the 2/3 way valve automatically, for example, by spring preload, in its de-energized position, in which the pressure line is connected to the pressure relief valve, via which then pressure is reduced. In normal load operation or coasting of the internal combustion engine, however, the 2/3 way valve is energized by the engine control unit, so that the suction jet pump is connected to the pressure line.

Gemäß einer weiteren Ausführungsform der Erfindung erfolgt die Ansteuerung des Magnetventils in Abhängigkeit von einem Füllgrad des den zweiten Bereich des Kraftstoffreservoirs bildenden Kraftstoffbehälters mit Kraftstoff. Innerhalb des Kraftstoffbehälters ist dann der den ersten Bereich des Kraftstoffreservoirs bildende, die Kraftstoffpumpe aufnehmende Topf als Reservoir für den Reservekraftstoff angeordnet. Falls man das Magnetventil schließt, wenn der Füllpegel des Kraftstoffbehälters in einem Bereich zwischen maximaler Füllung und einem Pegelstand liegt, welcher im wesentlichen mit einem oberen Rand des Topfes fluchtet, wird der Kraftstoff nicht mehr über die durch das geschlossene Magnetventil außer Betrieb gesetzte Saugstrahlpumpe vom Kraftstoffbehälter in den Topf gefördert. Vielmehr fließt dann der Kraftstoff zum Pegelausgleich aus dem Kraftstoffbehälter über den Rand des Topfes in diesen hinein. Bei ausreichendem Füllgrad des Kraftstoffbehälters kann die Saugstrahlpumpe folglich außer Betrieb gesetzt werden, was in einer merklichen Reduzierung der von der Kraftstoffpumpe geforderten Pumpleistung, in einer Erhöhung des Systemwirkungsgrades, in einer geringeren Bordnetzbelastung, in einer geringeren Tankaufheizung sowie in einer längeren Lebensdauer der Kraftstoffpumpe resultiert.According to a further embodiment of the invention, the control of the solenoid valve takes place as a function of a degree of filling of the second region the fuel reservoir forming fuel tank with fuel. Within the fuel tank, the pot forming the first region of the fuel reservoir and receiving the fuel pump is then arranged as a reservoir for the reserve fuel. If the solenoid valve is closed when the fill level of the fuel tank is in a range between maximum charge and a level substantially flush with an upper rim of the pot, the fuel will no longer travel past the fuel injector via the closed solenoid valve promoted in the pot. Rather, the fuel then flows to compensate for levels from the fuel tank over the edge of the pot in this. With sufficient filling level of the fuel tank, the ejector can therefore be put out of operation, resulting in a significant reduction in the required by the fuel pump power, in an increase in system efficiency, in a lower electrical system load, in a lower tank heating and in a longer life of the fuel pump.

Eine weitere Ausführungsform sieht vor, dass das Magnetventil durch ein Schaltventil gebildet wird, welches zur Regelung des Treibdrucks der Saugstrahlpumpe getaktet angesteuert ist. Gemäß einer Alternative hierzu kann das Magnetventil auch ein Proportionalventil sein, das zur Regelung des Treibdrucks der Saugstrahlpumpe angesteuert ist. In beiden Fällen kann die Saugstrahlpumpe stets in einem Bereich höchsten Wirkungsgrades betrieben werden.A further embodiment provides that the solenoid valve is formed by a switching valve, which is controlled clocked to control the driving pressure of the suction jet pump. According to an alternative to this, the solenoid valve may also be a proportional valve, which is controlled to control the driving pressure of the suction jet pump. In both cases, the suction jet pump can always be operated in a region of highest efficiency.

Folglich dient das Magnetventil im Sinne einer Mehrfachfunktion nicht nur für eine besonders vorteilhafte Regelung des Systemdrucks und der Kraftstoffmenge während des Schiebebetriebs und bei Stillstand sondern auch für weitere energiesparende Maßnahmen.Consequently, the solenoid valve in the sense of a multiple function not only for a particularly advantageous control of the system pressure and the amount of fuel during coasting and at a standstill but also for further energy-saving measures.

Weitere vorteilhafte Ausgestaltungen und Weiterbildungen der Erfindung sind in den restlichen Unteransprüchen beschrieben.Further advantageous embodiments and modifications of the invention are described in the remaining subclaims.

Zeichnungendrawings

Ausführungsbeispiele der Erfindung sind in der Zeichnung dargestellt und in der nachfolgenden Beschreibung näher erläutert. In der Zeichnung zeigt

Fig.1
eine schematische Darstellung einer bevorzugten Ausführungsform eines erfindungsgemäßen Kraftstoffversorgungssystems;
Fig.2
eine schematische Darstellung einer weiteren Ausführungsform eines erfindungsgemäßen Kraftstoffversorgungssystems.
Embodiments of the invention are illustrated in the drawings and explained in more detail in the following description. In the drawing shows
Fig.1
a schematic representation of a preferred embodiment of a fuel supply system according to the invention;
Fig.2
a schematic representation of another embodiment of a fuel supply system according to the invention.

Beschreibung der AusführungsbeispieleDescription of the embodiments

Das in Fig.1 insgesamt mit 1 bezeichnete rücklauffreie Kraftstoffversorgungssystem dient beispielsweise zur Kraftstoffversorgung einer Brennkraftmaschine eines Fahrzeugs und beinhaltet als wesentliche Bauelemente eine innerhalb eines Dralltopfes 2 eines Kraftstoffbehälters 4 gehaltene Tankeinbaueinheit 6 umfassend eine Kraftstoffpumpe 8 mit einem vorlaufseitigen Saugfilter 10, ein bezogen auf die Kraftstoffpumpe 8 in einer druckseitigen Druckleitung 12 angeordnetes Rückschlagventil 14 sowie einen mit Einspritzventilen 16 in Strömungsverbindung stehenden Kraftstoffzuteiler 18 oder eine Benzin- oder Dieselhochdruckpumpe. In einem Bereich zwischen dem Rückschlagventil 14 und dem Kraftstoffzuteiler 18 misst ein Drucksensor 20 den Ist-Druck in der Druckleitung 12 und sendet über eine Signalleitung 22 ein entsprechendes Signal an ein Steuergerät, welches vorzugsweise durch ein zentrales Motorsteuergerät 24 (MOTRONIC) gebildet wird und in welchem abhängig von einer Regeldifferenz zwischen dem Ist-Druck und einem bedarfsorientierten Soll-Druck über eine elektrische Leitung 26 ein Steuersignal an ein elektronisches, mit der Kraftstoffpumpe 8 über elektrische Leitungen 28 verbundenes Kraftstoffpumpensteuergerät 30 ausgesteuert wird, um den Druck in der Druckleitung 12 über die Kraftstoffpumpe 8 bedarfsabhängig nachzuregeln.The generally designated 1 in Fig.1 return-free fuel supply system is used for example for fueling an internal combustion engine of a vehicle and includes as essential components held within a swirl pot 2 of a fuel tank 4 tank installation unit 6 comprising a fuel pump 8 with a suction side filter 10, based on the fuel pump 8 disposed in a pressure-side pressure line 12 check valve 14 and a fuel injector 16 in fluid communication with fuel injectors 18 or a gasoline or diesel high-pressure pump. In a region between the check valve 14 and the fuel meter 18, a pressure sensor 20 measures the actual pressure in the pressure line 12 and sends via a signal line 22 a corresponding signal to a control unit, which is preferably formed by a central engine control unit 24 (MOTRONIC) and in which is controlled as a function of a control difference between the actual pressure and a demand-based desired pressure via an electrical line 26, a control signal to an electronic, connected to the fuel pump 8 via electrical lines 28 fuel pump controller 30 to the pressure in the pressure line 12 via the Regulate fuel pump 8 demand-dependent.

Von einem bezogen auf das Rückschlagventil 14 stromabwärtigen Abschnitt der Druckleitung 12 zweigt an einer Verzweigungstelle 32 eine Saugstrahlpumpenleitung 34 ab, welche sich beispielsweise in mehrere, vorzugsweise in zwei Einzelleitungen 36 verzweigend in jedem Zweig 36 eine von Kraftstoff durchflossene Saugpumpe 38 beinhaltet, wobei die Einzelleitungen 36 in den Dralltopf 2 münden. Der Dralltopf 2 dient zum einen als Kraftstoffreservoir, zum andern verhindert er, dass bei starker Seitenbeschleunigung die Kraftstoffpumpe 8 kurzzeitig keinen Kraftstoff mehr ansaugen kann, weil dieser fliehkraftbedingt in einem von der Saugseite entfernten Abschnitt des Kraftstoffbehälters 4 konzentriert ist. In dem von Kraftstoff durchströmten Zustand saugen die Saugstrahlpumpen 38 Kraftstoff aus dem außerhalb des Dralltopfes gelegenen Bereich des Kraftstoffbehälters 4 in die beiden Einzelleitungen 36 hinein und sorgen in bekannter Weise für einen konstanten Kraftstoffpegel innerhalb des Dralltopfes 2.From a reference to the check valve 14 downstream portion of the pressure line 12 branches off at a branch point 32 from a Saugstrahlpumpenleitung 34, which branches, for example in several, preferably in two individual lines 36 branching in each branch 36 a fuel-carrying suction pump 38, wherein the individual lines 36 open into the swirl pot 2. The swirl pot 2 serves on the one hand as a fuel reservoir, on the other hand it prevents that with strong lateral acceleration the fuel pump 8 can no longer suck fuel for a short time, because this centrifugal force is concentrated in a remote from the suction side portion of the fuel tank 4. In the state through which fuel flows, the suction jet pumps 38 suck fuel from the area of the fuel tank 4 located outside the swirl pot into the two individual lines 36 and ensure a constant fuel level within the swirl pot 2 in a known manner.

In der von der Druckleitung 12 abzweigenden Saugstrahlpumpenleitung 34 ist ein elektrisch betätigbares Magnetventil 40 angeordnet, welches von dem zentralen Motorsteuergerät 24 über eine Steuerleitung 42 vorzugsweise in Abhängigkeit des gemessenen Drucks in der Druckleitung 12, der Temperatur des Kraftstoffs, dem Füllstand und/oder den Motorbetriebsbedingungen angesteuert ist. Das Magnetventil 40 ist ausgebildet, um den Querschnitt der Saugstrahlpumpenleitung 34 zu öffnen oder zu schliessen. Das Magnetventil 40 ist vorzugsweise unbestromt geschlossen und bestromt geöffnet.Arranged in the suction jet pump line 34 branching off from the pressure line 12 is an electrically actuated solenoid valve 40, which is controlled by the central engine control unit 24 via a control line 42, preferably as a function of the measured pressure in the pressure line 12, the temperature of the fuel, the level and / or the engine operating conditions is controlled. The solenoid valve 40 is designed to open or close the cross section of the suction jet pump line 34. The solenoid valve 40 is preferably closed and energized closed open.

Vor diesem Hintergrund ist die Funktionsweise des Kraftstoffversorgungssystems 1 wie folgt: Bei Lastbetrieb der Brennkraftmaschine saugt die Kraftstoffpumpe 8 Kraftstoff aus dem Dralltopf 2, wobei der Kraftstoffstrom unter Wirkung des Kraftstoffdrucks das Rückschlagventil 14 öffnet und ein Teil des Kraftstoffstroms an der Verzweigungsstelle 32 in die Saugstrahlpumpenleitung 34 fließt. Im Lastbetrieb bestromt das Motorsteuergerät 24 das Magnetventil 40, woraufhin dieses in Öffnungsstellung geschaltet ist, damit die Saugstrahlpumpen 38 Kraftstoff aus dem außerhalb des Dralltopfes 2 gelegenen Bereich des Kraftstoffbehälters 4 in den Dralltopf 2 hinein saugen können. Der andere Teil des Kraftstoffstromes wird entlang der Druckleitung 12 dem Kraftstoffzuteiler 18 bedarfsabhängig zugeführt, um über die Einspritzventile 16 in Brennräume der Brennkraftmaschine eingespritzt zu werden.Against this background, the operation of the fuel supply system 1 is as follows: In load operation of the internal combustion engine, the fuel pump sucks 8 fuel from the swirl pot 2, wherein the fuel flow opens the check valve 14 under the effect of fuel pressure and a portion of the fuel flow at the branch point 32 in the Saugstrahlpumpenleitung 34th flows. In load operation, the engine control unit 24 energizes the solenoid valve 40, whereupon this is switched to the open position, so that the suction jet pumps 38 fuel the region of the fuel tank 4 located outside of the swirl pot 2 can suck into the swirl pot 2. The other part of the fuel flow is fed to the fuel meter 18 as required depending along the pressure line 12 in order to be injected via the injection valves 16 into combustion chambers of the internal combustion engine.

Im Schiebebetrieb sind die Einspritzventile 16 geschlossen, so dass der Kraftstoffstrom in der Druckleitung 12 gleich Null ist, gleichwohl wird die Saugstrahlpumpenleitung 34 durch das weiterhin bestromte und dadurch geöffnet gehaltene Magnetventil 40 durchströmt und folglich Kraftstoff in den Dralltopf 2 gefördert.In the coasting mode, the injection valves 16 are closed, so that the fuel flow in the pressure line 12 is equal to zero, however, the Saugstrahlpumpenleitung 34 is flowed through the still energized and thereby kept open solenoid valve 40 and thus promoted fuel into the swirl pot 2.

Während einer Stillstandsphase der Brennkraftmaschine hingegen schaltet das Motorsteuergerät 24 das Magnetventil 40 stromlos, woraufhin dieses schließt. Folglich ist der stromabwärts des Rückschlagventils 14 angeordnete Abschnitt der Druckleitung 12 und der stromaufwärts des Magnetventils 40 angeordnete Abschnitt der Saugstrahlpumpenleitung 34 durch die geschlossenen Einspritzventile 16, das geschlossene Magnetventil 40 sowie durch das zur Kraftstoffpumpe 8 hin geschlossene Rückschlagventil 14 gegen die Umgebung abgedichtet, wobei der Druck der in diesen Abschnitten vorhandenen Kraftstoffmenge konstant gehalten werden soll. Ternperaturbedingt kann jedoch der Haltedruck zu hoch sein, was durch den Drucksensor 20 detektiert und an das zentrale Motorsteuergerät 24 gemeldet wird. Dann wird das Magnetventil 40 vom Motorsteuergerät 24 durch einen Stromimpuls kurzzeitig in Öffnungsstellung geschaltet, um den vorgegebenen Haltedruck zu reduzieren.During a standstill phase of the internal combustion engine, however, the engine control unit 24 switches the solenoid valve 40 de-energized, whereupon it closes. Consequently, the arranged downstream of the check valve 14 portion of the pressure line 12 and the upstream of the solenoid valve 40 disposed portion of the Saugstrahlpumpenleitung 34 is sealed by the closed injectors 16, the closed solenoid valve 40 and by the closed fuel pump 8 towards the check valve 14 against the environment, the Pressure of existing in these sections amount of fuel to be kept constant. Ternperaturbedingt however, the holding pressure may be too high, which is detected by the pressure sensor 20 and reported to the central engine control unit 24. Then, the solenoid valve 40 is briefly switched by the engine control unit 24 by a current pulse in the open position to reduce the predetermined holding pressure.

Bei dem zweiten Ausführungsbeispiel der Erfindung nach Fig.2 sind die gegenüber dem vorhergehenden Beispiel gleichbleibenden und gleichwirkenden Teile durch die gleichen Bezugszeichen gekennzeichnet. Als Magnetventil wird hier ein 2/3 Wegeventil 44 verwendet, von welchem ein Eingang 46 mit der Druckleitung 12, ein erster Ausgang 48 mit den Saugstrahlpumpen 38 und ein zweiter Ausgang 50 mit einem Druckbegrenzungsventil 52 verbunden ist. Das 2/3 Wegeventil 44 wird vom zentralen Motorsteuergerät 24 derart angesteuert, dass es in stromlosem Zustand den Eingang 46 mit dem zweiten Ausgang 50 und in bestromtem Zustand den Eingang 46 mit dem ersten Ausgang 48 verbindet. Vorzugsweise wird das 2/3-Wegeventil 44 während einer Stillstandsphase der Brennkraftmaschine stromlos geschaltet und ansonsten, d.h. im Lastbetrieb und im Schiebebetrieb bestromt. Folglich schaltet bei Stillstand der Brennkraftmaschine und stromlos deaktiviertem Motorsteuergerät 24 das 2/3-Wegeventil 44 automatisch, beispielsweise durch Federvorspannung, in seine stromlose Stellung, in welcher die Druckleitung 12 mit dem Druckbegrenzungsventil 52 verbunden ist, über welches dann Überdruck abgebaut werden kann. Im normalen Lastbetrieb oder im Schiebebetrieb der Brennkraftmaschine wird das 2/3 Wegeventil 44 hingegen vom Motorsteuergerät 24 bestromt, so dass die Saugstrahlpumpen 38 an die Druckleitung 12 angeschlossen sind.In the case of the second embodiment of the invention according to FIG. 2, the parts which are the same and function the same as in the preceding example are identified by the same reference numerals. As a solenoid valve here a 2/3 way valve 44 is used, of which an input 46 to the pressure line 12, a first output 48 to the suction jet 38 and a second output 50 is connected to a pressure relief valve 52. The 2/3 way valve 44 is controlled by the central engine control unit 24 such that it connects the input 46 to the second output 50 in the de-energized state and the input 46 to the first output 48 when energized. Preferably, the 2/3-way valve 44 is de-energized during a standstill phase of the internal combustion engine and otherwise energized, ie in load operation and in overrun operation. Consequently, at standstill of the engine and de-energized deactivated engine control unit 24, the 2/3-way valve 44 automatically, for example by spring preload, in its de-energized position, in which the pressure line 12 is connected to the pressure relief valve 52, via which then pressure can be reduced. In normal load operation or in coasting of the internal combustion engine, however, the 2/3 way valve 44 is energized by the engine control unit 24, so that the suction jet pumps 38 are connected to the pressure line 12.

Gemäß einer Fortbildung der ersten Ausführungsform von Fig.1 erfolgt die Ansteuerung des Magnetventils 40 in Abhängigkeit von einem Füllgrad des Kraftstoffbehälters 4 mit Kraftstoff. Falls man das Magnetventil 40 schließt, wenn der Füllpegel des Kraftstoffbehälters 4 in einem Bereich zwischen maximaler Füllung und einem Pegelstand liegt, welcher im wesentlichen mit einem oberen Rand 54 des Dralltopfes 2 fluchtet, wird der Kraftstoff nicht mehr über die durch das geschlossene Magnetventil 40 außer Betrieb gesetzte Saugstrahlpumpen 38 vom Kraftstoffbehälter 4 in den Dralltopf 2 gefördert. Vielmehr fließt dann der Kraftstoff zum Pegelausgleich aus dem Kraftstoffbehälter 4 über den Rand 54 des Dralltopfes 2 in diesen hinein. Bei ausreichendem Füllgrad des Kraftstoffbehälters 4 können die Saugstrahlpumpen 38 folglich außer Betrieb gesetzt werden. Weiter ist es möglich, den Abstelldruck in Abhängigkeit von der Temperatur und/oder von den Motorbetriebsbedingungen zu variieren.According to a development of the first embodiment of Figure 1, the control of the solenoid valve 40 takes place in dependence on a degree of filling of the fuel tank 4 with fuel. If the solenoid valve 40 is closed, when the filling level of the fuel tank 4 is in a range between maximum filling and a level that is substantially flush with an upper edge 54 of the swirl pot 2, the fuel is no longer beyond that through the closed solenoid valve 40 except Operation set Saugstrahlpumpen 38 from the fuel tank 4 in the swirl pot 2 promoted. Rather, the fuel then flows to level compensation from the fuel tank 4 via the edge 54 of the swirl pot 2 in this. With sufficient degree of filling of the fuel tank 4, the suction jet pumps 38 can thus be put out of operation. Further, it is possible to vary the shutdown pressure as a function of the temperature and / or of the engine operating conditions.

Die Außerbetriebnahme der Saugstrahlpumpen 38 sowie die Variation des Abstelldrucks kann auch durch das 3/2-Wegeventil 44 gemäß der zweiten Ausführungsform von Fig.2 erfolgen, falls es bei dem oben beschriebenen, ausreichenden Pegelstand im Kraftstoffbehälter 4 derart geschaltet wird, dass der Eingang 46 mit dem zweiten Ausgang 50 verbunden ist, welcher in das Druckbegrenzungsventil 52 mündet. Dann wird der stromabwärts des 2/3-Wegeventils 44 gelegene Teil der Saugstrahlpumpenleitung 34 bis zu einem vorbestimmten Druckniveau gesperrt, so dass die Saugstrahlpumpen 38 nicht mehr mit Kraftstoff versorgt sind.The decommissioning of the Saugstrahlpumpen 38 and the variation of the Abstelldrucks can also by the 3/2-way valve 44 according to the second embodiment 2, if it is switched in the above-described, sufficient water level in the fuel tank 4 such that the input 46 is connected to the second output 50, which opens into the pressure relief valve 52. Then, the part of the suction jet pump line 34 located downstream of the 2/3-way valve 44 is shut off to a predetermined pressure level, so that the suction jet pumps 38 are no longer supplied with fuel.

Da die Magnetventile 40, 44 gemäß der Ausführungsformen von Fig.1 und Fig.2 vorzugsweise Schaltventile sind, können sie zur Regelung des Treibdrucks der Saugstrahlpumpen 38 getaktet angesteuert werden. Gemäß einer Alternative hierzu kann das Magnetventil 40, 44 auch ein Proportionalventil sein, das zur Regelung des Treibdrucks der Saugstrahlpumpe angesteuert ist. Durch eine Regelung des Treibdrucks können die Saugstrahlpumpe 38 dann stets in einem Bereich höchsten Wirkungsgrades betrieben werden.Since the solenoid valves 40, 44 according to the embodiments of Figure 1 and Figure 2 are preferably switching valves, they can be controlled clocked to control the motive pressure of the ejector 38. According to an alternative to this, the solenoid valve 40, 44 may also be a proportional valve, which is controlled to control the driving pressure of the suction jet pump. By controlling the driving pressure, the suction jet pump 38 can then always be operated in a region of highest efficiency.

Claims (16)

  1. Non-return fuel supply system (1) for an internal combustion engine, with
    - at least one fuel pump (8) by means of which fuel can be conveyed out of a first region (2) of a fuel reservoir into a pressure region (12) connected to a fuel distributor (18),
    - at least one suction-jet pump (38), through which flows fuel conveyed through a suction-jet pump line (34) by means of the fuel pump (8) and by means of which fuel can be conveyed out of a second region (4) of the fuel reservoir into the first region (2),
    - at least one means (20, 24, 30) regulating and/or controlling the pressure in the pressure region (12),
    - at least one non-return valve (14), by means of which at least part of the pressure region (12) can be shut off with respect to the fuel pump (8),
    characterized in that the means (20, 24, 30) regulating and/or controlling the pressure in the pressure region (12) contain at least one electrically actuable solenoid valve (40; 44) which is arranged downstream of the non-return valve (14) in a suction-jet pump line (34).
  2. Non-return fuel supply system according to Claim 1, characterized in that the solenoid valve (40; 44) is arranged between the non-return valve (14) and the suction-jet pump (38).
  3. Non-return fuel supply system according to Claim 1 or 2, characterized in that the solenoid valve (40; 44) is activated by an electronic engine control apparatus (24).
  4. Non-return fuel supply system according to Claim 3, characterized in that the activation of the solenoid valve (40; 44) takes place as a function of the pressure measured by a pressure sensor (20) arranged in the pressure region (12).
  5. Non-return fuel supply system according to one of the preceding claims, characterized in that an inlet of the solenoid valve (40) is connected to the pressure region (12) and an outlet is connected to the suction-jet pump (38).
  6. Non-return fuel supply system according to Claim 5, characterized in that the solenoid valve (40) is closed, dead, during a standstill phase of the internal combustion engine and is open, live, otherwise.
  7. Non-return fuel supply system according to one of Claims 1 to 4, characterized in that the solenoid valve is formed by a 2/3-way valve (44), of which an inlet (46) is connected to the pressure region (12), a first outlet (48) is connected to the suction-jet pump (38) and a second outlet (50) is connected to a pressure-limiting valve (52).
  8. Non-return fuel supply system according to Claim 7, characterized in that the 2/3-way valve (44) is activated in such a way that, in the dead state, it connects the inlet (46) to the second outlet (50) and, in the live state, it connects the inlet (46) to the first outlet (48).
  9. Non-return fuel supply system according to Claim 8, characterized in that the 2/3-way valve (44) is dead during a standstill phase of the internal combustion engine and is live otherwise.
  10. Non-return fuel supply system according to one of the preceding claims, characterized in that the pressure region connected to the fuel distributor (18) is formed by a pressure line (12) which connects the fuel pump (8) to injection valves (16).
  11. Non-return fuel supply system according to Claim 10, characterized in that the suction-jet pump line (34) branches off, downstream of the non-return valve (14), from the pressure line (12).
  12. Non-return fuel supply system according to one of Claims 1 to 3, characterized in that the activation of the solenoid valve (40; 44) takes place as a function of a degree of filling of the second region (4) of the fuel reservoir with fuel.
  13. Non-return fuel supply system according to Claim 12, characterized in that the first region of the fuel reservoir is formed by a pot (2) which receives the fuel pump (8) and which is arranged within the second region (4) of the fuel reservoir.
  14. Non-return fuel supply system according to Claim 13, characterized in that the solenoid valve (40; 44) is closed when the filling level of the second region (4) of the fuel reservoir lies in a range between maximum filling and a level which is aligned essentially with an upper edge of the pot, and in that it is open otherwise.
  15. Non-return fuel supply system according to one of the preceding claims, characterized in that the solenoid valve (40; 44) is formed by a switching valve which is activated, clocked, in order to regulate the propulsive pressure of the suction-jet pump (38).
  16. Non-return fuel supply system according to one of Claims 1 to 3, characterized in that the solenoid valve is formed by a proportional valve (40; 44) which is activated in order to regulate propulsive pressure of the suction-jet pump (38).
EP03799428A 2002-12-07 2003-07-11 Non-return fuel supply system Expired - Lifetime EP1576272B1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
DE10257280 2002-12-07
DE10257280 2002-12-07
DE10327562 2003-06-18
DE10327562A DE10327562A1 (en) 2002-12-07 2003-06-18 Non-return fuel supply system for internal combustion engine has pressure pump supplying fuel to injectors from first region of tank and suction jet pumps supplying fuel from second region
PCT/DE2003/002336 WO2004053318A1 (en) 2002-12-07 2003-07-11 Non-return fuel supply system

Publications (2)

Publication Number Publication Date
EP1576272A1 EP1576272A1 (en) 2005-09-21
EP1576272B1 true EP1576272B1 (en) 2006-12-13

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Application Number Title Priority Date Filing Date
EP03799428A Expired - Lifetime EP1576272B1 (en) 2002-12-07 2003-07-11 Non-return fuel supply system

Country Status (5)

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US (1) US7275524B2 (en)
EP (1) EP1576272B1 (en)
BR (1) BR0307288A (en)
DE (1) DE50305995D1 (en)
WO (1) WO2004053318A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10319660B4 (en) * 2003-05-02 2018-04-19 Robert Bosch Gmbh Device for conveying fuel from a reservoir to an internal combustion engine
DE102004049286A1 (en) * 2004-10-09 2006-04-20 Robert Bosch Gmbh Device for conveying fuel
WO2007115102A2 (en) * 2006-03-29 2007-10-11 Robert Bosch Gmbh Fuel system with pressure regulation and pressure relief
EP1911962A1 (en) * 2006-09-29 2008-04-16 Inergy Automotive Systems Research (SA) Single piece dual jet pump and fuel system using it
DE102007039892A1 (en) * 2007-08-23 2009-02-26 Continental Automotive Gmbh Injection system for an internal combustion engine
DE102010062121A1 (en) * 2010-11-29 2012-05-31 Robert Bosch Gmbh Device for supplying fuel from fuel tank to combustion engine, comprises suction jet pump, entrainment pipe, which is supplying fluid to suction jet pump, and pressure control valve, which is provided in entrainment pipe
US9097217B2 (en) * 2011-08-31 2015-08-04 Gm Global Technology Operations. Llc Propulsion systems and modules for vehicles
US20140338752A1 (en) * 2013-05-14 2014-11-20 Delphi Technologies, Inc. Fuel supply system and method for operating
DE102013212267A1 (en) * 2013-06-26 2014-12-31 Robert Bosch Gmbh Fuel delivery system with partial pressure relief valve to drive line of a suction jet pump
US10451013B2 (en) * 2015-08-20 2019-10-22 Ford Global Technologies, Llc Method for operating a dual lift pump system

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4926829A (en) * 1988-11-28 1990-05-22 Walbro Corporation Pressure-responsive fuel delivery system
DE4123367A1 (en) 1991-07-15 1993-01-21 Magenwirth Gmbh Co Gustav Vehicle fuel tank with reserve section near pump - has return fuel flow driving venturi pump to top up reserve section
DE4224981C2 (en) * 1992-07-29 2003-06-26 Bosch Gmbh Robert Device for delivering fuel from a storage tank to the internal combustion engine of a motor vehicle
DE4242242C2 (en) * 1992-12-15 2003-04-30 Bosch Gmbh Robert Device for supplying the internal combustion engine of a motor vehicle with fuel present in a storage tank
US5732684A (en) * 1994-09-22 1998-03-31 Ford Global Technologies, Inc. Automotive fuel delivery system with pressure actuated auxiliary fuel pump
DE19540892A1 (en) * 1995-11-02 1997-05-07 Bayerische Motoren Werke Ag Fuel system
DE19628580A1 (en) * 1996-07-16 1998-01-22 Mannesmann Vdo Ag Flow valve
US6024064A (en) * 1996-08-09 2000-02-15 Denso Corporation High pressure fuel injection system for internal combustion engine
DE19913477B4 (en) * 1999-03-25 2004-08-26 Robert Bosch Gmbh Method for operating a fuel supply device of an internal combustion engine, in particular a motor vehicle
DE19950289A1 (en) * 1999-10-19 2001-04-26 Bosch Gmbh Robert Fuel supply unit for IC engine of motor vehicle with feed container in storage tank of vehicle from which delivery set sucks fuel and delivers this to engine and with return line
DE19951132A1 (en) 1999-10-23 2001-05-10 Bosch Gmbh Robert Method of releasing fuel pressure in a non-return fuel supply system
DE29922474U1 (en) * 1999-12-22 2001-05-03 Robert Bosch Gmbh, 70469 Stuttgart Fuel supply device for an internal combustion engine of a motor vehicle
DE10006622A1 (en) * 2000-02-15 2001-08-16 Bosch Gmbh Robert Device for supplying a motor vehicle's internal combustion engine with fuel has a feeder unit driven by an electric motor to feed fuel from a reservoir to an internal combustion engine, also pressure-limiting and reverse flow valves.
US6622707B2 (en) * 2000-06-28 2003-09-23 Delphi Technologies, Inc. Electronic returnless fuel system
US6532941B2 (en) * 2000-08-29 2003-03-18 Delphi Technologies, Inc. Electronic returnless fuel system
IT1320684B1 (en) * 2000-10-03 2003-12-10 Fiat Ricerche FLOW RATE CONTROL DEVICE OF A HIGH PRESSURE PUMP IN A COMMON COLLECTOR INJECTION SYSTEM OF A FUEL
DE10058674A1 (en) 2000-11-25 2002-06-06 Bosch Gmbh Robert Method, computer program and control and / or regulating device for operating an internal combustion engine
US6718948B2 (en) * 2002-04-01 2004-04-13 Visteon Global Technologies, Inc. Fuel delivery module for petrol direct injection applications including supply line pressure regulator and return line shut-off valve

Also Published As

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WO2004053318A1 (en) 2004-06-24
BR0307288A (en) 2004-12-28
EP1576272A1 (en) 2005-09-21
DE50305995D1 (en) 2007-01-25
US20050175488A1 (en) 2005-08-11
US7275524B2 (en) 2007-10-02

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