US2467413A - Liquid oxygen pumping system - Google Patents
Liquid oxygen pumping system Download PDFInfo
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- US2467413A US2467413A US647984A US64798446A US2467413A US 2467413 A US2467413 A US 2467413A US 647984 A US647984 A US 647984A US 64798446 A US64798446 A US 64798446A US 2467413 A US2467413 A US 2467413A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B43/00—Machines, pumps, or pumping installations having flexible working members
- F04B43/08—Machines, pumps, or pumping installations having flexible working members having tubular flexible members
- F04B43/10—Pumps having fluid drive
- F04B43/113—Pumps having fluid drive the actuating fluid being controlled by at least one valve
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L23/00—Valves controlled by impact by piston, e.g. in free-piston machines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B9/00—Piston machines or pumps characterised by the driving or driven means to or from their working members
- F04B9/08—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid
- F04B9/12—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid the fluid being elastic, e.g. steam or air
- F04B9/123—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid the fluid being elastic, e.g. steam or air having only one pumping chamber
- F04B9/127—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid the fluid being elastic, e.g. steam or air having only one pumping chamber rectilinear movement of the pumping member in the working direction being obtained by a single-acting elastic-fluid motor, e.g. actuated in the other direction by gravity or a spring
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C9/00—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0153—Details of mounting arrangements
- F17C2205/0176—Details of mounting arrangements with ventilation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0329—Valves manually actuated
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0332—Safety valves or pressure relief valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0335—Check-valves or non-return valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/011—Oxygen
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/04—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
- F17C2223/042—Localisation of the removal point
- F17C2223/046—Localisation of the removal point in the liquid
- F17C2223/047—Localisation of the removal point in the liquid with a dip tube
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/01—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
- F17C2225/0107—Single phase
- F17C2225/0123—Single phase gaseous, e.g. CNG, GNC
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/04—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by other properties of handled fluid after transfer
- F17C2225/042—Localisation of the filling point
- F17C2225/046—Localisation of the filling point in the liquid
- F17C2225/047—Localisation of the filling point in the liquid with a dip tube
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/01—Propulsion of the fluid
- F17C2227/0128—Propulsion of the fluid with pumps or compressors
- F17C2227/0135—Pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another fluid
- F17C2227/0311—Air heating
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0367—Localisation of heat exchange
- F17C2227/0388—Localisation of heat exchange separate
- F17C2227/0393—Localisation of heat exchange separate using a vaporiser
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/03—Treating the boil-off
- F17C2265/031—Treating the boil-off by discharge
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/03—Treating the boil-off
- F17C2265/032—Treating the boil-off by recovery
- F17C2265/033—Treating the boil-off by recovery with cooling
- F17C2265/034—Treating the boil-off by recovery with cooling with condensing the gas phase
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0186—Applications for fluid transport or storage in the air or in space
- F17C2270/0189—Planes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0186—Applications for fluid transport or storage in the air or in space
- F17C2270/0197—Rockets
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2931—Diverse fluid containing pressure systems
- Y10T137/3115—Gas pressure storage over or displacement of liquid
- Y10T137/3127—With gas maintenance or application
- Y10T137/313—Gas carried by or evolved from liquid
Definitions
- This invention relates to means for pumping of liquid oxygen, and more particularly to pumping systems utilizing heat energy absorbed by the liquid oxygen itself, to operate the pumps in a most eiilcient manner.
- Pumping oi liquid oxygen may be desired in transferring the liquid from one container to another, in pumping liquid from a container to an evaporator or vaporizer for filling of cylinders with gas, or in supplying gaseous or liquid oxygen to engines, jets, or rockets.
- the object of the present invention is to provide oxygen pumping means suitable for use in aircraft, projectiles and the like, and driven by oxygen gas obtained by evaporation of part of the liquid oxygen supply, wherein the exhaust oxygen from the driving means may be condensed and returned to the liquid oxygen supply.
- Another object is to provide a simple pumping system for liquid oxygen for delivery either directly in liquid form or through an evaporator or vaporizer in gaseous form as may be desired, using some of the gaseous oxygen as a source of suflicient motive fluid for operating the pump or pumps, and utilizing this portion of the gaseous oxygen, after it has served its purpose as a motive fluid by condensing and returning it to the liquid source, or by delivering it to the gaseous delivery line.
- Fig. 1 is a schematic diagram of a pumping system based on the present invention.
- Figs. 2 and 3 are partially schematic views of similar pumping systems showing two different forms of reciprocatingpumps which may be used therein particularly for small capacity installations.
- is evaporated by absorption of heat. Part of this gas is delivered to a gas motor 32 through a control valve 5.
- the gas is utilized in the gas motor 32 to drive the liquid pump 33, which takes liquid from the reservoir or tank 34 and delivers it under pressure.
- Liquid may be delivered through the manual or automatic control valve 20, or gas through the manual or automatic control valve 2
- the exhaust gas from the motor is shown as flowing through a heat interchanger 28, warming the delivered liquid and being itself cooled, or perhaps partially condensed. and thence to condense in the liquid supply.
- the heat interchanger 28 can be omitted, or placed in the evaporator circuit, or be made a part of the evaporator.
- may be either a coil of tubing absorbing heat from the atmosphere, or any other type of heat interchanger heated by any other means.
- the exhaust gas from the motor may be led directly, or through a pressure reducer. to the gas delivery line 29.
- the pump delivery pressure must be maintained high enough so that the exhaust pressure from the gas motor is equal to or greater than the line pressure desired.
- the exhaust gas may be used separately at a suflicient pressure, or allowed to escape it economy is not essential.
- the pressure reducing valve circuit 26 shown in Fig. 1 is not essential in all embodiments of this invention, but is desirable when the liquid is to be raised above its original level before enteringthe pump. Its purpose is to maintain the liquid pumped under a pressure greater than its equilibrium vapor pressure to avoid vapor lock in the pump.
- the warm gas delivered through the circuit 26 condenses only partially on the surface of the liquid in tank 34.
- the layer so condensed constitutes a relatively warm liquid layer of high vapor pressure. Because of the great change in density of liquifled oxygen with temperature, this surface layer will persist for a long time before the mass of the liquid is warmed to the same temperature. Thus, it is possible in this way to pressurize the main body of liquid without warming it.
- the circuit 26 can supply a pressure only equal to the pressure drop across the heat interchanger condenser circuit 3. If this is not sufficient the circuit 26 may be connected on the other side of the motor 32, or even on the other side of valve 5.
- a separate auxiliary gas supply (as from a tank of compressed gas or another liquid oxygen converter) may be utilized to sup- 3 ply pressure in this circuit through valve 30, particularly for starting.
- valve is closed. Valves 20 and 2
- the motor may be driven by an auxiliary gas supply, which is turned off at 30 as soon as the delivery pressure has built up sufficiently. Or, if some-pressure exists in the storage container, either because of vapor pressure being above atmospheric, or supplied from the pressure reducercircuit 26, the
- vent 21 may be opened momentarily, allowing liquid to flow through the pump, and into the evaporator.
- pressure builds up in the pump and evaporator circuit as the liquid evaporates. Opening the control valve 5 then starts the motor.
- the pressure delivered by the pump 33 must be greater than that required to drive the motor 32, the exhaust pressure greater than the gas pressure in the storage tank 34 if the exhaust gas is to be condensed, and the pressure in the storage tank 34 greater than the equilibrium vapor pressure by at least the lift from the tank to the pump.
- conduit 3 through the remaining liquid in the supply tank 34, and an atmospheric evaporator or vaporizer 3
- this system operates as follows: When the starting vent valve 4 and high pressure valve 5 are opened, gas pressure in the evaporator or vaporizer circuit starts the motor I, and valve 4 may then be closed. The pressure of gas in the evaporator or vaporizer circuit pushes the piston 6 to the left, forcing liquid in the pumping chamber 1 into the evaporator or vaporizing circuit.
- the valves 8 and 9 are moved to the other position at the end of the pumping stroke by the lost motion linkage 22, 23, 24, the driving gas is pushed out of the motor chamber In through outlet valve 8 as a result 01' the force of the compressed spring II and exhausts through a heat interchanger and through the check valve l9 and the conduit 3 to condense in the storage liquid.
- the cylinder vent I4 is provided to avoid compression, under the large end of the piston, and to vent blow-by gas. Operation may be started either as mentioned above, by opening the starting vent valve 4, with the storage liquid under somepressure, or by supplying gas under pressure to the motor inlet. To avoid vapor lock, the liquid should be supplied under pressure, either by pressurizing the supply container, or by installing the pump with a direct connection below the storage level. If the exhaust gas is used to pressurize the storage container, the pressure must not be so high but that the spring H can force the piston 6 to the right against the pressure acting on the differential area of the piston 6 and plunger l2.
- the dead volumein the chamber l0 should be as small as possible.
- the areas of the piston and the plunger may be made equal for convenience of construction. but if so, the spring must work oppositely, to pump the liquid, and the return stroke must be powered by the pressure of the liquid from the storage container. Some gas must be vented to permit this operation.
- FIG. 3 A form of pump embodying these principles is shown in Fig. 3, with a flexible bellows l6 shown as a preferred construction instead of a piston.
- the system here is the same as in Fig, 2, except for the action of the pump.
- the liquid is forced into the evaporator or vaporizer 3
- the valve positions reverse most of the gas in chamber l8 exhausts through the heat interchanger 28 and check valve 9 and conduit 3 to condense in the tank 34, but when the pressure falls below a certain value, the exhaust valv biased inwardly by a predetermined resilient force, opens and the remaining gas is vented to the atmosphere.
- the bellows 6 is expanded and the spring I5 stretched by liquid forced into the pump chamber 1' by the pressure over the storage liquid in tank 34.
- for gas delivery may be of any suitable type.
- the device is called a liquid oxygen pumping systern, but may be applied to the pumping of other liquified gases.
- a liquid oxygen pump apparatus comprising a storage tank for liquid oxygen, a heat interchanger, a liquid oxygen pump for pumping liquid from said storage tank to a delivery line through said interchanger, an evaporator connected to said line for evaporating a portion of the liquid supplied thereby, a gas delivery line connected to said evaporator, a gas motor for driving said pump energized by gas supplied from said gas delivery line through a control valve, a conduit for conducting the exhaust gas from said motor to'said heat interchanger for cooling said gas, and another conduit for conof the liquid supplied thereby, a gas delivery line connected to said evaporator, a gas motor for driving said pump energized by gas supplied from said gas delivery line through a control valve, a conduit for conductin the exhaust gas from said motor to said heat interchanger for cooling said gas, another conduit for conducting the cooled gas from said heat interchanger to the liquid in said storage tank for condensation therein, and a connection between the gas in said heat interchanger and the gas phase in said storage tank having a pressure reducing valve there
- a liquid oxygen pump apparatus comprising a storage tank for liquid oxygen, a heat interchanger, a liquid oxygen pump for pumping liquid from said storage tank to a delivery line through said interchanger, an evaporator connected to said line for evaporating a portion of the liquid supplied thereby, a gas delivery line connected to said evaporator, a gas motor for driving said pump energized by gas supplied from said gas delivery line through a control valve, a conduit for conducting the exhaust gas from said motor to said heat interchanger for cooling said gas, another conduit for conducting the gas from said heat interchanger to the liquid in said storage tank for condensation therein, and a starting vent valve connected to the motor exhaust gas conduit.
- Apparatus as defined in claim 1 wherein the pump and motor is a combined piston unit of the reciprocating type, spring actuated in one direction and gas pressure actuated in the other, having a vent conduit for conducting the blow oil gas from the rear of said motor piston to the exhaust gas conduit and to relieve the pressure at the rear of the motor piston.
- Apparatus as defined in claim 3 wherein the pump and motor are combined into a bellowstype reciprocating unit, spring drawn in one direction, and difierential pressure actuated in the other direction by relieving the pressure on the outside of the bellows to atmospheric whenever said pressure is reduced to a predetermined limit, and a spring pressed exhaust valve opening inwardly by spring pressure, connected to the motor exhaust gas conduit for opening the latter to the atmosphere.
- a pumping system for liquified gas comprising a liquified gas container, a pump driven by a gas motor for pumping said liquified gas from said container, an evaporator connected between said pump discharge and said motor, said motor being powered by gas obtained from the evaporation of some ofthe liquid being pumped, and means for condensing the spent motive gas from the motor in the storage liquid;
- a pumping system for liquified gas comprising a liquified gas container, a pump driven by a gas motor for pumping said liquified gas from said container, an evaporator connected between said pump discharge and said motor, said motor being powered by gas obtained from the evaporation of some of the liquid being pumped, means for condensing the spent motive gas from the motor in the storage liquid, and means for maintaining pressure above the storage liquid at a value greater than its equilibrium value.
- a pump for pumping liquified gas from a container driven by a motor operating by gas under pressure, atmospheric heat absorbing means for evaporating a suflicient amount of the discharge from said pump to supply the motive gas to said motor,'a return conduit for the exhausted gas from said motor to the liquified gas from the container for condensation therein, and a heat exchanger in said return conduit for cooling said exhausted gas by the cooler discharge from the pump.
- a pump for pumping liquified gas from a container driven by a motor operating by gas under pressure, atmospheric heat absorbing means for evaporating a suflicient amount of the discharge from said pump to supply the motive gas to said motor, a return conduit for the exhausted gas from said motor to the liquified gas from the container for condensation therein, a heat exchanger in said return conduit for cooling said exhausted gas by the cooler discharge from the pump, and means for maintaining pressure above the liquified gas in the container at a greater valuethan its equilibrium vapor pressure.
- a pump for pumping liquified gas from a container driven by a motor operating by gas under pressure, atmospheric heat absorbing means for evaporating a sufiicient amount of the discharge from said pump to supply the motive gas to said motor, a return conduit for the exhaust gas from said motor to the liquified gas from the container for condensation therein, a heat exchanger in said return conduit for cooling said exhausted gas by the cooler discharge from the pump, means for maintaining pressure above liquified gas in the container at a greater value than its equilibrium vapor pressure, and a conduit with a pressure reducing valve between a sufliciently high pressure point in the discharge from said pump and the container to control and maintain said greater value of pressure in the container.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Reciprocating Pumps (AREA)
Description
W. A. WILDHACK LIQUID OXYGEN PUMPING SYSTEM April 19, 1949; 2,467,413
2 Sheets-Sheet 1 Filed Feb. 15, 1946 Pressure Reducing 2 VWRIZER MOTOR L/OU/D 32 Vem um v v v LIQUID m'YGEN TANK 3 T0 AUX/7W) V 2/ 27 Gas Supply 29 Fig.
E VAPORA TOR Adjustable 10 To Aux/712 GasSupp/y William A. Mid/lack m W/Jf Fig; 2
Patented Apr. 19, 1949 UNITED STATES PATENT OFFICE (Granted under the act of March 3, 1883, as amended April 30, 1928; 370 0. G. 757) This invention relates to means for pumping of liquid oxygen, and more particularly to pumping systems utilizing heat energy absorbed by the liquid oxygen itself, to operate the pumps in a most eiilcient manner.
Pumping oi liquid oxygen may be desired in transferring the liquid from one container to another, in pumping liquid from a container to an evaporator or vaporizer for filling of cylinders with gas, or in supplying gaseous or liquid oxygen to engines, jets, or rockets.
The object of the present invention is to provide oxygen pumping means suitable for use in aircraft, projectiles and the like, and driven by oxygen gas obtained by evaporation of part of the liquid oxygen supply, wherein the exhaust oxygen from the driving means may be condensed and returned to the liquid oxygen supply.
Another object is to provide a simple pumping system for liquid oxygen for delivery either directly in liquid form or through an evaporator or vaporizer in gaseous form as may be desired, using some of the gaseous oxygen as a source of suflicient motive fluid for operating the pump or pumps, and utilizing this portion of the gaseous oxygen, after it has served its purpose as a motive fluid by condensing and returning it to the liquid source, or by delivering it to the gaseous delivery line.
Other and more specific objects will appear in the course of the following description of the illustrative forms oi. this invention, having reference to the accompanying drawings, wherein:
Fig. 1 is a schematic diagram of a pumping system based on the present invention; and
Figs. 2 and 3 are partially schematic views of similar pumping systems showing two different forms of reciprocatingpumps which may be used therein particularly for small capacity installations.
The operation can be understood by reference to Fig. 1, in which the flow directions are shown by arrows. Liquid pumped under pressure into a vaporizer 3| is evaporated by absorption of heat. Part of this gas is delivered to a gas motor 32 through a control valve 5. The gas is utilized in the gas motor 32 to drive the liquid pump 33, which takes liquid from the reservoir or tank 34 and delivers it under pressure. Liquid may be delivered through the manual or automatic control valve 20, or gas through the manual or automatic control valve 2|. At least part of the liquid pumped passes through the evaporator or vaporizer 3|, thence through the control valve 5 and the motor. The exhaust gas from the motor is shown as flowing through a heat interchanger 28, warming the delivered liquid and being itself cooled, or perhaps partially condensed. and thence to condense in the liquid supply.
If delivery of liquid at low vapor pressure is desired, the heat interchanger 28 can be omitted, or placed in the evaporator circuit, or be made a part of the evaporator. The evaporator or vaporizer 3| may be either a coil of tubing absorbing heat from the atmosphere, or any other type of heat interchanger heated by any other means.
If delivery of gas is desired. the exhaust gas from the motor may be led directly, or through a pressure reducer. to the gas delivery line 29. For this use, the pump delivery pressure must be maintained high enough so that the exhaust pressure from the gas motor is equal to or greater than the line pressure desired. Obviously, the exhaust gas may be used separately at a suflicient pressure, or allowed to escape it economy is not essential.
The pressure reducing valve circuit 26 shown in Fig. 1 is not essential in all embodiments of this invention, but is desirable when the liquid is to be raised above its original level before enteringthe pump. Its purpose is to maintain the liquid pumped under a pressure greater than its equilibrium vapor pressure to avoid vapor lock in the pump. The warm gas delivered through the circuit 26 condenses only partially on the surface of the liquid in tank 34. The layer so condensed constitutes a relatively warm liquid layer of high vapor pressure. Because of the great change in density of liquifled oxygen with temperature, this surface layer will persist for a long time before the mass of the liquid is warmed to the same temperature. Thus, it is possible in this way to pressurize the main body of liquid without warming it.
It has been found by experience that the condensation of gas introduced into the space above the liquid proceeds slowly, so that excessively high pressures may be generated by adding more and more gas without special provision for con densing, as is provided in my invention.
As shown, the circuit 26 can supply a pressure only equal to the pressure drop across the heat interchanger condenser circuit 3. If this is not sufficient the circuit 26 may be connected on the other side of the motor 32, or even on the other side of valve 5. A separate auxiliary gas supply (as from a tank of compressed gas or another liquid oxygen converter) may be utilized to sup- 3 ply pressure in this circuit through valve 30, particularly for starting.
-To stop the operation of the system, the valve is closed. Valves 20 and 2| may then be closed, or check valves may be provided to prevent return flow if the apparatus supplied maintains pressure. To start the operation, the motor may be driven by an auxiliary gas supply, which is turned off at 30 as soon as the delivery pressure has built up sufficiently. Or, if some-pressure exists in the storage container, either because of vapor pressure being above atmospheric, or supplied from the pressure reducercircuit 26, the
In operation, the pressure delivered by the pump 33 must be greater than that required to drive the motor 32, the exhaust pressure greater than the gas pressure in the storage tank 34 if the exhaust gas is to be condensed, and the pressure in the storage tank 34 greater than the equilibrium vapor pressure by at least the lift from the tank to the pump.
Obviously, it is simpler if the pump 33 can be installed in or below the storage tank with no lift required. However, the embodiment shown was selected to show how satisfactory operation merely bubbling the exhaust gas flowing out of,
Referring to Fig. 2, this system operates as follows: When the starting vent valve 4 and high pressure valve 5 are opened, gas pressure in the evaporator or vaporizer circuit starts the motor I, and valve 4 may then be closed. The pressure of gas in the evaporator or vaporizer circuit pushes the piston 6 to the left, forcing liquid in the pumping chamber 1 into the evaporator or vaporizing circuit. When the valves 8 and 9 are moved to the other position at the end of the pumping stroke by the lost motion linkage 22, 23, 24, the driving gas is pushed out of the motor chamber In through outlet valve 8 as a result 01' the force of the compressed spring II and exhausts through a heat interchanger and through the check valve l9 and the conduit 3 to condense in the storage liquid. A the compression spring moves the piston 6 to the right, the plunger portion |2 on piston 6 draws liquid from the storage supply through conduit l3 into the pumping chamber 1, and the cycle then repeats. The cylinder vent I4 is provided to avoid compression, under the large end of the piston, and to vent blow-by gas. Operation may be started either as mentioned above, by opening the starting vent valve 4, with the storage liquid under somepressure, or by supplying gas under pressure to the motor inlet. To avoid vapor lock, the liquid should be supplied under pressure, either by pressurizing the supply container, or by installing the pump with a direct connection below the storage level. If the exhaust gas is used to pressurize the storage container, the pressure must not be so high but that the spring H can force the piston 6 to the right against the pressure acting on the differential area of the piston 6 and plunger l2.
For most eflicient utilization of gas and power. the dead volumein the chamber l0 should be as small as possible.
The areas of the piston and the plunger may be made equal for convenience of construction. but if so, the spring must work oppositely, to pump the liquid, and the return stroke must be powered by the pressure of the liquid from the storage container. Some gas must be vented to permit this operation.
A form of pump embodying these principles is shown in Fig. 3, with a flexible bellows l6 shown as a preferred construction instead of a piston.
The system here is the same as in Fig, 2, except for the action of the pump. Here the liquid is forced into the evaporator or vaporizer 3| circuit by the action of th tension spring l5 compressing the bellows IS, the pressures being essentially equal on the two sides of the bellows when the inlet valve 9' is open. When the valve positions reverse most of the gas in chamber l8 exhausts through the heat interchanger 28 and check valve 9 and conduit 3 to condense in the tank 34, but when the pressure falls below a certain value, the exhaust valv biased inwardly by a predetermined resilient force, opens and the remaining gas is vented to the atmosphere. The bellows 6 is expanded and the spring I5 stretched by liquid forced into the pump chamber 1' by the pressure over the storage liquid in tank 34.
The delivery valves 20 for liquid delivery and 2| for gas delivery may be of any suitable type.
The device is called a liquid oxygen pumping systern, but may be applied to the pumping of other liquified gases.
Various modifications in the form and ar rangement of the parts herein disclosed may be made without departing from the spirit and scope of the present invention, as defined in the appended claims.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
Whatisclaimedis:
1. A liquid oxygen pump apparatus comprising a storage tank for liquid oxygen, a heat interchanger, a liquid oxygen pump for pumping liquid from said storage tank to a delivery line through said interchanger, an evaporator connected to said line for evaporating a portion of the liquid supplied thereby, a gas delivery line connected to said evaporator, a gas motor for driving said pump energized by gas supplied from said gas delivery line through a control valve, a conduit for conducting the exhaust gas from said motor to'said heat interchanger for cooling said gas, and another conduit for conof the liquid supplied thereby, a gas delivery line connected to said evaporator, a gas motor for driving said pump energized by gas supplied from said gas delivery line through a control valve, a conduit for conductin the exhaust gas from said motor to said heat interchanger for cooling said gas, another conduit for conducting the cooled gas from said heat interchanger to the liquid in said storage tank for condensation therein, and a connection between the gas in said heat interchanger and the gas phase in said storage tank having a pressure reducing valve therein for maintaining a pressure differential to provide return flow of said cooled gas to the liquid in said storage tank through said other conduit.
3. A liquid oxygen pump apparatus comprising a storage tank for liquid oxygen, a heat interchanger, a liquid oxygen pump for pumping liquid from said storage tank to a delivery line through said interchanger, an evaporator connected to said line for evaporating a portion of the liquid supplied thereby, a gas delivery line connected to said evaporator, a gas motor for driving said pump energized by gas supplied from said gas delivery line through a control valve, a conduit for conducting the exhaust gas from said motor to said heat interchanger for cooling said gas, another conduit for conducting the gas from said heat interchanger to the liquid in said storage tank for condensation therein, and a starting vent valve connected to the motor exhaust gas conduit.
4. Apparatus as defined in claim 1 wherein the pump and motor is a piston unit of the reciprocating type, spring actuated in one direction and gas pressure actuated in the other.
5. Apparatus as defined in claim 1 wherein the pump and motor is a combined piston unit of the reciprocating type, spring actuated in one direction and gas pressure actuated in the other, having a vent conduit for conducting the blow oil gas from the rear of said motor piston to the exhaust gas conduit and to relieve the pressure at the rear of the motor piston.
- 6. Apparatus as defined in claim 3 wherein the pump and motor are combined into a bellowstype reciprocating unit, spring drawn in one direction, and difierential pressure actuated in the other direction by relieving the pressure on the outside of the bellows to atmospheric whenever said pressure is reduced to a predetermined limit, and a spring pressed exhaust valve opening inwardly by spring pressure, connected to the motor exhaust gas conduit for opening the latter to the atmosphere.
7. A pumping system for liquified gas comprising a liquified gas container, a pump driven by a gas motor for pumping said liquified gas from said container, an evaporator connected between said pump discharge and said motor, said motor being powered by gas obtained from the evaporation of some ofthe liquid being pumped, and means for condensing the spent motive gas from the motor in the storage liquid;
8. A pumping system for liquified gas comprising a liquified gas container, a pump driven by a gas motor for pumping said liquified gas from said container, an evaporator connected between said pump discharge and said motor, said motor being powered by gas obtained from the evaporation of some of the liquid being pumped, means for condensing the spent motive gas from the motor in the storage liquid, and means for maintaining pressure above the storage liquid at a value greater than its equilibrium value.
9. A pump for pumping liquified gas from a container, driven by a motor operating by gas under pressure, atmospheric heat absorbing means for evaporating a suflicient amount of the discharge from said pump to supply the motive gas to said motor,'a return conduit for the exhausted gas from said motor to the liquified gas from the container for condensation therein, and a heat exchanger in said return conduit for cooling said exhausted gas by the cooler discharge from the pump.
.10. A pump for pumping liquified gas from a container, driven by a motor operating by gas under pressure, atmospheric heat absorbing means for evaporating a suflicient amount of the discharge from said pump to supply the motive gas to said motor, a return conduit for the exhausted gas from said motor to the liquified gas from the container for condensation therein, a heat exchanger in said return conduit for cooling said exhausted gas by the cooler discharge from the pump, and means for maintaining pressure above the liquified gas in the container at a greater valuethan its equilibrium vapor pressure.
11. A pump for pumping liquified gas from a container, driven bya motor operating by gas under pressure, atmospheric heat absorbing means for evaporating a sufiicient amount of the discharge from said pump to supply the motive gas to said motor, a return conduit for the exhaust gas from said motor to the liquified gas from the container for condensation therein, a heat exchanger in said return conduit for cooling said exhausted gas by the cooler discharge from the pump, means for maintaining pressure above liquified gas in the container at a greater value than its equilibrium vapor pressure, and a conduit with a pressure reducing valve between a sufliciently high pressure point in the discharge from said pump and the container to control and maintain said greater value of pressure in the container.
WILLIAM A. WILDHACK.
REFERENCES CITED I The following references are of record in the file of this patent:
UNITED STATES PATENTS Germany June 17, 1940
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US647984A US2467413A (en) | 1946-02-15 | 1946-02-15 | Liquid oxygen pumping system |
GB3746/47A GB631196A (en) | 1946-02-15 | 1947-02-07 | Liquified gas pumping systems |
FR946232D FR946232A (en) | 1946-02-15 | 1947-02-15 | Pumping systems for oxygen or other liquefied gases |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US647984A US2467413A (en) | 1946-02-15 | 1946-02-15 | Liquid oxygen pumping system |
Publications (1)
Publication Number | Publication Date |
---|---|
US2467413A true US2467413A (en) | 1949-04-19 |
Family
ID=24598990
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US647984A Expired - Lifetime US2467413A (en) | 1946-02-15 | 1946-02-15 | Liquid oxygen pumping system |
Country Status (3)
Country | Link |
---|---|
US (1) | US2467413A (en) |
FR (1) | FR946232A (en) |
GB (1) | GB631196A (en) |
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2641907A (en) * | 1950-08-31 | 1953-06-16 | Carson D Baucom | Self-aid high-pressure metering system |
US2685174A (en) * | 1951-06-07 | 1954-08-03 | Joy Mfg Co | Method of and apparatus for the separation of gases |
US2700876A (en) * | 1951-12-03 | 1955-02-01 | Air Liquide | Plant for forcing gas under pressure from the liquefied gas |
US2750753A (en) * | 1955-09-14 | 1956-06-19 | Richard W Armstrong | Self-powered liquid oxygen pump and vaporizer |
DE944669C (en) * | 1951-10-23 | 1956-06-21 | Knapsack Ag | Process for the recovery of the exhaust gases produced when pumping low-boiling liquefied gases |
US2854826A (en) * | 1955-01-12 | 1958-10-07 | John Blue Company Inc | Method and system for transferring a pressurized normally gaseous liquid |
US2895305A (en) * | 1954-12-20 | 1959-07-21 | Phillips Petroleum Co | L.p.g. removal from underground storage |
US3018634A (en) * | 1958-04-11 | 1962-01-30 | Phillips Petroleum Co | Method and apparatus for vaporizing liquefied gases and obtaining power |
US3105361A (en) * | 1961-11-20 | 1963-10-01 | Thompson Ramo Wooldridge Inc | Zero gravity vent system |
US3123983A (en) * | 1961-01-16 | 1964-03-10 | Means for removal of liquefied gas | |
US3127752A (en) * | 1961-11-22 | 1964-04-07 | John P Smith | Automatic mobile liquid petroleum transfer device |
US3154928A (en) * | 1962-04-24 | 1964-11-03 | Conch Int Methane Ltd | Gasification of a liquid gas with simultaneous production of mechanical energy |
US3304730A (en) * | 1965-06-09 | 1967-02-21 | Robert B Gorham | Device to aid pumping of volatile gases |
US3591962A (en) * | 1969-03-26 | 1971-07-13 | Systems Capital Corp | Cryogenic power source for starting jet engines |
US3800550A (en) * | 1971-12-01 | 1974-04-02 | Chicago Bridge & Iron Co | System for reliquefying boil-off vapor from liquefied gas |
US4310491A (en) * | 1980-03-05 | 1982-01-12 | Hitachi, Ltd. | Apparatus for supplying raw liquid and relieving pressure of high-pressure product liquid |
US4314447A (en) * | 1979-07-02 | 1982-02-09 | Carrier Corporation | Refrigerant motor |
US4373750A (en) * | 1979-10-30 | 1983-02-15 | Societe Anonyme Dite: Vallourec | Joint for pipe intended for petroleum industry |
EP0099037A1 (en) * | 1982-07-01 | 1984-01-25 | Linde Aktiengesellschaft | Process and device for the supply of pressurized gas |
US4487025A (en) * | 1983-04-18 | 1984-12-11 | Halliburton Company | Passive booster for pumping liquified gases |
US4905719A (en) * | 1987-12-30 | 1990-03-06 | Lawless James C | Flurocarbon pumping system |
US4910964A (en) * | 1988-11-14 | 1990-03-27 | The Boc Group, Inc. | Liquid cryogenic transfer system |
US5211743A (en) * | 1989-05-29 | 1993-05-18 | Aga Aktiebolag | Treatment of a melt with a gas and means therefor |
US5678411A (en) * | 1995-04-26 | 1997-10-21 | Ebara Corporation | Liquefied gas supply system |
US5893707A (en) * | 1994-03-03 | 1999-04-13 | Simmons; John M. | Pneumatically shifted reciprocating pump |
US6203289B1 (en) * | 1997-06-09 | 2001-03-20 | Institut Francais Du Petrole | Hydraulic alternating volumetric pumping system |
US20050091991A1 (en) * | 2003-10-29 | 2005-05-05 | Consultoria Ss-Soluciones Sociedad Anonima | System and method for storing gases at low temperature using a cold recovery system |
US20070266846A1 (en) * | 2006-05-18 | 2007-11-22 | Simmons Tom M | Reciprocating pump, system or reciprocating pumps, and method of driving reciprocating pumps |
US11553998B2 (en) * | 2019-12-09 | 2023-01-17 | Shenzhen Yunding Information Technology Co., Ltd. | Water toothpick |
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US1871244A (en) * | 1931-08-19 | 1932-08-09 | Arthur B Steuart | Air conditioning system |
DE683153C (en) * | 1938-02-17 | 1939-10-31 | Julius Pintsch Kom Ges | Process for the production of compressed gas |
DE692326C (en) * | 1938-02-17 | 1940-06-17 | Julius Pintsch Kom Ges | Process for transferring liquefied gases |
-
1946
- 1946-02-15 US US647984A patent/US2467413A/en not_active Expired - Lifetime
-
1947
- 1947-02-07 GB GB3746/47A patent/GB631196A/en not_active Expired
- 1947-02-15 FR FR946232D patent/FR946232A/en not_active Expired
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US1871244A (en) * | 1931-08-19 | 1932-08-09 | Arthur B Steuart | Air conditioning system |
DE683153C (en) * | 1938-02-17 | 1939-10-31 | Julius Pintsch Kom Ges | Process for the production of compressed gas |
DE692326C (en) * | 1938-02-17 | 1940-06-17 | Julius Pintsch Kom Ges | Process for transferring liquefied gases |
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2641907A (en) * | 1950-08-31 | 1953-06-16 | Carson D Baucom | Self-aid high-pressure metering system |
US2685174A (en) * | 1951-06-07 | 1954-08-03 | Joy Mfg Co | Method of and apparatus for the separation of gases |
DE944669C (en) * | 1951-10-23 | 1956-06-21 | Knapsack Ag | Process for the recovery of the exhaust gases produced when pumping low-boiling liquefied gases |
US2700876A (en) * | 1951-12-03 | 1955-02-01 | Air Liquide | Plant for forcing gas under pressure from the liquefied gas |
US2895305A (en) * | 1954-12-20 | 1959-07-21 | Phillips Petroleum Co | L.p.g. removal from underground storage |
US2854826A (en) * | 1955-01-12 | 1958-10-07 | John Blue Company Inc | Method and system for transferring a pressurized normally gaseous liquid |
US2750753A (en) * | 1955-09-14 | 1956-06-19 | Richard W Armstrong | Self-powered liquid oxygen pump and vaporizer |
US3018634A (en) * | 1958-04-11 | 1962-01-30 | Phillips Petroleum Co | Method and apparatus for vaporizing liquefied gases and obtaining power |
US3123983A (en) * | 1961-01-16 | 1964-03-10 | Means for removal of liquefied gas | |
US3105361A (en) * | 1961-11-20 | 1963-10-01 | Thompson Ramo Wooldridge Inc | Zero gravity vent system |
US3127752A (en) * | 1961-11-22 | 1964-04-07 | John P Smith | Automatic mobile liquid petroleum transfer device |
US3154928A (en) * | 1962-04-24 | 1964-11-03 | Conch Int Methane Ltd | Gasification of a liquid gas with simultaneous production of mechanical energy |
US3304730A (en) * | 1965-06-09 | 1967-02-21 | Robert B Gorham | Device to aid pumping of volatile gases |
US3591962A (en) * | 1969-03-26 | 1971-07-13 | Systems Capital Corp | Cryogenic power source for starting jet engines |
US3800550A (en) * | 1971-12-01 | 1974-04-02 | Chicago Bridge & Iron Co | System for reliquefying boil-off vapor from liquefied gas |
US4314447A (en) * | 1979-07-02 | 1982-02-09 | Carrier Corporation | Refrigerant motor |
US4373750A (en) * | 1979-10-30 | 1983-02-15 | Societe Anonyme Dite: Vallourec | Joint for pipe intended for petroleum industry |
US4310491A (en) * | 1980-03-05 | 1982-01-12 | Hitachi, Ltd. | Apparatus for supplying raw liquid and relieving pressure of high-pressure product liquid |
EP0099037A1 (en) * | 1982-07-01 | 1984-01-25 | Linde Aktiengesellschaft | Process and device for the supply of pressurized gas |
US4487025A (en) * | 1983-04-18 | 1984-12-11 | Halliburton Company | Passive booster for pumping liquified gases |
US4905719A (en) * | 1987-12-30 | 1990-03-06 | Lawless James C | Flurocarbon pumping system |
US4910964A (en) * | 1988-11-14 | 1990-03-27 | The Boc Group, Inc. | Liquid cryogenic transfer system |
US5211743A (en) * | 1989-05-29 | 1993-05-18 | Aga Aktiebolag | Treatment of a melt with a gas and means therefor |
US5893707A (en) * | 1994-03-03 | 1999-04-13 | Simmons; John M. | Pneumatically shifted reciprocating pump |
US5678411A (en) * | 1995-04-26 | 1997-10-21 | Ebara Corporation | Liquefied gas supply system |
US6203289B1 (en) * | 1997-06-09 | 2001-03-20 | Institut Francais Du Petrole | Hydraulic alternating volumetric pumping system |
US20050091991A1 (en) * | 2003-10-29 | 2005-05-05 | Consultoria Ss-Soluciones Sociedad Anonima | System and method for storing gases at low temperature using a cold recovery system |
US7024885B2 (en) | 2003-10-29 | 2006-04-11 | Consultoria Ss-Soluciones Sociedad Anonima | System and method for storing gases at low temperature using a cold recovery system |
US20070266846A1 (en) * | 2006-05-18 | 2007-11-22 | Simmons Tom M | Reciprocating pump, system or reciprocating pumps, and method of driving reciprocating pumps |
US7458309B2 (en) | 2006-05-18 | 2008-12-02 | Simmons Tom M | Reciprocating pump, system or reciprocating pumps, and method of driving reciprocating pumps |
US11553998B2 (en) * | 2019-12-09 | 2023-01-17 | Shenzhen Yunding Information Technology Co., Ltd. | Water toothpick |
Also Published As
Publication number | Publication date |
---|---|
GB631196A (en) | 1949-10-28 |
FR946232A (en) | 1949-05-27 |
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