Tank assembly collar mount
09671066 ยท 2017-06-06
Assignee
Inventors
Cpc classification
F17C2270/0173
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0604
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/234
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0171
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0394
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0636
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/037
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0673
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/32
GENERAL 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
F17C2270/0194
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0338
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0323
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/228
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0189
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0305
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/2154
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0178
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0176
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0646
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A tank assembly having a gas impermeable liner having a neck for storing a compressed gas is provided. The neck has a threaded bore. An annular collar having a generally circular opening is disposed around the neck. A structural layer substantially envelopes the liner and secures the collar to the neck.
Claims
1. A tank assembly comprising: a gas impermeable liner having a neck having a threaded bore to receive a valve for providing compressed gas; an annular collar having a generally circular opening, the annular collar being disposed around the neck; an annular mounting bracket including a generally circular opening for being rotatably mounted on the annular collar to surround the valve; and a structural layer substantially enveloping the liner and securing the annular collar to the neck, wherein the annular mounting bracket includes a mounting portion for receiving and securing a regulator thereon, the regulator being in fluid communication with the valve to regulate a flow of the compressed gas therefrom.
2. The tank assembly of claim 1 wherein the annular mounting bracket includes a first end for being rotatably mounted on the annular collar and a second end for receiving the regulator.
3. The tank assembly of claim 2 further comprising a fitting positioned above annular mounting bracket for being coupled to the valve and to the regulator for providing the compressed gas from the valve to the regulator.
4. The tank assembly of claim 3 wherein the fitting includes a threaded portion at one end thereof for engaging the valve.
5. The tank assembly of claim 1 wherein the annular collar includes a raised annular flange for receiving the annular mounting bracket.
6. The tank assembly of claim 5 wherein the raised annular flange defines a plurality of mounting bores, one or more of the plurality of mounting bores being arranged to receive a fastener to secure the annular mounting bracket to the raised annular flange.
7. A tank assembly for a vehicle comprising: a gas impermeable liner having a neck to receive a valve for providing compressed gas; an annular collar having a generally circular opening, a first surface, and an annular flange protruding above the first surface and disposed generally concentrically with the opening, the annular collar being disposed around the neck such that the first surface is substantially coplanar with an upper surface of the neck; an annular mounting bracket including a generally circular opening for being rotatably mounted on the annular collar to surround the valve; and a structural layer substantially enveloping the liner and securing the annular collar to the neck, wherein the annular mounting bracket includes a mounting portion for receiving and securing a regulator thereon, the regulator being in fluid communication with the valve to regulate a flow of the compressed gas therefrom.
8. The tank assembly of claim 7 wherein the annular mounting bracket includes a first end for being rotatably mounted on the annular collar and a second end for receiving the regulator.
9. The tank assembly of claim 8 further comprising a fitting positioned above the annular mounting bracket for being coupled to the valve and to the regulator for providing the compressed gas from the valve to the regulator.
10. The tank assembly of claim 9 wherein the fitting includes a threaded portion at one end thereof for engaging the valve.
11. A tank assembly comprising: a liner including a neck having a threaded bore to receive a valve for providing compressed gas; an annular collar being disposed around the neck; an annular mounting bracket including a first end for being rotatably mounted on the annular collar and for surrounding the valve and a second end for receiving a regulator; and a structural layer substantially enveloping the liner and securing the annular collar to the neck.
12. The tank assembly of claim 11 wherein the annular collar includes a raised annular flange for receiving the annular mounting bracket.
13. The tank assembly of claim 12 wherein the raised annular flange defines a plurality of mounting bores, one or more of the plurality of mounting bores being arranged to receive a fastener to secure the annular mounting bracket to the raised annular flange.
14. The tank assembly of claim 11 wherein the annular mounting bracket includes a mounting portion for receiving and securing the regulator thereon, the regulator being in fluid communication with the valve to regulate a flow of the compressed gas therefrom.
15. The tank assembly of claim 14 further comprising a fitting positioned above the annular mounting bracket for being coupled to the valve and to the regulator for providing the compressed gas from the valve to the regulator.
16. The tank assembly of claim 15 wherein the fitting includes a threaded portion at one end thereof for engaging the valve.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The description herein makes reference to the accompanying drawings wherein like reference numerals refer to like parts throughout the several views, and in which:
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION OF THE ILLUSTRATED EMBODIMENT(S)
(6) Detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention that may be embodied in various and alternative forms. The figures are not necessarily drawn to scale, some features may be exaggerated or minimized to show details of particular components. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for the claims and/or as a representative basis for teaching one skilled in the art to variously employ the present invention.
(7) In view of the high pressures at which compressed gases such as hydrogen may be maintained, it may be desirable to reduce the pressure of such compressed gas after the compressed gas has been discharged from the tank assembly in which it is stored. This condition may be accomplished by mounting a regulator close to the outlet/valve of the tank assembly. Mounting the regulator in close proximity to the outlet may eliminate the need for extensive high pressure lines/hoses. Such a mounting condition may reduce leakage from the fuel containment system as well as reduce the cost associated with providing high pressure line/hose.
(8) A conventional tank assembly is configured to receive and store high pressure compressed hydrogen or other gases at pressures up to and exceeding 10,000 psi include a gas impermeable liner made from materials including, but not limited to, plastics, or metal. The liner is enveloped/encased within an outer structural layer that provides the strength to contain the high pressure compressed gas and prevent the liner from rupturing. Conventionally, the structural layer comprises a composite material such as, but not limited to, carbon fiber.
(9) The liner has a neck portion having a diameter that is smaller than a diameter of the remainder of the liner. A valve is mounted to the neck, in some cases through threaded engagement between threads formed on an internal wall of the neck and threads formed on an outer wall of the valve. This arrangement permits the valve to be screwed into position in a bore formed by an internal wall of the neck.
(10) In accordance with the embodiments of the present invention, an annular or ring-like collar is positioned around the neck of the liner prior to, or during, the application of the composite material to the liner. An underside of the collar includes a channel to receive and engage with the strands of the composite material. The liner, collar, and composite material is then heated until the composite material and/or an epoxy resin on the composite material cures, forming a robust casing around the liner and collar.
(11) The collar is further configured to permit attachment of a mounting bracket to the collar. The mounting bracket is configured to receive and retain a regulator or any other device. The mounting bracket is further configured to move with respect to the collar to permit adjustment of the angle and proximity of the regulator with respect to the outlet of the valve of the tank assembly to permit proper alignment and close proximity between the regulator and the valve. In other embodiments, the collar may be placed elsewhere on the liner to permit the mounting of bodies/apparatuses to any desirable portion of the tank assembly.
(12) A greater understanding of the embodiments of the invention disclosed herein may be obtained through a review of the detailed description below as well as a review of the illustrations accompanying this application.
(13) With respect to
(14) Tank assembly 20 includes a liner 22. Liner 22 is a gas impermeable container for containing the compressed gas. Liner 22 may be made of any gas impermeable material including, but not limited to, metal, or plastic. In at least one embodiment, liner 22 may comprise aluminum.
(15) Liner 22 includes a neck 24. Neck 24 has a smaller diameter than the remainder of liner 22 and serves as a pathway for gasses to enter and exit to and from liner 22. Neck 24 defines a central bore and is threaded along an internal wall. The threads of neck 24 are configured to engage corresponding threads defined in an outer surface of a valve 26. The valve 26 generally controls the flow of the gas from the liner 22. While
(16) An annular collar 28 is positioned adjacent an external wall of neck 24. In the illustrated embodiment, annular collar 28 is ring-like structure and defines an internal annular collar bore 30. Annular collar 28 includes a first surface 32 which is substantially flush with an upper surface of neck 24. In other embodiments, the first surface 32 may be disposed above or below an upper surface of neck 24 without departing from the teachings of the present invention.
(17) Annular collar 28 further includes a raised flange 34 adjacent first surface 32 and protruding above first surface 32. Raised flange 34 is generally circular and is generally concentric with internal annular collar bore 30. Raised flange 34 includes a plurality of mounting bores 36 defined in an upper surface thereof. In the illustrated embodiment, mounting bores 36 are threaded and are configured to receive threaded fasteners, discussed below. In other embodiments, a greater or lesser number of mounting bores 36 may be employed without departing from the teachings of the present invention. In still other embodiments, mounting bores 36 may not be threaded.
(18) Annular collar 28 further includes a channel 38 defined in a second surface 40. Channel 38 extends around annular collar 28 in a generally circular configuration and is generally concentric with internal annular collar bore 30 and raised flange 34. In other embodiments, channel 38 may be non-circular and/or non-concentric with raised flange 34 or with internal annular collar bore 30 without departing from the teachings of the present invention. Channel 38 is configured to receive a sealing member 42 (see
(19) Annular collar 28 further includes a retaining channel 44 defined in an underside of annular collar 28. Retaining channel 44 is configured to engage structural layer 46 (as discussed below) and to cooperate with structural layer 46 to retain annular collar 28 in a substantially stationary position with respect to neck 24. Retaining channel 44 generally resembles the letter J in cross-section. In other embodiments, retaining channel 44 may have any other shape or configuration that is conducive to engagement with structural layer 46 and retention of annular collar 28 on neck 24. In the illustrated embodiment, retaining channel 44 extends in circular fashion around an entire underside of annular collar 28. In other embodiments, retaining channel 44 may comprise a plurality of channel segments disposed intermittently around an underside of annular collar 28.
(20) Tank assembly 20 further includes structural layer 46. As illustrated in
(21) In some embodiments, structural layer 46 may be wrapped around liner 22 by a manufacturing process wherein liner 22 is turned as strands of composite material are wrapped or draped around liner 22. As the strands of carbon fiber are wrapped around the outer portion of neck 24, they enter and engage with retaining channel 44. The wrapping of liner 22 with carbon fiber strands continues until structural layer 46 has reached a desired level of thickness. The greater the pressure of the compressed gas, the thicker will be structural layer 46. Once the desired thickness has been achieved, the tank assembly 20, including the wound strands of structural layer 46, are heated. This causes the carbon fiber strands of structural layer 46 and/or an epoxy or other resin applied thereto to melt and/or bond to form a generally unified, monolithic structure.
(22) Once structural layer 46 is assembled and cured, the only portion of liner 22 that is visible from outside tank assembly 20 is an upper surface of liner 22. Similarly, only an upper portion of annular collar 28 is visible from outside tank assembly 20. The underside, and in particular, retaining channel 44 are hidden from view.
(23)
(24) As illustrated
(25) With respect to
(26) As illustrated, threaded fasteners 54 include a head portion 56 and a threaded portion 58 (see
(27) With respect to
(28) When tank assembly 20 is mounted in the trunk or cargo portion of a vehicle, there is a risk that the compressed gas may leak out of tank assembly 20 and enter the passenger compartment of the vehicle. The manufacturer is required to provide an airtight vent box (or enclosure as noted above) to direct such leaked gas to an area outside of the passenger compartment. By providing a sealing member 42 between annular mounting bracket 48 and annular collar 28, an airtight seal is provided that prevents gas from passing between annular collar 28 and annular mounting bracket 48. This permits a manufacturer to design and install the vent box that can attach to annular mounting bracket 48 instead of one which needs to be attached directly to annular collar 28. Various mounting holes as shown on the annular mounting bracket 48 facilitate coupling the vent box thereon. This arrangement can afford a manufacturer greater flexibility when designing the vent box.
(29) With respect to
(30) As illustrated in
(31) While embodiments of the invention have been illustrated and described, it is not intended that these embodiments illustrate and describe all possible forms of the invention. Rather, the words used in the specification are words of description rather than limitation, and it is understood that various changes may be made without departing from the spirit and scope of the invention.