USPatent applicationPatented

Fuel tank having a venting system

Granted 15 Nov 2005 · 1 office action

Assignee: TI Group Automotive Systems, L.L.C.

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Inventors: Martin Stickel · Examiner: Carl S. Miller · AU 3747 · TC 3700

Life of the application

10 dated events
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Abstract

A venting system for a fuel tank has an inlet opening that is communicated with a liquid separator arranged between the inlet opening and a vapor canister that preferably has an activated carbon filter. The liquid separator is preferably arranged in the interior of the fuel tank. In a preferred embodiment of the invention, a plurality of vent lines are arranged in the interior of the tank with the inlet openings of the vent lines spaced apart from each other so that there is always at least one inlet opening not exposed to liquid fuel. A line between the liquid separator and the activated carbon filter communicates with the upper region of the liquid separator. These measures ensure that the fuel vapors which are to be vented can pass undisturbed through the liquid separator while any liquid fuel which enters the separator collects in its lower region.

Description

6 parts
›Applicant claims the benefit of German Patent Application…

Applicant claims the benefit of German Patent Application Serial No. DE 102 09 491.8 filed Mar. 5, 2002.

›FIELD OF THE INVENTION

The invention relates to a fuel tank, and more particularly to a fuel tank having a venting system.

›BACKGROUND OF THE INVENTION

In addition to the liquid fuel volume, fuel tanks also contain a gas volume, which is formed by fuel vapors and/or air. Temperature fluctuations lead to corresponding internal-pressure fluctuations in the tank. Excess pressures which occur have to be reduced, but emission regulations mean that fuel vapors must not escape into the atmosphere. The pressure is therefore reduced via an activated carbon filter (ACF) into which a vent line leads. However, it has to be ensured that liquid fuel does not pass into the activated carbon filter via the vent line. Up to now, a valve, for example a float valve, has therefore been arranged at the inlet opening of the vent line, the valve closing in the presence of liquid fuel, such as may occur if the vehicle is on a slope and/or during sloshing of the fuel. To ensure that the fuel tank can be vented during a wide range of circumstances which occur, two or more venting locations are provided with corresponding lines and valves, with the result that if one valve dips into liquid fuel, another valve, which is preferably arranged in the opposite region of the tank, may be open. These valves are subject to mechanical faults and cause additional costs during production of the fuel tank.

›SUMMARY OF THE INVENTION

A venting system for a fuel tank has an inlet opening that is communicated with a liquid separator arranged between the inlet opening and a vapor canister that preferably has an activated carbon filter. The liquid separator is preferably arranged in the interior of the fuel tank. In a preferred embodiment of the invention, a plurality of vent lines are arranged in the interior of the tank with the inlet openings of the vent lines spaced apart from each other so that there is always at least one inlet opening not exposed to liquid fuel. The vent lines may each be connected individually to the liquid separator, but they preferably lead into a manifold or branch section which communicates with the liquid separator through a short connecting line. A line between the liquid separator and the activated carbon filter communicates with the upper region of the liquid separator. These measures ensure that the fuel vapors which are to be vented can pass undisturbed through the liquid separator while any liquid fuel which enters the separator collects in its lower region.

In a preferred embodiment of the invention, at least one vent line is arranged in the interior of the tank in such a manner that, during changes in inclination of the tank and/or fuel-sloshing movements which occur in the operation of a motor vehicle, at least a subregion of the line runs above the fuel level. This forms a siphon which prevents relatively large quantities of liquid from entering into the vent line.

The removal of liquid fuel from the separator preferably takes place via a line which is connected to the lower region of the liquid separator and is connected to a low-pressure source, which is preferably a jet pump arranged in the container and driven by a portion of the fuel discharged from a fuel pump arranged in the fuel tank.

In order to prevent liquid fuel from entering into the line leading from the separator to the activated carbon filter, the liquid separator preferably has a baffle plate arrangement arranged upstream of the line.

A preferably electromagnetically actuable shutoff valve can be arranged at an outlet of the activated carbon filter leading into the atmosphere, the shutoff valve can be switched in accordance with an electronic engine control system and/or a position sensor or filling-level sensor. The shutoff valve may be closed, for example for building up a counterpressure when filling the tank, so that the counterpressure causes the fuel nozzle to shut-off before the tank is overfilled, i.e. before the fuel level reaches the inlet openings of the vent lines, or to prevent fuel from running out in the event of the vehicle overturning.

›BRIEF DESCRIPTION OF THE DRAWINGS

These and other objects, features and advantages of this invention will be apparent from the following detailed description of the preferred embodiments and best mode, appended claims and accompanying drawings in which:

FIG. 1 shows a fuel system having a fuel tank with a venting system according to one presently preferred embodiment of the invention;

FIG. 2 shows the tank according to FIG. 1 , with different fuel levels arising due to lateral inclination of the tank being indicated;

FIG. 3 shows an enlarged illustration of a liquid separator of the system of FIG. 1 ; and

FIG. 4 is a schematic view of some of the components of the fuel system.

›DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

Referring in more detail to the drawings, FIGS. 1-4 illustrate a fuel system including a fuel tank 10 having an interior for a supply of fuel in which two vent lines 12 , 14 having open inlet openings 16 , 18 are arranged in the upper region of the tank interior. The vent lines 12 , 14 have another end opposite the inlet openings 16 , 18 leading a liquid separator 20 . From there, a line 22 leads to a vapor canister 34 preferably providing an activated carbon filter (ACF) which is preferably arranged outside the tank and in which the vented fuel vapors can be collected and either added to the combustion air fed to an engine via a line 24 (cyclic regeneration in accordance with an electronic control system) or the cleaned air can be passed into the atmosphere via a line 26 .

Also arranged in the tank are a fuel pump 28 and a jet pump 30 . The latter has the following function: A portion of the fuel discharged from the fuel pump 28 (which may discharge fuel at a relatively high pressure, for example, without limitation, 4 bar) is routed to the jet pump 30 by line 32 . This flow of fuel is the driving flow for the jet pump 30 , and causes a low pressure to be produced in the area of the jet pump housing. The low pressure pumps liquid fuel from the tank 10 into a storage tank or container (not illustrated) and/or out of a second tank chamber when the tank is designed as a “saddle tank”. A solenoid valve 36 can be arranged at the output of the vapor canister 34 leading into the atmosphere, the solenoid valve may have the function of providing an onboard diagnosis. If the solenoid valve is closed, pressure builds up in the tank. If the pressure which has built up and is measured by a pressure sensor is not within certain limits, this may indicate a malfunction of the valve 36 or possible leakages from the tank 10 . Within the context of the invention, this valve 36 may carry out an additional function, which is explained in more detail below.

Even when the tank is fully filled, the open vent lines 12 , 14 are open at least partially in the gas space 38 above the fuel level 40 . During operation of the vehicle, however, static or dynamic operating states occur, in which, as illustrated in FIG. 2 , one of the inlet openings 16 , 18 is situated below the fuel level. The line routing ensures, however, that at least part of the line 12 , 14 from this inlet opening to the liquid separator 20 lies above the liquid level 40 (formation of a siphon) in at least a wide range of and preferably substantially all orientations, attitudes, or inclinations of the fuel tank, with the result that a relatively large amount of fuel cannot flow through the respective line 12 , 14 into the separator 20 . In such a case, the venting function is ensured by the other vent line which has its inlet opening above the level of liquid fuel in the fuel tank.

If an excess pressure does not prevail in the tank and the inlet openings 16 , 18 are normally situated above the liquid level, the vapor is sucked or drawn via the jet pump, which is arranged on the outlet side of the separating tank, and recycled into the tank. This corresponds to the situation as known from prior art, for example in the case of a saddle tank construction. Although fuel does not foam up to a great extent, it is nevertheless ensured that the fuel pump does not suck up any air.

Although liquid fuel can pass via the lines 12 , 14 into the separator 20 , it collects there in its lower region and is removed from there by the jet pump 30 while a gas space is formed above the liquid level in an upper region of the separator 20 . An arrangement of baffle plates 42 ( FIG. 3 ) is provided upstream of the vent line 22 and ensures that liquid cannot enter into the vent line 22 even during sloshing movements.

In the event of the vehicle overturning, an upside-down position of the fuel tank and other components may occur. In this case, even the baffle plate arrangement 42 cannot prevent liquid fuel from entering into the line 22 and the vapor canister 34 . It then has to be ensured in another manner that liquid fuel does not pass to the outside. In order to prevent the liquid from escaping to the outside, the solenoid valve 36 at the outlet of the vapor canister is activated by a position sensor arranged on the vehicle.

As an alternative, relatively large quantities of fuel can also be prevented from running out by use of a suitable routing of the line 22 in the tank 10 by providing the line 22 with a siphon in the form of a loop 44 (shown in dashed line in FIG. 2 ) guided to the bottom of the tank.

The venting of the tank 10 as it is being filled can be realized in two ways. Firstly, a vent line (not illustrated) from or on the tank filler neck can protrude into the tank. As soon as the vent line is flooded by the rising liquid level, the fuel fill nozzle is shut off. Secondly, legal regulations may make it necessary to conduct the fuel vapors displaced during filling of the tank through the activated carbon filter. In this case, it can be ensured with the venting system according to the invention that the fuel level does not reach the open inlet openings 16 , 18 of the vent lines 12 , 14 . In order to achieve this, a signal of a filling-level transmitter arranged in the tank 10 is used to establish when the desired level is reached. The signal tapped off from the filling-level transmitter is used for actuating the solenoid valve 36 at the outlet of the vapor canister filter 34 . When the valve 36 is closed, a counterpressure builds up in the tank 10 resulting in the fuel nozzle being shut off and therefore ending the filling process.

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Claims as granted

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Classifications

10 codes
IPC · International Patent Classification
Section B — Performing operations; transporting
  • B60K15/077
  • B65D90/34
  • B60K15/035
Section F — Mechanical engineering; lighting; heating; weapons
  • F02M25/08
  • F02M37/20
  • F02M37/00
  • F02M37/18
USPC · US Patent Classification
123/516123/519137/565.34

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File wrapper

⤢ drag to zoomJan 2003Jul 2003Jan 2004Jul 2004Jan 2005Jul 2005Jan 2006USPTOApplicantNon-final rejectionResponse after non-finalNotice of allowance
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Pendency
2.7 y
987 days filing → grant
Office actions
1
non-final + final
Responses
1
no RCE
Examiner
Carl S. Miller
art unit 3747 · TC 3700
Citations: 13 back · 6 forward

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