Fuel vapor emission control system employing vacuum

Information

  • Patent Grant
  • 6418915
  • Patent Number
    6,418,915
  • Date Filed
    Saturday, August 5, 2000
    24 years ago
  • Date Issued
    Tuesday, July 16, 2002
    22 years ago
Abstract
A fuel system and a method for refueling a fuel tank within the fuel system both employ a fuel tank having contained therein a fuel vapor, where the fuel tank also has a refueling detection device which is activated incident to refueling the fuel tank with a liquid fuel. The fuel system and the method for refueling the fuel tank also employ a fuel vapor valve which is activated by the refueling detection device, wherein: (1) the fuel vapor valve directs the fuel vapor from the fuel tank to a first fuel vapor conduit connected to a fuel vapor absorption device when the refueling detection device is activated; and (2) the fuel vapor valve directs the fuel vapor from the fuel tank to a second fuel vapor conduit connected to an engine which is powered by the liquid fuel when the refueling detection device is not activated.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates generally to fuel vapor emission control for fuel systems in vehicles with internal combustion engines. More particularly, the present invention relates to fuel tank fuel vapor emission control in such vehicles.




2. Description of the Related Art




Modern transportation vehicles which employ a liquid fuel for internal combustion engines conventionally also employ for storage of the liquid fuel a fuel tank. Similarly, since most liquid fuels are highly volatile, such a fuel tank typically contains in addition to the liquid fuel a fuel vapor. A concentration of fuel in the fuel vapor within the fuel tank is generally related to the temperature of the liquid fuel and the temperature of the fuel vapor.




While the fuel vapor within a fuel tank does not typically impair operation of a transportation vehicle powered by an engine which employs a liquid fuel extracted from the fuel tank, upon refueling of the fuel tank with additional liquid fuel the fuel vapor must of necessity be displaced. For environmental protection purposes and for economic reasons, it is desirable for such displaced fuel vapor not to be released into the atmosphere.




Various apparatus, systems and methods have been disclosed within the art of fuel system design for attenuating, upon refueling of a fuel tank, release of fuel vapor into the atmosphere. Well known in this regard are fuel system designs which incorporate the use of carbon filled canisters for cyclical absorptive capture and desorptive controlled release of fuel vapor displaced incident to refueling of a fuel tank. Examples of such fuel system designs are disclosed within U.S. Pat. No. 3,937,198, U.S. Pat. No. 5,456,238, U.S. Pat. No. 5,617,832 and Japan No. 4-124,449, all of which are incorporated herein fully by reference.




While any of the disclosed fuel system designs provides upon refueling of a fuel tank and during operation of the vehicle between refueling with a liquid fuel an attenuated displaced fuel vapor release into the atmosphere, such desirable result is often achieved only with complicated piping and valving schemes. In addition, carbon canisters have limited capacity for attenuating vapor release between refuelings.




There thus exists within the art of fuel tank design and fuel system design a continuing need for comparatively simple apparatus, systems and methods for attenuating release of a displaced or evolved fuel vapor into the atmosphere. It is towards that object that the present invention is directed.




SUMMARY OF THE INVENTION




In order to realize the object towards which the present invention is directed, the present invention provides in the first instance a fuel system comprising a fuel tank within which is contained a fuel vapor. The fuel tank is also fabricated to have a refueling detection means which is activated incident to refueling the fuel tank with a liquid fuel. The fuel system also has a fuel vapor valve which is activated by the refueling detection means, wherein: (1) the fuel vapor valve directs the fuel vapor displaced from the fuel tank to a first fuel vapor conduit connected to a fuel vapor absorption means when the refueling detection means is activated; and (2) the fuel vapor valve directs the fuel vapor from the fuel tank to a second fuel vapor conduit connected to an engine which is powered by the liquid fuel when the refueling detection means is not activated. Within the present invention, the second fuel vapor conduit does not incorporate a fuel vapor absorption means, in particular as interposed between the fuel vapor valve and the engine.











BRIEF DESCRIPTION OF THE DRAWINGS




The objects, features and advantages of the present invention are understood within the context of the Description of the Preferred Embodiment, as set forth below. The Description of the Preferred Embodiment is understood within the context of the accompanying drawing, which forms a material part of this disclosure, wherein:





FIG. 1

shows a schematic diagram of a fuel system fabricated in accord with a preferred embodiment of the invention.











DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring now to

FIG. 1

, there is shown a schematic diagram of a fuel system fabricated in accord with a preferred embodiment of the present invention.




Shown in

FIG. 1

is a fuel tank


10


having formed integral thereto, as illustrated within a phantom outline which includes a portion of the fuel tank


10


, a fuel filler pipe


11


. Also shown within

FIG. 1

contained within the fuel tank


10


is a liquid fuel


12




a


and a fuel vapor


12




b


. Similarly, there is also shown in

FIG. 1

connected to the top of the fuel tank


10


a vacuum release valve


14


. Finally, there is also shown within

FIG. 1

, and also connected to the top of the fuel tank


10


, a fuel vapor vent conduit


16


intended to convey upon refueling of the fuel tank


10


with an additional quantity of a liquid fuel, such as the liquid fuel


12




a


, the fuel vapor


12




b


from the fuel tank


10


to a fuel vapor valve


18


.




Within the preferred embodiment of the present invention with respect to the fuel vapor valve


18


, the fuel vapor valve


18


upon actuation with an actuator


20


which is connected to the fuel vapor valve


18


provides an option of directing the fuel vapor


12




b


from the fuel tank


10


through either: (1) a second fuel vapor conduit


22


which leads directly to a mass flow monitor/controller


32


which is connected to an intake manifold


34


which in turn is connected to an engine


36


which is otherwise fueled with the liquid fuel


12




a


when extracted from the fuel tank


10


, or in the alternative; (2) a first fuel vapor conduit


24


which has a bifurcated connection leading to either: (a) a fuel vapor absorption canister


26


which in turn has connected thereto a cutoff valve


28


; or (b) a throttle/cutoff valve


30


which may be employed for impeding or eliminating flow of the fuel vapor


12




b


through the second fuel vapor conduit


24


prior to reaching the mass flow monitor/controller


32


which is connected to the intake manifold


34


which in turn is connected to the engine


36


.




While

FIG. 1

illustrates in static format a schematic diagram of a fuel system in accord with the preferred embodiment of the present invention, it is also significant to describe within the context of the present invention and the preferred embodiment of the present invention the dynamics of operation of the fuel system of the preferred embodiment of the present invention, as illustrated within the schematic diagram of FIG.


1


. To assist in that goal, there is also illustrated within the schematic diagram of

FIG. 1

several phantom lines which assist in illustrating operation of the fuel system of the preferred embodiment of the present invention.




In that regard, there is shown in

FIG. 1

, in a first instance, and in phantom, a rectangular enclosure which includes the fuel filler pipe


11


of the fuel tank


10


. Although not specifically illustrated within the schematic diagram of

FIG. 1

, the rectangular enclosure which includes the fuel filler pipe


11


of the fuel tank


10


is intended to indicate that there exists a refilling detection means which is activated incident to an event which is related to refueling of the fuel tank


10


with an additional quantity of a liquid fuel, such as the liquid fuel


12




a


. The refueling detection means may comprise, but is not limited to, a switch or a sensor as is otherwise generally conventional in the art of fuel system fabrication. The particular refueling event which may be employed to trigger the refueling detection means may be selected from the group including but not limited to a fuel filler door opening refueling event, a fuel filler pipe cap removal refueling event or an actual physical introduction of the additional quantity of the liquid fuel into the fuel tank


10


as a refueling event. Within the present invention and the preferred embodiment of the present invention, the refueling detection means actuates the actuator


20


and the fuel vapor valve


18


independent of whether the engine


36


is operating.




Although not specifically completely illustrated within the schematic diagram of

FIG. 1

, upon actuation of the refueling detection means, the actuator


20


actuates the fuel vapor valve


18


in a fashion such that the fuel vapor


12




b


which upon refueling is displaced from the fuel tank


10


is directed into the first fuel vapor conduit


24


. Similarly, the refueling detection means also actuates the throttle/cutoff valve


30


to a completely closed position such that all of the fuel vapor


12




b


displaced from the fuel tank


10


upon refueling of the fuel tank


10


is directed through the fuel vapor absorption canister


26


, which is typically and preferably filled with a carbon absorbent material, although other organic and inorganic absorbent materials may also be employed within the fuel vapor absorption canister


26


. Finally, during periods of refueling, the refueling detection means also assures that the cutoff valve


28


which is connected to the fuel vapor absorption canister


26


is open, such that a purge of the fuel vapor


12




b


through the fuel vapor absorption canister


26


may be fully and completely effected.




In contrast, under circumstances where the engine


36


is operating and the fuel tank


10


is not being refueled, a secondary set of controls, which derives in part from the mass flow monitor/controller


32


, controls various of the valves as illustrated within the fuel system whose schematic diagram is illustrated in FIG.


1


. In that regard, the mass flow monitor/controller


32


provides control over: (1) the fuel vapor valve


18


which is relocated to a position which connects the fuel vapor vent conduit


16


with the second fuel vapor conduit


22


(or in the adjunct or alternative over an additional fuel vapor valve disposed within the second fuel vapor conduit


22


downstream of the fuel vapor valve


18


); and (2) the throttle/cutoff valve


30


, such that an appropriate amount of fuel vapor


12




b


is introduced into the intake manifold


34


from purging of each of the fuel tank


10


and the fuel vapor absorption canister


26


. Thus, it is generally intended within the present invention and the preferred embodiment of the present invention that under circumstances other than refueling of the fuel tank


10


, and when the engine


36


is operating, that the fuel tank


10


is maintained at a negative pressure which draws fuel vapor


12




b


from the fuel tank


10


into the intake manifold


34


. Similarly, it is also generally intended within the present invention and the preferred embodiment of the present invention that the fuel vapor absorption canister


26


not breathe with respect to the fuel tank, but rather only capture displaced fuel vapor


12




b


when the fuel tank


10


is refueled and desorb such captured displaced fuel vapor


12




b


to the engine


36


when the engine


36


is operating and the fuel tank


10


is not being refueled. Finally, the mass flow monitor/controller


32


also assures that the cutoff valve


28


is completely open when the engine


36


is operating in order to assure for complete and effective purging of absorbed fuel vapor


12




b


from the fuel vapor absorption canister


26


.




Finally, under circumstances when the engine


36


is not operating and thus neither liquid fuel


12




a


nor the fuel vapor


12




b


is being consumed, and further when the fuel tank


10


is not being refueled: (1) the cutoff valve


28


to the fuel vapor absorption canister


26


is closed; and (2) the fuel vapor valve


18


is actuated to a neutral position which seals the fuel vapor vent conduit


16


, thus providing, at least initially, the fuel tank


10


at a negative pressure. The pressure of the fuel vapor


12




b


within the fuel tank


10


will then be controlled at a lower level by the vacuum release valve


14


(which is typically fabricated to provide a vacuum release at about 5.0 pounds per square inch within the fuel tank


10


. Similarly, the pressure of the fuel vapor


12




b


within the fuel tank


10


will than be controlled at an upper level by a diurnal temperature variation or other unexpected temperature excursion of the liquid fuel


12




a


and the fuel vapor


12




b


within the fuel tank. Within the context of most foreseeable temperature excursions, it is expected that the upper level of fuel vapor


12




b


pressure within the fuel tank


10


is unlikely to exceed about 3.5 pounds per square inch.




Upon fabrication of a fuel system in accord with the fuel system whose schematic diagram is illustrated in

FIG. 1

, there is provided a fuel system of comparatively simple design which further provides for attenuated release into the atmosphere of a fuel vapor when refueling with a liquid fuel a fuel tank which comprises a portion of the fuel system.




As is understood by a person skilled in the art, the preferred embodiment of the present invention is illustrative of the present invention rather than limiting of the present invention. Revisions and modifications may be made to methods, materials, structure and dimensions through which is fabricated a fuel system in accord with the preferred embodiment of the present invention, while still fabricating a fuel system in accord with the present invention, further in accord with the appended claims.



Claims
  • 1. A fuel system comprising:a fuel tank having contained therein a fuel vapor, the fuel tank also having a refueling detection means which is activated incident to refueling the fuel tank with a liquid fuel; a fuel vapor valve which is activated by the refueling detection means, wherein: the fuel vapor valve directs the fuel vapor from the fuel tank to a first fuel vapor conduit connected to a fuel vapor absorption means when the refueling detection means is activated; and the fuel vapor valve directs the fuel vapor from the fuel tank to a second fuel vapor conduit not connected to a fuel vapor absorption means, but connected to an engine which is powered by the liquid fuel, when the refueling detection means is not activated.
  • 2. The fuel system of claim 1 wherein the refueling detection means is triggered by a refueling event selected from the group consisting of a fuel filler door opening refueling event, a fuel cap removal refueling event and introduction of the liquid fuel into the fuel tank as a refueling event.
  • 3. The fuel system of claim 1 wherein the fuel tank is maintained under a vacuum from the engine when the engine is operating and the fuel tank is not being refueled.
  • 4. A method for refueling a fuel tank comprising:providing a fuel tank having contained therein a fuel vapor, the fuel tank also having a refueling detection means which is activated incident to refueling the fuel tank with a liquid fuel; activating by means of the refueling detection means a fuel vapor valve, wherein: the fuel vapor valve directs the fuel vapor from the fuel tank to a first fuel vapor conduit connected to a fuel vapor absorption means when the refueling detection means is activated; and the fuel vapor valve directs the fuel vapor from the fuel tank to a second fuel vapor conduit not connected to a fuel vapor absorption means, but connected to an engine which is powered by the liquid fuel, when the refueling detection means is not activated.
  • 5. The method of claim 4 wherein the refueling detection means is triggered by a refueling event selected from the group consisting of a fuel filler door opening refueling event, a fuel cap removal refueling event and introduction of the liquid fuel into the fuel tank as a refueling event.
  • 6. The method of claim 4 wherein the fuel tank is maintained under a vacuum from the engine when the engine is operating and the fuel tank is not being refueled.
US Referenced Citations (14)
Number Name Date Kind
3937198 Sudhir Feb 1976 A
5174265 Sekine Dec 1992 A
5220898 Kidokoro et al. Jun 1993 A
5235955 Osaki Aug 1993 A
5441031 Kiyomiya et al. Aug 1995 A
5456238 Horiuchi et al. Oct 1995 A
5603349 Harris Feb 1997 A
5617832 Yamazaki et al. Apr 1997 A
5809976 Cook et al. Sep 1998 A
5878727 Huls Mar 1999 A
6029635 Sekine et al. Feb 2000 A
6158270 Garman et al. Dec 2000 A
6167920 Enge Jan 2001 B1
6260544 Spry et al. Jul 2001 B1
Foreign Referenced Citations (1)
Number Date Country
4-124449 Apr 1992 JP