Hydrocyclone for cryogenic gas-vapor separation
10328384 ยท 2019-06-25
Assignee
Inventors
- Larry Baxter (Orem, UT, US)
- Christopher Hoeger (Provo, UT, US)
- Aaron Sayre (Spanish Fork, UT, US)
- Skyler Chamberlain (Provo, UT, US)
- Kyler Stitt (Lindon, UT, US)
- Eric Mansfield (Spanish Fork, UT, US)
- Stephanie Burt (Provo, UT, US)
- Andrew Baxter (Spanish Fork, UT, US)
- Jacom Chamberlain (Provo, UT, US)
- Nathan Davis (Bountiful, UT, US)
Cpc classification
F25J3/061
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02P70/10
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
F25J2205/90
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/0655
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2205/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/0695
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/0625
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/0635
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B04C5/14
PERFORMING OPERATIONS; TRANSPORTING
Y02C20/40
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
B01D2257/408
PERFORMING OPERATIONS; TRANSPORTING
F25J2205/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/067
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2270/904
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B04C2009/008
PERFORMING OPERATIONS; TRANSPORTING
B04C5/13
PERFORMING OPERATIONS; TRANSPORTING
B01D53/18
PERFORMING OPERATIONS; TRANSPORTING
B04C9/00
PERFORMING OPERATIONS; TRANSPORTING
F25J2290/44
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01D2257/404
PERFORMING OPERATIONS; TRANSPORTING
B01D7/02
PERFORMING OPERATIONS; TRANSPORTING
F25J2210/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B04C9/00
PERFORMING OPERATIONS; TRANSPORTING
B04C5/14
PERFORMING OPERATIONS; TRANSPORTING
B01D5/00
PERFORMING OPERATIONS; TRANSPORTING
B01D7/02
PERFORMING OPERATIONS; TRANSPORTING
F25J3/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B04C5/13
PERFORMING OPERATIONS; TRANSPORTING
B04C5/00
PERFORMING OPERATIONS; TRANSPORTING
B01D53/18
PERFORMING OPERATIONS; TRANSPORTING
B01D53/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A hydrocyclone for separating a vapor from a carrier gas is disclosed. The hydrocyclone comprises one or more nozzles. A cryogenic liquid is injected to a tangential feed inlet at a velocity that induces a tangential flow and a cyclone vortex in the hydrocyclone. The carrier gas is injected into the cryogenic liquid, causing the vapor to dissolve, condense, desublimate, or a combination thereof, forming a vapor-depleted carrier gas and a vapor-enriched cryogenic liquid. The vapor-depleted carrier gas is drawn through a vortex finder and the vapor-enriched cryogenic liquid is drawn through an apex nozzle outlet. In this manner, the vapor is removed from the carrier gas.
Claims
1. A hydrocyclone for separating a vapor from a carrier gas, the apparatus comprising: a vessel having a generally cylindrical shape with a generally circular cross-section; a tangential feed inlet for a cryogenic liquid, attached to a cylindrical wall of the vessel on an upper end of the vessel, wherein the cryogenic liquid is injected to the tangential feed inlet at a velocity that induces a tangential flow and a cyclone vortex in the hydrocyclone; at least a portion of a wall of the hydrocyclone comprising one or more nozzles, wherein the carrier gas is injected into the cryogenic liquid, causing the vapor to desublimate, forming a vapor-depleted carrier gas and a vapor-enriched cryogenic liquid, wherein the one or more nozzles have injection points that are flush with an inner side of the wall of the hydrocyclone, and wherein any surface of the injection points exposed to the cryogenic liquid comprise a material that inhibits adsorption of gases, prevents deposition of solids, or a combination thereof; a vortex finder outlet on a top of the inner vessel, perpendicular to the tangential feed inlet, through which the vapor-depleted gas is drawn; a lower section of the inner vessel that tapers conically down in size to an apex nozzle outlet through which the vapor-enriched cryogenic liquid is drawn; and, the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet sized to cause a gas/liquid separation; whereby the vapor is removed from the carrier gas.
2. The apparatus of claim 1, wherein the vapor comprises carbon dioxide, nitrogen oxide, sulfur dioxide, nitrogen dioxide, sulfur trioxide, hydrogen sulfide, hydrogen cyanide, water, hydrocarbons with a freezing point above 0 C., or combinations thereof.
3. The apparatus of claim 1, wherein the carrier gas comprises combustion flue gas, syngas, natural gas, steam reforming gas, any hydrocarbon that has higher volatility than water, or combinations thereof.
4. The apparatus of claim 1, wherein the cryogenic liquid comprises any compound or mixture of compounds with a freezing point below a temperature at which a solid forms from the vapor.
5. The apparatus of claim 1, wherein the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet comprise aluminum, stainless steel, polymers, ceramics, or combinations thereof.
6. The apparatus of claim 1, wherein the material comprises ceramics, polytetrafluoroethylene, polychlorotrifluoroethylene, natural diamond, man-made diamond, chemical-vapor deposition diamond, polycrystalline diamond, or combinations thereof.
7. A hydrocyclone for separating a vapor from a carrier gas, the apparatus comprising: a vessel having a generally cylindrical shape with a generally circular cross-section; a tangential feed inlet for a cryogenic liquid, attached to a cylindrical wall of the vessel on an upper end of the vessel, wherein the cryogenic liquid is injected to the tangential feed inlet at a velocity that induces a tangential flow and a cyclone vortex in the hydrocyclone; at least a portion of a wall of the hydrocyclone comprising one or more nozzles, wherein the carrier gas is injected into the cryogenic liquid, causing the vapor to desublimate, forming a vapor-depleted carrier gas and a vapor-enriched cryogenic liquid, wherein the one or more nozzles have injection points that are flush with an inner side of the wall of the hydrocyclone, and wherein the one or more nozzles are attached parallel to the tangential feed inlet to cause a tangential carrier gas stream to inject with the tangential flow of the cryogenic liquid; a vortex finder outlet on a top of the inner vessel, perpendicular to the tangential feed inlet, through which the vapor-depleted gas is drawn; a lower section of the inner vessel that tapers conically down in size to an apex nozzle outlet through which the vapor-enriched cryogenic liquid is drawn; and, the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet sized to cause a gas/liquid separation; whereby the vapor is removed from the carrier gas.
8. The apparatus of claim 7, wherein the vapor comprises carbon dioxide, nitrogen oxide, sulfur dioxide, nitrogen dioxide, sulfur trioxide, hydrogen sulfide, hydrogen cyanide, water, hydrocarbons with a freezing point above 0 C., or combinations thereof.
9. The apparatus of claim 7, wherein the carrier gas comprises combustion flue gas, syngas, natural gas, steam reforming gas, any hydrocarbon that has higher volatility than water, or combinations thereof.
10. The apparatus of claim 7, wherein the cryogenic liquid comprises any compound or mixture of compounds with a freezing point below a temperature at which a solid forms from the vapor.
11. The apparatus of claim 7, wherein the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet comprise aluminum, stainless steel, polymers, ceramics, or combinations thereof.
12. The apparatus of claim 7, wherein any surface of the injection points exposed to the cryogenic liquid comprise a material that inhibits adsorption of gases, prevents deposition of solids, or a combination thereof.
13. The apparatus of claim 12, wherein the material comprises ceramics, polytetrafluoroethylene, polychlorotrifluoroethylene, natural diamond, man-made diamond, chemical-vapor deposition diamond, polycrystalline diamond, or combinations thereof.
14. A hydrocyclone for separating a vapor from a carrier gas, the apparatus comprising: a vessel having a generally cylindrical shape with a generally circular cross-section; a tangential feed inlet for a cryogenic liquid, attached to a cylindrical wall of the vessel on an upper end of the vessel, wherein the cryogenic liquid is injected to the tangential feed inlet at a velocity that induces a tangential flow and a cyclone vortex in the hydrocyclone; at least a portion of a wall of the hydrocyclone comprising one or more nozzles, wherein the carrier gas is injected into the cryogenic liquid, causing the vapor to desublimate, forming a vapor-depleted carrier gas and a vapor-enriched cryogenic liquid, wherein the one or more nozzles have injection points that are flush with an inner side of the wall of the hydrocyclone, and wherein the one or more nozzles are attached anti-parallel to the tangential feed inlet to cause a tangential carrier gas stream to inject against the tangential flow of the cryogenic liquid; a vortex finder outlet on a top of the inner vessel, perpendicular to the tangential feed inlet, through which the vapor-depleted gas is drawn; a lower section of the inner vessel that tapers conically down in size to an apex nozzle outlet through which the vapor-enriched cryogenic liquid is drawn; and, the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet sized to cause a gas/liquid separation; whereby the vapor is removed from the carrier gas.
15. The apparatus of claim 14, wherein the vapor comprises carbon dioxide, nitrogen oxide, sulfur dioxide, nitrogen dioxide, sulfur trioxide, hydrogen sulfide, hydrogen cyanide, water, hydrocarbons with a freezing point above 0 C., or combinations thereof.
16. The apparatus of claim 14, wherein the carrier gas comprises combustion flue gas, syngas, natural gas, steam reforming gas, any hydrocarbon that has higher volatility than water, or combinations thereof.
17. The apparatus of claim 14, wherein the cryogenic liquid comprises any compound or mixture of compounds with a freezing point below a temperature at which a solid forms from the vapor.
18. The apparatus of claim 14, wherein the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet comprise aluminum, stainless steel, polymers, ceramics, or combinations thereof.
19. The apparatus of claim 14, wherein any surface of the injection points exposed to the cryogenic liquid comprise a material that inhibits adsorption of gases, prevents deposition of solids, or a combination thereof.
20. The apparatus of claim 19, wherein the material comprises ceramics, polytetrafluoroethylene, polychlorotrifluoroethylene, natural diamond, man-made diamond, chemical-vapor deposition diamond, polycrystalline diamond, or combinations thereof.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In order that the advantages of the invention will be readily understood, a more particular description of the invention briefly described above will be rendered by reference to specific embodiments illustrated in the appended drawings. Understanding that these drawings depict only typical embodiments of the invention and are not therefore to be considered limiting of its scope, the invention will be described and explained with additional specificity and detail through use of the accompanying drawings, in which:
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DETAILED DESCRIPTION
(8) It will be readily understood that the components of the present invention, as generally described and illustrated in the Figures herein, could be arranged and designed in a wide variety of different configurations. Thus, the following more detailed description of the embodiments of the invention, as represented in the Figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of certain examples of presently contemplated embodiments in accordance with the invention.
(9) Referring to
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(15) In some embodiments, the vapor comprises carbon dioxide, nitrogen oxide, sulfur dioxide, nitrogen dioxide, sulfur trioxide, hydrogen sulfide, hydrogen cyanide, water, hydrocarbons with a freezing point above 0 C, or combinations thereof. In some embodiments, the carrier gas comprises combustion flue gas, syngas, producer gas, natural gas, steam reforming gas, any hydrocarbon that has higher volatility than water, light gases, or combinations thereof. In some embodiments, the cryogenic liquid comprises any compound or mixture of compounds with a freezing point below a temperature at which a solid forms from the vapor.
(16) In some embodiments, the vessel, the tangential feed inlet, the vortex finder, the lower section, and the apex nozzle outlet comprise aluminum, stainless steel, polymers, ceramics, or combinations thereof.
(17) In some embodiments, any surface of the nozzles exposed to the cryogenic liquid comprises a material that inhibits adsorption of gases, prevents deposition of solids, or a combination thereof. This material may comprise ceramics, polytetrafluoroethylene, polychlorotrifluoroethylene, natural diamond, man-made diamond, chemical-vapor deposition diamond, polycrystalline diamond, or combinations thereof.
(18) In some embodiments, the hydrocyclone is insulated. This insulation may comprise perlite, vacuum-chamber, or combinations thereof. In some embodiments, the insulation comprises active cooling.
(19) In some embodiments, the vortex finder operates under a partial vacuum.