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WO1996033367A1 - Appareil destine a prelever un liquide d'un recipient et procede associe - Google Patents

Appareil destine a prelever un liquide d'un recipient et procede associe Download PDF

Info

Publication number
WO1996033367A1
WO1996033367A1 PCT/US1996/004107 US9604107W WO9633367A1 WO 1996033367 A1 WO1996033367 A1 WO 1996033367A1 US 9604107 W US9604107 W US 9604107W WO 9633367 A1 WO9633367 A1 WO 9633367A1
Authority
WO
WIPO (PCT)
Prior art keywords
liquid
container
conduit
pressure
pick
Prior art date
Application number
PCT/US1996/004107
Other languages
English (en)
Inventor
Dominick J. Frustaci
James P. Dominiak
Original Assignee
Figgie International Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Figgie International Inc. filed Critical Figgie International Inc.
Priority to AU54316/96A priority Critical patent/AU5431696A/en
Priority to DE69601309T priority patent/DE69601309T2/de
Priority to EP96911426A priority patent/EP0824647B1/fr
Publication of WO1996033367A1 publication Critical patent/WO1996033367A1/fr

Links

Classifications

    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B7/00—Respiratory apparatus
    • A62B7/06—Respiratory apparatus with liquid oxygen or air; Cryogenic systems
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B7/00—Respiratory apparatus
    • A62B7/02—Respiratory apparatus with compressed oxygen or air
    • 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
    • F17C7/00—Methods or apparatus for discharging liquefied, solidified, or compressed gases from pressure vessels, not covered by another subclass
    • F17C7/02—Discharging liquefied gases
    • F17C7/04—Discharging liquefied gases with change of state, e.g. vaporisation
    • 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
    • F17C9/02—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure with change of state, e.g. vaporisation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
    • B63C11/00—Equipment for dwelling or working underwater; Means for searching for underwater objects
    • B63C11/02—Divers' equipment
    • B63C11/18—Air supply
    • B63C11/22—Air supply carried by diver
    • B63C2011/2263—Air supply carried by diver using breathing gas stored in its liquid phase, e.g. cryogenic breathing gas
    • 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
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0104—Shape cylindrical
    • F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
    • 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
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05—Size
    • F17C2201/056—Small (<1 m3)
    • 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
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/03—Thermal insulations
    • F17C2203/0391—Thermal insulations by vacuum
    • 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
    • F17C2205/0123—Mounting arrangements characterised by number of vessels
    • F17C2205/013—Two or more vessels
    • 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
    • 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
    • F17C2205/0338—Pressure regulators
    • 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
    • F17C2205/0382—Constructional details of valves, regulators
    • F17C2205/0385—Constructional details of valves, regulators in blocks or units
    • 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
    • F17C2205/0388—Arrangement of valves, regulators, filters
    • F17C2205/0391—Arrangement of valves, regulators, filters inside the pressure vessel
    • 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
    • F17C2205/0388—Arrangement of valves, regulators, filters
    • F17C2205/0394—Arrangement of valves, regulators, filters in direct contact with the pressure vessel
    • F17C2205/0397—Arrangement of valves, regulators, filters in direct contact with the pressure vessel on both sides of the pressure vessel
    • 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
    • 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
    • F17C2221/014—Nitrogen
    • 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
    • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • 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
    • 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
    • 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
    • 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
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/0408—Level of content in the vessel
    • F17C2250/0413—Level of content in the vessel with floats
    • 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
    • F17C2270/02—Applications for medical applications
    • F17C2270/025—Breathing
    • 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
    • F17C2270/05—Applications for industrial use
    • F17C2270/0509—"Dewar" vessels

Definitions

  • the present invention generally relates to liquid withdrawal from a container. More particularly, the present invention relates to an apparatus that provides for withdrawal of the liquid contents from a closed container, independent of the spatial orientation thereof.
  • the apparatus is useful in a self contained breathing apparatus (SCBA) type respirator for withdrawal of a liquefied breathable gas mixture from the container.
  • SCBA self contained breathing apparatus
  • the present apparatus is useful for withdrawal of any liquid from a closed container by the pressure differential communicated between the inside of the container and a removal means located outside the container through a flexible conduit.
  • One preferred embodiment of the liquid withdrawal apparatus of the present invention includes a flexible conduit disposed inside a container and in fluid flow communication with an external heat exchanger.
  • the heat exchanger serves to input heat energy from the ambient atmosphere to the withdrawn liquid to thereby provide a breathable gas mixture.
  • the pick-up end of the flexible conduit is weighted to ensure only liquid withdrawal, independent of the spatial orientation of the container.
  • the flexible conduit transmits through a pressure barrier at the container outlet to communicate with the heat exchanger.
  • the pressure barrier seals around the flexible conduit to ensure that there is little to no communication of pressure between the inside of the container and the heat exchanger, other than the fluid flow communication path provided by the conduit itself.
  • U.S. Patent No. 3,572,048 to Murphy describes an omnipositional cryogenic underwater breathing apparatus comprising a reservoir tank having two weighted liquid air pick-up tubes disposed transverse through the length of the tank.
  • the pick-up tubes each are in turn connected to coiled tube sections which have spring like properties that permit the weighted ends of the pick-up tubes to fully move about the cross-section of the reservoir under the force of gravity.
  • the pick-up tubes are not flexible and the coiled tube sections only permit movement of the pick-up tubes about the cross-section of the tank, not about the entire volume enclosed by the tank, as in the present invention.
  • the Murphy breathing apparatus is not provided with a barrier structure at the tank outlet to regulate pressure communication between the inside of the tank and the heat exchangers.
  • U.S. Patent No. 3,318,307 to Nicastro describes a breathing pack for converting liquid air or liquid oxygen into a breathable gas.
  • This device includes a weighted liquid withdrawal tube extending laterally outwardly from a lower swivel.
  • the lower swivel is connected by a pivot tube to an upper swivel which in turn has a gas pressurizing tube extending laterally outwardly therefrom, but in an opposite direction with respect to the liquid withdrawal tube.
  • the weighted liquid withdrawal tube ensures that the liquid contents are fed to a heat exchanger to vaporize the liquid.
  • the liquid withdrawal tube is not flexible and it would not be in contact with the liquid contents in all intended orientations of use of the container, for example, if the container was positioned upside down.
  • the withdrawal structure does not ensure liquid removal throughout the entire volume of the container. Instead, there can be withdrawal of the gaseous contents.
  • the weighted pick-up head of the present invention precludes this from occurring. Since the liquid withdrawal conduit is flexible and its pick-up end is weighted, only the liquid contents are removed from the container. When the liquid contents are a liquefied, breathable gas mixture, this ensured that only the withdrawn liquid is flowed to the endothermic heat exchanger, which transfers heat energy from the ambient atmosphere to the liquid to vaporize the liquid to a breathable gas having concentrations of the various constituents at a similar relative content as they are in the liquid phase. In other words, vaporization of the liquid contents only occurs in the heat exchangers at a rate relative to consumption at the facepiece. In this manner, the oxygen content of the vaporized gas remains at a concentration level similar to that of the cryogenic liquid.
  • U.S. Patent No. 5,353,835 to Mills describes a compressed air tank having a venturi drain used to extract fluid from the bottom of the tank as the stored air is simultaneously withdrawn therefrom.
  • the venturi drain includes a flexible suction tube extending from a tank port to a lower position in the tank where the tube's terminal open end is held by a weight.
  • the opposite proximal open end of the suction tube is positioned within the tank port, and as compressed air is withdrawn from the tank a venturi effect creates a suction in the tube which in turn withdraws the liquid from the bottom of the tank.
  • This device would not function properly in all intended spatial orientations of use, for example, in an upside down position.
  • a venturi device is not practical with the present invention because such a structure would prevent the creation of a pressure differential along a fluid flow communication path provided by the liquid withdrawal conduit extending between the container interior and the external heat exchanger.
  • the pressure differential is created by an inhalation event of the user breathing from downstream of the heat exchanger, and the pressure differential is responsible for regulated delivery of the breathable gas to the user.
  • the gas removed from the container is a breathable gas, the gas used to drive the venturi will mix with the breathable gas and contaminate it.
  • the liquid withdrawal apparatus of the present invention includes a flexible conduit provided with a pick-up head at an upstream end thereof.
  • the pick-up head keeps the withdrawal conduit in contact with the liquid contents of, for example, a liquefied-gas container, at all times and even when the liquid contents are nearly depleted, independent of the spatial orientation of the container.
  • the withdrawal conduit comprises a multiplicity of relatively small diameter, flexible tubes.
  • the pick-up head is an asymmetrically weighted flotation device that ensures that the pick-up end of the withdrawal conduit is always submerged below the liquid surface rather than in communication with the gaseous head.
  • the outlet end of the withdrawal conduit delivers the liquid contents to one or more endothermic heat exchangers, sufficiently downstream from the Dewar container to ensure rapid vaporization of the liquid to a warmed, breathable gas.
  • a barrier structure such as a septum and the like, is provided at the entrance to the heat exchanger, upstream from the outlet end of the withdrawal conduit to ensure that there is little to no communication of pressure (and consequently fluid) from the inside of the Dewar to the heat exchanger, other than the pressure communication path provided by the withdrawal conduit itself. It is the pressure differential between the inside of the Dewar container, as generated by the liquid saturated to some pressure P d , and the pressure in the heat exchange P h , which is the driving force for delivering liquid to the heat exchanger.
  • a multi-component liquid such as a liquefied, breathable gas mixture comprising nitrogen and oxygen
  • the withdrawn liquid is than vaporized to a gaseous phase. Since the liquid is vaporized in a relatively closed system, i.e., in the heat exchanger, the percentage of the various constituents in the gaseous phase is similar to the liquid phase.
  • the present invention prevents withdrawal from the head space of the container. Withdrawal from the head space is undesirable because the constituent with the lower vapor pressure, i.e., nitrogen, flashes before oxygen to give a nitrogen rich gas at the breathing regulator.
  • Fig. 1 is a view, partly elevational, partly cross- sectional, partly schematic and partly in block diagram of a Dewar container 10 including a liquid withdrawal conduit means 58 of the present invention associated with a pick-up head-means 60 floating on the surface of the cryogenic liquid 16.
  • Fig. 2 is an enlarged and broken away, partial elevational, partial cross-sectional view of one pair of capillary tubes 136 of the liquid withdrawal conduit means 58 passing through a septum 140.
  • Fig. 3 is a cross-sectional view of one embodiment of a float-type liquid pick-up head means 68 of the present invention.
  • Fig. 4 is a partial elevational, partial cross- sectional view of the Dewar container 10 shown in Fig. l provided with a sinker-type liquid pick-up head means 66 submerged in the cryogenic liquid 16.
  • Fig. 5 is a broken away, partial cross-sectional view of the Dewar container 10 shown in Fig. 4 rotated 90 degrees into a horizontal position.
  • Fig. 6 is a cross-sectional view of another embodiment of a float-type liquid pick-up head means 78 according to the present invention.
  • Fig. 7 is a cross-sectional view of the float-type liquid pick-up head means 78 shown in Fig. 6 and floating in the cryogenic liquid 16.
  • Fig. 8 is a bottom plan view of the sinker-type liquid pick-up head means 94 shown in Figs. 2 to 3.
  • Fig 9 is a cross-sectional view along line 9-9 of Fig. 8.
  • Fig. 10 is an enlarged and broken away, partial elevational, partial cross-sectional view of the Dewar container 10 according to the present invention including a sinker-type pick-up head 116.
  • Figs. 1, 4 and 10 show a cryogenic fluid Dewar container 10, partly in elevation, partly in schematic and partly in cross- section, which is suitable for use with the liquid withdrawal apparatus of the present invention. It should be understood that container 10 is merely exemplary, and in that respect, container 10 represents one embodiment of a container that is useful with the liquid withdrawal apparatus of the present invention.
  • the present liquid withdrawal apparatus is useful with many types of containers whose shape and construction are only limited by the imagination of those skilled in the art.
  • container 10 is shown having a generally cylindrical shape closed at both ends, the present liquid withdrawal apparatus can be adapted for use with containers having a myriad of shapes other than cylindrical.
  • the container does need to be closed.
  • the cryogenic liquid Dewar container 10 comprises an outer container means or outer shell 12 mounted around and surrounding an inner container means or inner shell 14 containing a cryogenic liquid 16.
  • the cryogenic liquid 16 is a liquefied-gas mixture capable of supplying a breathable gas mixture to a breathing regulator 18 and an associated facepiece 20, as indicated in block diagram representation in Fig. 1.
  • the outer shell 12 has a generally cylindrical side wall extending along and around the longitudinal axis of the container 10 with first and second dome portions 12A and 12B closing the opposed ends thereof.
  • the inner shell 14 has a cylindrical side wall extending along and around the longitudinal axis with first and second dome portions 14A and 14B closing the opposed ends thereof.
  • the space 22 formed between the coaxially aligned outer and inner shells 12 and 14 is evacuated and provided with an insulation material (not shown) that helps to thermally insulate the cryogenic liquid 16 from the ambient environment.
  • a getter material 24 is mounted on the outside of the second dome 14B of the inner shell 14 to remove any residual gases in the evacuated space 18 between the shells 12 and 14 by a sorption process.
  • This insulation structure is typically referred to as super insulation and is commonly used in the construction of liquified gas containers.
  • a liquid fill valve 26 is mounted on the second dome 12B of the outer shell 12.
  • Valve 26 serves as a connection means for connecting the Dewar container 10 to a pressurized liquefied-gas supply (not shown) for filling the cryogenic liquid 16 into the inner shell 14.
  • a tube 28 supports a manifold block 30 positioned spaced above the first dome 14A of the inner shell 14, as oriented with respect to Fig. 1. Tube 28 depends into the interior of the inner shell 14, to provide a vent space where a gas pocket forms to prevent the inner shell from being overfilled, as is well known to those skilled in the art.
  • the saturation vapor pressure of the cryogenic liquid 16 inside the inner shell 14 is about 60 psig minimum, and more preferably at about 100 to 130 psig.
  • a relief valve (not shown) , compatible with cryogenic fluids, communicates with the interior of the inner shell 14. In case of over pressurization of the inner shell, the relief valve is set to actuate at about 140 psig.
  • Valve 26 leads to a gas trap 32 forming a 360 degree loop in the insulating space 22 between the shells 12 and 14. When valve 26 is closed and with cryogenic liquid 16 provided in the inner shell 14, there will always be a high side of the trap 32 that is filled with gas.
  • the difference in the coefficient of heat transfer of a gas compared to a liquid is on the order of magnitude of about ten to as much as a thousand for a boiling liquid. That way, trap 32 helps prevent ambient heat from conducting to the cryogenic liquid 16 in the inner shell 14.
  • a first opening 34 is provided in the upper dome 12A of the outer shell 12 and a second opening 36 is provided in the upper dome 14A of the inner shell 14.
  • the perimeter of opening 34 is spaced from a cylinder 38 having its lower end secured to the perimeter of the second opening 36 aligned along the longitudinal axis of the container 10.
  • An annular flange 42 has an enlarged base portion 44 secured to the perimeter of opening 34, spaced from the side wall of cylinder 38 with an inwardly extending upper annular rim 46 secured to the cylinder 38 adjacent to the annular connection.
  • a cap 48 is threaded on flange 42.
  • Cap 48 is provided with a central recess 50, a bottom wall 52 of which has an opening.
  • Bottom wall 52 supports a sleeve 54 fitted in a closely spaced relationship around a portion of the tube 28 communicating between the interior of the inner shell 14 and the exterior thereof.
  • a compression nut 56 is threaded on sleeve 54 to align the tube 28 and the manifold block 30.
  • Tube 28 partially sheaths a flexible liquid withdrawal conduit means 58 (shown partly in elevation and partly in dashed lines in Figs. 1 and 4) having an end disposed inside of a pick-up head means 60 (Figs. 1, 4 and 5) that ensures that the pick-up end of the conduit means 58 is always submerged below the surface of the cryogenic liquid 16, independent of the spatial orientation of the container 10.
  • the pick-up means 60 preferably has a spherical shape with a polished finish. This allows the pick-up head means 60 to translate on the inner surface of the inner shell 14 and decreases the coefficient of sliding friction between the pick-up head means 60 and the inner shell 14.
  • the inner surface of the inner shell preferably have a continuously curved configuration (not shown in Figs. 1, 4, 5 and 10) .
  • the first type consists of a float-type pick-up head 64 (Fig. 1) which rests on the surface of the cryogenic liquid 16.
  • Float 64 is asymmetrically weighted to ensure that the pick-up end of the liquid withdrawal conduit means 58 is always in contact with the cryogenic liquid 16 as the liquid moves in the inner shell 14 in response to changing Dewar container 10 orientations.
  • Another type of liquid pick-up head means 60 comprises a weighted member, such as a sinker-type 66, as shown in Figs. 4 and 5. In this latter embodiment, the pick-up end of the liquid withdrawal conduit means 58 is submerged in the cryogenic liquid 16 with the sinker 66 readily following the low side (Fig. 3) of the inner surface of the inner shell 14.
  • the sinker 66 ensures that the liquid withdrawal conduit means 58 is always in fluid flow communication with the liquid 16 until the liquid is essentially depleted from the inner shell 14, independent of the spatial orientation thereof.
  • the pick-up head means comprising the float-type 64 and the sinker-type 66 will be described in detail presently.
  • one embodiment of the float- type liquid pick-up head 64 comprises a spherically- shaped member 68 having a main opening 70 provided with a grommet 72.
  • the liquid withdrawal conduit means 58 pass through the grommet 72 and extend to a differential weight 74 disposed inside the sphere 68 opposite the main opening 70.
  • the pick-up end of the four withdrawal conduits 58 each terminate at respective openings 76 in the sphere 68. This structure maintains each of the withdrawal conduits 58 in fluid flow communication with the cryogenic liquid 16 in the inner shell 14 as the sphere 68 rests on the surface thereof.
  • Figs. 6 and 7 show one embodiment of a sinker-type liquid pick-up head 66 comprising a spherically-shaped member 78.
  • Sphere 78 has a plurality of openings or perforations 80 therein for fluid flow communication of the cryogenic liquid 16 into the interior of the sphere 78.
  • a wicking material 82 such as a felt material and the like, is disposed inside the sphere 78 supporting a secondary sphere 84 at a central location therein.
  • the secondary sphere 84 is also hollow with a plurality of openings or perforations 86 that provide for fluid flow communication of the cryogenic fluid 16 therein.
  • the sphere 78 includes a main opening 88 provided with a grommet 90 having the withdrawal conduits 58 passing therethrough.
  • the withdrawal conduits 58 enter the secondary sphere 84 with their pick-up ends 92 positioned approximately at the center of the secondary sphere 84.
  • the liquid 16 enters the sphere 78 through the openings 80.
  • the wicking material 82 draws the cryogenic liquid 16 up into the sphere 78 to a level such that the cryogenic liquid 16 flows through the openings 92 and fills into the secondary sphere 84.
  • the cryogenic liquid 16 fills the secondary sphere 84 by capillary action to a level above the center point thereof and sufficient for fluid flow communication with the pick-up end of the withdrawal conduits 58.
  • the pick-up end of conduits 58 are fixed at the center point of secondary sphere 84 so that no matter the orientation of sphere 84, there is always fluid flow communication with the conduits 58.
  • FIG. 8 Another embodiment of the sinker-type liquid pick- up head 66 is shown in Figs. 8 and 9, and it comprises a spherically-shaped weighted member 94.
  • sphere 94 is preferably made of a metal material having a sufficient mass to seek the low side of the inner surface of the inner shell 14, it can also be made of a plastic or other materials. In the latter case, the sphere 94 is weighted, for example by differential weight 74 shown in Fig. 3, to ensure that the withdrawal conduits 58 are always immersed in the cryogenic liquid 16 at the low side of the inner shell 14.
  • Spherical member 94 is provided with a sufficient number of through bores to receive the withdrawal conduits 58. There can be as few as one conduit 58, or as many as four or more of them.
  • Fig. 9 shows an exemplary conduit bore 96 comprising a first diameter passage 98 extending from an upper position on sphere 94 to an outwardly tapered frusto-conically shaped section 100. Passage 98 is sized to receive the withdrawal conduits 58 in a closely spaced relationship.
  • Frusto- conical section 100 leads to a threaded bore 102 having a diameter sized to receive a threaded insert 104.
  • Insert 104 has a first, large diameter opening 106 leading to a second inner fluid opening 108 having a lesser diameter extending to a central tap 110 provided with a frusto-conical shape.
  • the insert 104 is threaded therein to cause the tap 110 to capture the pick-up end of the withdrawal conduits 58 between the tap 110 and the frusto-conical section 100 of passage 98.
  • a lock ring 112 is then inserted into the threaded bore 102 abutting the insert 104 to lock the insert 104 and captured conduit 62 in place.
  • the spherical member 94 is completed by a plurality of blind bores 114 drilled or otherwise formed extending therein.
  • the blind bores 114 are provided from both upper and lower positions on the sphere 94 and serve to remove weight from the sphere.
  • Fig. 10 shows still another embodiment of a sinker- type liquid pick-up head 66 comprising a generally hollow sphere 116 having the withdrawal conduits 58 associated therewith.
  • Sphere 116 has a plurality of openings or perforations 118 through its sidewall which provide for fluid flow of the cryogenic liquid 16 into and out of the interior thereof.
  • a weighted block 120 having a sufficient number of bores to receive the respective withdrawal conduits 58 is enclosed inside sphere 116.
  • Bore 122 is exemplary and it has a first portion 124 sized to receive one of the withdrawal conduits 58 in a closely spaced relationship therewith.
  • the first portion 124 of bore 122 leads to a second portion 126 having an outwardly extending frusto-conical taper that in turn forms into a cylindrically shaped portion.
  • the cylindrical portion threadingly receives an insert 138 that captures the pick-up end of the withdrawal conduit 58 there and in fluid flow communication with the cryogenic liquid 16 when the sphere 116 is immersed in the liquid.
  • Sphere 116 is not shown immersed in cryogenic liquid 16 in Fig. 10.
  • Sphere 116 is further provided with a number of tube openings 130 that receive the withdrawal conduits 58 for passage therein and eventually into the block 120.
  • An elastomeric washer 132 is fitted around each withdrawal conduit on the inside of sphere 116 while individual grommets 134 surround the tubes 62 proximate the outer surface of the sphere 116. The grommets 134 abut the outer surface of the sphere 116 and help prevent chaffing and wear of the withdrawal conduits 58 against the opening 130.
  • the withdrawal conduits 58 are in fluid flow communication between the pick-up head 60 through tube 28 to an upper end thereof where they separate into two pairs of conduits 134 and 138.
  • Each conduit pair 136 and 138 passes through a corresponding pressure barrier, such as septums 140 and 142 disposed inside passages in the manifold block 30 and lead into respective heat exchangers 144 and 146 (shown in dashed lines in Fig. 1) .
  • the bifurcation of the withdrawn liquid into two heat exchangers 144 and 146 benefits the dynamics of vaporization of the liquid to a gaseous phase and helps maintain a uniform pressure profile through the entire length of the system.
  • Septum 140 is exemplary. As particularly shown in Fig. 4, the pair of conduits 136 communicate through the septum 140 received in a passage 148 in the manifold block 30.
  • the septum 140 is secured in passage 148 with a nut 150 threaded therein.
  • a washer 152 abuts the nut 150 and is locked in place with a fitting 154 threaded into the passage 148.
  • the downstream end of fitting 154 is provided with an inner frusto-conically shaped taper 156 that receives an annular elastomeric wedge 158 sealed around an intermediate conduit 160 leading to a heat exchanger conduit 162 connected to heat exchanger 144.
  • a union nut 164 is threaded onto the downstream end of the fitting 154 to secure the seal 158 around the intermediate conduit 160.
  • This construction ensures that the septum 140 captures the pair of conduits 136 sealed in respective openings therethrough so that there is little or no communication of pressure (or mass) between the inside of the inner shell 14 and the endothermic heat exchanger 144, other than the communication path afforded by the inside of the pair of conduits 136 themselves.
  • the other pair of conduits 138 and its septum 142 is similar in construction and, as shown in Figs.
  • the heat exchangers 144 and 146 each receive about one half of the withdrawn liquid and they serve to transfer heat from the ambient atmosphere to the cryogenic liquid 16, which preferably is a liquefied breathable gas mixture, to vaporize the liquid to a gas and then to warm the gas to a breathable temperature.
  • An outboard end of the endothermic heat exchangers 144, 146 merges at a manifold (not shown) that connects to a flexible breathing hose 176 that supplies the warmed gas to the breathing pressure regulator 18 and an associated facepiece 20 worn by the user breathing the gas mixture, as shown schematically in Fig. 1.
  • the septa 140, 142 ensure that the sole path of pressure and mass communication between the inside of the inner shell 14 and the heat exchangers 144, 146 is through the withdrawal conduit 58 to maintain the uniform system pressure up to the regulator.
  • the cryogenic liquid 16 is preferably at a saturated liquid pressure of between about 100 to 130 psig, and this operating pressure is transmitted through the entire length of the withdrawal system.
  • Dewar container 10 is intended for use by people needing to breath in a hostile environment where the atmosphere may not be conducive to supporting life. In that respect and initially referring to Fig. 1, a user will first don the facepiece 20 and associated breathing gas regulator 18 while the container 10 is carried on the back by a harness, as is well known to those of ordinary skill in the art.
  • Inner shell 14 has previously been filled with cryogenic liquid 16 at a liquid saturation pressure of about 100 to 130 psig.
  • the cryogenic liquid 16 is preferably a breathable gas mixture.
  • the regulator 18 associated with the facepiece 20 is then actuated and breathing begins.
  • the various pick-up heads means 60 i.e. the float-type members 64 shown in Figs. 1 and 3 and the sinker-type members 66 shown in Figs. 4 to 10 ensure that the inlet to the withdrawal conduits 58 are in fluid flow communication with the liquid 16, independent of the spatial orientation of the Dewar 10.
  • the withdrawal conduits split into the conduit pairs 136 and 138 which transmit through the septa 140, 142 and deliver the liquid 16 to the respective heat exchangers 144 and 146.
  • the septa 140, 142 ensure that the only communication path between the inside of the inner shell 14 and the endothermic heat exchangers 144, 146 is afforded by the withdrawal conduit 58 themselves.
  • the outlet of the withdrawal conduit 58 empties into the heat exchangers 144, 146 which transfer heat from the ambient atmosphere to the cryogenic liquid, thereby vaporizing the liquid to a gas and then warm the gas to about ambient temperature. Alternatively, the gas can be warmed to a cooler temperature than ambient if so desired.
  • the heat exchangers 144 and 146 maintain the concentration of the various constituents consisting of the liquified gas mixture at a similar concentration as they are in the liquid phase.
  • the breathable gas mixture flows from the heat exchangers to a manifold
  • cryogenic liquid 16 at about 100 to 130 psig is transmitted through the conduit pairs 136 and 138 and the heat exchangers 144 and 146 where heat is transferred to the liquid to first provide a raised fluid and as further heat is transferred, the gas is warmed to about ambient temperature and made suitable for breathing.
  • this breathable gas communicates to the regulator 18 attached to the facepiece 20 such that the entire system including the liquid withdrawal conduit means 58, the heat exchangers 144 and 146 and the breathing hose 176 leading to the facepiece regulator 18 are approximately at the pressure of the saturated liquid, i.e.
  • the regulator provides the breathing gas to the facepiece 20 on demand while maintaining a positive pressure inside the facepiece of about 0 to 2 inches water column above the pressure outside the facepiece.
  • the regulator 18 also can be used in a constant flow mode or any other mode of operation, as is well known to those skilled in the art.
  • the pressure differential again causes liquid 16 to flow in the flexible withdrawal conduits 58 from the relatively high pressure Dewar container to the lower pressure heat exchanger 144 and 146 side to replace the gaseous volume removed or consumed from the heat exchangers 144 and 146 during the breathing event until pressure equilibrium is again established. Consequently, fluid flow from the inner shell 14 of the Dewar container 10 to the heat exchangers 144 and 146 is governed by any withdrawal or removal of gas from the system, for example, the user's respiratory demand requirements.
  • the inner shell 14 is charged with a liquid mixture saturated at a pressure within this range.
  • the head gases inside the inner shell 14 do not get consumed during the respiratory demand cycles because of the septa 140, 142, and the liquid removal or withdrawal system operates at 100 to 130 psig until the liquid contents are depleted.

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  • Health & Medical Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Emergency Medicine (AREA)
  • Pulmonology (AREA)
  • General Health & Medical Sciences (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Automatic Analysis And Handling Materials Therefor (AREA)

Abstract

Appareil destiné à prélever le liquide présent dans un récipient fermé (14) indépendamment de l'orientation spatiale de ce dernier, qui comporte des conduits (58) de prélèvement souples placés à l'intérieur du récipient et en communication fluidique avec des échangeurs de chaleur (144, 146) externes. Lesdits échangeurs de chaleur servent à transférer de la chaleur au liquide prélevé afin de fournir ainsi un mélange gazeux respirable. Les extrémité de captage des conduits de prélèvement (58) sont lestées pour assurer le prélèvement de liquide pendant les changements d'orientation du récipient, tandis que l'extrémité de sortie des tubes (62) communique par l'intermédiaire de diaphragmes (140, 142) qui garantissent une communication minime, voire inexistante, de pression entre l'intérieur du récipient et les échangeurs de chaleur, outre la communication fluidique assurée par les conduits eux-mêmes. Un différentiel de pression entre l'intérieur du récipient et les échangeurs de chaleur externes, normalement provoqué par l'inspiration de l'utilisateur, fournit la force motrice permettant de prélever le liquide du récipient par l'intermédiaire des conduits.
PCT/US1996/004107 1995-04-20 1996-03-22 Appareil destine a prelever un liquide d'un recipient et procede associe WO1996033367A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
AU54316/96A AU5431696A (en) 1995-04-20 1996-03-22 Apparatus for withdrawal of liquid from a container and meth od
DE69601309T DE69601309T2 (de) 1995-04-20 1996-03-22 Apparat und methode zur entnahme von flüssigkeiten aus einem behälter
EP96911426A EP0824647B1 (fr) 1995-04-20 1996-03-22 Appareil destine a prelever un liquide d'un recipient et procede associe

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US42591695A 1995-04-20 1995-04-20
US08/425,916 1995-04-20

Publications (1)

Publication Number Publication Date
WO1996033367A1 true WO1996033367A1 (fr) 1996-10-24

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EP (1) EP0824647B1 (fr)
AU (1) AU5431696A (fr)
DE (1) DE69601309T2 (fr)
WO (1) WO1996033367A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999019663A1 (fr) * 1997-10-15 1999-04-22 Scott Technologies, Inc. Appareil permettant de prelever le liquide d'un recipient, et procede associe
WO2008155656A3 (fr) * 2007-03-06 2009-03-19 Honda Motor Co Ltd Equipement de gestion de l'écoulement de gaz pour réservoirs de stockage haute pression
WO2009040667A3 (fr) * 2007-03-19 2009-05-22 Honda Motor Co Ltd Gestion thermique de réservoirs de stockage de gaz à haute pression

Citations (4)

* 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
WO1994008177A2 (fr) * 1992-10-06 1994-04-14 Oceaneering International, Inc. Appareil de stockage et de distribution de cryogene liquide et ses appareil et procede de remplissage
US5353835A (en) * 1993-09-23 1994-10-11 Ingersoll-Rand Company Air tank drain
US5357758A (en) * 1993-06-01 1994-10-25 Andonian Martin D All position cryogenic liquefied-gas container

Patent Citations (4)

* 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
WO1994008177A2 (fr) * 1992-10-06 1994-04-14 Oceaneering International, Inc. Appareil de stockage et de distribution de cryogene liquide et ses appareil et procede de remplissage
US5357758A (en) * 1993-06-01 1994-10-25 Andonian Martin D All position cryogenic liquefied-gas container
US5353835A (en) * 1993-09-23 1994-10-11 Ingersoll-Rand Company Air tank drain

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999019663A1 (fr) * 1997-10-15 1999-04-22 Scott Technologies, Inc. Appareil permettant de prelever le liquide d'un recipient, et procede associe
WO2008155656A3 (fr) * 2007-03-06 2009-03-19 Honda Motor Co Ltd Equipement de gestion de l'écoulement de gaz pour réservoirs de stockage haute pression
WO2009040667A3 (fr) * 2007-03-19 2009-05-22 Honda Motor Co Ltd Gestion thermique de réservoirs de stockage de gaz à haute pression

Also Published As

Publication number Publication date
DE69601309D1 (de) 1999-02-18
AU5431696A (en) 1996-11-07
EP0824647A1 (fr) 1998-02-25
EP0824647B1 (fr) 1999-01-07
DE69601309T2 (de) 1999-08-26

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