High pressure tank, method of manufacturing high pressure tank and method of designing liner shape
US-2016341359-A1 · Nov 24, 2016 · US
US10648620B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10648620-B2 |
| Application number | US-201715460340-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 16, 2017 |
| Priority date | Mar 16, 2016 |
| Publication date | May 12, 2020 |
| Grant date | May 12, 2020 |
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An apparatus is configured to be positioned between a boss and a shell of a pressure vessel. The boss includes a bore therethrough, and the bore has a longitudinal axis. The apparatus includes an annular body and a gas permeable feature. The annular body includes an inner surface configured to abut the boss and an outer surface configured to abut the shell. The annular body has opposite first and second ends relative to the longitudinal axis. The gas permeable feature is provided on the inner surface and extends at least from the first end to the second end. The disclosure also describes a pressure vessel including a shell, and boss, and an apparatus positioned between the boss and the shell. A method for forming a pressure vessel includes mounting a boss on a mandrel, positioning an annular fitting about a neck of the boss, forming a liner, and forming an outer shell.
Opening claim text (preview).
What is claimed is: 1. An apparatus configured to be positioned between a boss and a shell of a pressure vessel, the boss including a bore therethrough, and the bore having a longitudinal axis, the apparatus including: an annular body including: an inner surface configured to contact and abut the boss and an outer surface configured to abut the shell; opposite first and second ends relative to the longitudinal axis; a neck adjacent the first end; and a flange adjacent the second end, wherein the flange extends away from the longitudinal axis relative to the neck; and a gas permeable feature provided on the inner surface and extending at least from the first end to the second end. 2. The apparatus of claim 1 , wherein the gas permeable feature includes a plurality of channels. 3. The apparatus of claim 2 , wherein at least one of the plurality of channels is substantially aligned with the longitudinal axis. 4. The apparatus of claim 2 , wherein at least some of the plurality of channels are substantially evenly circumferentially spaced about the inner surface. 5. The apparatus of claim 2 , wherein at least one of the plurality of channels has a substantially rectangular cross-sectional profile. 6. The apparatus of claim 1 , wherein the neck is tapered radially inward from the first end. 7. The apparatus of claim 1 , wherein the second end abuts a liner disposed within the shell. 8. A pressure vessel including: a shell; a boss including a bore therethrough, the bore having a longitudinal axis; an apparatus positioned between the boss and the shell, the apparatus including: an annular body including: an inner surface configured to contact and abut the boss and an outer surface configured to abut the shell; opposite first and second ends relative to the longitudinal axis; a neck adjacent the first end; and a flange adjacent the second end, wherein the flange extends away from the longitudinal axis relative, to the neck; and a gas permeable feature provided on the inner surface and extending at least from the first end to the second end. 9. The pressure vessel of claim 8 including an interface between the liner and the shell, and wherein the gas permeable feature is in fluid communication with the interface at the second end and with an exterior of the vessel at the first end. 10. The pressure vessel of claim 8 wherein the gas permeable feature includes a plurality of channels. 11. The pressure vessel of claim 10 wherein at least one of the plurality of channels is substantially aligned with the longitudinal axis. 12. The pressure vessel of claim 10 , wherein at least some of the plurality of channels are substantially evenly circumferentially spaced about the inner surface. 13. The pressure vessel of claim 8 , wherein the neck is tapered radially inward from the first end. 14. The pressure vessel of claim 8 , wherein the second end abuts a liner disposed within the shell. 15. The pressure vessel of claim 8 , wherein the shell is bonded to an outer surface of the annular body.
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