BOSS WITH INTERNAL BEARING
20170370527 · 2017-12-28
Inventors
- Brad James Moutray (Sioux Falls, SD, US)
- John Allen Eihusen (Lincoln, NE, US)
- Brian Christopher Yeggy (Lincoln, NE, US)
Cpc classification
F17C13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T403/32196
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
F17C13/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0305
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/058
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C23/043
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/056
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0119
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
Y10T403/32704
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
International classification
Abstract
A boss configured for attachment to a pressure vessel includes a first bore therein and a bearing disposed at least partially within the first bore. A system for supporting a pressure vessel on a vessel mount includes a boss, a bearing, and an attachment element. The boss is attached to the pressure vessel and has a first bore therein. The bearing is disposed at least partially within the first bore and has a second bore therethrough. The attachment element is configured to be affixed to the vessel mount, wherein a portion of the attachment element extends through the second bore and is slidable within the first and second bores substantially along a longitudinal axis of the pressure vessel. A method is described for supporting a pressure vessel on a vessel mount.
Claims
1. A boss configured for attachment to a pressure vessel, the boss including: a first bore therein; and a bearing disposed at least partially within the first bore.
2. The boss of claim 1 wherein the bearing is spherical.
3. The boss of claim 2 wherein the first bore includes a surface that is at least partially spherical and corresponds to a portion of an outer spherical surface of the bearing.
4. The boss of claim 1, wherein the bearing includes a second bore therethrough.
5. The boss of claim 4 wherein the first bore and the second bore have co-axial longitudinal axes.
6. The boss of claim 2 further including a retainer disposed between a portion of an outer spherical surface of the bearing and a portion of the first bore.
7. The boss of claim 6 wherein the retainer includes an inner surface that is at least partially spherical and corresponds to the portion of the outer spherical surface of the bearing.
8. The boss of claim 6 wherein: the first bore includes a shoulder; and the retainer includes an interior end surface configured to abut the shoulder.
9. The boss of claim 6 wherein the retainer is annular.
10. The boss of claim 6 wherein: the first bore includes a groove; and the retainer is configured to at least partially fit into the groove.
11. A system for supporting a pressure vessel on a vessel mount, the system including: a boss attached to the pressure vessel and having a first bore therein; a bearing disposed at least partially within the first bore and having a second bore therethrough; and an attachment element configured to be affixed to the vessel mount, wherein a portion of the attachment element extends through the second bore and is slidable within the first and second bores substantially along a longitudinal axis of the pressure vessel.
12. The system of claim 11 wherein: the bearing is spherical; and the first bore includes a surface that is at least partially spherical and corresponds to an outer spherical surface of the bearing.
13. The system of claim 12 further including a retainer disposed between a portion of an outer spherical surface of the bearing and a portion of the first bore.
14. The system of claim 13 wherein the retainer includes an inner surface that is at least partially spherical and corresponds to the portion of the outer spherical surface of the bearing.
15. The system of claim 13 wherein: the first bore includes a shoulder; and the retainer includes an inner end surface configured to abut the shoulder.
16. The system of claim 13 wherein the retainer is annular.
17. The system of claim 13 wherein: the first bore includes a groove; and the retainer is configured to at least partially fit into the groove.
18. The system of claim 11 wherein the attachment element is configured as a pin.
19. A method for supporting a pressure vessel having a boss on a vessel mount, the boss having a first bore therein, a bearing disposed at least partially within the first bore and having a second bore therethrough, the method including: inserting a first portion of an attachment element through the second bore and a portion of the first bore; and mounting a second portion of the attachment element to the vessel mount.
20. The method of claim 19 wherein the bearing is spherical, the method further including passing the first portion of the attachment element through a retainer that keeps the bearing at least partially within the first bore.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0049] The disclosed subject matter will be further explained with reference to the attached figures, wherein like structure or system elements are referred to by like reference numerals throughout the several views.
[0050]
[0051]
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[0055]
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[0057] While the above-identified figures set forth one or more embodiments of the disclosed subject matter, other embodiments are also contemplated, as noted in the disclosure. In all cases, this disclosure presents the disclosed subject matter by way of representation and not limitation. It should be understood that numerous other modifications and embodiments can be devised by those skilled in the art which fall within the scope and spirit of the principles of this disclosure.
[0058] The figures may not be drawn to scale. In particular, some features may be enlarged relative to other features for clarity. Moreover, where terms such as above, below, over, under, top, bottom, side, right, left, etc., are used, it is to be understood that they are used only for ease of understanding the description. It is contemplated that structures may be oriented otherwise.
DETAILED DESCRIPTION
[0059] U.S. Pat. No. 6,986490 by Eihusen et al., entitled “Method and apparatus for mounting a fluid containment cylinder,” which is hereby fully incorporated by reference, describes a prior art vessel securement method and apparatus that provides for securely fastening a pressure vessel against axial and rotational movement while enabling the pressure vessel mounting structures to accommodate a degree of misalignment without unduly stressing the neck of the pressure vessel.
[0060] As shown in
[0061]
[0062]
[0063] In the exemplary embodiment shown in
[0064] As shown in
[0065] As shown in
[0066] In an exemplary embodiment of boss 12, internal threads 32 are provided on at least a portion of a surface of bore 26 to allow boss 12 to be mounted on a mandrel (not shown), such as for forming liner 34 and shell 36 of pressure vessel 10 about boss 12. In an exemplary embodiment, bore 26 includes partially spherical inner surface 38 that is shaped to conform to an outer spherical surface 40 of bearing 18. In an exemplary embodiment, bore 26 includes a substantially cylindrical inner surface 42 configured to correspond in shape to cylindrical outer surface 44 of retainer 20. Moreover, retainer 20 has an inner surface 46 that is partially spherical to conform to the shape of a portion of outer spherical surface 40 of bearing 18. Bearing 18 in an exemplary embodiment includes an interior end surface 48 and an exterior end surface 52. As shown in
[0067] In an exemplary embodiment, retainer 20 includes interior end surface 58, configured to abut shoulder 50 of bore 26. Retainer 20 also includes exterior end surface 60, configured to be adjacent retaining ring 22. Retaining ring 22 in an exemplary embodiment has an outer diameter and thickness to allow it to at least partially fit into and snap into groove 62 of bore 26. Retaining ring 22 also has an inner diameter surface with a partially spherical configuration to conform to an outer portion of spherical surface 40 of bearing 18.
[0068] As shown in
[0069] Although the subject of this disclosure has been described with reference to several embodiments, workers skilled in the art will recognize that changes may be made in form and detail without departing from the scope of the disclosure. For example, in exemplary embodiments, bearing 18 is a spherical bearing that allows for multiple degrees of freedom in the mounting of pressure vessel 10 to external structures (not shown) via pin 14, shown in