US20010003990A1 - Device for venting a fuel tank - Google Patents

Device for venting a fuel tank Download PDF

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Publication number
US20010003990A1
US20010003990A1 US09/736,227 US73622700A US2001003990A1 US 20010003990 A1 US20010003990 A1 US 20010003990A1 US 73622700 A US73622700 A US 73622700A US 2001003990 A1 US2001003990 A1 US 2001003990A1
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Prior art keywords
float
venting
partitions
tank
fuel
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Granted
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US09/736,227
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US6443177B2 (en
Inventor
Christian Romanek
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ITW de France SAS
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ITW de France SAS
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Assigned to I.T.W. DE FRANCE reassignment I.T.W. DE FRANCE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ROMANEK, CHRISTIAN
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K24/00Devices, e.g. valves, for venting or aerating enclosures
    • F16K24/04Devices, e.g. valves, for venting or aerating enclosures for venting only
    • F16K24/042Devices, e.g. valves, for venting or aerating enclosures for venting only actuated by a float
    • F16K24/044Devices, e.g. valves, for venting or aerating enclosures for venting only actuated by a float the float being rigidly connected to the valve element, the assembly of float and valve element following a substantially translational movement when actuated, e.g. also for actuating a pilot valve
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/0753Control by change of position or inertia of system
    • Y10T137/0874Vent opening or closing on tipping container
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2931Diverse fluid containing pressure systems
    • Y10T137/3003Fluid separating traps or vents
    • Y10T137/3084Discriminating outlet for gas
    • Y10T137/309Fluid sensing valve
    • Y10T137/3099Float responsive

Definitions

  • the present invention concerns a device for venting a fuel tank, notably for a motor vehicle.
  • the purpose of venting the fuel tank of a motor vehicle is to prevent any overpressure or negative pressure in the tank.
  • a device for opening to atmosphere is thus provided on the tank in order to preserve a reasonable internal pressure in it, whatever the external temperature and altitude at which the tank is situated.
  • the tank is thus prevented from deforming significantly, notably under negative pressure.
  • a device for venting a fuel tank is known, as described in the French patent application FR 98 06727, which has a chamber communicating on the one hand with the tank and on the other hand, through an outlet orifice, with a pipe for opening to atmosphere.
  • this device for venting has a float, housed in a chamber, adapted to force a needle upwards when the level of fuel reaches the device, the needle then closing off the orifice so as to prevent any leakage of fuel to the outside.
  • such a device for venting is generally incorporated in a top wall 11 of the fuel tank 2 .
  • the device for venting thus occupies the space separating the fuel tank 2 from the chassis 3 of the vehicle.
  • a minimum distance G must separate the bottom of the tank 2 from the ground 4 .
  • a safety distance m is provided between the device for venting 1 immersed in the tank 2 and the maximum level M of fuel in this tank when the vehicle is stopped.
  • the purpose of the present invention is notably to reduce the overall bulk of a device for venting a fuel tank.
  • the present invention relates to a device for venting a fuel tank having a chamber communicating on the one hand with the tank and on the other hand, through an outlet orifice, with a pipe for opening to atmosphere, and a float, housed in the chamber, having an external skirt delimiting an internal space in the float and a needle adapted to close off the outlet orifice when the fuel level exceeds a predetermined threshold in the chamber.
  • the float has at least one partition adapted to divide up the internal volume of the float, with a height substantially equal to the height of the external skirt.
  • the float has a tubular external skirt and at least one internal tubular partition.
  • FIG. 1 illustrates schematically the arrangement of a device for opening a fuel tank to atmosphere in a motor vehicle
  • FIG. 2 is a view in longitudinal section of a device for opening to atmosphere according to a first embodiment of the invention
  • FIG. 3 is a view in transverse section of the float of FIG. 2;
  • FIG. 4 is a view in longitudinal section of a device for opening to atmosphere in accordance with a second embodiment of the invention.
  • FIG. 5 is a view in transverse section of the float of FIG. 4.
  • This device 10 is placed at the top part of a fuel tank 2 , a top wall 11 of which, when the vehicle is in a normal position on horizontal ground, is substantially horizontal, has been shown in part.
  • the device 10 thus has a housing 12 which extends partly outside the tank and partly inside it, by virtue of an opening 13 provided in the top wall 11 of the tank.
  • the housing 12 has essentially a cylindrical barrel 14 which extends through the orifice 13 towards the inside of the tank.
  • This cylindrical barrel 14 is closed on the one hand by a transverse top wall 15 , with an outlet orifice in it, and by a bottom transverse wall 16 .
  • a chamber 17 is thus defined by the cylindrical barrel 14 and the two transverse walls 15 , 16 .
  • the bottom transverse wall 16 is produced in the form of an attached piece fixed for example by clipping to the inside of the barrel 14 .
  • This bottom transverse wall 16 has at least one orifice 18 (two in number in FIG. 2), which enables the chamber 17 to communicate with the tank.
  • This bottom transverse wall 16 slows down the fuel before it enters the chamber 17 .
  • the top transverse wall 15 also has an outlet orifice 19 , situated in this example substantially at the centre of the chamber 17 .
  • the chamber 17 can communicate with a pipe for opening to atmosphere 20 .
  • This top transverse wall 15 has substantially a tapered shape, which opens out towards the top, the outlet orifice 19 opening out at the centre of this tapered part.
  • This top transverse wall 15 is extended upwards by a cylindrical wall 21 .
  • the housing 12 also has a part forming a cap 22 covering this cylindrical wall 21 .
  • An intermediate chamber 23 is thus defined by this cap 22 , the cylindrical wall 21 and the top transverse wall 15 .
  • the pipe for opening to atmosphere 20 opens out in this intermediate chamber 23 by virtue of orifices provided for this purpose in the cap 22 and cylindrical wall 21 .
  • a ball 24 is housed in this intermediate chamber 23 .
  • This ball 24 has a diameter sufficient to close off the outlet orifice 19 in the transverse wall 15 .
  • the ball 24 When the vehicle is in the normal position, the ball 24 is, by gravity, in contact with the tapered surface of the top transverse wall 15 and, when the vehicle is at rest, this ball 24 closes off the outlet orifice 19 .
  • the device for opening to atmosphere 10 also has a float 25 mounted so as to be able to move in the chamber 17 .
  • This float 25 has essentially a top transverse wall 26 and an external tubular skirt 27 delimiting an internal space in the float.
  • the float 25 is thus essentially a tubular body with a substantially vertical axis A which is open at its bottom end and closed at its top end.
  • the top face of the top transverse wall 26 carries a needle 28 which is substantially conical and tapered towards the top. This needle 28 is intended to close off the outlet orifice 19 when the float 25 is in a closure position, that is to say when the float 25 is close to the top transverse wall 15 of the chamber 17 .
  • this float 25 has partitions 29 adapted to divide up the internal space of the float 25 .
  • the external skirt 27 of the float 25 and the partitions 29 are concentric, as better illustrated in FIG. 3.
  • the float 25 has two concentric partitions 29 thus defining two annular internal spaces 30 inside the float 25 and a cylindrical central space 31 .
  • partitions 29 are thus in this example two tubular cylindrical collars 29 with the same axis as the axis A of the float 25 and which extend downwards from the bottom face of the top transverse partition 26 of the float 25 .
  • the length along the axis A of the float 25 of these partitions 29 is equal to the length of the external skirt 27 so that the end 27 a of the external skirt 27 and the ends 29 a of the partitions 29 are situated substantially in the same plane, this plan being perpendicular to the axis A of the float 25 .
  • FIGS. 4 and 5 illustrate a second embodiment of the invention.
  • the device for venting 10 is in every respect identical to that described with reference to FIGS. 2 and 3, apart from the structure of the float 25 , which will be detailed below.
  • the float 25 has as before a top transverse partition 26 extended downwards by an external tubular skirt 27 .
  • It also comprises intermediate partitions 29 , two in number in this example, with a cylindrical tubular shape and concentric with the external skirt 27 .
  • the float 25 also has a second series of partitions 32 , perpendicular to the concentric partitions 29 , and adapted to divide up the annular internal spaces 30 defined by the concentric partitions 29 and the external skirt 27 .
  • this second series of partitions 32 includes a series of radial partitions disposed at a regular pitch in each annular space 30 .
  • the radial partitions 32 of the adjacent annular spaces 30 are disposed so as to be staggered with respect to each other.
  • the concentric partitions 29 and the radial partitions 32 thus define a series of compartments 33 inside the float 25 .
  • the concentric partitions 29 and the radial partitions 32 have a length, as from the top transverse partition 26 of the float 25 , equal to the length of the external skirt 27 .
  • the ball 24 closes off the outlet orifice 19 so that there is no communication between the inside of the tank 2 and the circuit for opening to atmosphere to which the pipe 20 for opening to atmosphere is connected.
  • the gases can circulate freely through the chamber 17 , the intermediate chamber 23 and the pipe 20 for opening to atmosphere.
  • the device 10 for venting thus in a first function preserves an internal pressure in the tank within an acceptable range of pressures.
  • Such a case may arise for example when the vehicle is resting on a surface having a high declivity or during acceleration, braking or on a bend.
  • the ebb and flow of the fuel inside the tank under running conditions is such that the surface of the fuel is generally sloping, for example, as illustrated, at approximately 45°with respect to the axis A of the device 10 for venting.
  • FIGS. 2 and 4 Such a situation is illustrated in FIGS. 2 and 4, in which the surface of the fuel is shown aslant in the float 25 , by dot and dash lines.
  • the device for opening to atmosphere must under no circumstances allow a leakage of fuel whatever the running conditions, and if applicable when the vehicle turns over.
  • the fuel can enter inside the chamber 17 , through orifices 18 in the bottom transverse wall 16 of the housing 12 , the fuel also enters inside the external skirt 27 of the float 25 .
  • the fuel encloses, within this float 25 , a volume of gas V which is included between the fuel surface, the external skirt 27 and the top transverse partition 26 so that the float 25 is pushed upwards inside the chamber 27 and the needle 28 closes off the outlet orifice 19 , thus preventing any risk of escape of fuel through this orifice 29 in the direction of the pipe 20 for opening to atmosphere.
  • the useful flotation volume is increased, that is to say the gaseous volume V trapped between the surface of the fuel, the top transverse partition 26 , the skirt 27 and the concentric partitions 29 , and possibly the radial partitions 32 .
  • the presence of the internal partitions 29 , 32 makes it possible to trap gas in each compartment 30 , 31 , 33 since the surface of the fuel comes in contact with the bottom ends 29 a of the internal partitions 29 , 32 .
  • the float 25 could have a single concentric supplementary partition 29 , or on the other hand concentric partitions 29 greater than two in number.
  • the float 25 could have only partitions 32 perpendicular to the external skirt 27 , to the exclusion of any concentric partition 29 . It could thus have one or more partitions disposed along a diameter of the external skirt 27 .
  • the float 25 and the whole of the device 10 could also have a shape other than tubular.

Abstract

A device (10) for venting a fuel tank has a chamber (17) communicating on the one hand with the tank and on the other hand, through an outlet orifice (19), with a pipe (20) for opening to atmosphere.
A float (25) has an external skirt (27) delimiting an internal space in the float (25) and a needle (28) adapted to close off the outlet orifice (19) when the fuel level exceeds a predetermined threshold in the chamber (17).
The float (25) has at least one partition (29) adapted to divide the internal space in the float (25), with a height substantially equal to the height of the external skirt (27).

Description

  • The present invention concerns a device for venting a fuel tank, notably for a motor vehicle. [0001]
  • The purpose of venting the fuel tank of a motor vehicle is to prevent any overpressure or negative pressure in the tank. A device for opening to atmosphere is thus provided on the tank in order to preserve a reasonable internal pressure in it, whatever the external temperature and altitude at which the tank is situated. [0002]
  • The tank is thus prevented from deforming significantly, notably under negative pressure. [0003]
  • Thus, as the tank gradually empties of its fuel, it is necessary to admit air inside the tank in order to prevent the pressure from dropping excessively. On the other hand, when the reservoir is exposed to a high rise in temperature, for example when the vehicle is parked in the sun, the vapour pressure contained in the tank can increase greatly and it is then necessary to discharge some of these vapours to the outside. [0004]
  • In addition to this function of venting the tank, it is also necessary to provide means for preventing the fuel being able to emerge through the device for venting when the level of fuel close to this device increases significantly, for example following acceleration undergone by the vehicle, or if this vehicle turns over. [0005]
  • A device for venting a fuel tank is known, as described in the French patent application FR 98 06727, which has a chamber communicating on the one hand with the tank and on the other hand, through an outlet orifice, with a pipe for opening to atmosphere. [0006]
  • In order to provide a system for preventing leakage of fuel under all running conditions, and if necessary when the vehicle turns over, this device for venting has a float, housed in a chamber, adapted to force a needle upwards when the level of fuel reaches the device, the needle then closing off the orifice so as to prevent any leakage of fuel to the outside. [0007]
  • As illustrated in FIG. 1, such a device for venting is generally incorporated in a [0008] top wall 11 of the fuel tank 2.
  • The device for venting thus occupies the space separating the [0009] fuel tank 2 from the chassis 3 of the vehicle.
  • In addition, a minimum distance G must separate the bottom of the [0010] tank 2 from the ground 4.
  • Finally, a safety distance m is provided between the device for [0011] venting 1 immersed in the tank 2 and the maximum level M of fuel in this tank when the vehicle is stopped.
  • These technical constraints related to the mounting of the [0012] reservoir 2 in the vehicle, between the chassis 3 and ground 4, limit the space available for the device for opening to atmosphere.
  • The purpose of the present invention is notably to reduce the overall bulk of a device for venting a fuel tank. [0013]
  • To this end, the present invention relates to a device for venting a fuel tank having a chamber communicating on the one hand with the tank and on the other hand, through an outlet orifice, with a pipe for opening to atmosphere, and a float, housed in the chamber, having an external skirt delimiting an internal space in the float and a needle adapted to close off the outlet orifice when the fuel level exceeds a predetermined threshold in the chamber. [0014]
  • In accordance with the invention, the float has at least one partition adapted to divide up the internal volume of the float, with a height substantially equal to the height of the external skirt. [0015]
  • This internal partitioning of the float thus increases the useful flotation volume when the surface of the fuel in contact with the float is no longer [0016]
  • According to a characteristic which is particularly simple to implement, the float has a tubular external skirt and at least one internal tubular partition. [0017]
  • Other particularities and advantages of the invention will also emerge from the following description. [0018]
  • In the accompanying drawings, given by way of non-limitative example: [0019]
  • FIG. 1 illustrates schematically the arrangement of a device for opening a fuel tank to atmosphere in a motor vehicle; [0020]
  • FIG. 2 is a view in longitudinal section of a device for opening to atmosphere according to a first embodiment of the invention; [0021]
  • FIG. 3 is a view in transverse section of the float of FIG. 2; [0022]
  • FIG. 4 is a view in longitudinal section of a device for opening to atmosphere in accordance with a second embodiment of the invention; and [0023]
  • FIG. 5 is a view in transverse section of the float of FIG. 4. [0024]
  • A description will be given first of all, with reference to FIG. 2, of a [0025] device 10 for venting a motor vehicle fuel tank according to a first embodiment of the invention.
  • This [0026] device 10 is placed at the top part of a fuel tank 2, a top wall 11 of which, when the vehicle is in a normal position on horizontal ground, is substantially horizontal, has been shown in part.
  • The [0027] device 10 thus has a housing 12 which extends partly outside the tank and partly inside it, by virtue of an opening 13 provided in the top wall 11 of the tank.
  • The [0028] housing 12 has essentially a cylindrical barrel 14 which extends through the orifice 13 towards the inside of the tank.
  • This [0029] cylindrical barrel 14 is closed on the one hand by a transverse top wall 15, with an outlet orifice in it, and by a bottom transverse wall 16.
  • A [0030] chamber 17 is thus defined by the cylindrical barrel 14 and the two transverse walls 15, 16.
  • In this example, and non-limitatively, the bottom [0031] transverse wall 16 is produced in the form of an attached piece fixed for example by clipping to the inside of the barrel 14.
  • This bottom [0032] transverse wall 16 has at least one orifice 18 (two in number in FIG. 2), which enables the chamber 17 to communicate with the tank.
  • This bottom [0033] transverse wall 16, thus with orifices 18 in it, slows down the fuel before it enters the chamber 17.
  • The top [0034] transverse wall 15 also has an outlet orifice 19, situated in this example substantially at the centre of the chamber 17.
  • By virtue of this [0035] outlet orifice 19, the chamber 17 can communicate with a pipe for opening to atmosphere 20.
  • This top [0036] transverse wall 15 has substantially a tapered shape, which opens out towards the top, the outlet orifice 19 opening out at the centre of this tapered part.
  • This top [0037] transverse wall 15 is extended upwards by a cylindrical wall 21.
  • The [0038] housing 12 also has a part forming a cap 22 covering this cylindrical wall 21.
  • An [0039] intermediate chamber 23 is thus defined by this cap 22, the cylindrical wall 21 and the top transverse wall 15.
  • The pipe for opening to [0040] atmosphere 20 opens out in this intermediate chamber 23 by virtue of orifices provided for this purpose in the cap 22 and cylindrical wall 21.
  • A [0041] ball 24 is housed in this intermediate chamber 23.
  • This [0042] ball 24 has a diameter sufficient to close off the outlet orifice 19 in the transverse wall 15.
  • When the vehicle is in the normal position, the [0043] ball 24 is, by gravity, in contact with the tapered surface of the top transverse wall 15 and, when the vehicle is at rest, this ball 24 closes off the outlet orifice 19.
  • The device for opening to [0044] atmosphere 10 also has a float 25 mounted so as to be able to move in the chamber 17.
  • This [0045] float 25 has essentially a top transverse wall 26 and an external tubular skirt 27 delimiting an internal space in the float.
  • The [0046] float 25 is thus essentially a tubular body with a substantially vertical axis A which is open at its bottom end and closed at its top end.
  • The top face of the top [0047] transverse wall 26 carries a needle 28 which is substantially conical and tapered towards the top. This needle 28 is intended to close off the outlet orifice 19 when the float 25 is in a closure position, that is to say when the float 25 is close to the top transverse wall 15 of the chamber 17.
  • In accordance with the invention, this [0048] float 25 has partitions 29 adapted to divide up the internal space of the float 25.
  • In this embodiment, the [0049] external skirt 27 of the float 25 and the partitions 29 are concentric, as better illustrated in FIG. 3.
  • The height of these [0050] partitions 29 and of the external skirt 27 of the float 25 are substantially equal.
  • As better illustrated in FIG. 3, in this preferred embodiment, the [0051] float 25 has two concentric partitions 29 thus defining two annular internal spaces 30 inside the float 25 and a cylindrical central space 31.
  • These [0052] partitions 29 are thus in this example two tubular cylindrical collars 29 with the same axis as the axis A of the float 25 and which extend downwards from the bottom face of the top transverse partition 26 of the float 25.
  • The length along the axis A of the [0053] float 25 of these partitions 29 is equal to the length of the external skirt 27 so that the end 27 a of the external skirt 27 and the ends 29 a of the partitions 29 are situated substantially in the same plane, this plan being perpendicular to the axis A of the float 25.
  • FIGS. 4 and 5 illustrate a second embodiment of the invention. [0054]
  • In these figures, the device for [0055] venting 10 is in every respect identical to that described with reference to FIGS. 2 and 3, apart from the structure of the float 25, which will be detailed below.
  • The [0056] float 25 has as before a top transverse partition 26 extended downwards by an external tubular skirt 27.
  • It also comprises [0057] intermediate partitions 29, two in number in this example, with a cylindrical tubular shape and concentric with the external skirt 27.
  • In this embodiment, the [0058] float 25 also has a second series of partitions 32, perpendicular to the concentric partitions 29, and adapted to divide up the annular internal spaces 30 defined by the concentric partitions 29 and the external skirt 27.
  • Preferably, as illustrated in FIG. 5, this second series of [0059] partitions 32 includes a series of radial partitions disposed at a regular pitch in each annular space 30.
  • In this embodiment, the [0060] radial partitions 32 of the adjacent annular spaces 30 are disposed so as to be staggered with respect to each other.
  • The [0061] concentric partitions 29 and the radial partitions 32 thus define a series of compartments 33 inside the float 25.
  • The [0062] concentric partitions 29 and the radial partitions 32 have a length, as from the top transverse partition 26 of the float 25, equal to the length of the external skirt 27.
  • A description will now be given more particularly of the functioning of the device for venting [0063] 10 according to the invention.
  • When the vehicle is at rest on a substantially horizontal surface, the [0064] ball 24 closes off the outlet orifice 19 so that there is no communication between the inside of the tank 2 and the circuit for opening to atmosphere to which the pipe 20 for opening to atmosphere is connected.
  • On the other hand, as soon as an overpressure occurs inside the tank, for example due to a heating of the gases contained in it, or when the vehicle travels, simply because of the vibration which is inevitably transmitted to the tank and to the device for venting [0065] 10, the ball 24 is moved so that the outlet orifice 19 is released.
  • Thus the gases can circulate freely through the [0066] chamber 17, the intermediate chamber 23 and the pipe 20 for opening to atmosphere.
  • The [0067] device 10 for venting thus in a first function preserves an internal pressure in the tank within an acceptable range of pressures.
  • Moreover, it happens that the level of fuel in the tank, close to the [0068] device 10 for opening to atmosphere, becomes higher than the level of the bottom transverse wall 16 of the housing 12.
  • Such a case may arise for example when the vehicle is resting on a surface having a high declivity or during acceleration, braking or on a bend. [0069]
  • In these cases, the ebb and flow of the fuel inside the tank under running conditions is such that the surface of the fuel is generally sloping, for example, as illustrated, at approximately 45°with respect to the axis A of the [0070] device 10 for venting.
  • Such a situation is illustrated in FIGS. 2 and 4, in which the surface of the fuel is shown aslant in the [0071] float 25, by dot and dash lines.
  • Under these conditions of use, the device for opening to atmosphere must under no circumstances allow a leakage of fuel whatever the running conditions, and if applicable when the vehicle turns over. [0072]
  • Since the fuel can enter inside the [0073] chamber 17, through orifices 18 in the bottom transverse wall 16 of the housing 12, the fuel also enters inside the external skirt 27 of the float 25.
  • However, as soon as the level of fuel is sufficient inside the [0074] float 25, the fuel encloses, within this float 25, a volume of gas V which is included between the fuel surface, the external skirt 27 and the top transverse partition 26 so that the float 25 is pushed upwards inside the chamber 27 and the needle 28 closes off the outlet orifice 19, thus preventing any risk of escape of fuel through this orifice 29 in the direction of the pipe 20 for opening to atmosphere.
  • In accordance with the invention, by compartmentalising the internal space of the [0075] float 25, the useful flotation volume is increased, that is to say the gaseous volume V trapped between the surface of the fuel, the top transverse partition 26, the skirt 27 and the concentric partitions 29, and possibly the radial partitions 32.
  • This is because, without [0076] internal partitions 29, 32, the useful flotation volume is defined solely by the skirt 27, the top transverse partition 26 and the surface of the fuel sloping from the bottom end 27 a of the external skirt 27.
  • On the other hand, the presence of the [0077] internal partitions 29, 32 makes it possible to trap gas in each compartment 30, 31, 33 since the surface of the fuel comes in contact with the bottom ends 29 a of the internal partitions 29, 32.
  • It is thus possible, considering a [0078] float 25 with the same external diameter, to reduce the overall height of the float 25 according to the invention.
  • The addition of [0079] supplementary partitions 29 and 32 makes it possible to reduce the height of the float 25 by approximately 30% compared with a conventional float.
  • It is thus possible to reduce the overall bulk of the [0080] device 10 for venting, which facilitates its mounting within a motor vehicle.
  • Naturally, many modifications could be made to the example embodiments described above without departing from the scope of the invention. [0081]
  • Thus the [0082] float 25 could have a single concentric supplementary partition 29, or on the other hand concentric partitions 29 greater than two in number.
  • Moreover, the [0083] float 25 could have only partitions 32 perpendicular to the external skirt 27, to the exclusion of any concentric partition 29. It could thus have one or more partitions disposed along a diameter of the external skirt 27.
  • The [0084] float 25 and the whole of the device 10 could also have a shape other than tubular.

Claims (6)

1. Device for venting a fuel tank, having a chamber (17) communicating on the one hand with the tank (2) and on the other hand, through an outlet orifice (19), with a pipe for opening to atmosphere (20) and a float (25), housed in the chamber (17), having an external skirt (27) delimiting an internal space in the float (25) and a needle (28) adapted to close off the outlet orifice (19) when the fuel level exceeds a predetermined threshold in the chamber (17), characterised in that the float (25) has at least one partition (29, 32) adapted to divide up the internal space in the float (25), with a height substantially equal to the height of the external skirt (27).
2. Device for venting according to
claim 1
, characterised in that the external skirt (27) of the float (25) and said partition (29) are concentric.
3. Device for venting according to one of claims 1 or 2, characterised in that the float (25) has several concentric partitions (29).
4. Device for venting according to
claim 1
, characterised in that the external skirt (27) of the float (25) and said partition (31) are perpendicular.
5. Device for venting according to one of
claims 1
to
4
, characterised in that the float (25) has a first series of concentric partitions (29) delimiting annular internal spaces (30) in the float (25), and a second series of partitions (32), perpendicular to the partitions (29) in the first series and adapted to divide the annular internal spaces (30).
6. Device for opening to atmosphere according to one of
claims 1
to
5
, characterised in that the float (25) has a tubular external skirt (27) and at least one internal tubular partition (29).
US09/736,227 1999-12-17 2000-12-15 Device for venting a fuel tank Expired - Fee Related US6443177B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9915989 1999-12-17
FR9915989A FR2802481B1 (en) 1999-12-17 1999-12-17 DEVICE FOR BREAKING DOWN A FUEL TANK

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US20010003990A1 true US20010003990A1 (en) 2001-06-21
US6443177B2 US6443177B2 (en) 2002-09-03

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US (1) US6443177B2 (en)
AU (1) AU759202B2 (en)
CA (1) CA2328547C (en)
FR (1) FR2802481B1 (en)
IT (1) IT1321112B1 (en)
MX (1) MXPA00012469A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070267064A1 (en) * 2006-05-16 2007-11-22 Gm Global Technology Operations, Inc. Dual Float Rollover Valve
US20110155751A1 (en) * 2009-12-24 2011-06-30 Inergy Automotive Systems Research (Societe Anonyme) Valve for the venting circuit of a liquid tank
US20110315240A1 (en) * 2010-06-23 2011-12-29 Alfmeier Prazision Ag Baugruppen Und Systemlosungen Ventilation valve
CN111520514A (en) * 2020-03-25 2020-08-11 国网浙江省电力有限公司紧水滩水力发电厂 Quick-response mechanical exhaust device

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6857445B2 (en) * 2003-06-30 2005-02-22 Carrier Corporation Float valve for pulsating flow
US7225826B2 (en) * 2003-12-04 2007-06-05 Moeller Marine Products Marine fuel tank vent valve
US7422027B2 (en) 2004-12-03 2008-09-09 Tony Riviezzo Marine fuel tank vent valve
DE102011013959A1 (en) * 2011-03-14 2012-09-20 Kautex Textron Gmbh & Co. Kg Pressure compensation valve for fuel or secondary fluid reservoir on a motor vehicle
JP2013024288A (en) * 2011-07-19 2013-02-04 Aisan Industry Co Ltd Fuel cutoff valve
US9360872B2 (en) * 2011-12-22 2016-06-07 Eaton Corporation Fuel tank vent valve assembly and method of assembly

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5666989A (en) * 1994-11-08 1997-09-16 Stant Manufacturing Inc. Tank venting control assembly
US5960819A (en) * 1996-08-07 1999-10-05 Borg-Warner Automotive, Inc. Valve having multi-part valve housing

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5640989A (en) * 1995-01-12 1997-06-24 Nok Corporation Fuel cut-off valve
IL112444A (en) * 1995-01-25 1998-01-04 Raviv Precision Injection Mold Roll over vent valve
JP3346962B2 (en) 1995-08-03 2002-11-18 京三電機株式会社 Fuel cut valve
US5944044A (en) * 1996-05-10 1999-08-31 Stant Manufacturing Inc. Tank venting control system
JPH1113572A (en) 1997-06-20 1999-01-19 Nok Corp Liquid cutoff valve device
US5960817A (en) * 1997-11-03 1999-10-05 Walbro Corporation Control valve and system for fuel vapor recovery
FR2774636B1 (en) * 1998-02-12 2000-05-05 Journee Paul Sa DEVICE FOR BREAKING IN THE FREE AIR OF A MOTOR VEHICLE FUEL TANK
FR2779100B1 (en) * 1998-05-28 2000-08-18 Journee Paul Sa MOTOR VEHICLE FUEL TANK RELEASING DEVICE

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5666989A (en) * 1994-11-08 1997-09-16 Stant Manufacturing Inc. Tank venting control assembly
US5960819A (en) * 1996-08-07 1999-10-05 Borg-Warner Automotive, Inc. Valve having multi-part valve housing

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070267064A1 (en) * 2006-05-16 2007-11-22 Gm Global Technology Operations, Inc. Dual Float Rollover Valve
US8291929B2 (en) * 2006-05-16 2012-10-23 GM Global Technology Operations LLC Dual float rollover valve
US20110155751A1 (en) * 2009-12-24 2011-06-30 Inergy Automotive Systems Research (Societe Anonyme) Valve for the venting circuit of a liquid tank
US8763626B2 (en) * 2009-12-24 2014-07-01 Inergy Automotive Systems Research (Societe Anonyme) Valve for the venting circuit of a liquid tank
US20110315240A1 (en) * 2010-06-23 2011-12-29 Alfmeier Prazision Ag Baugruppen Und Systemlosungen Ventilation valve
CN111520514A (en) * 2020-03-25 2020-08-11 国网浙江省电力有限公司紧水滩水力发电厂 Quick-response mechanical exhaust device

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CA2328547C (en) 2005-07-26
AU7229100A (en) 2001-06-21
FR2802481B1 (en) 2002-03-01
IT1321112B1 (en) 2003-12-30
CA2328547A1 (en) 2001-06-17
AU759202B2 (en) 2003-04-10
ITTO20001174A1 (en) 2002-06-15
US6443177B2 (en) 2002-09-03
ITTO20001174A0 (en) 2000-12-15
FR2802481A1 (en) 2001-06-22

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