Method for producing pressure vessels
US-2019017655-A1 · Jan 17, 2019 · US
US10648616B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10648616-B2 |
| Application number | US-201415517010-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 7, 2014 |
| Priority date | Oct 7, 2014 |
| Publication date | May 12, 2020 |
| Grant date | May 12, 2020 |
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A pressure vessel assembly includes a plurality of lobes, each lobe having at least one vertically arranged interior wall, the lobes positioned in a side by side arrangement such that a first interior wall of a first lobe is positioned adjacent a second interior wall of a second lobe, the first interior wall having a first wall top and bottom side, the second interior wall having a second wall top and bottom side, the first wall top side joined to the second wall top side and the first wall bottom side joined to the second wall bottom side. Also included are first and second end wall surfaces of each of the plurality of lobes. Further included is a plurality of end caps, each of the end caps joined to the end wall surfaces of the lobes, each of the end caps joined to at least one adjacent end cap.
Opening claim text (preview).
What is claimed is: 1. A pressure vessel assembly comprising: a first lobe being circumferentially continuous, and including a first interior wall, a first outer wall, and a first shoulder region joined to and disposed between the first interior wall and the first outer wall, wherein the first shoulder region includes a thickness that is greater than a remainder of the first lobe; and a second lobe being circumferentially continuous, and including a second interior wall, a second outer wall, and a second shoulder region joined to and disposed between the second interior wall and the second outer wall, wherein second shoulder region includes a thickness that is greater than a remainder of the second lobe, the first interior wall is positioned adjacent to the second interior wall, and the first shoulder region is positioned adjacent to the second shoulder region, wherein the first and second shoulder regions each include an outer surface that transitions into respective curved portions of the respective first and second outer walls. 2. A pressure vessel assembly comprising: a first lobe being circumferentially continuous, and including a first interior wall, a first outer wall, and a first shoulder region joined to and disposed between the first interior wall and the first outer wall, wherein the first shoulder region includes a thickness that is greater than a remainder of the first lobe; a second lobe being circumferentially continuous, and including a second interior wall, a second outer wall, and a second shoulder region joined to and disposed between the second interior wall and the second outer wall, wherein second shoulder region includes a thickness that is greater than a remainder of the second lobe, the first interior wall is positioned adjacent to the second interior wall, and the first shoulder region is positioned adjacent to the second shoulder region; and a weld adapted to join the first and second shoulder regions.
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