US3174294A - Oxygen dispensing - Google Patents

Oxygen dispensing Download PDF

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US3174294A
US3174294A US781609A US78160958A US3174294A US 3174294 A US3174294 A US 3174294A US 781609 A US781609 A US 781609A US 78160958 A US78160958 A US 78160958A US 3174294 A US3174294 A US 3174294A
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liquid
oxygen
container
outlet
pressure
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US781609A
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Joseph S Lawrence
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Airco Inc
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Air Reduction Co Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D10/00Flight suits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C9/00Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
    • F17C9/02Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure with change of state, e.g. vaporisation

Definitions

  • the invention relates to systems for dispensing or supplying gaseous oxygen, and is more particularly directed to novel methods and means for enabling a liquid oxygen converter system to operate reliably and effectively when the system is subjected to an adverse gravitational environment, or an environment where the force of gravity is non-existent or insufiicient to establish the desired separation of the liquid and gaseous phases of the oxygen.
  • the proper operation of the usual or conventional liquid oxygen converter system requires that the fluid discharged into the system from the container, which holds the supply of liquid oxygen and contains both the liquid and gas phases, shall be of uniform density. Except where the rate of consumption of gas is small, practical considerations require that the liquid form of the oxygen be delivered to the system for vaporization externally of the container. In the event of intermittent discharge of oxygen from the liquid and gaseous phases, the delivery fluid is of non-uniform density, which detrimentally affects the maintenance of the desired operating conditions of the system. In conventional types of liquid oxygen converters, the delivery from the container of oxygen of uniform density depends upon the force of gravity to separate the liquid from the gas.
  • An object of the invention is to provide a method and means wherein, despite the absence of the full force of gravity, the liquid phase of oxygen may be maintained separately from the gaseous phase, thereby allowing delivery of oxygen of uniform density under controlled conditions.
  • Another object of the invention is to provide a method and means wherein, despite the absence of the full force of gravity, a liquid seal may be provided at the container outlet of a liquid oxygen converter system, thereby enabling the maintenance of the desired operating pressure in the container, and the delivery of oxygen of uniform density to the system.
  • a further object of the invention is to provide a method and means wherein, despite the absence of the full force of gravity, the liquid phase of oxygen may be maintained separately from the gaseous phase so that liquid oxygen may be made available for delivery from the container and the controlled vaporization thereof externally of the container.
  • a magnetic field upon liquid oxygen is effective to attract, sustain or maintain the liquid phase of oxygen in preference to the gaseous phase.
  • the preferential elfect of a magnetic field upon liquid oxygen is utilized to separate the liquid from the gaseous phase to insure the delivery of oxygen having a uniform density, as distinguished from an intermittent discharge of the liquid and the gas.
  • such preferential effect of a magnetic field upon the liquid phase of oxygen serves to effectively separate the liquid from the gas to permit oxygen of uniform density to be delivered to the system under controlled conditions, though the system is located in an environment where the force of gravity normally acting to separate the liquid and gaseous phases is either non-existent or adverse.
  • the preferential effect of a magnetic field for the liquid phase of oxygen is utilized to provide a mass or quantity of liquid oxygen at the outlet of the oxygen container for the converter system.
  • the container which holds the oxygen in both the liquid and gaseous phases, is thereby provided with a liquid seal at or over the outlet.
  • the container pressure may be maintained at a desired value, and oxygen of uniform density may be circulated in the system.
  • an operative quantity of liquid oxygen is made available for delivery from the container to an evaporating coil, where the liquid may be controllably vaporized, and the resultant gas delivered to the point of use at the desired temperature and pressure. Any known or suitable means may be used to furnish the desired container pressure to deliver the operative quantity of liquid oxygen sustained at the outlet to the external evaporating coil.
  • the magnetic field may be furnished by an electromagnet or by a permanent magnet.
  • FIG. 1 is a schematic view of one type of liquid oxygen converter system which may be provided wtih a magnetic separating means of the invention
  • FIG. 2 is an enlarged, vertical cross-sectional view of the outlet area of the container shown in FIG. 1;
  • FIG. 3 is a top plan view taken in the direction of line 3-3 of FIG. 2;
  • FIG. 4 illustrates a permanent magnet assembly which may be used in lieu of the electro-magnet shown in FIG. 2; r
  • FIG. 5 is a top plan view of the permanent magnet assembly shown in FIG. 4;
  • FIG. 6 is a schematic view of another type of liquid oxygen converter system which may be provided with a magnetic ,separatingmeans of the invention.
  • FIG. 7 is a view similar to FIG. 2, but showing another form of the invention insofar as the positional relationship of the magnetic means with respect to the container outlet.
  • an insulated container or chamber 10 for supplying oxygen to a converter system, the container having a discharge outlet, generally designated 12, on the bottom side thereof.
  • the container comprises an inner shell 14 and an outer shell 16 spaced therefrom.
  • the shells may be made of copper, aluminum or stainless steel.
  • the space between the shells is evacuated and/ or filled with a suitable insulating mate- 3 rial to provide the desired insulating characteristics.
  • the top side of the container is provided with a neck 18 closed by a cap 20 connected to the neck, as by mating threads 22.
  • a filling line 24 extends through the cap 20 and into the container.
  • the filling line is provided with a filler valve 26 so that a liquid oxygen source or tank may be connected to the valve to fill the container when empty.
  • a magnetic field is provided at, or in the vicinity of, the outlet 12.
  • the outlet is provided with a liquid seal.
  • the magnetic field maintains an operative quantity of liquid oxygen at the outlet to insure that the liquid phase, designated B, will be available for delivery to the supply circuit under the influence of the pressure provided by the gaseous phase, designated A, within the container.
  • the supply circuit includes an evaporating and superheating coil 28, one side of which is in communication with the outlet 12 through a conduit or line 30, the other side of the coil being in communication with a supply valve 32.
  • the supply valve is adapted for connection to a line to furnish the gas evaporated and warmed by the coil 28 to the point of use.
  • a high-pressure relief valve 34 is disposed between the coil and the supply valve.
  • a spring loaded liquid check valve 36 is located in the line between the supply circuit and a gas pressurizing circuit which will be subsequently described.
  • the outlet 12 is in the form of a tube 38, which may be made a part of an electro-magnet assembly, generally designated 39.
  • the tube which is formed of a non-magnetic material, such as aluminum, is suitably wound with a wire in a plurality of adjacent or helical turns to provide a coil 40.
  • the wire wound tube may be enclosed in a second tube 42, also of a non-magnetic material.
  • the coil is encased or potted in a suitable insulating material 44, such as an epoxy resin compound.
  • the electro-magnet is preferably positioned to extend between the inner and outer shells 14 and 16, and is secured in place, as by welding portions of the tube 42 to adjacent portions of the shells at the areas 46.
  • the outlet tube 38 is of suflicient length so that the lower end thereof may be secured to the line 30 outside the shell 16.
  • the connection may be accomplished by a clamp 48, as shown, or the tube and the line may be matingly threaded.
  • the exterior of the container outlet area, including the described surrounding electro-magnet, is provided with an insulating wall 50 to minimize heat leakage.
  • the insulating wall is connected or secured to the outer shell 16, and is of a contour to furnish a chamber 52.
  • the insulating Wall is provided with an aperture 54 to allow the line 36 to extend therethrough.
  • the ends of the coil are brought out through a hermetically sealed plug 56 secured in the insulating wall so that the coil may be connected to a suitable source of power.
  • Gas pressurizing means is provided to maintain the desired container pressure so that the operative quantity 'of liquid oxygen magnetically maintained at the container outlet may be delivered to the supply circuit and the evaporating coil 28.
  • the pressurizing means includes heating means intheform of an electrical resistance heating element or coil 58. As shown, the coil is positioned within the container and over the container outlet; also, the coil is located within or adjacent to the magnetic field provided by the magnet.
  • the straight portions 60, 60' of the coil extend through, and are supported by, the inner and "outer shells 14 and 16. The extremities of the coil are connected to conductors or wires 62, 62 which terminate in a socket 64 secured to extend through the insulation wall 59.
  • a gas or vapor line 66 extends through the cap 20 and is in communication with the neck end 18 of the container.
  • a relief or vent valve68 and a pressure gauge 70 are disposed in the line.
  • a pressure-opening valve 72 and a gas check valve 74 are positioned between the upper or gas side of the container and the supply circuit, a line 76 being provided between the pressure-opening valve and the liquid supply line 30.
  • pressure control means or a gas pressure responsive switch 78 is provided in the line 66.
  • the pressure responsive switch senses any drop in container pressure below a desired predetermined value to energize the coil 58, and to restore the pressure to the desired value.
  • the pressure responsive switch is connected to the heating coil by electrical conductors or leads 8!), 80', which terminate in a plug 82 received within the socket 64.
  • a source 83 of electrical power for example, a battery, provides the energy for heating the coil 58.
  • the gas pressure responsive switch may be of any suitable type.
  • a suitable trap means is provided at or near the juncture of the liquid supply line 30 and the container outlet within a heat insulated zone, such as the area between the container shells or the described chamber 52.
  • the trap means may comprise a check valve, generally designated 84, positioned within the outlet tube 38.
  • the check valve made of non-magnetic components, may be of any suitable construction.
  • the valve may comprise a seat 86 formed integrally with the tube 38 and extending radially inward thereof for a portion of the tube diameter to provide a valve opening 88.
  • a disk 90 at the end of a stem 92 is adapted for engagement with the seat.
  • the stem extends through a bore provided by a hollow cylinder 94, the stem being held against separation from the cylinder by a cross-pin 96 therethrough, which also limits the extent of opening movement of the valve disk.
  • the cylinder is supported at the center of a plurality of circumferentially and equidistantly spaced vanes 98 which are secured to and extend radially inward from the tube 38.
  • the check valve prevents the back flow of vapor into the container and the continuous feeding of liquid from the container to the supply line 30 when the converter is not in operation.
  • liquid will tend to flow by gravity through the outlet into the supply line 30 where heat imparted from the surrounding atmosphere will cause it to become vaporized.
  • Such vaporized liquid will then pass backwardly to the container and be replaced by further gravitational feed of liquid. This cycle normally would proceed continuously with the result that the container pressure would rapidly increase and eventually vent to the atmosphere permitting a loss of some of the oxygen contents.
  • the initial pressure produced by vaporization of the liquid in the supply line will prevent any further delivery of liquid from the container until the supply valve of the converter is opened, permitting the discharge of the contents of the container under the propelling influence of the differential pressure between the container and the pressure of the supply line.
  • the trap means is similarly effective while the converter is not in operation even under a non-gravitational environment. It may be seen, for example, that under such condition, the liquid oxygen within the container exhibits a tendency to become symmetrically disposed under the influence of the magnetic field of the magnet 39.
  • the liquid or a portion of the liquid mass so influenced may become located in a region which is exposed to a relatively high input of heat from the surrounding atmosphere, causing such liquid to become vaporized.
  • the check valve then operates in substantially the same manner as under gravity conditions so that such vaporization, if and when it may occur, will cause the valve to close and prevent the passage of liquid oxygen to such region until the supply valve of the delivery circuit is opened. It may be seen, of course, that when the delivery tube from the container is arranged to pass upwardly and through the top of the container, trap means or a check valve device would then not be needed.
  • a liquid oxygen source is connected to the filler valve 26, and the vent valve 68 is opened. Liquid oxygen flows into the converter, from which it is boiled off while cooling the internal parts of the system down to the temperature of the liquid oxygen. The resulting gas is vented through the vent valve. When liquid oxygen begins to issue from the vent valve, the filling operation is stopped and the filler and vent valves .are closed.
  • the electro-magnet is energized, thereby sustaining a mass of the liquid within its field to provide a liquid seal and maintain an operative quantity of liquid oxygen at the container outlet.
  • the supply valve 32 is then opened. Before the magnetically sustained liquid oxygen is delivered from the container to the supply line and to the coil 28, a limited quantity of gas accumulated in the container at a pressure exceeding the desired operating pressure is economized and delivered to the supply valve.
  • the pressure-opening valve 72 is set to automatically open at a desired value and permit gas to flow through the check valve 74 and to the supply circuit and supply valve.
  • the gas check valve 74 and the liquid check valve 36 prevent reverse flow.
  • the pressure loading of the check valve 36 requires a slight differential pressure across the check valve to allow the flow of liquid from the container through the line 30 so that such flow of liquid may not occur as long as the opening valve 72 is open and vapor from the container is being delivered therethrough.
  • the pressure-opening valve 72 closes automatically slightly above the desired operating pressure, and such pressure is maintained by the control aiforded by the described pressure responsive switch and heating coil arrangement. The maintenance by the magnetic field of an operative quantity of liquid oxygen to cover the container outlet, and the pressure of the gas upon the liquid, assures that only liquid oxygen will be transferred to the evaporating coil 28 for its controlled vaporization and warming, and delivery to the supply valve.
  • the magnetic means of the invention may be utilized to concentrate a mass of liquid oxygen within an area of the container for the purpose of controllably vaporizing the liquid within the container at such area by suitable heating means, such as the heating coil 58.
  • suitable heating means such as the heating coil 58.
  • the resultant gas delivered from the container then need only be warmed to permit its use. When the gas phase is thus taken from the container, the trap means is unnecessary.
  • the magnetic means may be in the form of a permanent magnet, generally designated 100.
  • the permanent magnet may comprise an assembly of a plurality of magnets, for example, four magnets 102a, 102b, 1020 and 102d as shown.
  • the permanent magnets are preferably equidistantly spaced from one another and supported between inner and outer tubes 104 and 106, respectively.
  • Like pole faces are located at the same ends of the assembly, and the assembly may be secured in position between the inner and outer shells at the areas 108.
  • valve trap 84 may be separately provided for in a tubular element 110, instead of being made a part of, and located within, the outlet tube of the magnet assembly, as shown in FIG. 2.
  • the tube is suitably secured to the lower end of outlet tube 104, which forms part of the magnet assembly.
  • the connection between the parts may be by means of a clamp 112, and the valve-containing tube may be suitably secured, as by a clamp 114, to the conduit or line 30.
  • the provision of the check valve in a separate element is an alternative arrangement for manufacturing purposes, and may also be used with the electro-rnagnet of FIG. 2.
  • the intensity of the magnetic field required to sustain and maintain oxygen in liquid form separately from the gas in the absence of gravity is less than the field intensity required in a condition of adverse gravity, as when the converter is positioned during upside-down flight.
  • the electro-magnet Under an adverse gravity condition the electro-magnet will furnish a higher field intensity than the permanent magnet for a given size and weight.
  • an adverse gravity condition it is preferred to use an electro-magnet arrangement.
  • FIG. 6 shows the magnetic separating means of the invention in relation to another type of liquid oxygen converter system.
  • gas pressurizing means in the form of a pressure build-up circuit, including an evaporating coil 116 which also receives liquid oxygen, may be used.
  • One side of the coil is in communication with the container outlet 12 through a line 118 for the delivery of liquid oxygen to the coil.
  • the opposite side of the coil is in communication with the top side or the neck 18 of the container through a line 120.
  • a build-up valve 122, a pressure-closing valve 124 and a low-pressure relief valve 126 are disposed within the pressurizing circuit, between the gas side of the coil and top or gas side of the container.
  • suitable circulating means such as a pump 128 may be provided.
  • the elements of the supply circuit are essentially the same as hereinbefore described in connection with FIG. 1, as are the elements for filling the container, for venting gas, for connecting the pressurizing circuit to the Supply circuit and to economize gas, and for indicating pressure. Such like elements are indicated by the same nu merals primed.
  • the line 68' is in communication with the line 120 and the pressure build-up coil 116, as well as with the gas side of the container.
  • the buildup valve 122 With the container filled with liquid oxygen, the buildup valve 122 is opened to permit liquid oxygen to flow into the build-up coil 116 under the influence of gravity.
  • the liquid oxygen evaporates in the build-up coil causing pressure in the system to increase.
  • the pressure-closing valve 124 closes automatically to prevent any more liquid oxygen from being evaporated.
  • a liquid oxygen converter is not perfectly insulated, and therefore some heat leakage may be expected. Heat leakage will cause a further increase in pressure in the system.
  • the low-pressure relief valve 126 prevents excessive pressure build-up in the pressurizing circuit by venting at a predetermined pressure above the desired pressure in the system, for example, above 110 p.s.i for 70 p.s.i.g. sytem If the pressure in the supply circuit exceeds p.s.i. in such a system, the high-pressure relief valve 34' will vent excess gas from the supply circuit. A higher pressure may exist in the supply circuit than in the pressurizing circuit.
  • the two check valves 36 and 74' prevent reverse flow.
  • the pressure opening valve 72' functions substantially identically to the valve 72 described above in connection with FIG. 1.
  • this valve is open when the pressure within the container is above a predetermined pressure so that upon opening of the delivery valve 32, the vapor within the container is first allowed to exhaust to the delivery system.
  • the valve 72' closes. Thereafter, the delivery of gas to the valve 32 occurs from the liquid phase of the container.
  • the pressure of the container drops below its desired operating pressure, for example 70 p.s.i.g., the pressure-closing valve 124 of the pressurizing circuit reopens to permit liquid to enter the build-up coil 116.
  • the desired operating pressure for example 70 p.s.i.g.
  • the magnetic field imposed upon a mass of liquid oxygen at the container outlet insures the delivery of liquid oxygen to the coil 116 of the pressurizing circuit, when needed, and to the evaporating coil 28' of the supply circuit, though the force of gravity normally acting to separate the liquid and gaseous phases in the container and causing flow of the liquid to the circuits is absent.
  • the supply valve 32' When the supply valve 32' is opened, the operating pressure of the gas upon the operative quantity of liquid magnetically sustained at the container outlet, forces the liquid through the outlet and into the evaporating and superheating coil 28'. Here the liquid is converted to gas which is heated to the desired temperature for delivery to the supply valve.
  • the electro-magnet assembly of FIG. 2, or the permanent magnet assembly shown in FIG. 4 may be used in conjunction with the container outlet for supplying the liquid oxygen to the pressurizing and supply circuits shown in FIG. 6.
  • the pressure upon the liquid oxygen made available for delivery to the evaporating and superheating coil 28' by the magnetic means of the invention will tend to drop as the supply of oxygen in the container is used. Such pressure drop will be compensated for to some extent by normal heat leakage into the container; also, there will be a certain amount of additional heat leakage through the build-up circuit portion of the apparatus.
  • the converter may function suitably in an adverse gravitational environment for a reasonable length of time.
  • suitable gas circulating means such as the pump 128, which is made responsive to pressure drop, may be employed to provide the desired pressure differential so that the magnetically sustained liquid oxygen will be transferred from the container to the coils.
  • the supply outlet is disposed in close proximity to the magnetic means as hereinabove illustrated and the second outlet would be disposed near or adjacent to the magnetic means for the first outlet, or suitably related to a second magnetic means.
  • FIG. 7 shows another embodiment of the invention from the standpoint of the positional relationship of the magnetic means with respect to the liquid line from the container outlet.
  • this embodiment of the invention is illustrated with relation to the converter system shown in FIG. 6, it will be understood that the illustrated arrangement may be used with the converter system shown in FIG. 1.
  • a tube having a length greater than the distance between the inner and outer shells 14 and 16 extends between the shells, with the lower end of the tube projecting exteriorly of the outer shell.
  • the projecting portion of the tube 130 is received within and secured to the upper end of the inner tube element of the magnet assembly 132.
  • the magnet assembly may be an electro-magnet as shown, or a permanent magnet assembly.
  • the magnet may be provided with a check valve 84 within its confines and as part of the magnet assembly as shown, or the check valve may be provided in a separate element as shown in FIG. 4.
  • the inner tube of the magnet assembly is secured in communication with a liquid line 134 discharging to the supply circuit, as in the converter system shown in FIG. 1, or in communication with both the supply circuit and the pressurizing circuit, as in the system shown in FIG. 6.
  • liquid and gaseous phases of oxygen are separately maintained by utilizing the preferential effect of a magnetic field for the liquid phase.
  • a magnetic field By magnetically maintaining a quantity of liquid oxygen separately from the gaseous phase with which it is related in a container for a liquid oxygen converter system, a single phase of oxygen or oxygen of uniform density may be delivered from the container and to the system, despite the absence of the full force of gravity normally acting to separate the liquid from the gas.
  • a liquid seal is provided at such outlet to enable the necessary operating pressure to be maintained in the container and to assure transfer of oxygen uniformly of a single phase to the system.
  • a method of delivering liquid oxygen from a container holding a supply of oxygen in the liquid and gaseous phases to an evaporating coil of a liquid oxygen converter in the absence of the full force of gravity normally acting to deliver the liquid to the coil comprising subjecting the oxygen to a magnetic field at an outlet area of the container to preferentially maintain a mass of liquid phase oxygen separately from the gaseous phase, thereby providing a liquid seal at the outlet and enabling the desired operating pressure to be maintained in the container, and delivering liquid oxygen from the container to the coil.
  • a liquid oxygen converter including a container having an outlet for the oxygen, the container, the wall of which is impermeable to the passage of liquid and gaseous oxygen, holding a supply consisting essentially of oxygen in the liquid and gaseous phases, the improvement comprising magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet in the absence of the full force of gravity upon the liquid oxygen.
  • a liquid oxygen converter including a container for the oxygen, said container holding a supply consisting essentially of oxygen in the liquid and gaseous phases and comprising spaced inner and outer, oxygen-impermeable 10 shells, an outlet tube extending between said inner and outer shells, and magnetic means positioned in surrounding relationship with respect to the outlet tube to maintain a supply of oxygen in liquid form within said tube.
  • a liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit, said container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, the wall of the container being impermeable to the passage of the liquid and gaseous oxygen, magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coil in the absence of the full force of gravity upon the liquid oxygen, and means for controllably producing vapor pressure in said container.
  • a liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit, magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coil in the absence of the full force of gravity upon the liquid oxygen, and pressurizing means comprising heating means disposed within the container adjacent the field provided by the magnetic means and pressure responsive means to actuate the heating means.
  • a liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit and an evaporating coil in a pressurizing circuit, said container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, the wall of the container being impermeable to the passage of the liquid and gaseous oxygen, and magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coils in the absence of the full force of gravity upon the liquid oxygen.
  • a liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit, magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coil in the absence of the full force of gravity upon the liquid oxygen, trap means to prevent vapor which may form in the supply circuit from entering the container, and means effective to controllably maintain a desired vapor pressure within said container.

Description

March 23, 1965 J. s. LAWRENCE 3,174,294
OXYGEN DISPENSING Filed Dec. 19, 1958 3 Sheets-Sheet 1 2e 12. 4 68 1 9 32 1 M Q 24 34 w 20 2/ T 15 IO 80 n A A p/ m n A n F 76 r" M A K XIX a2 \50 'III/I/IIIIII/IIII/I 'IIIIIIIIIIII:
'llIIIIIIIIIIIIIIIIIIIIIIIIII INVEN TOR.
JOSEPH s. LAwRzucc ATTORNEY 4 AGE March 23, 1965 v J. 5. LAWRENCE OXYGEN DISPENSING 3 Sheets-Sheet 5 Filed Dec. 19, 1958 INVHVTOR. JOSEPH s. LAWRENCE ATTORNEY AGENT United States Patent 3,174,294 OXYGEN DISPENSING Joseph S. Lawrence, Merchantville, N.J., assignor to Air Reduction Company Incorporated, New York, N.Y., a corporation of New York Filed Dec. 19, 1958, Ser. No. 781,609 13 Claims. (CI. 62-51) The invention relates to systems for dispensing or supplying gaseous oxygen, and is more particularly directed to novel methods and means for enabling a liquid oxygen converter system to operate reliably and effectively when the system is subjected to an adverse gravitational environment, or an environment where the force of gravity is non-existent or insufiicient to establish the desired separation of the liquid and gaseous phases of the oxygen. The expression in the absence of the full force of gravity. as hereinafter used, refers to such environmental conditions.
The development of equipment designed to travel at extremely high altitudes or in outer space imposes on such equipment, by virtue of the flight paths, an environment where the force of gravity may be adverse or nonexistent. It has already been accomplished that man has been placed in such environments, and by further extension and development of such equipment the sustenance of man for prolonged periods under such conditions and under varying circumstances is becoming of greater significance. In any event, the proper functioning of certain apparatus involved in such travel, or for the sustenance of man therein, requires the delivery of gaseous oxygen under controlled conditions. A liquid oxygen converter system, because of its low weight and minimal space requirements per unit of oxygen gas delivered, is particularly useful in environments of the kind under consideration.
The proper operation of the usual or conventional liquid oxygen converter system requires that the fluid discharged into the system from the container, which holds the supply of liquid oxygen and contains both the liquid and gas phases, shall be of uniform density. Except where the rate of consumption of gas is small, practical considerations require that the liquid form of the oxygen be delivered to the system for vaporization externally of the container. In the event of intermittent discharge of oxygen from the liquid and gaseous phases, the delivery fluid is of non-uniform density, which detrimentally affects the maintenance of the desired operating conditions of the system. In conventional types of liquid oxygen converters, the delivery from the container of oxygen of uniform density depends upon the force of gravity to separate the liquid from the gas.
An object of the invention is to provide a method and means wherein, despite the absence of the full force of gravity, the liquid phase of oxygen may be maintained separately from the gaseous phase, thereby allowing delivery of oxygen of uniform density under controlled conditions.
Another object of the invention is to provide a method and means wherein, despite the absence of the full force of gravity, a liquid seal may be provided at the container outlet of a liquid oxygen converter system, thereby enabling the maintenance of the desired operating pressure in the container, and the delivery of oxygen of uniform density to the system.
A further object of the invention is to provide a method and means wherein, despite the absence of the full force of gravity, the liquid phase of oxygen may be maintained separately from the gaseous phase so that liquid oxygen may be made available for delivery from the container and the controlled vaporization thereof externally of the container.
In accordance with the invention generally, these, and other objects, advantages and improved results are obtained by imposing a magnetic field upon liquid oxygen. A magnetic field or flux is effective to attract, sustain or maintain the liquid phase of oxygen in preference to the gaseous phase. The preferential elfect of a magnetic field upon liquid oxygen is utilized to separate the liquid from the gaseous phase to insure the delivery of oxygen having a uniform density, as distinguished from an intermittent discharge of the liquid and the gas. In a liquid oxygen converter system, such preferential effect of a magnetic field upon the liquid phase of oxygen serves to effectively separate the liquid from the gas to permit oxygen of uniform density to be delivered to the system under controlled conditions, though the system is located in an environment where the force of gravity normally acting to separate the liquid and gaseous phases is either non-existent or adverse.
Preferably, the preferential effect of a magnetic field for the liquid phase of oxygen is utilized to provide a mass or quantity of liquid oxygen at the outlet of the oxygen container for the converter system. The container, which holds the oxygen in both the liquid and gaseous phases, is thereby provided with a liquid seal at or over the outlet. By providing such liquid seal, the container pressure may be maintained at a desired value, and oxygen of uniform density may be circulated in the system. More particularly, an operative quantity of liquid oxygen is made available for delivery from the container to an evaporating coil, where the liquid may be controllably vaporized, and the resultant gas delivered to the point of use at the desired temperature and pressure. Any known or suitable means may be used to furnish the desired container pressure to deliver the operative quantity of liquid oxygen sustained at the outlet to the external evaporating coil.
The magnetic field may be furnished by an electromagnet or by a permanent magnet.
In greater detail, reference is made to the following detailed description, together with the accompanying drawings illustrating several preferred embodiments of the invention, wherein:
FIG. 1 is a schematic view of one type of liquid oxygen converter system which may be provided wtih a magnetic separating means of the invention;
FIG. 2 is an enlarged, vertical cross-sectional view of the outlet area of the container shown in FIG. 1;
FIG. 3 is a top plan view taken in the direction of line 3-3 of FIG. 2;
FIG. 4 illustrates a permanent magnet assembly which may be used in lieu of the electro-magnet shown in FIG. 2; r
FIG. 5 is a top plan view of the permanent magnet assembly shown in FIG. 4;
FIG. 6 is a schematic view of another type of liquid oxygen converter system which may be provided with a magnetic ,separatingmeans of the invention; and
FIG. 7 is a view similar to FIG. 2, but showing another form of the invention insofar as the positional relationship of the magnetic means with respect to the container outlet.
As shown in FIGS. 1 and 2, an insulated container or chamber 10 is provided for supplying oxygen to a converter system, the container having a discharge outlet, generally designated 12, on the bottom side thereof. The container comprises an inner shell 14 and an outer shell 16 spaced therefrom. The shells may be made of copper, aluminum or stainless steel. The space between the shells is evacuated and/ or filled with a suitable insulating mate- 3 rial to provide the desired insulating characteristics. The top side of the container is provided with a neck 18 closed by a cap 20 connected to the neck, as by mating threads 22. A filling line 24 extends through the cap 20 and into the container. The filling line is provided with a filler valve 26 so that a liquid oxygen source or tank may be connected to the valve to fill the container when empty.
In order to enable the delivery of oxygen having a uniform density to the converter system and to allow the desired operating pressure within the container to be maintained, despite the absence of the full force of gravity, a magnetic field is provided at, or in the vicinity of, the outlet 12. By magnetically maintaining a mass of liquid oxygen at or over the outlet, the outlet is provided with a liquid seal. In the form of the converter system illus trated, which is of the type in which liquid oxygen is intended for delivery to a supply circuit externally of the container, the magnetic field maintains an operative quantity of liquid oxygen at the outlet to insure that the liquid phase, designated B, will be available for delivery to the supply circuit under the influence of the pressure provided by the gaseous phase, designated A, within the container.
The supply circuit includes an evaporating and superheating coil 28, one side of which is in communication with the outlet 12 through a conduit or line 30, the other side of the coil being in communication with a supply valve 32. The supply valve is adapted for connection to a line to furnish the gas evaporated and warmed by the coil 28 to the point of use. A high-pressure relief valve 34 is disposed between the coil and the supply valve. A spring loaded liquid check valve 36 is located in the line between the supply circuit and a gas pressurizing circuit which will be subsequently described.
As shown in greater detail in FIG. 2, the outlet 12 is in the form of a tube 38, which may be made a part of an electro-magnet assembly, generally designated 39. The tube, which is formed of a non-magnetic material, such as aluminum, is suitably wound with a wire in a plurality of adjacent or helical turns to provide a coil 40. The wire wound tube may be enclosed in a second tube 42, also of a non-magnetic material. The coil is encased or potted in a suitable insulating material 44, such as an epoxy resin compound. v
The electro-magnet is preferably positioned to extend between the inner and outer shells 14 and 16, and is secured in place, as by welding portions of the tube 42 to adjacent portions of the shells at the areas 46. As shown, the outlet tube 38 is of suflicient length so that the lower end thereof may be secured to the line 30 outside the shell 16. The connection may be accomplished by a clamp 48, as shown, or the tube and the line may be matingly threaded. The exterior of the container outlet area, including the described surrounding electro-magnet, is provided with an insulating wall 50 to minimize heat leakage. The insulating wall is connected or secured to the outer shell 16, and is of a contour to furnish a chamber 52. The insulating Wall is provided with an aperture 54 to allow the line 36 to extend therethrough. The ends of the coil are brought out through a hermetically sealed plug 56 secured in the insulating wall so that the coil may be connected to a suitable source of power.
Gas pressurizing means is provided to maintain the desired container pressure so that the operative quantity 'of liquid oxygen magnetically maintained at the container outlet may be delivered to the supply circuit and the evaporating coil 28. In the form of the invention illustrated in FIGS. 1 and 2, the pressurizing means includes heating means intheform of an electrical resistance heating element or coil 58. As shown, the coil is positioned within the container and over the container outlet; also, the coil is located within or adjacent to the magnetic field provided by the magnet. The straight portions 60, 60' of the coil extend through, and are supported by, the inner and " outer shells 14 and 16. The extremities of the coil are connected to conductors or wires 62, 62 which terminate in a socket 64 secured to extend through the insulation wall 59.
A gas or vapor line 66 extends through the cap 20 and is in communication with the neck end 18 of the container. A relief or vent valve68 and a pressure gauge 70 are disposed in the line. A pressure-opening valve 72 and a gas check valve 74 are positioned between the upper or gas side of the container and the supply circuit, a line 76 being provided between the pressure-opening valve and the liquid supply line 30.
In order to controllably maintain a predetermined gas pressure within the container, and upon the liquid sustained at the container outlet, pressure control means or a gas pressure responsive switch 78 is provided in the line 66. The pressure responsive switch senses any drop in container pressure below a desired predetermined value to energize the coil 58, and to restore the pressure to the desired value. The pressure responsive switch is connected to the heating coil by electrical conductors or leads 8!), 80', which terminate in a plug 82 received within the socket 64. A source 83 of electrical power, for example, a battery, provides the energy for heating the coil 58. The gas pressure responsive switch may be of any suitable type.
A suitable trap means is provided at or near the juncture of the liquid supply line 30 and the container outlet within a heat insulated zone, such as the area between the container shells or the described chamber 52. As shown in FIGS. 2 and 3, the trap means may comprise a check valve, generally designated 84, positioned within the outlet tube 38. The check valve, made of non-magnetic components, may be of any suitable construction. As shown, the valve may comprise a seat 86 formed integrally with the tube 38 and extending radially inward thereof for a portion of the tube diameter to provide a valve opening 88. A disk 90 at the end of a stem 92 is adapted for engagement with the seat. The stem extends through a bore provided by a hollow cylinder 94, the stem being held against separation from the cylinder by a cross-pin 96 therethrough, which also limits the extent of opening movement of the valve disk. The cylinder is supported at the center of a plurality of circumferentially and equidistantly spaced vanes 98 which are secured to and extend radially inward from the tube 38.
The check valve prevents the back flow of vapor into the container and the continuous feeding of liquid from the container to the supply line 30 when the converter is not in operation. Thus, after filling and under the influence of a normal gravitational environment, liquid will tend to flow by gravity through the outlet into the supply line 30 where heat imparted from the surrounding atmosphere will cause it to become vaporized. Such vaporized liquid will then pass backwardly to the container and be replaced by further gravitational feed of liquid. This cycle normally would proceed continuously with the result that the container pressure would rapidly increase and eventually vent to the atmosphere permitting a loss of some of the oxygen contents. By the provision of a trap or check valve device at the outlet of the container as above described, the initial pressure produced by vaporization of the liquid in the supply line will prevent any further delivery of liquid from the container until the supply valve of the converter is opened, permitting the discharge of the contents of the container under the propelling influence of the differential pressure between the container and the pressure of the supply line. The trap means is similarly effective while the converter is not in operation even under a non-gravitational environment. It may be seen, for example, that under such condition, the liquid oxygen within the container exhibits a tendency to become symmetrically disposed under the influence of the magnetic field of the magnet 39. Under some circumstances, the liquid or a portion of the liquid mass so influenced may become located in a region which is exposed to a relatively high input of heat from the surrounding atmosphere, causing such liquid to become vaporized. The check valve then operates in substantially the same manner as under gravity conditions so that such vaporization, if and when it may occur, will cause the valve to close and prevent the passage of liquid oxygen to such region until the supply valve of the delivery circuit is opened. It may be seen, of course, that when the delivery tube from the container is arranged to pass upwardly and through the top of the container, trap means or a check valve device would then not be needed.
With an empty system, a liquid oxygen source is connected to the filler valve 26, and the vent valve 68 is opened. Liquid oxygen flows into the converter, from which it is boiled off while cooling the internal parts of the system down to the temperature of the liquid oxygen. The resulting gas is vented through the vent valve. When liquid oxygen begins to issue from the vent valve, the filling operation is stopped and the filler and vent valves .are closed.
To ready the system for operation in an environment where the force of gravity is adverse or non-existent, the electro-magnet is energized, thereby sustaining a mass of the liquid within its field to provide a liquid seal and maintain an operative quantity of liquid oxygen at the container outlet. The supply valve 32 is then opened. Before the magnetically sustained liquid oxygen is delivered from the container to the supply line and to the coil 28, a limited quantity of gas accumulated in the container at a pressure exceeding the desired operating pressure is economized and delivered to the supply valve. The pressure-opening valve 72 is set to automatically open at a desired value and permit gas to flow through the check valve 74 and to the supply circuit and supply valve. The gas check valve 74 and the liquid check valve 36 prevent reverse flow. It will be seen also that the pressure loading of the check valve 36 requires a slight differential pressure across the check valve to allow the flow of liquid from the container through the line 30 so that such flow of liquid may not occur as long as the opening valve 72 is open and vapor from the container is being delivered therethrough. The pressure-opening valve 72 closes automatically slightly above the desired operating pressure, and such pressure is maintained by the control aiforded by the described pressure responsive switch and heating coil arrangement. The maintenance by the magnetic field of an operative quantity of liquid oxygen to cover the container outlet, and the pressure of the gas upon the liquid, assures that only liquid oxygen will be transferred to the evaporating coil 28 for its controlled vaporization and warming, and delivery to the supply valve.
While it is preferred to utilize the magnetic means of the invention to assure the delivery of liquid oxygen from the container for controlled vaporization of the liquid externally of the container, where the rate of consumption of the gas is relatively small, the magnetic means may be utilized to concentrate a mass of liquid oxygen within an area of the container for the purpose of controllably vaporizing the liquid within the container at such area by suitable heating means, such as the heating coil 58. The resultant gas delivered from the container then need only be warmed to permit its use. When the gas phase is thus taken from the container, the trap means is unnecessary.
As shown in FIGS. 4 and 5, the magnetic means may be in the form of a permanent magnet, generally designated 100. The permanent magnet may comprise an assembly of a plurality of magnets, for example, four magnets 102a, 102b, 1020 and 102d as shown. The permanent magnets are preferably equidistantly spaced from one another and supported between inner and outer tubes 104 and 106, respectively. Like pole faces are located at the same ends of the assembly, and the assembly may be secured in position between the inner and outer shells at the areas 108.
As also shown in FIG. 4, where a trap or check valve 6. is included for cooperation with the container outlet, the valve trap 84 may be separately provided for in a tubular element 110, instead of being made a part of, and located within, the outlet tube of the magnet assembly, as shown in FIG. 2. In such an arrangement, the tube is suitably secured to the lower end of outlet tube 104, which forms part of the magnet assembly. The connection between the parts may be by means of a clamp 112, and the valve-containing tube may be suitably secured, as by a clamp 114, to the conduit or line 30. The provision of the check valve in a separate element is an alternative arrangement for manufacturing purposes, and may also be used with the electro-rnagnet of FIG. 2.
The intensity of the magnetic field required to sustain and maintain oxygen in liquid form separately from the gas in the absence of gravity is less than the field intensity required in a condition of adverse gravity, as when the converter is positioned during upside-down flight. Under an adverse gravity condition the electro-magnet will furnish a higher field intensity than the permanent magnet for a given size and weight. Thus, where an adverse gravity condition will be encountered, it is preferred to use an electro-magnet arrangement.
FIG. 6 shows the magnetic separating means of the invention in relation to another type of liquid oxygen converter system. Instead of the previously described heating coil and pressure responsive switch arrangement to provide the container pressure for delivering the operative quantity of magnetically sustained liquid oxygen to the supply circuit, gas pressurizing means in the form of a pressure build-up circuit, including an evaporating coil 116 which also receives liquid oxygen, may be used. One side of the coil is in communication with the container outlet 12 through a line 118 for the delivery of liquid oxygen to the coil. The opposite side of the coil is in communication with the top side or the neck 18 of the container through a line 120. A build-up valve 122, a pressure-closing valve 124 and a low-pressure relief valve 126 are disposed within the pressurizing circuit, between the gas side of the coil and top or gas side of the container. To assist in circulating the liquid through the pressure build-up coil, suitable circulating means, such as a pump 128 may be provided.
The elements of the supply circuit are essentially the same as hereinbefore described in connection with FIG. 1, as are the elements for filling the container, for venting gas, for connecting the pressurizing circuit to the Supply circuit and to economize gas, and for indicating pressure. Such like elements are indicated by the same nu merals primed. The line 68', however, is in communication with the line 120 and the pressure build-up coil 116, as well as with the gas side of the container.
With the container filled with liquid oxygen, the buildup valve 122 is opened to permit liquid oxygen to flow into the build-up coil 116 under the influence of gravity. The liquid oxygen evaporates in the build-up coil causing pressure in the system to increase. When the system pressure reaches the desired value, for example 70 or 300 p.s.i.g., the pressure-closing valve 124 closes automatically to prevent any more liquid oxygen from being evaporated.
A liquid oxygen converter is not perfectly insulated, and therefore some heat leakage may be expected. Heat leakage will cause a further increase in pressure in the system. The low-pressure relief valve 126 prevents excessive pressure build-up in the pressurizing circuit by venting at a predetermined pressure above the desired pressure in the system, for example, above 110 p.s.i for 70 p.s.i.g. sytem If the pressure in the supply circuit exceeds p.s.i. in such a system, the high-pressure relief valve 34' will vent excess gas from the supply circuit. A higher pressure may exist in the supply circuit than in the pressurizing circuit. The two check valves 36 and 74', however, prevent reverse flow.
The pressure opening valve 72' functions substantially identically to the valve 72 described above in connection with FIG. 1. Thus, this valve is open when the pressure within the container is above a predetermined pressure so that upon opening of the delivery valve 32, the vapor within the container is first allowed to exhaust to the delivery system. When such vapor has been discharged sufficiently to reduce the container pressure to a value slightly above the desired predetermined operating pressure of the container, the valve 72' closes. Thereafter, the delivery of gas to the valve 32 occurs from the liquid phase of the container. It will be seen that when the pressure of the container drops below its desired operating pressure, for example 70 p.s.i.g., the pressure-closing valve 124 of the pressurizing circuit reopens to permit liquid to enter the build-up coil 116. The resulting vaporization of such liquid will produce a corresponding increase in the pressure of the container so that the desired operating pressure may be maintained.
The magnetic field imposed upon a mass of liquid oxygen at the container outlet insures the delivery of liquid oxygen to the coil 116 of the pressurizing circuit, when needed, and to the evaporating coil 28' of the supply circuit, though the force of gravity normally acting to separate the liquid and gaseous phases in the container and causing flow of the liquid to the circuits is absent. When the supply valve 32' is opened, the operating pressure of the gas upon the operative quantity of liquid magnetically sustained at the container outlet, forces the liquid through the outlet and into the evaporating and superheating coil 28'. Here the liquid is converted to gas which is heated to the desired temperature for delivery to the supply valve. it will be understood that either the electro-magnet assembly of FIG. 2, or the permanent magnet assembly shown in FIG. 4, may be used in conjunction with the container outlet for supplying the liquid oxygen to the pressurizing and supply circuits shown in FIG. 6.
The pressure upon the liquid oxygen made available for delivery to the evaporating and superheating coil 28' by the magnetic means of the invention will tend to drop as the supply of oxygen in the container is used. Such pressure drop will be compensated for to some extent by normal heat leakage into the container; also, there will be a certain amount of additional heat leakage through the build-up circuit portion of the apparatus. For relatively small flow rates, such as for respiration purposes, the converter may function suitably in an adverse gravitational environment for a reasonable length of time. However, Where relatively large flow rates are required, and to utilize the full contents of the container, suitable gas circulating means, such as the pump 128, which is made responsive to pressure drop, may be employed to provide the desired pressure differential so that the magnetically sustained liquid oxygen will be transferred from the container to the coils.
To minimize heat leakage, it is advantageous to have a single, common outlet for both the pressurizing and supply circuits in the converter system shown in FIG. 6. It is within the scope of the invention, however, to provide a system in which there is, in addition to the supply outlet, a separate or second outlet from the container so that each circuit is in communication with an individual container outlet. It may be seen that depending upon whether it is desired to deliver vapor phase or liquid phase to the supply outlet that the supply outlet would be arranged in relation to the magnetic means so as to insure the access to such outlet of fluid of uniform density. Where the fluid is to be delivered to the supply circuit for example from the liquid phase, the supply outlet is disposed in close proximity to the magnetic means as hereinabove illustrated and the second outlet would be disposed near or adjacent to the magnetic means for the first outlet, or suitably related to a second magnetic means.
FIG. 7 shows another embodiment of the invention from the standpoint of the positional relationship of the magnetic means with respect to the liquid line from the container outlet. Though this embodiment of the invention is illustrated with relation to the converter system shown in FIG. 6, it will be understood that the illustrated arrangement may be used with the converter system shown in FIG. 1. In this form of the invention, a tube having a length greater than the distance between the inner and outer shells 14 and 16 extends between the shells, with the lower end of the tube projecting exteriorly of the outer shell. The projecting portion of the tube 130 is received within and secured to the upper end of the inner tube element of the magnet assembly 132. The magnet assembly may be an electro-magnet as shown, or a permanent magnet assembly. The magnet may be provided with a check valve 84 within its confines and as part of the magnet assembly as shown, or the check valve may be provided in a separate element as shown in FIG. 4. The inner tube of the magnet assembly is secured in communication with a liquid line 134 discharging to the supply circuit, as in the converter system shown in FIG. 1, or in communication with both the supply circuit and the pressurizing circuit, as in the system shown in FIG. 6.
It is believed that the advantages of the invention will be apparent from the foregoing detailed description. The liquid and gaseous phases of oxygen are separately maintained by utilizing the preferential effect of a magnetic field for the liquid phase. By magnetically maintaining a quantity of liquid oxygen separately from the gaseous phase with which it is related in a container for a liquid oxygen converter system, a single phase of oxygen or oxygen of uniform density may be delivered from the container and to the system, despite the absence of the full force of gravity normally acting to separate the liquid from the gas. By locating the magnetic field at a liquid delivery outlet, a liquid seal is provided at such outlet to enable the necessary operating pressure to be maintained in the container and to assure transfer of oxygen uniformly of a single phase to the system. By positioning the magnetic field adjacent the outlet, delivery to a supply coil of an operative quantity of liquid oxygen for controlled vaporization externally of the container is assured; also, delivery of an operative quantity of liquid oxygen to a pressure build-up coil, and the maintenance of a desired operating pressure is assured.
While several preferred forms of the invention have been illustrated and described, it will be apparent that various changes or modifications may be made without departing from the spirit and scope of the invention, as sought to be defined in the following claims.
I claim:
1. A method of dispensing oxygen of uniform density from a container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, said container, the wall of which is impermeable to the passage of liquid and gaseous oxygen, to be subjected to an environment in which the force of gravity normally acting to separate the liquid and gaseous phases is absent, said method comprising subjecting the oxygen to a magnetic field to preferentially maintain a mass of liquid phase oxygen separately from the gaseous phase, and delivering a separate single phase of the oxygen from the container.
2. A method of dispensing liquid oxygen from a container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, said container, the wall of which is impermeable to the passage of liquid and gaseous oxygen, to be subjected to an environment in which the force of gravity normally acting to separate the liquid and gaseous phases is absent, said method comprising subjecting the oxygen to a magnetic field within the container to preferentially maintain a mass of liquid phase oxygen separately from the gaseous phase, and delivering the separate liquid phase of oxygen from the container.
3. A method of dispensing gaseous oxygen from a container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, said container, the wall of which is impermeable to the passage of liquid and gaseous oxygen, to be subjected to an environment in which the force of gravity normally acting to separate the liquid and gaseous phases is absent, said method comprising subjecting the oxygen to a magnetic field within the container to preferentially maintain a mass of liquid phase oxygen separately from the gaseous phase, vaporizing the liquid mass thus separated, and delivering the resultant gas from the container.
4. A method of dispensing oxygen of uniform density from a container holding a supply of oxygen in the liquid and gaseous phases, said container to be subjected to an environment in which the force of gravity normally acting to separate the liquid and gaseous phases is absent, said method comprising subjecting the oxygen to a magnetic field at an outlet area of the container to preferentially maintain a mass of liquid phase oxygen separately from the gaseous phase, thereby providing a liquid seal at the outlet and enabling the desired operating pressure to be maintained in the container, and delivering a separate single phase of the oxygen from the container.
5. A method of delivering liquid oxygen from a container holding a supply of oxygen in the liquid and gaseous phases to an evaporating coil of a liquid oxygen converter in the absence of the full force of gravity normally acting to deliver the liquid to the coil, said method comprising subjecting the oxygen to a magnetic field at an outlet area of the container to preferentially maintain a mass of liquid phase oxygen separately from the gaseous phase, thereby providing a liquid seal at the outlet and enabling the desired operating pressure to be maintained in the container, and delivering liquid oxygen from the container to the coil.
6. A method of supplying gaseous oxygen from a container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, said container, the wall of which is impermeable to the liquid and gaseous oxygen, to be subjected to an environment in which the full force of gravity normally acting to separate the liquid from the gas is absent, said method comprising imposing a magnetic field upon a mass of liquid oxygen at an outlet area of the container to preferentially maintain the liquid mass separately from the gas and provide a liquid seal at said outlet, and vaporizing the liquid mass within the magnetic field.
7. In a liquid oxygen converter including a container having an outlet for the oxygen, the container, the wall of which is impermeable to the passage of liquid and gaseous oxygen, holding a supply consisting essentially of oxygen in the liquid and gaseous phases, the improvement comprising magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet in the absence of the full force of gravity upon the liquid oxygen.
8. A liquid oxygen converter including a container for the oxygen, said container holding a supply consisting essentially of oxygen in the liquid and gaseous phases and comprising spaced inner and outer, oxygen-impermeable 10 shells, an outlet tube extending between said inner and outer shells, and magnetic means positioned in surrounding relationship with respect to the outlet tube to maintain a supply of oxygen in liquid form within said tube.
9. A liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit, said container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, the wall of the container being impermeable to the passage of the liquid and gaseous oxygen, magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coil in the absence of the full force of gravity upon the liquid oxygen, and means for controllably producing vapor pressure in said container.
10. A liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit, magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coil in the absence of the full force of gravity upon the liquid oxygen, and pressurizing means comprising heating means disposed within the container adjacent the field provided by the magnetic means and pressure responsive means to actuate the heating means.
11. A liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit and an evaporating coil in a pressurizing circuit, said container holding a supply consisting essentially of oxygen in the liquid and gaseous phases, the wall of the container being impermeable to the passage of the liquid and gaseous oxygen, and magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coils in the absence of the full force of gravity upon the liquid oxygen.
12. A liquid oxygen converter system including a container having an outlet for the oxygen in communication with an evaporating coil in a supply circuit, magnetic means positioned with respect to the outlet to maintain a supply of oxygen in liquid form at the outlet for delivery to the coil in the absence of the full force of gravity upon the liquid oxygen, trap means to prevent vapor which may form in the supply circuit from entering the container, and means effective to controllably maintain a desired vapor pressure within said container.
13. A liquid oxygen converter system as set forth in claim 12, wherein the container comprises spaced inner and outer shells; wherein the container outlet comprises a tube extending between the shells; wherein the outlet tube is part of the magnetic means; and wherein the trap means comprises a check valve disposed within the outlet tube.
References Cited in the file of this patent UNITED STATES PATENTS 1,056,043 Morrison Mar. 18, 1913 1,273,929 Morrison July 30, 1918 1,364,136 Palmer Ian. 4, 1921 1,575,587 Haynes Mar. 3, 1926 2,657,542 Wildhack Nov. 3, 1953 2,873,582 Green Feb. 17, 1959

Claims (1)

1. A METHOD OF DISPENSING OXYGEN OF UNIFORM DENSITY FROM A CONTAINER HOLDING A SUPPLY CONSISTING ESSENTIALLY OF OXYGEN IN THE LIQUID AND GASEOUS PHASES, SAID CONTANIER, THE WALL OF WHICH IS IMPERMEABLE TO THE PASSAGE OF LIQUID AND GASEOUS OXYGEN, TO BE SUBJECTED TO AN ENVIRONMENT IN WHICH THE FORCE OF GRAVITY NORMALLY ACTING TO SEPARATE THE LIQUID AND GASEOUS PHASES IS ABSENT, SAID METHOD COMPRISING SUBJECTING THE OXYGEN TO A MAGNETIC FIELD TO PREFERENTIALLY MAINTAIN A MASS OF LIQUID PHASE OXYGEN SEPARATELY FROM THE GASEOUS PHASE, AND DELIVERING A SEPARATE SINGLE PHASE OF THE OXYGEN FROM THE CONTAINER.
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US3572048A (en) * 1968-10-14 1971-03-23 Wiremold Co Ominpositional cryogenic underwater breathind apparatus
US3699696A (en) * 1970-04-20 1972-10-24 Mc Donnell Douglas Corp Cryogenic storage and expulsion means
US3949565A (en) * 1974-08-09 1976-04-13 Fischer & Porter Co. Liquified gas evaporator
US4149388A (en) * 1977-04-25 1979-04-17 Schneider Richard N Portable cryogenic power system for pneumatically operated tools
US4838034A (en) * 1988-07-22 1989-06-13 International Cryogenics, Inc. Compressed-gas power source for portable gas-driven tools
US4947651A (en) * 1989-04-07 1990-08-14 Minnesota Valley Engineering, Inc. Pressure building circuit for a container for low temperature fluids
US5394704A (en) * 1993-11-04 1995-03-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Alternate method for achieving temperature control in the -160 to +90 degrees Celcius range

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US1056043A (en) * 1912-05-17 1913-03-18 Abraham Cressy Morrison Process of separating mixed liquefied gases.
US1273929A (en) * 1914-04-04 1918-07-30 Abraham Cressy Morrison Method of treating gases.
US1364136A (en) * 1918-10-28 1921-01-04 Charles S Palmer Process of and apparatus for treating mixed gases
US1575587A (en) * 1919-09-02 1926-03-02 Linde Air Prod Co Separation of gaseous or liquid mixtures
US2657542A (en) * 1946-02-05 1953-11-03 William A Wildhack Liquid oxygen converter apparatus
US2873582A (en) * 1957-01-25 1959-02-17 Garrett Corp Air conditioning system for space ships

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1056043A (en) * 1912-05-17 1913-03-18 Abraham Cressy Morrison Process of separating mixed liquefied gases.
US1273929A (en) * 1914-04-04 1918-07-30 Abraham Cressy Morrison Method of treating gases.
US1364136A (en) * 1918-10-28 1921-01-04 Charles S Palmer Process of and apparatus for treating mixed gases
US1575587A (en) * 1919-09-02 1926-03-02 Linde Air Prod Co Separation of gaseous or liquid mixtures
US2657542A (en) * 1946-02-05 1953-11-03 William A Wildhack Liquid oxygen converter apparatus
US2873582A (en) * 1957-01-25 1959-02-17 Garrett Corp Air conditioning system for space ships

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3572048A (en) * 1968-10-14 1971-03-23 Wiremold Co Ominpositional cryogenic underwater breathind apparatus
US3699696A (en) * 1970-04-20 1972-10-24 Mc Donnell Douglas Corp Cryogenic storage and expulsion means
US3949565A (en) * 1974-08-09 1976-04-13 Fischer & Porter Co. Liquified gas evaporator
US4149388A (en) * 1977-04-25 1979-04-17 Schneider Richard N Portable cryogenic power system for pneumatically operated tools
US4838034A (en) * 1988-07-22 1989-06-13 International Cryogenics, Inc. Compressed-gas power source for portable gas-driven tools
US4947651A (en) * 1989-04-07 1990-08-14 Minnesota Valley Engineering, Inc. Pressure building circuit for a container for low temperature fluids
US5394704A (en) * 1993-11-04 1995-03-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Alternate method for achieving temperature control in the -160 to +90 degrees Celcius range

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