EP0694691B1 - Dispositif d'alimentation de combustible d'un réservoir vers un moteur à combustion interne d'un véhicle automobile - Google Patents

Dispositif d'alimentation de combustible d'un réservoir vers un moteur à combustion interne d'un véhicle automobile Download PDF

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Publication number
EP0694691B1
EP0694691B1 EP95110247A EP95110247A EP0694691B1 EP 0694691 B1 EP0694691 B1 EP 0694691B1 EP 95110247 A EP95110247 A EP 95110247A EP 95110247 A EP95110247 A EP 95110247A EP 0694691 B1 EP0694691 B1 EP 0694691B1
Authority
EP
European Patent Office
Prior art keywords
opening
fuel
jet nozzle
storage container
fuel 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.)
Expired - Lifetime
Application number
EP95110247A
Other languages
German (de)
English (en)
Other versions
EP0694691A1 (fr
Inventor
Stephan Dipl.-Ing. Kleppner
Kurt Dipl.-Ing. Frank (Ba)
Ansgar Dipl.-Ing. Seitz
Hannelore Scheerer
Günter-Paul Ballier
Rolf Dipl.-Ing. Fischerkeller
Wolfgang Wuerl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP0694691A1 publication Critical patent/EP0694691A1/fr
Application granted granted Critical
Publication of EP0694691B1 publication Critical patent/EP0694691B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • 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
    • 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

Definitions

  • the invention relates to a device for conveying fuel from a storage container to the internal combustion engine of a motor vehicle according to the preamble of claim 1.
  • Such a device is known from DE-A-37 32 415.
  • This device has a fuel delivery unit which draws in from a partial area of the storage container and which is connected on the pressure side to the internal combustion engine.
  • a return line leads from the internal combustion engine back to the storage container and to this is connected a jet pump arranged in the storage container, through which fuel is conveyed into the partial area of the storage container.
  • An overflow valve is assigned to the jet pump, through which, when a certain pressure in the jet pump is exceeded, this fuel can flow out into the partial area of the storage container as a relief space.
  • the jet pump has a jet nozzle which has an additional overflow opening in the area between its inlet opening assigned to the return line and its outlet opening, the connection of which to the relief chamber to form the overflow valve can be controlled by a spring-loaded closing element.
  • the overflow valve is completely pre-assembled as a unit and consists of an insert, a closing element guided in the insert and a spring element clamped between the latter and the closing element in the form of a helical compression spring.
  • the jet pump has a receptacle into which the pre-assembled overflow valve can be inserted. This known embodiment requires a special design of the jet nozzle for receiving the overflow valve and the pre-assembly of the overflow valve and therefore requires a lot of parts and assembly.
  • the inventive design of the device with the features of claim 1, on the other hand, enables simple design and assembly of the jet pump and the overflow valve, for which only a few additional components are required.
  • FIG. 1 shows a device for conveying fuel from a storage container to the internal combustion engine of a motor vehicle in a simplified representation
  • FIG. 2 shows a jet pump with a storage container of the device from FIG. 1 according to a first exemplary embodiment
  • FIG. 3 shows a partial view in arrow direction III in FIG. 2
  • FIG. 4 the jet pump with storage container according to a second exemplary embodiment
  • FIG. 5 a partial view in arrow direction V in FIG. 4.
  • FIG. 1 a device is shown in simplified form in principle, which is used to convey fuel from a storage container 10 to the internal combustion engine 12 of a motor vehicle.
  • a storage container 14 is arranged in the storage container 10, from which a fuel delivery unit 16 sucks, which is arranged in the storage container 14.
  • a pressure line 20, which leads to the internal combustion engine 12, is connected to a pressure connection 18 of the fuel delivery unit 16.
  • a return line 22 also leads from the internal combustion engine 12 back to the storage container 10, through which excess fuel not used by the internal combustion engine 12 flows back into the storage container 12.
  • a jet pump 24, which is arranged within the storage container 10 and through which fuel is conveyed into the storage container 14, is connected to the return line 22.
  • the fuel delivery unit 16 delivers fuel from the storage container 14 to the internal combustion engine 12 and the fuel flowing back through the return line 22 drives the jet pump 24.
  • the storage container 10 and the storage container 14 are only shown in sections, the fuel delivery unit (not shown) being arranged in the storage container 14, and an overflow valve 25 assigned to the jet pump 24 according to a first exemplary embodiment.
  • the preferably made of plastic storage container 14 is arranged near the bottom 11 of the storage container 10 and fastened in the storage container 10 in a manner not shown.
  • a side wall 26 of the stowage container 14 there is an opening 30 close above the bottom 28 thereof, through which the interior of the stowage container 14 with the Storage container 10 is connected.
  • a hollow, approximately cylindrical receptacle 32 is formed in one piece on the storage container 14, which is arranged approximately coaxially with the opening 30 and is circular in cross section, but can also be designed in any other way, for example rectangular.
  • the cross section of the receptacle 32 is larger than that of the opening 30.
  • the storage container 14 has a wall part 34 which extends approximately horizontally above the opening 30.
  • a channel 36 open to the outside into the storage container 10 is formed.
  • a connector 38 protrudes from the wall part 34 into the interior of the storage container 14 and opens into the receptacle 32.
  • the socket 38 is provided with a seat 40 with which a closing member 42, for example in the form of a ball, interacts.
  • the seat 40 is designed to widen conically to the inside of the storage container 14.
  • a guide for the closing member 42 is formed on the seat 40 into the interior of the storage container 14, which is formed by a plurality of webs 43, shown in FIG. 3 and spaced apart from one another over the circumference of the connecting piece 38.
  • the closing member 42 is guided between the webs 43, but fuel can flow through the spaces 44 between the webs when the closing member 42 is lifted off the seat 40.
  • a spring element 46 in the form of a leaf spring is clamped at one end of a carrier 45 projecting into the storage container 14, the other free end of which acts on the closing member 42 and presses it against the seat 40.
  • a jet nozzle 48 of the jet pump 24 can be inserted into the receptacle 32 from the side facing away from the opening 30, which preferably is made of plastic.
  • One end of the jet nozzle 48 with its inlet opening 49 protrudes from the receptacle 32 on the side facing away from the opening 30 and the return line 22 is pushed onto this end.
  • the jet nozzle 48 In its area facing the return line 22, the jet nozzle 48 has the inlet opening 49 with a substantially constant cross section, and in its end area facing the opening 30, the free cross section tapers in the jet nozzle 48.
  • the end of the jet nozzle 48 facing the opening 30 protrudes somewhat out of the receptacle 32 into the channel 36.
  • the area of the jet nozzle 48 from which its cross-section tapers is provided with an overflow opening 54.
  • a circumferential annular groove 56 is formed in the outer periphery of the jet nozzle 48, into which the overflow opening 54 opens and which is arranged with the jet nozzle 48 arranged in the receptacle 32 in such a way that the nozzle 38 opens into it.
  • the annular groove 56 is provided in order to enable simple assembly of the jet nozzle 48 in the receptacle 32, since the connection of the overflow opening 54 to the nozzle 38 is always present through the annular groove 56 regardless of the rotational position of the jet nozzle about its longitudinal axis.
  • the overflow opening 54 forms, together with the spring-loaded closing member 42 which closes the socket 38, the overflow valve 25, through which fuel can flow out of the jet nozzle 48 into the storage container 14 as a relief space if that caused by the fuel flowing back through the return line 22 in the jet nozzle 48 Pressure exceeds a certain value that is sufficient to lift the closing member 42 against the force of the spring element 46 from the seat 40.
  • the receptacle 32 for the jet nozzle 48 is formed in one piece with the storage container 14.
  • the fuel emerging from the jet nozzle 48 through the driving nozzle opening 52 carries or travels through the open channel 36 with fuel from the storage container 10, which is conveyed through the opening 30 into the storage container 14, so that there is always enough fuel in the storage container 14 for the fuel delivery unit 16 is available.
  • the fuel flowing out through the overflow valve 25 also reaches the storage container 14, but without additionally carrying fuel from the storage container.
  • FIG. 4 shows a second exemplary embodiment of the overflow valve 125, in which the basic structure of the jet pump 124 and the accumulation container 114 is essentially the same as described above in the first exemplary embodiment.
  • the opening 130 is arranged closely above the bottom 128 thereof, and the receptacle 132 for the jet nozzle 148, which is designed as in the first exemplary embodiment, is arranged on the wall part 134 of the storage container 114.
  • the wall part 134 has an opening 138 through which the interior of the storage container 114 is connected to the receptacle 132.
  • the jet nozzle 148 made of plastic has the inlet opening 149 assigned to the return line 22, the outlet or driving nozzle opening 152 and on its circumference the overflow opening 154, the mouth of which on the outer circumference of the jet nozzle 148 widens conically as a seat 140 for the closing member 142. From the opening 138 project radially inward over their circumference spaced webs 143 shown in FIG. 5, between the ends of which the closing member 142 is guided. When the closing member 142 is lifted from the seat 140, fuel can flow through the spaces 144 between the webs 143 into the storage container 114.
  • the spring element 146 for the closing member 142 is arranged in the storage container 114 and is designed as a leaf spring clamped on one side on the carrier 145 projecting into the storage container 114.

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)
  • Fuel-Injection Apparatus (AREA)

Claims (5)

  1. Dispositif d'alimentation de carburant à partir d'un réservoir (10) d'un moteur à combustion interne (12) d'un véhicule automobile comportant
    - une unité de transfert de carburant (16) logée dans un réservoir (10), qui aspire dans une zone (14, 114) du réservoir (10) et dont le côté de pression est relié au moteur à combustion interne (12),
    - une conduite de retour (22) reliant le moteur à combustion interne (12) au réservoir (10),
    - une pompe à jet (24, 124) reliée à la conduite de retour (22) et logée dans le réservoir (10) qui transfert le carburant dans la zone (14, 114) du réservoir (10),
    - une soupape de débordement (25, 125) associée à la pompe à jet (24, 124) qui permet en cas de dépassement d'une certaine pression dans la pompe à jet (24, 124), au carburant de la pompe de passer dans la zone (14, 114) du réservoir constituant une chambre de décharge (14, 114),
    - la pompe à jet (24, 124) ayant une buse à jet (48, 148) munie dans la partie comprise entre l'orifice d'entrée (49, 149) associé à la conduite de retour (22) et son orifice de sortie (52, 152), dans sa périphérie, d'un orifice de débordement complémentaire (54, 154) dont la liaison avec la chambre de décharge (14, 114) est commandée pour former la soupape de débordement (25, 125) par l'intermédiaire d'un organe d'obturation (42, 142) chargé par un ressort,
    caractérisé en ce que
    la zone séparée du réservoir (10) est un réservoir de retenue (14, 114) logé dans le réservoir et l'élément à ressort chargeant l'organe d'obturation (42, 142) est un ressort lame (46, 146) placé à l'intérieur du réservoir de retenue (14, 114) et dont une extrémité est encastrée dans celui-ci.
  2. Dispositif selon la revendication 1,
    caractérisé par
    un logement (132) pour recevoir la buse à jet (148) qui entoure la périphérie de la buse à jet (148) et comporte une ouverture (138) associée à l'orifice de débordement (154) et l'embouchure de l'orifice de débordement (154) est réalisée comme siège (140) à la périphérie de la buse à jet (148) pour coopérer avec l'organe d'obturation (142).
  3. Dispositif selon la revendication 1,
    caractérisé par
    un logement (32) pour la buse à jet (48) qui entoure la périphérie de la buse à jet (48) et comporte un ajutage (38) communiquant avec l'orifice de débordement (54), ajutage dont la zone d'extrémité est munie d'un siège (40) avec lequel coopère l'organe d'obturation (42).
  4. Dispositif selon la revendication 2 ou 3,
    caractérisé en ce que
    le logement (32, 132) fait corps avec le réservoir de retenue (14, 114).
  5. Dispositif selon l'une des revendications 2 à 4,
    caractérisé en ce que
    la périphérie extérieure de la buse à jet (48) comporte une rainure annulaire périphérique (56) dans laquelle débouche l'orifice de débordement (54) et qui communique avec l'ajutage (38) ou l'ouverture (138) du logement (32, 132).
EP95110247A 1994-07-28 1995-06-30 Dispositif d'alimentation de combustible d'un réservoir vers un moteur à combustion interne d'un véhicle automobile Expired - Lifetime EP0694691B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4426667A DE4426667A1 (de) 1994-07-28 1994-07-28 Vorrichtung zum Fördern von Kraftstoff aus einem Vorratsbehälter zur Brennkraftmaschine eines Kraftfahrzeuges
DE4426667 1994-07-28

Publications (2)

Publication Number Publication Date
EP0694691A1 EP0694691A1 (fr) 1996-01-31
EP0694691B1 true EP0694691B1 (fr) 1997-09-03

Family

ID=6524310

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95110247A Expired - Lifetime EP0694691B1 (fr) 1994-07-28 1995-06-30 Dispositif d'alimentation de combustible d'un réservoir vers un moteur à combustion interne d'un véhicle automobile

Country Status (5)

Country Link
US (1) US5564397A (fr)
EP (1) EP0694691B1 (fr)
JP (1) JPH0849615A (fr)
KR (1) KR100387755B1 (fr)
DE (2) DE4426667A1 (fr)

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Also Published As

Publication number Publication date
US5564397A (en) 1996-10-15
EP0694691A1 (fr) 1996-01-31
JPH0849615A (ja) 1996-02-20
KR100387755B1 (ko) 2003-11-17
DE59500592D1 (de) 1997-10-09
DE4426667A1 (de) 1996-02-01

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