Device and Method for Discharging Fuel Vapor From a Fuel Supply System for an Internal Combustion Engine

Abstract

A device for discharging fuel vapor from a fuel supply system for an internal combustion engine has a container which is situated in the fuel supply system and contains liquid fuel under an upwardly limited pressure. A discharge line, which leads to a tank venting system, leads out of the container. The device also has a detector for detecting vaporous fuel in the container and a blocking device which is coupled to the detector and with which the discharge line can be opened or blocked depending on the detection. A method for discharging fuel vapor from a fuel supply system for an internal combustion engine continuously detects whether vaporous fuel is also present in the container which is situated in the fuel supply system and contains the liquid fuel under an upwardly limited pressure; opens the discharge line if the vaporous fuel has been detected and blocks the discharge line if no vaporous fuel has been detected; and discharges the vaporous fuel through the opened discharge line while retaining the liquid fuel.

Claims

1.-17. (canceled)

18. A device for discharging fuel vapor from a fuel supply system for an internal combustion engine, comprising: a container which is arranged in the fuel supply system and in which liquid fuel under an upwardly limited pressure is located; a discharge line which leads out of the container; a detector for detecting vaporous fuel in the container; and a blocking device which is coupled to the detector and by which the discharge line is released or blocked depending on the detection.

19. The device according to claim 18, wherein the discharge line leads to a tank ventilation system.

20. The device according to claim 18, wherein the blocking device is configured to keep the discharge line closed and releases the discharge line only when vaporous fuel is detected in the container.

21. The device according to claim 18, wherein the detector is a gas sensor.

22. The device according to claim 18, wherein the detector forms a structural unit with the blocking device.

23. The device according to claim 18, wherein the detector and the blocking device are constructed as a single component.

24. The device according to claim 18, wherein the blocking device comprises a controllable valve.

25. The device according to claim 24, wherein the controllable valve is a blocking valve.

26. The device according to claim 18, wherein the blocking device is electrically coupled to the detector.

27. The device according to claim 18, wherein the blocking device is mechanically coupled to the detector.

28. The device according to claim 18, wherein the discharge line leads out of the container at a top with respect to an installation position.

29. The device according to claim 28, wherein the blocking device and the detector are formed by a float in the container, a density of the float being less than that of the liquid fuel and greater than that of the vaporous fuel.

30. The device according to claim 29, wherein a shape of the float is adapted to a shape of a transition region between an upper end of the container and the discharge line such that, when the float is pressed onto the transition region, the discharge line is sealed.

31. The device according to claim 30, wherein the float is substantially spherical and the transition region tapers conically.

32. The device according to claim 31, wherein the transition region is substantially in the form of a hollow truncated cone and an angle between a covering face and a center axis of the truncated cone is in a range below 90°.

33. The device according to claim 31, wherein the angle is approximately 88°.

34. The device according to claim 30, further comprising: a non-return valve fitted in the discharge line and configured such that the pressure in the discharge line upstream in a throughflow direction of the non-return valve cannot press on the float.

35. A method for discharging fuel vapor from a fuel supply system, comprising: continuously detecting whether vaporous fuel is present in a container which is arranged in the fuel supply system and in which liquid fuel under an upwardly limited pressure is located; releasing a discharge line when vaporous fuel has been detected and blocking the discharge line when no vaporous fuel has been detected; and discharging vaporous fuel through the released discharge line whilst liquid fuel is retained.

36. The method according to claim 35, wherein the vaporous fuel is discharged to a tank ventilation system where the vaporous fuel accumulates and is supplied to an internal combustion engine for combustion.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0027] FIG. 1 is a schematic illustration of an exemplary device according to the invention for discharging fuel vapor from a fuel supply system.

[0028] FIG. 2 is a schematic sectioned view of a mechanical embodiment of the device according to the invention in a first operating state.

[0029] FIG. 3 shows the device from FIG. 2 in a second operating state.

DETAILED DESCRIPTION OF THE DRAWINGS

[0030] FIG. 1 shows the basic functional structure of a device 10 for discharging fuel vapor from a fuel supply system for an internal combustion engine of a motor vehicle. At a suitable location in the fuel supply system, in particular in or upstream of a high-pressure pump, a discharge line 16 leads out of a container 12 in which liquid fuel 14 under an upwardly limited pressure (in the order of magnitude of approximately 6 bar (relative)) is located. The discharge line 16 leads to a tank ventilation system by means of which a fuel container, in particular the tank of the motor vehicle, can be aerated and ventilated.

[0031] The discharge line 16 can be automatically released or blocked. To this end, a valve device having a blocking device 18 and a detector 20 which is coupled thereto is provided. The detector 20 is capable of recognizing whether—apart from the liquid fuel 14—vaporous fuel is also located in the container 12. The blocking device 18 keeps the discharge line 16 closed in principle. However, as soon as the detector 20 identifies the presence of fuel vapor in the container 12, the detector 20 controls the blocking device 18 in such a manner that it releases the discharge line 16. In this instance, the fuel vapor escapes via the discharge line 16 to the tank ventilation system. To this end, the discharge line 16 must be configured in such a manner that the fuel vapor which is produced preferably accumulates in the discharge line 16. For example, the discharge line 16 may be arranged geodetically higher than the container 12.

[0032] If no further fuel vapor is identified by the detector 20, the blocking device 18 closes the discharge line 16 again so that ideally no liquid fuel 14 reaches the discharge line 16.

[0033] The fuel vapor which has escaped via the discharge line 16 is accumulated in the tank ventilation system and then supplied to the internal combustion engine for combustion at the next start-up.

[0034] The detector 20 may be an independent sensor or may form a structural unit together with the blocking device 18. The detector 20 and the blocking device 18 may also be constructed as a single component, as in the embodiment which is described below and which is shown in FIGS. 2 and 3.

[0035] The blocking device 18 may comprise a valve, in particular a blocking valve. The coupling between the detector 20 and the blocking device 18 may in particular be configured in an electrical or purely mechanical manner. In the first instance, the blocking device 18 is preferably an electrically controllable blocking valve.

[0036] Ultimately, the device 10 enables fuel vapor to be discharged from the fuel supply system to the tank ventilation system, with liquid fuel 14 being retained.

[0037] FIGS. 2 and 3 illustrate a particularly simple, purely mechanical embodiment of the device 10 for discharging fuel vapor from the fuel supply system. With respect to the installation position, the discharge line 16 is guided upward out of the container 12. The transition region 22 between the upper end of the container 12 and the discharge line 16 is substantially in the form of a hollow truncated cone.

[0038] Inside the container 12 there is a float 24, the density of which is lower than that of the liquid fuel 14. For the float 24, for example, a material having a density of 650 kg/m.sup.3 or lower can be selected since the density of commercially available fuels is greater than this value.

[0039] The shape of the float 24 is adapted to the shape of the transition region 22 between the upper end of the container 12 and the discharge line 16 in such a manner that the float 24, when it is pressed upward, ideally completely seals the discharge line 16.

[0040] In the embodiment illustrated, the angle between the covering face and the center axis of the truncated cone is approximately 30°. The float 24 is a sphere whose diameter is selected in such a manner that there is a circumferential contact with the inner side of the transition region 22 when the float 24 is pressed upward.

[0041] The operating method of this embodiment is explained below. If in the fuel supply system, more specifically in the container 12, only liquid fuel 14 and no fuel vapor is present, the liquid fuel 14 which is under an upwardly limited pressure presses the float 24 upward against the inner wall of the conical transition region 22 and seals it. This situation is illustrated in FIG. 2. In this state, the discharge line 16 is blocked so that no liquid fuel 14 can escape from the fuel supply system.

[0042] If fuel vapor 26 is located in the container 12, however, it rises upward as a result of its substantially lower density so that the liquid level drops, as shown in FIG. 3. The float 24 then also sinks downward and is no longer pressed against the inner wall of the conical transition region 22. The discharge line 16 is consequently no longer sealed and the fuel vapor 26 can escape into the discharge line 16 and be discharged into the tank ventilation system.

[0043] When the fuel vapor 26 escapes, the liquid level in the container 12 rises again until the fuel vapor 26 is completely discharged and the liquid fuel 14 presses the float 24 upward again so that the discharge line 16 is sealed again and consequently blocked.

[0044] With regard to the general schematic depiction of FIG. 1, in the embodiment shown in FIGS. 2 and 3 the float 24 constitutes the detector 20 and at the same time also the blocking device 18. The float 24 therefore performs a dual function in this instance.

[0045] In order to prevent the pressure in the discharge line 16 from being able to press on the float 24, there may be fitted in the discharge line 16 a correspondingly configured non-return valve, which accordingly limits the pressure in the discharge line 16 in an upstream direction in the throughflow direction of the non-return valve.

[0046] In order to remove the fuel vapor 26 from the fuel supply system as effectively as possible, the container 12, more specifically the upper end thereof, is intended to be arranged at an upper, ideally at the geodetically highest, location of the high-pressure pump or the fuel supply system.

LIST OF REFERENCE NUMERALS

[0047] 10 Discharge device [0048] 12 Container [0049] 14 Liquid fuel [0050] 16 Discharge line [0051] 18 Blocking device [0052] 20 Detector [0053] 22 Transition region [0054] 24 Float [0055] 26 Fuel vapor