Basalt-based pressure vessel for gas storage and method for its production
10563818 ยท 2020-02-18
Assignee
Inventors
Cpc classification
F17C2205/0323
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0665
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/1393
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
F17C1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/1372
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
F17C2203/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/139
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
F17C2209/2163
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0394
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/067
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0663
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/1352
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
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0624
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
F17C2203/0634
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/1362
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 pressure vessel includes a first (base or innermost) layer composed of a resin-impregnated woven sleeve with chopped basalt fibers assembled in the voids of the sleeve and impregnated with an epoxy resin. A second and third layer is composed of continuous basalt fiber filaments arranged in a helical pattern, with the helical angle of the second layer being not equal to that of the third layer. A fourth layer is composed of continuous basalt fibers arranged in a hoop pattern. The fifth (outermost) layer is composed of randomly oriented chopped basalt fibers impregnated with a resin matrix and compacted with the subsequent wound filaments at up to ten pounds of tension.
Claims
1. A linerless pressure vessel comprising: an innermost composite material layer; and a next outermost composite material layer arranged at a helical angle; the innermost composite material layer including a resin-impregnated sleeve, fibers, and a nano-additive in voids of the sleeve.
2. The linerless pressure vessel of claim 1, further comprising: the helical angle being in a range 2 to 50.
3. The linerless pressure vessel of claim 1, wherein at least one of the innermost and next outermost composite material layers includes basalt fibers.
4. The linerless pressure vessel of claim 1, the innermost layer being a carbon-fiber free layer.
5. The linerless pressure vessel of claim 1, the innermost layer being an aramid-fiber free layer.
6. The linerless pressure vessel of claim 1, further comprising, another outermost composite material layer being a third layer arranged at a different helical angle.
7. The linerless pressure vessel of claim 6, the different helical angle being in a range of 50 to 80.
8. The linerless pressure vessel of claim 6, further comprising, a fourth composite material layer outward of, and adjacent to, the third layer and arranged in a hoop pattern.
9. The linerless pressure vessel of claim 8, further comprising, a fifth composite material layer outward of, and adjacent to, the fourth composite material layer and including randomly oriented fibers.
10. The linerless pressure vessel of claim 6, further comprising, at least one other composite material layer outward of the third layer and arranged differently than the third layer.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF THE INVENTION
(12) A basalt reinforced plastic material 10 made according to this invention is especially suited for use in high-pressure storage of gaseous matter such industrial and fuel gasses in compressed natural gas applications and compressed hydrogen fuel applications. A composite material made according to this invention also can be used to store other types of gasses, liquids and powders under pressure (or not under pressure).
(13) Referring first to
(14) The first (base or innermost) layer 11 is composed of a resin-impregnated woven basalt fiber sleeve, preferably 13 micron chopped basalt fibers about 12 millimeters in length assembled in the voids of the sleeve and impregnated with an epoxy resin.
(15) The second and third layers 13, 15 are composed of continuous basalt fiber roving arranged in a helical pattern, preferably arranged at about a 2 helical angle, with the third layer 15 being at a 54 helical angle.
(16) The fourth layer 17 is preferably composed of continuous 1200TEX 13 micron basalt fiber roving arranged in a hoop pattern, that is, generally perpendicular to a central longitudinal axis of the mandrel on which the layer is being formed.
(17) The fifth (outermost) layer 19 is preferably composed of randomly oriented chopped 15 micron basalt fibers about 12 millimeters in length impregnated with epoxy resin and compacted.
(18) An aramid fiber, such as DUPONT KEVLAR aramid fiber, may be placed on top of the fifth layer 19 or used as part of the fifth layer 19. Carbon fiber may also be placed on top of the fifth layer 19 or used as part of the fifth layer 19.
(19) Compared to current art materials for use in high-pressure storage of gaseous matter, a basalt fiber-based composite material 10 like that made according to this invention can reduce overall production costs of a pressure vessel like that of
(20) The mandrel 30 is a water-soluble mandrel or tooling (see e.g., R. J. Vaidyanathan et al., A water soluble tooling material for complex polymer composite components and honeycombs. SAMPE Conference Proceedings, (Long Beach, Calif., 2003), hereby incorporated by reference). Because the mandrel 30 is water-soluble, a pressure vessel 20 can be any shape desired for a particular application, including non-spherical shaped or non-cylindrical shaped.
(21) Preferred embodiments, and not all possible embodiments, of the pressure vessel have been described so as to enable of person of ordinary skill in the art to make and use the invention, which is defined by the claims listed below.