US20180259227A1 - Vortex tube - Google Patents
Vortex tube Download PDFInfo
- Publication number
- US20180259227A1 US20180259227A1 US15/975,951 US201815975951A US2018259227A1 US 20180259227 A1 US20180259227 A1 US 20180259227A1 US 201815975951 A US201815975951 A US 201815975951A US 2018259227 A1 US2018259227 A1 US 2018259227A1
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- United States
- Prior art keywords
- vortex tube
- heat exchanger
- tube
- diaphragm
- opening
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/02—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect
- F25B9/04—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect using vortex effect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
- B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/02—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect
Definitions
- This invention is directed to the field of vortex tubes. More particularly, the present invention relates to a manufacture using a method of a vortex tube design, which provides a vortex tube having a high efficiency by eliminating freeze up in operations with natural gas.
- a vortex tube comprises a slender tube with a diaphragm with a discharge hole in the center of the diaphragm, closing one end of the tube, one or more tangential inlet nozzles piercing the tube just inside of the diaphragm and, depending on the vortex tube's desirable performance, a controlled discharge opening (throttle valve) or plug (U.S. Pat. No. 5,911,740) on the other end of the slender tube.
- a controlled discharge opening throttle valve
- plug U.S. Pat. No. 5,911,740
- the inlet high-pressure gas passes through the tangential nozzles resulting in a pressure decrease and velocity increase of the gas.
- the low pressure highly rotating gas then undergoes energy separation (vortex phenomenon) forming two internal low-pressure currents.
- the present invention provides for improving the reliability of the vortex tubes designed per U.S. Pat. No. 5,749,231
- the improvement is achieved by specifying the VT diaphragm hole preferably in a range of 0.25 to 0.80 of the slender tube's diameter, the vortex tube's length, preferably, as no less than 3 diameters of the slender tube and the vortex tube's uncontrolled opening diameter as no greater than 0.60 of the slender tube's diameter.
- FIG. 1 is a schematic design and flow diagram of an embodiment of the invention.
- FIG. 2 is a schematic design and flow diagram of a preferred embodiment of the invention.
- FIG. 3 is a schematic design and flow diagram of a preferred embodiment of the invention.
- FIG. 4 is a schematic design and flow diagram of a preferred embodiment of the invention.
- the transmission of natural gas starts with the extraction point (typically a wellhead) at very high pressures through a pipeline to distribution hubs and then ultimately into low pressure networks for delivery of natural gas to the end user.
- This process from wellhead to end user is comprised of a series of pressure reducing operations. It is common practice to preheat the gas at pipeline pressure regulation stations along the transmission line in an effort to compensate for the Joule-Thompson temperature drop in depressurized gas. This pre-heating process prevents water in the form of hydrocarbons condensing and freezing in the pressure regulating valves along the transmission system.
- a glycol additive is used to prevent freezing.
- the problem to be solved to which the present invention is directed is how to prevent non-preheated, non-glycol treated natural gas (and other non-dried gases) from freezing as the gas is expanded in pressure regulation.
- the problem arises when the temperature of the gas being transmitted is dropped as a result of the pressure reduction that takes place with the use of a vortex tube in the transmission line. This results in cooling (refrigeration) in the vortex tube pressure reducing nozzle, which is what the present invention is directed to eliminate/reduce.
- One way in which this refrigeration effect is minimized is to use the hot portion air of the vortex tube and direct it onto the cold flow portion where freezing is occurring. See, Tunkel U.S. Pat. No. 5,749,231. Further, the present invention discloses vortex tube geometric relationships aimed at increasing the vortex tube thermal efficiency by generating more heat out of the “hot side” of the vortex tube. This facilitates the more efficient warming pressure reducing nozzle on the “cold side” of the vortex tube.
- a non-freeze vortex tube assembly 50 includes a vortex tube 10 provided with the inlet nozzle 12 , a diaphragm 14 provided with a central hole 16 , a slender tube 18 of the internal diameter D with its outlet opening 20 and a heat exchanger 22 provided with an inner passage 24 , two inlet openings 26 and 28 , one outlet opening 30 and an uncontrolled opening 32 set up on the inner passage's 24 surface.
- the uncontrolled opening 32 is a hole without any air throttling device associated with it. Openings 26 and 30 also serve as inner passage's 24 inlet and outlet, respectively.
- a gas flow in the direction of arrow 40 enters assembly 50 through the vortex tube's nozzles 12 and then undergoes an energy (temperature) separation forming a cold and hot fraction.
- a cold fraction is discharged from the vortex tube 10 through diaphragm hole 16 and enters into a heat exchanger inlet opening 26 , then goes through inner passage 24 in the heat exchanger and leaves or exits the heat exchanger 22 through its outlet opening 30 .
- a hot fraction passes through slender tube's 18 outlet opening 20 and is then directed through line 34 and its outlet 36 and enters into heat exchanger 22 through inlet opening 28 and goes toward the uncontrolled opening 32 simultaneously flowing over the surfaces on the inside of the heat exchanger 22 and leaves or exits the heat exchanger through uncontrolled opening 32 , mixing with the cold fraction exiting the vortex tube.
- the uncontrolled opening is preferably located on such side of the passage 30 which is opposite to the heat exchanger inlet 28 ; the opening diameter is, preferably, less than vortex tube's diaphragm diameter.
- the gas passing through the VT's pressure reducing nozzles generally, carries some liquid (water and hydrocarbons) condensed under the depressurized gas low thermodynamic temperatures and Joule-Thomson temperature drop.
- the condensed liquid due to its gravity, provides for a substantial portion of the by-pass flow.
- the two-phase chilled mixture mixing up with the vortex tube's cold outlet or with the vortex tube's single discharge flow results in freezing of the diaphragm hole which reduces the interior diameter of the orifice 16 and accordingly the vortex tube performance deteriorates.
- Reduction of the diaphragm's hole 16 diameter is an efficient way to reduce the by-pass stream flow rate.
- a smaller diaphragm hole increases the gas pressure in the vortex tube. This results in decreasing the vortex pressure ratio (ratio of the inlet gas pressure to the gas pressure in the vortex tube). This, in turn, reduces the intensity of the vortex energy division in the gas flow.
- the best results with the present invention can be achieved by specifying the diaphragm's hole diameter 16 , preferably, in a range of 0.25 to 0.80 of the slender tube diameter D. See, FIG. 3 .
- the length of the vortex tube shall allow for completing the vortex energy division, thus to efficiently warm the diaphragm in a heat exchanger as described US in U.S. Pat. No. 6,289,679.
- the uncontrolled opening 32 in a heat exchanger shall allow for efficient circulation of just the vortex hot (peripheral) flow without blending it with the vortex cold (central) flows.
- the optimal results with the present invention can be achieved by specifying the length of the vortex tube as no less than 3.0 diameters (D) of the slender tube (See FIG. 4 ) and the uncontrolled opening's diameter as no greater than 0.60 diameter (D) of the slender tube. See, FIG. 2 .
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
A vortex tube is disclosed. A vortex tube is a slender tube with a diaphragm closing one end of the tube with a discharge hole in the center of the diaphragm with tangential inlet nozzles. The vortex tube separates an inlet gas stream into two compartments. The present invention relates to an optional geometry of the vortex tube for use with compressed natural gas.
Description
- This application is a continuation-in-part and claims priority to U.S. Non-provisional application Ser. No. 14/559,334, filed Dec. 3, 2014.
- This invention is directed to the field of vortex tubes. More particularly, the present invention relates to a manufacture using a method of a vortex tube design, which provides a vortex tube having a high efficiency by eliminating freeze up in operations with natural gas.
- A vortex tube (VT) comprises a slender tube with a diaphragm with a discharge hole in the center of the diaphragm, closing one end of the tube, one or more tangential inlet nozzles piercing the tube just inside of the diaphragm and, depending on the vortex tube's desirable performance, a controlled discharge opening (throttle valve) or plug (U.S. Pat. No. 5,911,740) on the other end of the slender tube.
- In the vortex tube, the inlet high-pressure gas passes through the tangential nozzles resulting in a pressure decrease and velocity increase of the gas. The low pressure highly rotating gas then undergoes energy separation (vortex phenomenon) forming two internal low-pressure currents.
- One current is cold and the other is hot. Under some circumstances a cold fraction or cold gas discharged from the vortex tube through the diaphragm opening may freeze up and reduce the diameter of the discharge orifice due to the formation of ice, resulting in the vortex tube's performance deterioration.
- It is known to use a vortex tube's hot fraction to prevent freezing in the discharge diaphragm (U.S. Pat. No. 5,749,231 and U.S. Pat. No. 5,937,654) as well as, as it is practiced in the vortex tubes of the present invention to use the hot fraction to warm up the vortex tube's inlet nozzles.
- The present invention provides for improving the reliability of the vortex tubes designed per U.S. Pat. No. 5,749,231 |and U.S. Pat. No. 5,937,654 in operation with compressed natural gas. The improvement is achieved by specifying the VT diaphragm hole preferably in a range of 0.25 to 0.80 of the slender tube's diameter, the vortex tube's length, preferably, as no less than 3 diameters of the slender tube and the vortex tube's uncontrolled opening diameter as no greater than 0.60 of the slender tube's diameter.
-
FIG. 1 is a schematic design and flow diagram of an embodiment of the invention. -
FIG. 2 is a schematic design and flow diagram of a preferred embodiment of the invention. -
FIG. 3 is a schematic design and flow diagram of a preferred embodiment of the invention. -
FIG. 4 is a schematic design and flow diagram of a preferred embodiment of the invention. - The present invention will now be described in terms of the presently preferred embodiment thereof as illustrated in the drawings. Those of ordinary skill in the art will recognize that this embodiment is merely exemplary of the present invention and many obvious modifications may be made thereto without departing from the spirit or scope of the present invention as set forth in the appended claims.
- The transmission of natural gas starts with the extraction point (typically a wellhead) at very high pressures through a pipeline to distribution hubs and then ultimately into low pressure networks for delivery of natural gas to the end user. This process from wellhead to end user is comprised of a series of pressure reducing operations. It is common practice to preheat the gas at pipeline pressure regulation stations along the transmission line in an effort to compensate for the Joule-Thompson temperature drop in depressurized gas. This pre-heating process prevents water in the form of hydrocarbons condensing and freezing in the pressure regulating valves along the transmission system. At the wellhead—where heating the gas cannot be employed—a glycol additive is used to prevent freezing.
- The problem to be solved to which the present invention is directed is how to prevent non-preheated, non-glycol treated natural gas (and other non-dried gases) from freezing as the gas is expanded in pressure regulation. The problem arises when the temperature of the gas being transmitted is dropped as a result of the pressure reduction that takes place with the use of a vortex tube in the transmission line. This results in cooling (refrigeration) in the vortex tube pressure reducing nozzle, which is what the present invention is directed to eliminate/reduce.
- One way in which this refrigeration effect is minimized is to use the hot portion air of the vortex tube and direct it onto the cold flow portion where freezing is occurring. See, Tunkel U.S. Pat. No. 5,749,231. Further, the present invention discloses vortex tube geometric relationships aimed at increasing the vortex tube thermal efficiency by generating more heat out of the “hot side” of the vortex tube. This facilitates the more efficient warming pressure reducing nozzle on the “cold side” of the vortex tube.
- The flow diagram in FIG I illustrates an embodiment of the invention. A non-freeze
vortex tube assembly 50 according to the invention includes avortex tube 10 provided with the inlet nozzle 12, a diaphragm 14 provided with acentral hole 16, aslender tube 18 of the internal diameter D with its outlet opening 20 and aheat exchanger 22 provided with aninner passage 24, twoinlet openings uncontrolled opening 32 set up on the inner passage's 24 surface. Theuncontrolled opening 32 is a hole without any air throttling device associated with it.Openings arrow 40 entersassembly 50 through the vortex tube's nozzles 12 and then undergoes an energy (temperature) separation forming a cold and hot fraction. A cold fraction is discharged from thevortex tube 10 throughdiaphragm hole 16 and enters into a heat exchanger inlet opening 26, then goes throughinner passage 24 in the heat exchanger and leaves or exits theheat exchanger 22 through its outlet opening 30. A hot fraction passes through slender tube's 18 outlet opening 20 and is then directed throughline 34 and itsoutlet 36 and enters intoheat exchanger 22 through inlet opening 28 and goes toward theuncontrolled opening 32 simultaneously flowing over the surfaces on the inside of theheat exchanger 22 and leaves or exits the heat exchanger throughuncontrolled opening 32, mixing with the cold fraction exiting the vortex tube. The uncontrolled opening is preferably located on such side of thepassage 30 which is opposite to theheat exchanger inlet 28; the opening diameter is, preferably, less than vortex tube's diaphragm diameter. - It is known that a small portion of the vortex tube's inlet gas flow does not participate in the vortex energy division but moves alongside the diaphragm inward surface directly into the diaphragm hole. The existence of such a bypass flow is due to the presence of the radial pressure gradient uncompensated by the centrifugal forces in the stationary boundary layer on the wall of the diaphragm. Mixture of the bypass flow that keeps the original inlet gas temperature with the cold gas passing through the diaphragm hole increases the vortex cold outlet temperature. Such thermal influence, at times noticeable, does not affect the vortex tube operations unless compressed natural gas is used as the vortex tube's working medium.
- Here the gas passing through the VT's pressure reducing nozzles, generally, carries some liquid (water and hydrocarbons) condensed under the depressurized gas low thermodynamic temperatures and Joule-Thomson temperature drop. The condensed liquid, due to its gravity, provides for a substantial portion of the by-pass flow. The two-phase chilled mixture mixing up with the vortex tube's cold outlet or with the vortex tube's single discharge flow (per U.S. Pat. No. 5,911,740) results in freezing of the diaphragm hole which reduces the interior diameter of the
orifice 16 and accordingly the vortex tube performance deteriorates. - Reduction of the diaphragm's
hole 16 diameter is an efficient way to reduce the by-pass stream flow rate. However, a smaller diaphragm hole increases the gas pressure in the vortex tube. This results in decreasing the vortex pressure ratio (ratio of the inlet gas pressure to the gas pressure in the vortex tube). This, in turn, reduces the intensity of the vortex energy division in the gas flow. - The best results with the present invention can be achieved by specifying the diaphragm's
hole diameter 16, preferably, in a range of 0.25 to 0.80 of the slender tube diameter D. See,FIG. 3 . The length of the vortex tube shall allow for completing the vortex energy division, thus to efficiently warm the diaphragm in a heat exchanger as described US in U.S. Pat. No. 6,289,679. Theuncontrolled opening 32 in a heat exchanger shall allow for efficient circulation of just the vortex hot (peripheral) flow without blending it with the vortex cold (central) flows. The optimal results with the present invention can be achieved by specifying the length of the vortex tube as no less than 3.0 diameters (D) of the slender tube (SeeFIG. 4 ) and the uncontrolled opening's diameter as no greater than 0.60 diameter (D) of the slender tube. See,FIG. 2 .
Claims (3)
1. A method for a non-freeze enhancement in a vortex tube assembly, said non-freeze enhanced vortex tube assembly includes a heat exchanger having an uncontrolled opening with a diameter (d) in the heat exchanger's inner passage and a vortex tube comprising a slender tube with a diameter (D), the uncontrolled opening diameter (d) is no greater than 0.6 times the slender tube diameter (D), a diaphragm having a hole in the center thereof and closing one end of the vortex tube. one or more tangential nozzles piercing the slender tube just inside the diaphragm and an outlet opening on the other end of the vortex tube, the method comprises ways of connecting the non-freeze enhanced vortex tube as follows:
a. attaching the heat exchanger to an outward side of a vortex tube's diaphragm;
b. connecting a vortex tube's diaphragm for discharging a cold fraction flow with the heat exchanger's inlet opening and then connecting the inlet opening through the heat exchanger's inner passage with the heat exchanger's outlet opening to discharge gas flow from the non-freeze enhanced vortex tube assembly; and
c. connecting a vortex tube outlet opening at the far end of the vortex tube with another inlet opening of the heat exchanger, thus providing for the hot flow to flow over the surfaces on the inside of the heat exchanger and then leave or exit the heat exchanger through an uncontrolled opening in the heat exchanger's inner passage to mix with the cold fraction exiting the vortex tube.
2. A method for a non-freeze enhancement in a vortex tube assembly, said non-freeze enhanced vortex tube assembly includes a heat exchanger having an uncontrolled opening with a diameter (d) in the heat exchanger's inner passage and a vortex tube comprising a slender tube with a diameter (D), a diaphragm having a hole in the center thereof wherein the vortex tube diaphragm hole has a diameter in the range of 0.25 to 0.80 times the slender tube diameter (D) and closing one end of the vortex tube, one or more tangential nozzles piercing the slender tube just inside the diaphragm and an outlet opening on the other end of the vortex tube, the method comprises ways of connecting the non-freeze enhanced vortex tube as follows:
a. attaching the heat exchanger to an outward side of a vortex tube's diaphragm;
b. connecting a vortex tube's diaphragm for discharging a cold fraction flow with the heat exchanger's inlet opening and then connecting the inlet opening through the heat exchanger's inner passage with the heat exchanger's outlet opening to discharge gas flow from the non-freeze enhanced vortex tube assembly; and
c. connecting a vortex tube outlet opening at the far end of the vortex tube with another inlet opening of the heat exchanger, thus providing for the hot flow to flow over the surfaces on the inside of the heat exchanger and then leave or exit the heat exchanger through an uncontrolled opening in the heat exchanger's inner passage to mix with the cold fraction exiting the vortex tube.
3. A method for a non-freeze enhancement in a vortex tube assembly, said non-freeze enhanced vortex tube assembly includes a heat exchanger having an uncontrolled opening with a diameter (d) in the heat exchanger's inner passage and a vortex tube comprising a slender tube with a diameter (D), the length of the vortex tube is no less than 3 times the slender tube diameter (D), a diaphragm having a hole in the center thereof and closing one end of the vortex tube, one or more tangential nozzles piercing the slender tube just inside the diaphragm and an outlet opening on the other end of the vortex tube, the method comprises ways of connecting the non-freeze enhanced vortex tube as follows:
d. attaching the heat exchanger to an outward side of a vortex tube's diaphragm;
e. connecting a vortex tube's diaphragm for discharging a cold fraction flow with the heat exchanger's inlet opening and then connecting the inlet opening through the heat exchanger's inner passage with the heat exchanger's outlet opening to discharge gas flow from the non-freeze enhanced vortex tube assembly; and
f. connecting a vortex tube outlet opening at the far end of the vortex tube with another inlet opening of the heat exchanger, thus providing for the hot flow to flow over the surfaces on the inside of the heat exchanger and then leave or exit the heat exchanger through an uncontrolled opening in the heat exchanger's inner passage to mix with the cold fraction exiting the vortex tube.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/975,951 US20180259227A1 (en) | 2014-12-03 | 2018-05-10 | Vortex tube |
US16/696,486 US20200096237A1 (en) | 2014-12-03 | 2019-11-26 | Vortex tube |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/559,334 US20160158900A1 (en) | 2014-12-03 | 2014-12-03 | Vortex Tube |
US15/975,951 US20180259227A1 (en) | 2014-12-03 | 2018-05-10 | Vortex tube |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/559,334 Continuation-In-Part US20160158900A1 (en) | 2014-12-03 | 2014-12-03 | Vortex Tube |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US16/696,486 Continuation US20200096237A1 (en) | 2014-12-03 | 2019-11-26 | Vortex tube |
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US20180259227A1 true US20180259227A1 (en) | 2018-09-13 |
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Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
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US15/975,951 Abandoned US20180259227A1 (en) | 2014-12-03 | 2018-05-10 | Vortex tube |
US16/696,486 Pending US20200096237A1 (en) | 2014-12-03 | 2019-11-26 | Vortex tube |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
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US16/696,486 Pending US20200096237A1 (en) | 2014-12-03 | 2019-11-26 | Vortex tube |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11493239B2 (en) | 2018-09-28 | 2022-11-08 | Universal Vortex, Inc. | Method for reducing the energy necessary for cooling natural gas into liquid natural gas using a non-freezing vortex tube as a precooling device |
Citations (11)
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---|---|---|---|---|
US6289679B1 (en) * | 1999-07-13 | 2001-09-18 | Universal Vortex, Inc | Non-freeze enhancement in the vortex tube |
US6379411B1 (en) * | 2000-04-26 | 2002-04-30 | Bechtel Bwxt Idaho, Llc | Two stroke engine exhaust emissions separator |
US20020194988A1 (en) * | 1998-12-31 | 2002-12-26 | M. Betting | Supersonic separator apparatus and method |
US6962199B1 (en) * | 1998-12-31 | 2005-11-08 | Shell Oil Company | Method for removing condensables from a natural gas stream, at a wellhead, downstream of the wellhead choke |
US20060163054A1 (en) * | 2002-07-23 | 2006-07-27 | Ralf Spitzl | Plasma reactor for carrying out gas reactions and method for the plasma-supported reaction of gases |
US20060230765A1 (en) * | 2005-04-14 | 2006-10-19 | Fedorov Andrei G | Vortex tube refrigeration systems and methods |
US20080133110A1 (en) * | 2006-03-27 | 2008-06-05 | Jan Vetrovec | Turbocharged internal combustion engine system |
US7565808B2 (en) * | 2005-01-13 | 2009-07-28 | Greencentaire, Llc | Refrigerator |
US7654095B2 (en) * | 2007-06-06 | 2010-02-02 | Greencentaire, Llc | Energy transfer apparatus and methods |
US20100139292A1 (en) * | 2008-12-08 | 2010-06-10 | Ram Grand | Temperature adjustable airflow device |
US20130067905A1 (en) * | 2010-11-12 | 2013-03-21 | Eckert Engine Company, Inc. | Heat Exchanger for Engine |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5749231A (en) * | 1996-08-13 | 1998-05-12 | Universal Vortex, Inc. | Non-freezing vortex tube |
-
2018
- 2018-05-10 US US15/975,951 patent/US20180259227A1/en not_active Abandoned
-
2019
- 2019-11-26 US US16/696,486 patent/US20200096237A1/en active Pending
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020194988A1 (en) * | 1998-12-31 | 2002-12-26 | M. Betting | Supersonic separator apparatus and method |
US6962199B1 (en) * | 1998-12-31 | 2005-11-08 | Shell Oil Company | Method for removing condensables from a natural gas stream, at a wellhead, downstream of the wellhead choke |
US6289679B1 (en) * | 1999-07-13 | 2001-09-18 | Universal Vortex, Inc | Non-freeze enhancement in the vortex tube |
US6379411B1 (en) * | 2000-04-26 | 2002-04-30 | Bechtel Bwxt Idaho, Llc | Two stroke engine exhaust emissions separator |
US20060163054A1 (en) * | 2002-07-23 | 2006-07-27 | Ralf Spitzl | Plasma reactor for carrying out gas reactions and method for the plasma-supported reaction of gases |
US7565808B2 (en) * | 2005-01-13 | 2009-07-28 | Greencentaire, Llc | Refrigerator |
US20060230765A1 (en) * | 2005-04-14 | 2006-10-19 | Fedorov Andrei G | Vortex tube refrigeration systems and methods |
US20080133110A1 (en) * | 2006-03-27 | 2008-06-05 | Jan Vetrovec | Turbocharged internal combustion engine system |
US7654095B2 (en) * | 2007-06-06 | 2010-02-02 | Greencentaire, Llc | Energy transfer apparatus and methods |
US20100139292A1 (en) * | 2008-12-08 | 2010-06-10 | Ram Grand | Temperature adjustable airflow device |
US20130067905A1 (en) * | 2010-11-12 | 2013-03-21 | Eckert Engine Company, Inc. | Heat Exchanger for Engine |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11493239B2 (en) | 2018-09-28 | 2022-11-08 | Universal Vortex, Inc. | Method for reducing the energy necessary for cooling natural gas into liquid natural gas using a non-freezing vortex tube as a precooling device |
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US20200096237A1 (en) | 2020-03-26 |
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