EP0344063A1 - Degassing device for the fuel feeding of an internal combustion engine - Google Patents
Degassing device for the fuel feeding of an internal combustion engine Download PDFInfo
- Publication number
- EP0344063A1 EP0344063A1 EP89401412A EP89401412A EP0344063A1 EP 0344063 A1 EP0344063 A1 EP 0344063A1 EP 89401412 A EP89401412 A EP 89401412A EP 89401412 A EP89401412 A EP 89401412A EP 0344063 A1 EP0344063 A1 EP 0344063A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fuel
- tank
- valve
- degassing device
- return pipe
- 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
- 239000000446 fuel Substances 0.000 title claims abstract description 63
- 238000007872 degassing Methods 0.000 title claims abstract description 17
- 238000002485 combustion reaction Methods 0.000 title description 3
- 239000007788 liquid Substances 0.000 claims abstract description 13
- 230000001133 acceleration Effects 0.000 claims abstract description 4
- 239000007789 gas Substances 0.000 claims description 41
- 238000010908 decantation Methods 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 2
- 238000000926 separation method Methods 0.000 description 5
- 238000004064 recycling Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000012071 phase Substances 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229920002994 synthetic fiber Polymers 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 239000000839 emulsion Substances 0.000 description 1
- 239000008246 gaseous mixture Substances 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- F02M37/0011—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor
- F02M37/0023—Valves in the fuel supply and return system
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- F02M37/20—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 characterised by means for preventing vapour lock
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- F02M37/0047—Layout or arrangement of systems for feeding fuel
- F02M37/0052—Details on the fuel return circuit; Arrangement of pressure regulators
Definitions
- the supply fuel In internal combustion engines, the supply fuel must reach the carburetor free of any vapor or gas and at a temperature compatible with the fuel metering organ with the intake air.
- a fuel degassing device which comprises a decantation tank and a cover body tightly fixed on the decantation tank, said cover body being provided with a fuel inlet pipe, a gas and vapor return pipe to the tank, located in an upper part of the cover and an outlet pipe for the evacuation of the degassed liquid fuel towards the carburetor, and in which is mounted a valve loaded by a calibrated spring, which keeps the valve applied against a first seat as long as the settling tank contains gas, this then escaping towards the return pipe to the tank through low-loss passages load which by-pass the valve, while, when the settling tank is completely filled with liquid fuel, the valve is biased against the force of the spring, towards a closed position on a second seat o where it closes the return line to the tank.
- a first separation between the liquid phase and the gas phase of the fuel takes place under the effect of the impact of the incident flow of fuel on a deflector, then the fuel gets rid of another part of the gases which it contains by passing through a cylindrical filter cartridge.
- a fuel supply system for an internal combustion machine which comprises a gas separator, a recycling duct connected to the pressure outlet of a circulation pump and a Venturi tube arranged in the recycling duct to create a positive pressure drop between the interior space of the gas separator and the recycling duct, so that the gas coming from said space is sucked by the Venturi.
- the separator according to said patent is connected between the tank and the pump, its main function being to send gas-free fuel to the pump. But as we know, this can cause the formation of gases or emulsions at the outlet.
- GB-A-2 157 803 discloses a gas separator which comprises a valve constituted by a ball which, when in the high position, completely closes the orifice of the return pipe to the tank.
- the present invention provides a degassing device according to the preamble of claim 1, and which is much simpler, more effective and economical than the devices of the technique described above.
- This device is characterized by the following points: - the inlet manifold has in said cover a portion of narrowed diameter in which the fuel undergoes an acceleration, and which is extended by a portion which makes the fuel penetrate into the settling tank tangentially to the wall thereof, - downstream of the valve and in the return pipe to the tank is mounted a nozzle to which part of the incident fuel flow is derived by a channel connected to the inlet tubing, said nozzle creating a vacuum at the inlet of the return tubing.
- the settling tank according to the invention is much simpler and economical than the separator according to patent DE-A-1 235 067 since it only has three connections instead of four. Another important difference is that the settling tank is mounted between the pump and the engine and therefore sends liquid fuel to the latter free of air bubbles and gases.
- the settling tank is divided into two superposed stages, by a separating element in the form of an overturned funnel, the conical part of which defines with the internal wall of the tank a small interval for the 'flow of fuel from the inlet manifold, and the tubular part of which adapts to the upper part of the cover body, orifices being provided at the end of the tubular part to allow the evacuation of the gases s' accumulating in the upper stage towards the return pipe to the tank.
- Said separating element is closed at its narrowed end by a wall pierced with a calibrated hole for the evacuation of gases accumulating in the lower stage.
- a filter with suitable mesh intended to separate the last gas bubbles from the fuel, the degassed fuel being under the filter being sucked towards the outlet pipe by a cannula whose lower end crosses the filter tightly and dives into the fuel.
- the valve is pierced with a calibrated orifice allowing a low rate of fuel leakage towards the return pipe when the valve is in the closed position.
- the device according to the invention therefore performs degassing in three stages: - a first separation due to the acceleration of the die bit of fuel, then when it relaxes in the settling tank, where it is projected tangentially to the wall.
- the fuel undergoes a thermal shock by cicuring on said wall, which promotes the separation of gases; - the suction of gases by the vacuum created by the nozzle; - the residual gases and vapors are channeled through the funnel towards the return pipe to the tank.
- the degassing device 10 comprises a settling tank 11 and a cover body 12, made of a light metal or a synthetic material capable of withstanding the temperatures prevailing under the engine hood.
- the tank and the cover body can be assembled in various ways. For example, if the tank is made of metal, assembly can be carried out, as shown in FIG. 1, by crimping its upper edge 14 on a flange 16 formed on the periphery of the edge of the cover body, an O-ring 18 sealing. If the tank and the cover are made of synthetic material, they can be welded edge to edge, for example by the rotary process.
- dome-shaped element 26 intended to recover the gases and vapors inside the tank and to bring them back to the tube 24 back to the tank.
- said dome-shaped element is constituted by a disc having a concave lower face 28, for example with a slight taper centered on the axis of the tank.
- Said element 26 is pierced in its center with an axial orifice 30 which communicates with the return pipe 24. It has a flat upper face 32 which bears against the internal face of the cover body, and a projecting peripheral edge 34 which is clamped between the edge 16 of the cover and a shoulder formed on the upper edge of the settling tank.
- the inlet pipe 20 has a vertical portion 36 of narrowed diameter drilled in the element 26, in which the fuel accelerates.
- the portion 36 is extended by a substantially horizontal portion 38 oriented so that the outgoing jet of fuel strikes the internal wall of the tank under a substantially tangential incidence.
- the interior of the settling tank is divided into two stages by a deflector 40 in the form of an inverted funnel and of the same axis as the tank.
- the deflector comprises a frustoconical part 42 whose flared edge leaves a slight clearance with the inner wall of the tank. Said edge comprises for this purpose a plurality of protrusions 44 regularly spaced in contact with the wall of the tank, and which define with the latter narrow passages 46 in the form of an arc.
- the frustoconical part is extended by a tubular part 48 provided at its upper end with hooks 50 which snap onto shoulders provided in the axial orifice 30 of the element 26.
- the deflector 40 thus defines a stage upper annular 52 and a lower stage 54.
- the vapors and gases being in the upper stage can flow towards the return orifice 24 by several calibrated tangential orifices 56 formed at the upper end of the tubular part 48 of the deflector.
- the latter is closed by a wall pierced with an orifice 58 through which the vapors and gases forming in the lower stage are discharged.
- a small portion of the effluent fuel flow is diverted from the inlet pipe 20 through a narrow channel 60 to a nozzle 62 which is mounted in the return pipe 24.
- the fuel mixture jet leaving the nozzle creates a depression at the inlet of the return pipe which sucks the gases and vapors forming in the two stages of the tank.
- a valve 64 is slidably mounted between a low position (right part of FIG. 3) where it is applied against a first seat 66 secured to the element 26 and a high position (left part of FIG. 3) where it is applied against a second seat 68 located at the entrance to the return pipe.
- the valve struggles in a bore 70 provided with vertical grooves 72 which by-pass the valve when the latter is in the low position. These grooves offer different pressure drop passages for the liquid and gas phases.
- the valve is calibrated by a spring 74 which keeps it normally applied against the seat 66 as long as the pressure downstream of the valve is less than a predetermined pressure. It has a central orifice calibrated 76 through which a low flow rate of liquid fuel leakage can escape when the valve is in its high position.
- a filter 78 with a suitable mesh used to separate the last gas bubbles which may remain.
- the degassed fuel flows to the bottom of the tank and is sucked in through a tube 80 connected to the outlet pipe.
- the operation of the degassing device according to the invention will now be explained.
- the fuel pushed by the pump enters the device through the inlet manifold 20.
- Part of the flow is diverted to the nozzle 62 via the channel 60, from where it returns to the tank via the return manifold 24.
- this fraction of the flow creates a depression which sucks the gases and vapors forming in the upper stages 52 and lower 54.
- the rest of the fuel undergoes a deceleration in the vertical pipe, then a sudden increase in speed in the portion horizontal 38 of smaller diameter, which creates a gas mixture which expands in the upper stage 52.
- a first gas separation takes place at this level.
- the gaseous mixture is projected tangentially to the hot wall of the tank where it undergoes a thermal shock which still releases gases and vapors contained in the fuel. This separation continues under the effect of the vortex movement of the fuel and the centrifugal force.
- the gases accumulate towards the highest part of the concave element 26 and are evacuated through the orifices 56 and the valve 64 towards the return pipe 24.
- the liquid fuel practically free of gas, continues its rotational movement and passes to the lower stage 54.
- the last fraction of gas accumulates in the deflector and is discharged through the orifice 58 towards the valve 64 and the return pipe. .
- a non-return valve 82 can be integrated in the outlet pipe 22, in the case where the height or the distance between the carburetor and the device is large.
- the valve has a triangular section with rounded ends ( Figure 5) and struggles in a cylindrical bore 84 circumscribed to the valve, so that passages 86 are defined for the flow of liquid fuel.
- the valve At rest, the valve is supported under the action of its own weight on a first seat 88 (left part of Figure 5), while when degassed fuel flows, it is lifted and applied against a second seat 90 (right part of Figure 5) located at the entrance to the return pipe 22 which it only partially closes.
- the element 26 can be made in one piece with the body of the cover.
- the underside of the cover is concave.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
Description
Dans les moteurs Ă combustion interne, le carburant d'alimentation doit arriver au carburateur exempt de toute vapeur ou gaz et Ă une tempĂ©rature compatible avec l'orgaÂl'organe de dosage du carburant avec l'air d'admission.In internal combustion engines, the supply fuel must reach the carburetor free of any vapor or gas and at a temperature compatible with the fuel metering organ with the intake air.
Cette exigence devient problĂ©matique de nos jours, essentiellement en raison du fait que les essences actuelÂles sont plus volatiles, et Ă©galement en raison des tempĂ©Âratures très Ă©levĂ©es atteintes sous le capot moteur, surÂtout après des arrĂŞts de courte durĂ©e.This requirement is becoming problematic these days, mainly due to the fact that today's gasolines are more volatile, and also due to the very high temperatures reached under the engine hood, especially after short stops.
Par la demande de brevet français N° 87 10 385, on connaît déjà un dispositif de dégazage de carburant qui comporte une cuve de décantation et un corps de couvercle fixé de façon étanche sur la cuve de décantation, ledit corps de couvercle étant pourvu d'une tubulure d'arrivée du carburant, d'une tubulure de retour des gaz et vapeurs au réservoir, située dans une partie haute du couvercle et d'une tubulure de sortie pour l'évacuation du carburant liquide dégazé vers le carburateur, et dans laquelle est monté un clapet chargé par un ressort taré, qui maintient le clapet appliqué contre un premier siège tant que la cuve de décantation contient du gaz, celui-ci s'échappant alors vers la tubulure de retour au réservoir à travers des passages à faible perte de charge qui by-passent le clapet, tandis que, lorsque la cuve de décantation est entièrement emplie de carburant liquide, le clapet est sollicité à l'encontre de la force du ressort, vers une position de fermeture sur un second siège où il obture la tubulure de retour vers le réservoir.By French patent application No. 87 10 385, a fuel degassing device is already known which comprises a decantation tank and a cover body tightly fixed on the decantation tank, said cover body being provided with a fuel inlet pipe, a gas and vapor return pipe to the tank, located in an upper part of the cover and an outlet pipe for the evacuation of the degassed liquid fuel towards the carburetor, and in which is mounted a valve loaded by a calibrated spring, which keeps the valve applied against a first seat as long as the settling tank contains gas, this then escaping towards the return pipe to the tank through low-loss passages load which by-pass the valve, while, when the settling tank is completely filled with liquid fuel, the valve is biased against the force of the spring, towards a closed position on a second seat o where it closes the return line to the tank.
Une première sĂ©paration entre la phase liquide et la phase gazeuse du carburant s'effectue sous l'effet du choc du flux incident de carburant sur un dĂ©flecteur, puis le carburant se dĂ©barrase d'une autre partie des gaz qu'il contient en traversant une cartouche filtrante cylindriÂque.A first separation between the liquid phase and the gas phase of the fuel takes place under the effect of the impact of the incident flow of fuel on a deflector, then the fuel gets rid of another part of the gases which it contains by passing through a cylindrical filter cartridge.
Toutefois, l'expérience a montré que le dégazage avec un tel dispositif reste encore insuffisant du fait que des gaz se récréent lorsque le carburant traverse la cartouche filtrante. De plus, cette dernière introduit une importan te perte de charge, ce qui nécessite d'utiliser une pompe d'alimentation plus puissante.However, experience has shown that degassing with such a device is still insufficient because gases are recreated when the fuel passes through the filter cartridge. In addition, the latter introduces an important pressure drop, which requires using a more powerful feed pump.
D'autre part, par le brevet DE-A-1 235 067 on connaît un système d'alimentation en combustible pour machine à combustion interne, qui comprend un séparateur de gaz, un conduit de recyclage relié à la sortie sous pression d'une pompe de circulation et un tube de Venturi disposé dans le conduit de recyclage pour créer une chute de pression positive entre l'espace intérieur du séparateur de gaz et le conduit de recyclage, de sorte que le gaz provenant dudit espace est aspiré par le Venturi.On the other hand, from patent DE-A-1 235 067 a fuel supply system for an internal combustion machine is known, which comprises a gas separator, a recycling duct connected to the pressure outlet of a circulation pump and a Venturi tube arranged in the recycling duct to create a positive pressure drop between the interior space of the gas separator and the recycling duct, so that the gas coming from said space is sucked by the Venturi.
Toutefois, un tel système est d'une construction relativement compliquée étant donné que le séparateur comprend au moins quatre connexions avec les éléments avoisinants.However, such a system is of a relatively complicated construction since the separator comprises at least four connections with the neighboring elements.
De plus, le séparateur selon ledit brevet est branché entre le réservoir et la pompe, sa fonction principale étant d'envoyer du carburant exempt de gaz à la pompe. Mais comme on le sait, celle-ci peut provoquer la formation de gaz ou des émulsions à la sortie.In addition, the separator according to said patent is connected between the tank and the pump, its main function being to send gas-free fuel to the pump. But as we know, this can cause the formation of gases or emulsions at the outlet.
On connaît d'autre part par le brevet GB-A-2 157 803 un séparateur de gaz qui comprend un clapet constitué par une bille qui, lorsqu'elle est en position haute, obture complètement l'orifice de la tubulure de retour vers le réservoir.On the other hand, GB-A-2 157 803 discloses a gas separator which comprises a valve constituted by a ball which, when in the high position, completely closes the orifice of the return pipe to the tank.
La présente invention propose un dispositif de dégazage selon le préambule de la revendication 1, et qui est bien plus simple, plus efficace et économique que les dispositifs de la technique décrite ci-dessus. Ce dispositif ce caractérise par les points suivants :
- la tubulure d'arrivée présente dans ledit couvercle une portion de diamètre rétréci dans laquelle le carburant subit une accélération, et qui se prolonge par une portion qui fait pénétrer le carburant dans la cuve de décantation tangentiellement à la paroi de celle-ci,
- en aval du clapet et dans la tubulure de retour vers le réservoir est monté un gicleur vers lequel une partie du débit incident de carburant est dérivé par un canal branché sur la tubulure d'entrée, ledit gicleur créant une dépression à l'entrée de la tubulure de retour.The present invention provides a degassing device according to the preamble of claim 1, and which is much simpler, more effective and economical than the devices of the technique described above. This device is characterized by the following points:
- the inlet manifold has in said cover a portion of narrowed diameter in which the fuel undergoes an acceleration, and which is extended by a portion which makes the fuel penetrate into the settling tank tangentially to the wall thereof,
- downstream of the valve and in the return pipe to the tank is mounted a nozzle to which part of the incident fuel flow is derived by a channel connected to the inlet tubing, said nozzle creating a vacuum at the inlet of the return tubing.
La cuve de décantation selon l'invention est bien plus simple est économique que le séparateur selon le brevet DE-A-1 235 067 puisqu'elle ne comporte que trois connexions au lieu de quatre. Une autre différence importante réside dans le fait que la cuve de décantation est montée entre la pompe et le moteur et qu'elle envoie donc à ce dernier un carburant liquide exempt de bulles d'air et de gaz.The settling tank according to the invention is much simpler and economical than the separator according to patent DE-A-1 235 067 since it only has three connections instead of four. Another important difference is that the settling tank is mounted between the pump and the engine and therefore sends liquid fuel to the latter free of air bubbles and gases.
Selon une autre caractĂ©ristique avantageuse de l'invention, la cuve de dĂ©cantation est divisĂ©e en deux Ă©tages superposĂ©s, par un Ă©lĂ©ment de sĂ©paration en forme d'entonnoir retournĂ©, dont la partie conique dĂ©finit avec la paroi interne de la cuve un faible intervalle pour l'Ă©coulement du carburant venant de la tubulure d'entrĂ©e, et dont la partie tubulaire s'adapte Ă la partie haute du corps de couvercle, des orifices Ă©tant mĂ©nagĂ©s Ă l'extrĂ©ÂmitĂ© de la partie tubulaire pour permettre l'Ă©vacuation des gaz s'accumulant dans l'Ă©tage supĂ©rieur vers la tubulure de retour au rĂ©servoir.According to another advantageous characteristic of the invention, the settling tank is divided into two superposed stages, by a separating element in the form of an overturned funnel, the conical part of which defines with the internal wall of the tank a small interval for the 'flow of fuel from the inlet manifold, and the tubular part of which adapts to the upper part of the cover body, orifices being provided at the end of the tubular part to allow the evacuation of the gases s' accumulating in the upper stage towards the return pipe to the tank.
Ledit Ă©lĂ©ment de sĂ©paration est obturĂ© Ă son extrĂ©miÂtĂ© rĂ©trĂ©cie par une paroi percĂ©e d'un trou calibrĂ© pour l'Ă©vacuation des gaz s'accumulant dans l'Ă©tage infĂ©rieur.Said separating element is closed at its narrowed end by a wall pierced with a calibrated hole for the evacuation of gases accumulating in the lower stage.
A la partie infĂ©rieure de la cuve de dĂ©cantation est montĂ© un filtre Ă mailles appropriĂ©es destinĂ© Ă sĂ©parer les dernières bulles de gaz du carburant, le carburant dĂ©gazĂ© se trouvant sous le filtre Ă©tant aspirĂ© vers la tuÂbulure de sortie par une canule dont l'extrĂ©mitĂ© infĂ©rieuÂre traverse le filtre avec Ă©tanchĂ©itĂ© et plonge dans le carburant.At the lower part of the settling tank is mounted a filter with suitable mesh intended to separate the last gas bubbles from the fuel, the degassed fuel being under the filter being sucked towards the outlet pipe by a cannula whose lower end crosses the filter tightly and dives into the fuel.
Avantageuseument, le clapet est percé d'un orifice calibré autorisant un faible débit de fuite de carburant vers la tubulure de retour lorsque le clapet est en position fermée.Advantageously, the valve is pierced with a calibrated orifice allowing a low rate of fuel leakage towards the return pipe when the valve is in the closed position.
Le dispositif selon l'invention effectue donc le dĂ©Âgazage en trois Ă©tapes :
- une première sĂ©paration due Ă l'accĂ©lĂ©ration du dĂ©Â bit de carburant, puis Ă sa dĂ©tente dans la cuve de dĂ©canÂtation, oĂą il est projetĂ© tangentiellement Ă la paroi. Le carburant subit un choc thermique en cicurlant sur ladite paroi, ce qui favorise la sĂ©partion des gaz;
- l'aspiration des gaz par la dépression créée par le gicleur;
- les gaz et vapeurs résiduels sont canalisés par l'entonnoir vers la tubulure de retour au réservoir.The device according to the invention therefore performs degassing in three stages:
- a first separation due to the acceleration of the die bit of fuel, then when it relaxes in the settling tank, where it is projected tangentially to the wall. The fuel undergoes a thermal shock by cicuring on said wall, which promotes the separation of gases;
- the suction of gases by the vacuum created by the nozzle;
- the residual gases and vapors are channeled through the funnel towards the return pipe to the tank.
L'invention sera mieux comprise Ă la lecture de la description qui va suivre d'un mode de rĂ©alisation prĂ©fĂ©ÂrĂ©, en regard des dessins annexĂ©s dans lesquels:
- La figure 1 est une vue en coupe axiale d'un disposiÂtif de dĂ©gazage;
- La figure 2 est une vue en plan par le haut du dispoÂsitif, et partiellement en coupe;
- La figure 3 est une vue Ă plus grande Ă©chelle du claÂpet montĂ© dans la tubulure de retour au rĂ©servoir;
- La figure 4 représente un clapet anti-retour monté dans la tubulure de sortie; et
- La figure 5 est une vue en coupe du clapet selon la ligne V-V de la figure 4.
- Figure 1 is an axial sectional view of a degassing device;
- Figure 2 is a plan view from above of the device, and partially in section;
- Figure 3 is an enlarged view of the valve mounted in the return pipe to the tank;
- FIG. 4 represents a non-return valve mounted in the outlet pipe; and
- FIG. 5 is a sectional view of the valve along the line VV in FIG. 4.
Avec référence aux figures 1 et 2, le dispositif de dégazage 10 comprend une cuve de décantation 11 et un corps de couvercle 12, réalisés en un métal léger ou en une matière synthétique pouvant supporter les températures régnant sous le capot du moteur.With reference to Figures 1 and 2, the
La cuve et le corps de couvercle peut être assemblés de diverses façons. Par exemple, si la cuve est en métal, l'assemblage peut être effectué, comme le montre la figure 1, par sertissage de son bord supérieur 14 sur une bride 16 formée sur la périphérie du bord du corps de couvercle, un joint torique 18 assurant l'étanchéité. Si la cuve et le couvercle sont en matière synthétique, ils pourront être soudés bord à bord, par exemple par le procédé par rotation.The tank and the cover body can be assembled in various ways. For example, if the tank is made of metal, assembly can be carried out, as shown in FIG. 1, by crimping its
Avec le corps de couvercle viennent de moulage une tubulure d'arrivée 20 par laquelle le carburant qui est refoulé par la pompe à essence entre dans le dispositif de dégazage, une tubulure de sortie 22 pour le refoulement du carburant dégazé vers le carburateur et une tubulure 24 par laquelle le carburant en excès ou les gaz et vapeurs sont ramenés au réservoir.With the cover body there comes molding an
Dans la partie supérieure de la cuve de décantation s'adapte un élément en forme de dôme 26 destiné à récupérer les gaz et vapeurs se trouvant à l'intérieur de la cuve et à les ramener vers la tubulure 24 de retour au réservoir. A cet effet, ledit élément en forme de dôme est constitué par un disque présentant une face inférieure 28 concave, par exemple avec une légère conicité centrée sur l'axe de la cuve. Ledit élément 26 est percé en son centre d'un orifice axial 30 qui communique avec la tubulure de retour 24. Il comporte une face supérieure plate 32 qui s'applique contre la face interne du corps de couvercle, et un bord périphérique en saillie 34 qui est serré entre le bord 16 du couvercle et un épaulement formé sur le bord supérieur de la cuve de décantation.In the upper part of the settling tank there is a dome-
La tubulure d'arrivĂ©e 20 comporte une portion vertiÂcale 36 de diamètre rĂ©trĂ©ci percĂ©e dans l'Ă©lĂ©ment 26, dans laquelle le carburant s'accĂ©lère. La portion 36 se prolonÂge par une portion sensiblement horizontale 38 orientĂ©e de manière que le jet sortant de carburant frappe la paroi interne de la cuve sous une incidence sensiblement tangenÂtielle.The
L'intĂ©rieur de la cuve de dĂ©cantation est divisĂ© en deux Ă©tages par un dĂ©flecteur 40 en forme d'entonnoir renÂversĂ© et de mĂŞme axe que la cuve. Le dĂ©flecteur comporte une partie tronconique 42 dont le bord Ă©vasĂ© laisse un lĂ©ger jeu avec la paroi intĂ©rieure de la cuve. Ledit bord comporte Ă cet effet une pluralitĂ© d'excroissances 44 rĂ©gulièrement espacĂ©es en contact avec la paroi de la cuve, et qui dĂ©finissent avec cette dernière d'Ă©troits passages 46 en forme d'arc. La partie tronconique se prolonge par une partie tubulaire 48 pourvue Ă son extrĂ©mitĂ© supĂ©rieure de crochets 50 venant s'encliqueter sur des Ă©paulements prĂ©vus dans l'orifice axial 30 de l'Ă©lĂ©ment 26. Le dĂ©flecteur 40 dĂ©finit ainsi un Ă©tage supĂ©rieur annulaire 52 et un Ă©tage infĂ©rieur 54.The interior of the settling tank is divided into two stages by a
Les vapeurs et gaz se trouvant dans l'Ă©tage supĂ©rieur peuvent s'Ă©couler vers l'orifice de retour 24 par pluÂsieurs orifices calibrĂ©s tangentiels 56 mĂ©nagĂ©s Ă l'extrĂ©ÂmitĂ© supĂ©rieure de la partie tubulaire 48 du dĂ©flecteur. Cette dernière est obturĂ©e par une paroi percĂ©e d'un oriÂfice 58 par lequel s'Ă©vacuent les vapeurs et gaz se forÂmant dans l'Ă©tage infĂ©rieur.The vapors and gases being in the upper stage can flow towards the
Selon l'invention, de la tubulure d'arrivĂ©e 20 est dĂ©rivĂ©e, par un Ă©troit canal 60, une faible portion du dĂ©bit de carburant effluent, vers un gicleur 62 qui est montĂ© dans la tubulure de retour 24. Le jet de mĂ©lange du carburant sortant du gicleur crĂ©e Ă l'entrĂ©e de la tubuluÂre de retour une dĂ©pression qui aspire les gaz et vapeurs se formant dans les deux Ă©tages de la cuve.According to the invention, a small portion of the effluent fuel flow is diverted from the
De façon connue en soi, dans l'orifice de la tubulure de retour, un clapet 64 est monté coulissant entre une position basse (partie de droite de la figure 3) où il s'applique contre un premier siège 66 solidaire de l'élément 26 et une position haute (partie de gauche de la figure 3) où il s'applique contre un second siège 68 situé à l'entrée de la tubulure de retour. Le clapet se débat dans un alésage 70 pourvu de rainures verticales 72 qui by-passent le clapet lorsque celui-ci se trouve en position basse. Ces rainures offrent aux phases liquide et gazeuse des passages de perte de charges différentes. Le clapet est taré par un ressort 74 qui le maintient normalement appliqué contre le siège 66 tant que la pression en aval du clapet est inférieure à une pression prédéterminée. Il comporte un orifice central calibré 76 par lequel un faible débit de fuite de carburant liquide peut s'échapper lorsque le clapet est dans sa position haute.In a manner known per se, in the orifice of the return pipe, a
Dans la partie infĂ©rieure de la cuve est fixĂ© un filtre 78 Ă maille appropriĂ©e, servant Ă sĂ©parer les derÂnières bulles de gaz qui pourraient subsister. Le carbuÂrant dĂ©gazĂ© s'Ă©coule au fond de la cuve et est aspirĂ© par un tube 80 reliĂ© Ă la tubulure de sortie.In the lower part of the tank is fixed a
On expliquera Ă prĂ©sent le fonctionnement du disposiÂtif de dĂ©gazage selon l'invention. Le carburant poussĂ© par la pompe entre dans le dispositif par la tubulure d'arriÂvĂ©e 20. Une partie du dĂ©bit est dĂ©rivĂ©e vers le gicleur 62 via le canal 60, d'oĂą elle retourne au rĂ©servoir par la tubulure de retour 24. En sortant Ă grande vitesse du gicleur, cette fraction du dĂ©bit crĂ©e une dĂ©pression qui aspire les gaz et vapeurs se formant dans les Ă©tages supĂ©rieur 52 et infĂ©rieur 54. Le reste du carburant subit un ralentissement dans la tubulure verticale, puis une subite augmentation de vitesse dans la portion horizontale 38 de diamètre plus petit, ce qui provoque une crĂ©ation de mĂ©lange gazeux qui se dĂ©tend dans l'Ă©tage supĂ©rieur 52. Une première sĂ©paration de gaz s'effectue Ă ce niveau.The operation of the degassing device according to the invention will now be explained. The fuel pushed by the pump enters the device through the
Le mĂ©lange gazeux est projetĂ© tangentiellement Ă la paroi chaude de la cuve oĂą il subit un choc thermique qui libère encore des gaz et des vapeurs contenus dans le carÂburant. Cette sĂ©paration se poursuit sous l'effet du mouÂvement tourbillonnaire du carburant et de la force centriÂfuge. Les gaz s'accumulent vers la partie la plus haute de l'Ă©lĂ©ment concave 26 et sont Ă©vacuĂ©s Ă travers le orifices 56 et le clapet 64 vers la tubulure de retour 24.The gaseous mixture is projected tangentially to the hot wall of the tank where it undergoes a thermal shock which still releases gases and vapors contained in the fuel. This separation continues under the effect of the vortex movement of the fuel and the centrifugal force. The gases accumulate towards the highest part of the
Le carburant liquide, pratiquement exempt de gaz conÂtinue son mouvement de rotation et passe Ă l'Ă©tage infĂ©Ârieur 54. La dernière fraction de gaz s'accumule dans le dĂ©flecteur et est Ă©vacuĂ©e par l'orifice 58 vers le clapet 64 et la tubulure de retour.The liquid fuel, practically free of gas, continues its rotational movement and passes to the
En raison du tarage du clapet, la pression de gaz est insuffisante pour soulever le clapet. Celui-ci reste donc appliquĂ© contre son siège infĂ©rieur 66, les gaz passant Ă travers les rainures 72. Le carburant liquide ne peut s'Ă©chapper par le mĂŞme chemin car les rainures lui oppoÂsent une grande rĂ©sistance. Le carburant liquide continue Ă remplir le dispositif et lorsque la pression qu'il exerce contrebalance la force du ressort 74, le clapet 64 est soulevĂ© et appliquĂ© contre l'autre siège 68. La tubuÂlure de retour est alors obturĂ©e, seul un faible dĂ©bit de fuite s'Ă©coulant Ă travers le trou calibrĂ© 76. Le clapet ne se rouvre que lorsqu'un matelas de gaz d'Ă©paisseur sufÂfisante se sera reformĂ© sous le clapet.Due to the calibration of the valve, the gas pressure is insufficient to lift the valve. The latter therefore remains applied against its lower seat 66, the gases passing through the
Comme le montre la figure 4, un clapet anti-retour 82 peut ĂŞtre intĂ©grĂ© dans la tubulure de sortie 22, dans le cas oĂą la hauteur ou la distance entre le carburateur et le dispositif est grande. Le clapet prĂ©sente une section triangulaire Ă bouts arrondis (figure 5) et se dĂ©bat dans un alĂ©sage cylindrique 84 circonscrit au clapet, de sorte que des passages 86 sont dĂ©finis pour l'Ă©coulement du carburant liquide. Au repos, le clapet est en appui sous l'action de son propre poids sur un premier siège 88 (partie gauche de la figure 5), tandis que lorsque du carÂburant dĂ©gazĂ© s'Ă©coule, il est soulevĂ© et appliquĂ© contre un second siège 90 (partie de droite de la figure 5) situĂ©e Ă l'entrĂ©e de la tubulure de retour 22 qu'il n'obture que partiellement.As shown in FIG. 4, a
Il va de soi que l'élément 26 peut être réalisé en une seule pièce avec le corps du couvercle. Dans ce cas, c'est la face inférieure du couvercle qui est concave.It goes without saying that the
Claims (7)
- la tubulure d'arrivĂ©e (20) prĂ©sente dans ledit couvercle (12) une portion de diamètre rĂ©trĂ©ci (36) dans laquelle le carburant subit une accĂ©lĂ©ration, et qui se prolonge par une portion (38) qui fait pĂ©nĂ©trer le carbuÂrant dans la cuve de dĂ©cantation (11) tangentiellement Ă la paroi de celle-ci,
- en aval du clapet (64) et dans la tubulure de reÂtour vers le rĂ©servoir est montĂ© un gicleur (62) vers lequel une partie du dĂ©bit incident de carburant est dĂ©rivĂ© par un canal (60) branchĂ© sur la tubulure d'entrĂ©e (20), ledit gicleur crĂ©ant une dĂ©pression Ă l'entrĂ©e de la tubulure de retour.1.- Fuel degassing device which comprises a decantation tank and a cover body tightly fixed on the decantation tank, said cover body being provided with a fuel inlet pipe, a fuel pipe return to the gas and vapor reservoir, located in an upper part of the cover and of an outlet pipe for the evacuation of the degassed liquid fuel towards the carburetor, and in which is mounted a valve charged by a calibrated spring, which maintains the valve applied against a first seat as long as the settling tank contains gas, this then escaping towards the return pipe to the tank through passages with low pressure drop which by-pass the valve, while, when the settling tank is completely filled with liquid fuel, the valve is biased against the force of the spring, towards a closed position on a second seat where it closes the return pipe to the tank, characterized Ă© in that:
- the inlet pipe (20) has in said cover (12) a portion of narrowed diameter (36) in which the fuel undergoes an acceleration, and which is extended by a portion (38) which makes the fuel penetrate into the tank decantation (11) tangential to the wall thereof,
- downstream of the valve (64) and in the return pipe to the tank is mounted a nozzle (62) to which part of the incident fuel flow is diverted by a channel (60) connected to the inlet pipe (20 ), said nozzle creating a vacuum at the inlet of the return pipe.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8806941 | 1988-05-25 | ||
FR8806941A FR2632018B1 (en) | 1988-05-25 | 1988-05-25 | HIGH EFFICIENCY DEGASSING DEVICE FOR AN INTERNAL COMBUSTION ENGINE FUEL |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0344063A1 true EP0344063A1 (en) | 1989-11-29 |
EP0344063B1 EP0344063B1 (en) | 1992-01-08 |
Family
ID=9366590
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19890401412 Expired - Lifetime EP0344063B1 (en) | 1988-05-25 | 1989-05-24 | Degassing device for the fuel feeding of an internal combustion engine |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0344063B1 (en) |
DE (1) | DE68900671D1 (en) |
ES (1) | ES2029121T3 (en) |
FR (1) | FR2632018B1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU609960B2 (en) * | 1988-04-11 | 1991-05-09 | Outboard Marine Corporation | Vapor separator |
EP0578484A1 (en) * | 1992-07-09 | 1994-01-12 | Ford Motor Company Limited | Internal combustion engine fuel pickup and reservoir |
FR2783019A1 (en) * | 1998-09-04 | 2000-03-10 | Renault | Fuel feed for motor vehicle internal combustion engine has main pump feeding distribution tank connected to cylinder injectors |
EP1015755A2 (en) * | 1996-08-22 | 2000-07-05 | Jose M. Gonzalez | Fuel/vapor separator apparatus for diesel engines |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1235067B (en) * | 1959-05-13 | 1967-02-23 | Continental Motors Corp | Fuel supply system for internal combustion engines |
DE1979410U (en) * | 1966-07-16 | 1968-02-22 | Daimler Benz Ag | FUEL CONVEYOR DEVICE FOR INJECTION COMBUSTION MACHINES. |
US4079717A (en) * | 1975-06-23 | 1978-03-21 | Nissan Motor Company, Ltd. | Fuel injection system of internal combustion engine |
DE8522528U1 (en) * | 1985-08-05 | 1985-10-10 | Jenbacher Werke Vertriebsgesellschaft mbH, 7016 Gerlingen | Device for the automatic venting of fuel lines in diesel engines |
GB2157803A (en) * | 1984-04-25 | 1985-10-30 | Facet Enterprises | Vent-relief valve for a wet motor gerotor fuel pump |
DE3530970A1 (en) * | 1985-08-30 | 1987-05-07 | Vdo Schindling | Fuel system |
-
1988
- 1988-05-25 FR FR8806941A patent/FR2632018B1/en not_active Expired - Lifetime
-
1989
- 1989-05-24 ES ES89401412T patent/ES2029121T3/en not_active Expired - Lifetime
- 1989-05-24 DE DE8989401412T patent/DE68900671D1/en not_active Expired - Fee Related
- 1989-05-24 EP EP19890401412 patent/EP0344063B1/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1235067B (en) * | 1959-05-13 | 1967-02-23 | Continental Motors Corp | Fuel supply system for internal combustion engines |
DE1979410U (en) * | 1966-07-16 | 1968-02-22 | Daimler Benz Ag | FUEL CONVEYOR DEVICE FOR INJECTION COMBUSTION MACHINES. |
US4079717A (en) * | 1975-06-23 | 1978-03-21 | Nissan Motor Company, Ltd. | Fuel injection system of internal combustion engine |
GB2157803A (en) * | 1984-04-25 | 1985-10-30 | Facet Enterprises | Vent-relief valve for a wet motor gerotor fuel pump |
DE8522528U1 (en) * | 1985-08-05 | 1985-10-10 | Jenbacher Werke Vertriebsgesellschaft mbH, 7016 Gerlingen | Device for the automatic venting of fuel lines in diesel engines |
DE3530970A1 (en) * | 1985-08-30 | 1987-05-07 | Vdo Schindling | Fuel system |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU609960B2 (en) * | 1988-04-11 | 1991-05-09 | Outboard Marine Corporation | Vapor separator |
EP0578484A1 (en) * | 1992-07-09 | 1994-01-12 | Ford Motor Company Limited | Internal combustion engine fuel pickup and reservoir |
EP1015755A2 (en) * | 1996-08-22 | 2000-07-05 | Jose M. Gonzalez | Fuel/vapor separator apparatus for diesel engines |
EP1015755A4 (en) * | 1996-08-22 | 2000-10-18 | Jose M Gonzalez | Fuel/vapor separator apparatus for diesel engines |
FR2783019A1 (en) * | 1998-09-04 | 2000-03-10 | Renault | Fuel feed for motor vehicle internal combustion engine has main pump feeding distribution tank connected to cylinder injectors |
Also Published As
Publication number | Publication date |
---|---|
FR2632018A1 (en) | 1989-12-01 |
FR2632018B1 (en) | 1993-12-24 |
DE68900671D1 (en) | 1992-02-20 |
ES2029121T3 (en) | 1992-07-16 |
EP0344063B1 (en) | 1992-01-08 |
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