FUEL CONTAINER ASSEMBLY

Abstract

An assembly for stored containment of fuel including a high-strength, impact resistant container having a hermetically sealed, fuel containing chamber and a nozzle operatively connected in fluid communication with the chamber. The nozzle includes a conduit disposed in fluid communication with the chamber and a sleeve movable relative to the conduit, between an inward retracted position and an outwardly extended position. The conduit at least partially defines a liquid flow path out of the chamber and a gaseous flow path into the chamber is disposed between the conduit and the sleeve. A seal assembly is mounted on the sleeve and movable therewith relative to the conduit to define a first opening of the liquid flow path and a subsequent opening of the gaseous flow path, both into fluid communication with and between the chamber and an exterior of the nozzle.

Claims

1. An assembly for stored containment of fuel, said assembly comprising: a container including a chamber, structured for fuel containment, on the interior thereof, a nozzle structured for operative connection to said container in fluid communication with said chamber, said nozzle comprising first and second flow channels each operatively disposed in fluid communication with said chamber and successively disposed in open fluid communicating relation between said chamber and an exterior of said nozzle, concurrent to said operative connection of said nozzle, said first flow channel defining a path of liquid flow out of said chamber and said second flow channel defining a path of gaseous flow into said chamber, said nozzle comprising a primary conduit at least partially defining said first flow channel and an outer sleeve movable between an outwardly extended position and an inwardly retracted position; and said outer sleeve movably disposed in surrounding, telescopic relation to a length of said conduit and said second flow path disposed between said primary conduit and said outer sleeve.

2. The assembly as recited in claim 1 further comprising a cover fixedly connected to said nozzle in surrounding telescopic relation to at least a portion of said outer sleeve, at least concurrent to said retracted position.

3. The assembly as recited in claim 2 wherein said cover is disposed in interruptive, movement restricting engagement with said outer sleeve, concurrent to said inwardly retracted position.

4. The assembly as recited in claim 2 wherein said nozzle comprises a biasing structure disposed to normally bias said sleeve in said outer extended position; said cover fixedly disposed in overlying, protective relation to said biasing structure, concurrent to said outwardly extended and inwardly retracted positions of said sleeve.

5. The assembly as recited in claim 1 further comprising a pocket mounted on said container within said chamber and including a dry interior disposed in segregated relation to fluid within said chamber; said dry interior cooperatively dimensioned and configured with said nozzle for retained storage thereof.

6. An assembly as recited in claim 1 wherein said chamber includes a liquid fuel and an inert gas collectively retained within a substantial entirety of said chamber.

7. An assembly as recited in claim 1 wherein said container is structured to define said chamber being hermetically sealed, relative to an exterior of said container, at least prior to said operative connection of said nozzle.

8. An assembly as recited in claim 1 further comprising a seal assembly mounted on said sleeve and movable therewith between said outwardly extended and inwardly retracted positions; said seal assembly comprising a plurality of seal structures disposed in fluid sealing relation between said sleeve and an exterior of said conduit, at least concurrent to said outwardly extended position.

9. An assembly as recited in claim 8 wherein said plurality of seal structures are cooperatively disposed relative, to said conduit, to at least partially define said successive disposition of said first and second flow channels in said open fluid communication between said chamber and an exterior of said nozzle.

10. An assembly as recited in claim 8 wherein an exterior of said conduit is dimensioned and configured to establish a non-sealing relation of said plurality of seal structures with said conduit, concurrent to said sleeve being in said inwardly retracted position.

11. An assembly as recited in claim 8 wherein an exterior of said conduit comprises a plurality of release segments, each dimensioned and configured to establish a non-sealing relation to correspondingly positioned ones of said plurality of seal structures, one of said plurality of seal structures movable with said sleeve into aligned, non-sealing relation to a first of said release segments to define a disposition of said first flow channel in open fluid communication between said chamber and an exterior of said nozzle.

12. An assembly as recited in claim 11 wherein one other of said plurality of seal structures movable with said sleeve into aligned, non-sealing relation to a second of said release segments to define a disposition of said second flow channel in open fluid communication between said chamber and an exterior of said nozzle.

13. An assembly as recited in claim 12 wherein said one other seal structure is disposed relative to said second release segment to establish said disposition of said second flow channel in said open fluid communication between said chamber and said exterior said nozzle, subsequent to said disposition of first flow channel in said open fluid communication between said chamber and an exterior of said nozzle.

14. An assembly as recited in claim 1 further comprising a valve structure disposed in interconnecting relation between said nozzle and said container, said valve structure selectively disposed between a closed orientation and an open orientation; said open orientation at least partially defining said operative connection of said nozzle to said container, in fluid communication with said chamber.

15. An assembly as recited in claim 14 wherein said valve structure comprises a first flow channel segment and a second flow channel segment; said open orientation comprising said first and second flow channel segments concurrently disposed in aligned, interconnecting fluid communication between said chamber and said first and second flow channels within said nozzle.

16. An assembly as recited in claim 15 wherein said valve structure is rotationally connected to said container concurrent to attachment thereof to said nozzle; said valve structure movable relative to said container between a predetermined angle of rotation to define disposition thereof into an out of said open orientation.

17. An assembly as recited in claim 1 further comprising a handle mounted on one end of said container and a cover disposed on an opposite end of said container; said cover of one container configured to removably receive said handle of one other of said containers therein, concurrent to an axially stacked array of at said one container and said one other container.

18. An assembly as recited in claim 1 further comprising a static charge inhibitor assembly including a conductive cord disposable in conductive connection between said container and a fuel receiving receptacle; a retractable reel housing said conductive cord; said cord movable on said retractable reel into an out of said conductive connection with the fuel receiving receptacle.

19. An assembly as recited in claim 18 further comprising a magnetic mount member connected to said cord and operative to magnetically connect said cord to said fuel receptacle.

20. An assembly for stored containment of fuel, said assembly comprising: a container including a hollow interior defining a chamber for fuel containment, said container formed of a high-strength metallic material assembled to define a hermetic sealing of said chamber, a nozzle operably connected to said container in fluid communication with said chamber, said nozzle comprising a conduit disposed in fluid communication with said chamber and the sleeve movable relative to said conduit between an inwardly retracted position and an outwardly extended position; said sleeve disposed in telescopically surrounding relation to said conduit, said conduit at least partially defining a liquid flow path out of said chamber; a gaseous flow path into said chamber disposed between said conduit and said sleeve, a seal assembly mounted on said sleeve and movable therewith, between said inward retracted position and said outwardly extended position, and said plurality of seal structures cooperatively disposed relative to said conduit to define a first opening of said liquid flow path and the subsequent opening of said gaseous flow path in fluid communication with and between said chamber and an exterior of said nozzle.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0027] For a fuller understanding of the nature of the present invention, reference should be had to the following detailed description taken in connection with the accompanying drawings in which:

[0028] FIG. 1 is a perspective view of the fuel container assembly of the present invention in use.

[0029] FIG. 2 is a's perspective view of a container of the fuel container assembly the present invention.

[0030] FIG. 3A is a longitudinal sectional view in schematic form of the embodiment of Figures 1 and 2.

[0031] FIG. 3B is a schematic representation of a nozzle assembly associated with the fuel container assembly of the present invention.

[0032] FIG. 4 is a longitudinal sectional view of the embodiment of FIGS. 3A and 3B in assembled form.

[0033] FIG. 5 is a bottom perspective view of the embodiment of FIG. 2.

[0034] FIG. 6A is a front perspective view in partial cutaway of the embodiment of FIGS. 1-5 in assembled form with a valve structure.

[0035] FIG. 6B is a perspective view of a cover for the discharge end of the container as represented in FIG. 6A.

[0036] FIG. 7A is a perspective view of a plurality of fuel containers arranged in a co-axially oriented stacked array.

[0037] FIG. 7B is a perspective view of a plurality of fuel containers positioned to be positioned in the stacked array as represented in FIG. 7A.

[0038] FIGS. 8A-8D are schematic representations representing successively performed operative features of one embodiment of the nozzle of the present invention.

[0039] FIG. 9A-9E are perspective views in partial cutaway of a valve structure operatively associated with at least one embodiment of the fuel container structure of the present invention.

[0040] FIG. 10 is a sectional view in partial cutaway of the valve structure of FIGS. 9A-9E in operation and partially assembled form.

[0041] FIGS. 11A-11D are sectional views in schematic form representing successive steps of operation of the nozzle and valve structure defining an operative connection of the nozzle to the container via the valve structure.

[0042] FIG. 12 is an elevation view in partial cutaway and schematic form representing utilization of the fuel container assembly of the present invention.

[0043] FIG. 13A is a top perspective view of a static charge inhibiting assembly utilized while refueling.

[0044] FIG. 13B is a bottom perspective view of the embodiment of FIG. 13A

[0045] Like reference numerals refer to like parts throughout the several views of the drawings.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

[0046] The invention will now be described more fully hereinafter with reference to the accompanying drawings in which illustrative embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.

[0047] With initial reference to at least FIGS. 1-6, the present invention is directed to a fuel container assembly, generally indicated as 10, structured to safely store fuel 200 including, but not limited to, gasoline for a relatively prolonged period of time in a manner which does not provide danger to property or individuals. Moreover, the versatility of the fuel container assembly 10 of the present invention facilitates the storage and transportation of fuel 200 in various types of motor vehicle 100 thereby facilitating the at least partial refueling of the vehicle 100 such as when the original fuel supply has been exhausted.

[0048] The structural and operative features of the fuel container assembly 10 accomplish safe storage and dispensing due, at least in part, to the structural and operative features of the various components of the fuel container assembly 10. It is to be noted that one primary feature of the fuel container assembly 10 is the ability to prolong the storage of fuel and safely facilitate its transportation in a vehicle 100 until dispensing of the stored fuel is required or desired. Such safety features associated with the fuel supply assembly 10, during prolonged storage and transportation in a vehicle, include the elimination of vapors, odors, etc. escaping from the stored fuel into surrounding or adjacent areas.

[0049] For purposes of clarity, it is emphasized that the fuel container assembly 10 can be utilized to dispense fuel in a variety of practical applications other than to vehicles 100. Accordingly, the term “fuel receiving receptacle” is meant to include different types of motor vehicles, including passenger and commercial vehicles, as at 100, or different internal combustion (IC) motor powered devices, other than motor vehicles which may require the replenishment of fuel.

[0050] The elimination of vapor/odor escape is accomplished, at least in part, by the structuring and assembling of a container 12 of the fuel container assembly 10, in a manner which hermetically seals an interior fuel containing chamber 14 of the container 12, thereby eliminating or significantly restricting the possibility of vapor or odor escape. Also, the fuel container assembly 10 of the present invention is structured to eliminate or at least significantly restrict dangers from explosion or leakage of the contained fuel 200, during an emergency event of the vehicle 100, such as the occurrence of an accident, crash, collision, etc. As also represented in FIG. 6A, a substantially inert atmosphere is established and maintained within the chamber 14 by adding an inert gas such as, but not limited to, nitrogen or argon, instead of air/oxygen, into interior of the chamber 14. This serves to reduce the gasoline or other fuel vapors out of the flammable range. Therefore, this feature protects against the remote possibility of self-ignition by sudden gas compression, such as may occur because of deformation of the container 12 in a crash, collision, etc. of the vehicle in which the container 10 is stored.

[0051] Further, the procedure of dispensing the stored fuel 200 from the container 12 into a vehicle or other fuel receiving receptacle 100 is also rendered safer to the individual doing the dispensing as well as the environment in general. As described in greater detail hereinafter with primary reference to at least FIGS. 8A-8D, 10 and 11A-11D, the fuel container assembly 10, including a plurality of its operative components, is structured to efficiently dispense the fuel 200 from the interior chamber 14 of the container 12 and concurrently collect vapor or other “gaseous fluid” from the interior of the fuel tank 102 of the vehicle or fuel receiving receptacle 100, being replenished with fuel. It is emphasized that for purposes of clarity and accuracy showing the proper sequence of liquid flow from the interior of the container and vapors or gaseous fluid into the container 12, FIGS. 8A-8D are schematic representations showing the nozzle 40 connected directly to the container 12, absent the valve 70. Similarly, FIG. 10 schematically represents liquid flow out through the valve 70 and vapor or gaseous fluid into and through the valve 70, wherein the nozzle 40 is not represented as being attached thereto. However, the correct and intended operative connection of the nozzle 40 to the container 12 is represented in FIGS. 11A-11D, wherein the nozzle 40 is interconnected to the container 12 in fluid communication with the interior chamber 14, via the valve 70.

[0052] Accordingly, and as set forth above, the fuel container assembly 10 includes the container 12 preferably, but not necessarily, having a cylindrical configuration and including a hollow interior defining a chamber 14 in which fuel 200 may be contained and stored for a substantially prolonged period. Also, the size of the container 12 and the resulting dimensions of the interior chamber 14 may vary dependent, at least in part, on the area of the vehicle or other location in which the container 12 is stored and the quantity of fuel 200 desired to be contained within the interior chamber 14. Further, the container 12 is preferably formed from a high-strength, impact resistant material such as a high-strength metallic material including steel, stainless steel, etc. As noted, the strength of the material from which the container 12 is formed should be sufficiently impact resistant to structurally survive without damage, in case of vehicle emergencies including crash, collision etc. Therefore, the structural parameters of the container 12 and the material from which it is formed should be such as to allow the container 12 to withstand a six-foot, freefall impact test, while filled with liquid.

[0053] As indicated, safety features regarding the prevention of escaping odors, vapors from the interior chamber 14 are facilitated by the structuring and/or assembling of the container 12 in a manner which facilitates the establishment of the chamber 14 being “air tight” or hermetically sealed from the exterior thereof. Such hermetic sealing is also facilitated by structuring any type closure, such as associated with an access opening 16 into the chamber 14, to include effective sealing structure which will maintain the hermetically sealed or air tight condition of the chamber 14 until the closure of the access opening 16 is removed. As you should also be apparent the hermetic sealing of the container is also negated when the chamber 14 is purposely exposed to ambient conditions, such as prior to dispensing the fuel 200 there from. The structuring or assembling of the container 12 to establish and maintain the airtight, hermetically sealed conditions, may include the welding of the metallic/high-strength material or the utilization of other manufacturing/assembling techniques which effectively eliminates the possibility of vapor escape from the chamber through any types of seams, joints, junctions, etc.

[0054] Additional structural and operative features of the container include a handle 18 as represented in at least FIGS. 4, 5 and 7B. The handle 18 preferably includes an elongated rigid material rod or shaft, which in one embodiment is fixedly secured to the bottom or base end 20 of the container 12. In the represented disposition, the handle 18 facilitates the lifting and carrying of the container 12 by an individual in an at least partially inverted orientation. In cooperation therewith, a second or additional gripping structure or handle 22 is mounted on the top or “discharge end” 24 of the container 12. As represented, the additional or top and handle 22 is also formed from a rigid rod like structure having a curved configuration so as to be disposed in at least partially surrounding relation to the top end 24 of the container 12. As represented in FIG. 1, the handles 18 and 22 are cooperatively positioned to facilitate an individual positioning or manipulating the container 12 as the fuel 200 within the chamber 14 is dispensed into the vehicle or other fuel receiving receptacle 200.

[0055] In addition, the top, upper or discharge end 24 of the container 12 may include a cover or closure 26, dimensioned and configured to over lie and cover the valve structure 70 connected to the discharge end 24. Also, the cover or closure 26 may include an apertured grip 26′, facilitating the mounting and removal of the cover 26. The cover 26 is also at least partially structured to accommodate an arrangement of two or more of the containers 12 and 12′, as represented in FIG. 7A and 7B, in a coaxially/vertically stacked array. In such a stacked array, a portion of the cover 26, includes an exposed receiving structure 28 in the form of a recess, groove or other structure which is appropriately configured and dimensioned to at least partially correspond to the configuration and dimension of the handle 18. As result, disposition and maintenance of a plurality of at least two of the containers 12 and 12′ in the aforementioned stacked array of FIG. 7A is facilitated by the handle 18 of container 12′ being removably disposed at least partially within the receiving structure 28 formed in the cover 26 of the lower container 12, as represented in FIG. 7B. It is to be noted that the configuration and dimension of the handle 18 may vary from the elongated rod-like structure as represented. In cooperation therewith, the receiving structure 28 should be at least partially, correspondingly dimensioned and configured to facilitate the removable receipt of the handle 18 of another container therein.

[0056] As represented in FIGS. 3A, 3B, and 4, additional structural features of the container 12 include the provision of a “dry pocket” 30 mounted on the container 12 within an interior of the chamber 14. The pocket includes an interior more specifically defined as a “dry interior” 32 due to the fact that it is segregated from the liquid fuel 200 retained within the interior chamber 14. The pocket 30 and in particular the dry interior 32 are cooperatively dimensioned and configured to removably receive and store a nozzle component 40 of the fuel container assembly 10 therein, schematically represented in FIGS. 3B and 4. As such, the efficiency and space-saving advantage of the cylindrical configuration of the container 12, in terms of being stored in an area of reduced volume, is maintained. This is based on the fact that the storage or mounting of the nozzle 40 is within the interior chamber 14 and not on or within a storage area on its an exterior portion of a container, wherein the exterior of a typical or conventional portable container may have to be reshaped to be larger and/or bulkier. The preferred dry and protected condition of the nozzle 40 when disposed within the interior 32 is further facilitated by a closure 34 and/or locking or retaining structure 34′.

[0057] As indicated, the fuel container assembly 10 of the present invention includes a nozzle 40 structured for operative connection to the container 12, wherein such operative connection may be defined as the nozzle 40 interconnected to the container 12, via the valve 70, in a manner which disposes the nozzle 40 in fluid communication with the interior of the chamber 14, as represented in FIGS. 11A-11D. As also indicated, the nozzle 40 is structured for the concurrent dispensing of liquid fuel 200 from the interior of the chamber 14 into the vehicle or other fluid receiving receptacle 100, concurrently to the collection and passage of gaseous fluid 210 from the fuel tank 102 of the vehicle's 100 into the chamber 14. The aforementioned “gaseous fluid” 210 may comprise vapor, air, and other gases exiting the fuel tank 102 of the vehicle or fuel receiving receptacle 100, as the stored liquid fuel 200 from the container 12 is supplied thereto.

[0058] Therefore, the nozzle 40 comprises first and second flow channels 42 and 44 respectively, each operatively disposed in fluid communication with the chamber 14 and successively disposed in open fluid communication between the chamber 14 and an exterior of the nozzle 40 such as through the discharge end 41, when the nozzle 40 is operatively connected to the container 12. The first flow channel 42 defines a path of liquid flow out of the chamber 14 as the liquid fuel is delivered to the fuel tank 102 of the vehicle or other fuel delivering receptacle 100. The second flow channel 44 defines a path of gaseous flow into the chamber 14, such as when the vapors, air, other gases, etc. pass from the fuel tank 102 of the vehicle 100 into the interior of the chamber 14.

[0059] For purposes of clarity FIGS. 8A-8D are a schematic representation indicating both the structural and operative features of the nozzle 40 in specific relation to the opening and closing of the first and second flow channels 42 and 44. Somewhat similarly, FIG. 11A-11D indicate one embodiment of the fuel container assembly 10 of the present invention, wherein an intended operative connection is defined by the nozzle 40 and container 12 being interconnected to one another, via the valve structure 70, such that the nozzle 40 and valve 70 are or may be disposed in fluid communication with the interior chamber 14.

[0060] Accordingly, the nozzle 40 comprises a primary conduit 46, the interior of which at least partially defines the first flow channel 42. The nozzle 40 also comprises as an outer sleeve 48 which is telescopically movable between an outwardly extended position (see FIGS. 8A and 11A) and a fully inwardly retracted position (see FIGS. 8D and 11D). A biasing structure 50 is disposed on an interior portion of the nozzle 40 and serves to normally bias the outer sleeve 48 towards and into the fully extended position of FIGS. 8A and 11A. Moreover, the outer sleeve 48 is movably disposed in surrounding, telescopic relation to at least a portion of a length of the primary conduit 46, wherein the second flow path 44 is disposed within and at least partially defined by the space between the primary conduit 46 and the outer sleeve 48. In addition, a cover 52 is fixedly connected or mounted on the nozzle 40 in surrounding telescopic relation to at least a portion of the outer sleeve 48, at least concurrent to the outer sleeve 48 being in the inwardly retracted position. However, in at least one embodiment, the cover 52 is dimensions to extend over and in surrounding, protective relation to at least a portion of the outer sleeve 48 when it is disposed in both the outwardly extended position of FIGS. 8A and 11A and the fully, inwardly retracted position of FIGS. 8D and 11D.

[0061] It is also to be noted that movement of the sleeve 48 into the aforementioned inwardly retracted position typically occurs as a nozzle component of the fuel container assembly 10 enters the entrance or like structure of the fuel tank in which the liquid fuel is to be dispensed. The relatively larger size of the nozzle such as at 48′ or other entering portion of the nozzle 40 than that of the aperture or fill pipe 103 of the vehicle 100, through which the dispensed fuel 200 will flow is sufficiently different to cause a forced movement of the sleeve 48 into the inwardly retracted position, as at least partially represented in FIG. 1.

[0062] Further, the cover 52 and the sleeve 48 are cooperatively disposed and dimensioned to position the cover 52 in interruptive, movement restricting engagement with the outer sleeve 48, concurrent to the sleeve 48 being disposed in the fully inwardly retracted position. More specifically, as represented in FIGS. 8A-D and 11A-D the outer sleeve 48 includes at least one portion 48′ which has an increased outer transverse dimension by extending laterally or transversely outward beyond the outer surface or outer transverse dimension of the closure 52. As such, as represented in FIGS. 8D and 11D, inward retraction of the outer sleeve 48 will be limited due to the movement restricting engagement of the end portion 53 of the cover 52 with the outwardly extending portion 49 of the segment 48′ of the outer sleeve 48. As set forth above, the biasing structure 50 is disposed to normally bias the sleeve 48 towards and into the fully outer extended position and the cover 52. In addition, the cover 52 is also disposed in overlying, protective relation to the biasing structure 50, concurrent to the outer sleeve 48 being in either or both the extended or retracted positions. Therefore, the biasing structure 50 is protected from inadvertent contact or interruptive engagement with individuals using the fuel container assembly 10 or variety of objects which may be disposed in or about the storage area of the fuel container assembly 10.

[0063] As described, the first and second flow and channels 42 and 44 are disposed separately and successively into open fluid communication between the chamber 14 and an exterior of the nozzle 40 via the discharge opening 41 of the outer sleeve 48. Such successive openings are facilitated by operation and disposition of a seal assembly generally indicated as 60, mounted on the outer sleeve 48 and movable therewith between the outwardly extended and inwardly retracted positions. As represented in both FIGS. 8A-8D and 11A-11D, the seal assembly 60 preferably comprises a plurality of seal structures, including at least seal structures 62, 63, 64, etc. Each or at least some of the seal structures 62-64 may be in the form of specifically structured, disposed and/or installed O-rings. However, other forms of seal structures may be utilized. Further, at least some seal structures, as at least 62 and 64 are disposed in fluid sealing relation between the sleeve 48 and an exterior of the conduit 46, at least when the sleeve 48 is disposed in the fully outwardly extended position. At least some of the plurality of seal structures, as at least 62 and 64, are cooperatively disposed relative to the outer surface of the conduit 46 to at least partially define the liquid flow path/first flow path 42 opening first and before a subsequent opening of the gaseous flow path/second flow path 44. The aforementioned sealing engagement of the sealing structures, at least 62 and 64, occurs by a compression of the respective seals into sealed engagement with the outer surface of the conduit 46 thereby restricting liquid or gaseous fluid flow thereby.

[0064] In order to further facilitate the successive opening of the first and second flow paths 42 and 44, the primary conduit 46 or more specifically exterior portions thereof define “release segments” as at 45 and 47. The release segments 45 and 47are dimensioned, disposed and configured to disengage the outer surface of the conduit 46 from the seal structures, at least 62 and 64 thereby establishing a non-sealing relation with at least some of the plurality of seal structures. Such a non-sealing alignment between the release segments 45 and 47 and at least some of the seal structures 62 and 64 occurs upon movement of the outer sleeve 48 into and towards the fully inwardly retracted position of FIGS. 8D and 11D. As a result, non-sealing relation of some of the plurality of seal structures, including at least seal structures 62 and 64, with the exterior of the conduit 46 will result in the opening of the first and second flow paths 42 and 44, albeit separately and successively, thereby establishing fluid communication between the interior of the chamber 14 and the exterior of the nozzle 40 through or about discharge opening 41. Each of the plurality of release segments 45 and 47 include a recess, groove, channel or other structure demonstrating smaller or reduced exterior surface, transverse dimensions of the conduit 46.

[0065] With reference to both FIGS. 8A-8D and 11A-11D, when the sleeve 48 is in its fully, outwardly extended position the distance or spacing “A” between the engaging points 49 and 53 on the sleeve 48 and the cover 52 is greatest. With reference to FIGS. 8B and 11B, as the sleeve begins to retract inwardly, the seal structures 62 and 64 also move inwardly along the length of the outer surface of the conduit 46 and eventually assume a spacing “B” between the engaging or contact points 49 and 53. However, both seal structures 62 and 64 remain in sealed engagement with the outer surface of the conduit 46, at this point of inward retraction. It is a further note that upon movement of the sleeve 48 into a position where the spacing has lessened, as at “B′”, a pressure pulse 220 will be delivered to the interior chamber 14. The existence or delivery of the pressure pulse 220 is based at least in part on a reduction of the space coincident with the biasing structure 50 and a forcing of the air there from into the interior of the chamber 14.

[0066] Such a pressure pulse 220 will have the effect of at least minimally increasing the pressure within the chamber 14 thereby facilitating flow of liquid fuel 200 from the chamber 14 into and along the length of the nozzle as evidenced by directional arrows 200′ in FIGS. 8C-8D and 11C-11D, as the outer sleeve 48 continues to retract, resulting in a further reduction of the spacing to a size schematically represented as “C” between the engagement or contact points 49 and 53 and the beginning of liquid fuel flow into the first flow path 42 within interior of the conduit 46. However, at this point of inwardly directed retraction of the sleeve 48, at least one seal structure 62 is disposed in a line, non-sealing relation with a first release segment 45, thereby serving to first open the first flow path/liquid flow path 42. However, at this point in the retraction (spacing “C”) of the outer sleeve 48, at least one additional seal structure 64 remains in sealing engagement with the outer surface of the conduit 46, resulting in the second flow path/gaseous flow path 48 remaining closed.

[0067] Upon a fully retracted positioning of the outer sleeve 48 and the engagement of the contact points 49 and 51, as represented in FIGS. 8D and 11D, the seal structure 64 will be aligned with a second release segment 47 thereby establishing a non-sealing relation between the seal assembly 60 and the outer surface of the conduit 46. In turn, this will result in the second flow path 44 being opened, subsequent to the opening of the first flow path 42. Upon opening of the second flow path 44, the gaseous fluid 210 will enter the interior of the nozzle 40, between the inner surface of the sleeve 48 and the outer surface of the conduit 46, and pass into the interior of the chamber 14, as represented.

[0068] Due to the fact that at least one seal structure 62 is disposed dimensionally closer to the corresponding first release segment 45, a non-sealing engagement therebetween will occur first during the retraction of the sleeve 48, resulting in the opening of the first flow path 42. In contrast, the distance between at least one other of the seal structures, as at 64 and a second release segment 47 is farther than the distance between seal structure 62 and release segment 45. As a result, the non-sealing alignment therebetween seal structure 64 and the second release segment 47 will occur after or subsequent to the non-sealing alignment between the seal structure 62 and release segment 45. Accordingly, the first flow path 42 will be opened first and before the opening of the second flow path 44.

[0069] One or more embodiments of the fuel container assembly 10 of the present invention also comprises the aforementioned valve structure 70 represented in detail in FIGS. 9A-9E, 10 and in its assembled interconnecting position in FIGS. 11A-11D. For purposes of clarity, FIG. 10 represents the valve structure 70 attached to the container 12 but not connected to the nozzle 40. However, as used, the valve structure 70 is disposed in interconnecting relation between the nozzle 40 and the container 12 at threaded, sealed junction, or connection 55 and is selectively disposed between a closed orientation and an open orientation. In the open orientation, the valve structure 70 at least partially defines the operative connection and fluid communication of the nozzle 40 to the container 12, in fluid communication with the interior chamber 14. More specifically, as represented the valve structure 70 comprises a first flow channel segment 72 and a second flow channel segment 74. In the aforementioned open orientation, the first and second flow channel segments 72 and 74 are concurrently disposed in aligned, interconnecting fluid communication between the chamber 14 and the first and second flow channels 42 and 44 within the nozzle 40. In contrast, in the closed orientation, first and second channel segments 72 and 74 of the valve structure 70 are disposed out of fluid communication with interior of the nozzle 40 and the chamber 14.

[0070] Movement of the valve structure 70 between the open and closed orientations preferably occurs, in at least one embodiment, by manipulation of a stem 75 resulting in a rotational movement of the valve structure 70 relative to the container 12. Such rotational movement may occur concurrent to the nozzle 40 being attached to the valve structure 70, such that the nozzle 40 and attached valve structure 70 move or rotate together relative to the container 12, between the aforementioned open and closed orientations. Such preferred rotational movement of the valve structure 70 relative to the container 12 occurs through a predetermined or preferred angle of rotation which, due to cooperative structuring between the container interface 73 and the valve structure 70 defines the disposition thereof into an out of the open orientation. Such predetermined angle of rotation of the valve structure 70 may be defined by substantially a one quarter turn or through an arc of approximately 90° . This facilitates the user being able to efficiently open and close the valve structure to establish the aforementioned fluid communication between the nozzle 40 and the chamber 14. Moreover, a locking pin or other locking structure 77 may be incorporated in the valve structure 70 such that it is removably locked or maintained in both the open and closed orientations. Manipulation of the locking pin or other type locking structure 77 may be easily accomplished by finger manipulation by the user. In addition, as represented in FIGS. 6A and 9A, prior to the attachment of the nozzle 40 to the valve structure 70, a closure cap 71 may be secured in sealing relation to the valve structure 70 so as to assure maintenance of the airtight or hermetically sealed condition of the chamber 14.

[0071] As noted herein, the structural and operative features of the fuel container assembly 10 of the present invention facilitate safe storage and transportation as well as the delivery of fuel to the fuel tank 102 of a vehicle or other fuel receiving receptacle 100. Accordingly, one or more embodiments of the present invention include a static charge inhibitor assembly generally indicated as 80 in FIGS. 12 and 13A-13B. The static charge inhibitor assembly 80 comprises a conductive material cord 82 attachable in electrically conductive relation to and between the container 12 and the vehicle or a fuel receiving receptacle 100. More specifically, a magnetic mount 86 is secured to a distal extremity 82′ and serves to magnetically attach the cord 82 to the vehicle 100. Also, a retractable reel 84 serves to house the conductive cord or cable 82, such that the cord 82 is movable on the retracted reel 84 into an out of the interior of the retractable real 84 and the magnetic, conductive mount 86 with the vehicle or fuel receiving receptacle 100. Moreover, in at least one embodiment a magnetic mount or attachment member 86 is secured in electrically conductive relation to an outer, distal end of the cord 82 and is operative to magnetically connect the cord 82 to the fuel receiving receptacle 100. At the same time, the retractable real 84 is secured directly to the metallic material container 12 by virtue of a connector 87. The connector 87 may also be formed of an electrically conductive, magnetic material and be magnetically or otherwise attached to the exterior of the container 12. Therefore, as operatively assembled and as represented in both FIGS. 1 and 12 there is a removable but sustainable electrical, conductive relation between the container 12 and the vehicle or fluid receiving receptacle 100. As a result of such a conductive connection between the vehicle 100 and the container 12, electrical potential therebetween is substantially equalized, serving to eliminate or significantly restrict the possibility of a static charge developing, during a dispensing of the liquid fuel 200.

[0072] Since many modifications, variations and changes in detail can be made to the described preferred embodiment of the invention, it is intended that all matters in the foregoing description and shown in the accompanying drawings be interpreted as illustrative and not in a limiting sense. Thus, the scope of the invention should be determined by the appended claims and their legal equivalents.