US20090301104A1 - Container for cryogenic liquids - Google Patents
Container for cryogenic liquids Download PDFInfo
- Publication number
- US20090301104A1 US20090301104A1 US12/297,006 US29700607A US2009301104A1 US 20090301104 A1 US20090301104 A1 US 20090301104A1 US 29700607 A US29700607 A US 29700607A US 2009301104 A1 US2009301104 A1 US 2009301104A1
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- US
- United States
- Prior art keywords
- container
- support
- inner containers
- longitudinal axis
- containers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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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
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
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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
- 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
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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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/014—Suspension means
- F17C2203/015—Bars
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0617—Single wall with one layer
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- 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
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0619—Single wall with two layers
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- 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
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0639—Steels
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/066—Plastics
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/0663—Synthetics in form of fibers or filaments
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- 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
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
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- F17C2203/0663—Synthetics in form of fibers or filaments
- F17C2203/0673—Polymers
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- 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
- F17C2205/0103—Exterior arrangements
- F17C2205/0111—Boxes
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- 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
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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
- F17C2205/0123—Mounting arrangements characterised by number of vessels
- F17C2205/013—Two or more vessels
- F17C2205/0134—Two or more vessels characterised by the presence of fluid connection between vessels
- F17C2205/0138—Two or more vessels characterised by the presence of fluid connection between vessels bundled in series
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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
- F17C2205/0123—Mounting arrangements characterised by number of vessels
- F17C2205/013—Two or more vessels
- F17C2205/0134—Two or more vessels characterised by the presence of fluid connection between vessels
- F17C2205/0142—Two or more vessels characterised by the presence of fluid connection between vessels bundled in parallel
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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
- F17C2221/03—Mixtures
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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
- F17C2221/03—Mixtures
- F17C2221/038—Refrigerants
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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
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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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
- F17C2223/035—High pressure (>10 bar)
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- 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
- F17C2227/04—Methods for emptying or filling
- F17C2227/041—Methods for emptying or filling vessel by vessel
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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
- F17C2227/04—Methods for emptying or filling
- F17C2227/046—Methods for emptying or filling by even emptying or filling
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- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
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- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/012—Reducing weight
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- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/031—Dealing with losses due to heat transfer
- F17C2260/033—Dealing with losses due to heat transfer by enhancing insulation
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- 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
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
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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
Definitions
- the invention relates to a container for cryogenic liquids, composed of an outer container and a number of inner containers, with a vacuum preferably prevailing in the space between the inner containers and the outer container in order to provide thermal insulation.
- Containers of said type are intended for installation in motor vehicles, aircraft or spacecraft. They contain liquefied gases which are extracted from the container for use either as a propellant or for other purposes (for example as a cooling medium).
- the vacuum insulation is intended to impede the introduction of heat and therefore an evaporation of the cryogenic liquids, and the associate pressure rise.
- the cryogenic liquid may however also be stored at high pressure. In this way, firstly, the stored quantity is increased for the same volume, but secondly, the container becomes heavier in order to withstand the pressure loading.
- the outer container is loaded from the outside by atmospheric pressure, because the vacuum prevails in its interior.
- the inner containers are loaded by the full inner pressure because they are surrounded by a vacuum. Said pressures are manageable in the case of an entirely cylindrical container.
- a longitudinal axis direction is to be understood to mean a direction substantially parallel to the direction of the longitudinal axes of the adjacent inner containers.
- small deviations from a parallel alignment fall within the scope of protection.
- the container is a tank of flat design, but with certain deviations within the context of a slight curvature of the top, base and/or side surfaces of the outer tank being permitted and falling within the scope of protection.
- a plurality of inner containers are arranged in the outer container, with the longitudinal axes being arranged substantially parallel and in a plane. Slight deviations with regard to the parallel alignment of the longitudinal axes, or a slight axial offset of an inner container from a common plane, are however permitted and encompassed by the scope of protection.
- the outer container can be stabilized against occurring compressive and tensile loadings from the inside and from the outside.
- Such compressive and tensile loadings may for example be brought about by an evacuation of the outer tank or by mechanical external loads on the outer tank.
- the inner containers are cylinders which are arranged adjacent to one another and have a base at both sides, and in that the planar wall parts of the outer container are supported with respect to one another by means of supports which are arranged between the cylinders. Thanks to the arrangement of a plurality of inner containers adjacent to one another (wherein it is not necessary for all the inner containers to be arranged strictly in a plane adjacent to one another), the cylindrical shape, which is particularly expedient in the case of an internal pressure, can be maintained. This makes it possible to store the cryogenic liquid under high pressure even in the case of a relatively small wall thickness. There is also the advantage that the cylinders can be used in a modular fashion, in different numbers and different configurations, for containers with different outer dimensions.
- the support is a compressive support, that is to say a support for providing support of/against compressive forces, and/or a tension support, for providing support of/against tensile forces.
- the inner containers are provided as separate containers, for example as structurally separate cylindrical tank containers which are filled and/or emptied by means of a suitable device, if appropriate together or separately.
- the support of the planar wall parts with respect to one another makes it possible for a plurality of inner containers to be surrounded by a common outer container, because atmospheric pressure which acts on the planar surfaces which are thereby created can be absorbed without subjecting the inner containers to any loading.
- Said support makes it possible to considerably reduce the wall thickness of the outer container, and permits a corresponding weight reduction
- the support has, as viewed in the section of the support with the plane of the longitudinal axes of the adjacent inner container, a maximum length extent measured in the longitudinal axis direction, and normally with respect thereto, a maximum width extent measured between the adjacent inner tanks.
- the ratio of maximum length extent to maximum width extent is at least 1.25:1. This results in particularly good stability of the container according to the invention.
- the support between two inner containers is composed of a plurality of support elements arranged along the longitudinal axis, then the maximum length extents or maximum width extents of the support elements are added in order to determine the effective overall length extent or overall width extent of the support which acts between the inner containers.
- overlaps of two or more compressive support elements in the longitudinal or width direction are counted only once in the determination of the effective overall length or the effective overall width of the support.
- the effective overall length or overall width of the support elements determined in this way is considered to be the dimension (length extent, width extent) of the support.
- the support elements are arranged symmetrically or at approximately uniform intervals with respect to one another in the direction of the longitudinal axis of the inner container. In this way, it is ensured that the introduction of force via the outer container takes place uniformly without distortion of the container structure.
- the ratio of maximum length extent to maximum width extent is at least 2:1.
- the ratio of maximum length extent to maximum width extent is at least 5:1.
- the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 10% of the length of the outer container by the support.
- the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 25% of the length of the outer container by the support.
- the compressive support has a minimum length of at least 10%, in particular of at least 25%, of the longitudinal dimension of the outer container.
- the compressive support has a minimum length of at least 10%, in particular of at least 25%, of the longitudinal dimension of the inner container.
- the support which is arranged longitudinally between the at least two inner containers has a plurality of separate support elements.
- the support extends over the entire length of the at least two inner containers.
- the at least two inner containers are of cylindrical design.
- the at least two inner containers are suspended at their ends on the side walls of the outer containers, such that thermal expansions in the longitudinal direction are absorbed.
- the inner containers are composed of high-grade steel.
- the inner containers are surrounded by carbon fibers embedded in a plastics matrix.
- the inner containers are suspended at their bases, at both sides, on end walls of the outer containers, such that thermal expansions in the longitudinal direction are absorbed.
- the inner containers are fixedly connected at one end to an end wall of the outer container, and at the other end are freely movable in the longitudinal direction.
- the outer container is composed of thin sheet metal and is wrapped in fibers embedded in a plastics matrix.
- the support may also be formed such that it at least partially supports the inner container transversely (that is to say transversely with respect to the longitudinal axis direction) either in the direction of the width of the outer container and/or in the direction of the height of the outer container, or at least partially holds the inner container in position in said directions.
- FIG. 1 shows an axonometric view of a container according to the invention
- FIG. 2 shows a plan view of the same
- FIG. 3 shows a side view of the same
- FIG. 4 shows a section according to C-C in FIG. 3 .
- FIG. 5 shows an alternative embodiment to FIG. 4 .
- FIG. 6 shows a longitudinal section according to VI-VI in FIG. 5 .
- FIG. 7 shows an alternative embodiment to FIG. 2 , in section according to VII-VII in FIG. 8 , and
- FIG. 8 shows a section according to VIII-VIII in FIG. 7 .
- the outer container is denoted generally by 1
- the inner containers which are arranged adjacent to one another in parallel in said outer container 1 are denoted by 2 , 3 and 4 .
- the inner containers are cylindrical tubes, preferably composed of high-grade steel.
- the outer container 1 which surrounds said inner containers with a spacing can thereby have a flat design.
- Said outer container 1 is substantially a flat cuboid whose side surfaces may be rounded. In any case, however, said outer container has two planar wall parts 10 , 11 .
- a vacuum prevails in the space 5 between the inner containers 2 , 3 , 4 and the outer container 1 , which vacuum, together with further measures, forms a so-called “super insulation” arrangement.
- the planar wall parts 10 , 11 are pressed together by the atmospheric pressure.
- the inner containers 2 , 3 , 4 are pressed outward even with atmospheric pressure prevailing in them. If the cryogenic liquid in the inner containers 2 , 3 , 4 is stored at a relatively high pressure, the tensile loading of the cylindrical walls and of the bases 7 , 8 of the inner containers 2 , 3 , 4 is correspondingly greater.
- said wall parts 10 , 11 are supported with respect to one another by supports 12 , 13 .
- said supports 12 , 13 connect the two planar wall parts 10 , 11 , with said supports 12 , 13 extending between the inner containers 2 , 3 and 3 , 4 , preferably without coming into contact with the latter.
- the supports 12 , 13 are individual supports.
- the inner containers 2 , 3 , 4 can, in a known way, be suspended on the side walls 14 , 15 by means of suspension arrangements 17 , 18 , which are known per se, at both sides.
- FIGS. 5 and 6 differs from this in that the supports 22 , 23 extend over the length of the inner containers 2 , 3 , 4 and in that the inner containers 2 , 3 , 4 are fastened only at one side, by means of heat-insulating feet 32 , to an end wall 33 of the outer container 1 , and are freely movable with their other end.
- the supports 23 , 24 are I-shaped profiles whose foot parts 24 , 25 bear at the inside against the planar walls 10 , 11 and whose web parts have reinforcement ribs 26 in order to increase their buckling resistance.
- the inner containers 2 , 3 , 4 With the inner containers 2 , 3 , 4 arranged at a sufficient distance, said inner containers 2 , 3 , 4 may be wrapped in carbon fibers 30 embedded in a plastics matrix in order to withstand high internal pressures while having the lowest possible weight.
- the outer container 1 may also be composed of a very thin metal sheet if it is likewise provided with fiber-reinforced wrapping 31 .
- FIG. 7 and FIG. 8 illustrate a further possible embodiment of a container according to the invention for cryogenic liquid.
- the container has an outer container 40 with a length L, a width B and a structural height H.
- FIG. 7 and FIG. 8 differs from other embodiments in that the support 34 has two separate, elongate support elements 35 and 36 which are arranged the along longitudinal axes 37 of the inner container 38 , that is to say in the longitudinal axis direction.
- FIG. 7 shows a section of the support along the plane through the two longitudinal axes 37 of the inner containers 38 .
- the longitudinal extent (along the longitudinal axis of the cylindrical inner container) of the support is, in cross section, a multiple of the width extent of said support.
- the maximum length dimensions or maximum width dimensions of the cross section of the individual support elements, arranged in each case between two inner containers are added. Portions of the cross section of the support elements which overlap in the direction of the longitudinal axis or in the direction of the width (section with the plane through the two longitudinal axes 37 ) are counted only once in said addition.
- the support 34 has an additional reinforcement 39 in the region of the base wall and of the top wall of the outer container 40 . In this way, the mutual introduction of force between the outer tank and the support can be improved.
- FIG. 7 and FIG. 8 it can be seen that, in the illustrated embodiment, the cumulative extent of the cross-sectional area of the support 34 in the direction of the longitudinal axis is significantly greater than in the direction between the inner containers and at right angles to the longitudinal axis, that is to say in the direction of the width of the outer container 40 .
- the outer container 40 is illustrated in each case only schematically in FIG. 7 and FIG. 8 .
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
A container for cryogenic liquids, comprising an evacuable outer container, wherein the outer container has a substantially flat base wall, a substantially flat ceiling wall and side walls. A support is arranged between inner containers, wherein the support is larger in the direction of the longitudinal axis of the inner container than in the direction between the inner containers and at right angles to the longitudinal axis of the inner container.
Description
- The invention relates to a container for cryogenic liquids, composed of an outer container and a number of inner containers, with a vacuum preferably prevailing in the space between the inner containers and the outer container in order to provide thermal insulation. Containers of said type are intended for installation in motor vehicles, aircraft or spacecraft. They contain liquefied gases which are extracted from the container for use either as a propellant or for other purposes (for example as a cooling medium).
- The vacuum insulation, usually improved using further measures, is intended to impede the introduction of heat and therefore an evaporation of the cryogenic liquids, and the associate pressure rise. The cryogenic liquid may however also be stored at high pressure. In this way, firstly, the stored quantity is increased for the same volume, but secondly, the container becomes heavier in order to withstand the pressure loading.
- As a result of the vacuum insulation, however, a pressure acts on the containers in any case. The outer container is loaded from the outside by atmospheric pressure, because the vacuum prevails in its interior. The inner containers are loaded by the full inner pressure because they are surrounded by a vacuum. Said pressures are manageable in the case of an entirely cylindrical container.
- The cylindrical container shape is however very impractical for use in vehicles for reasons of space. Development is therefore proceeding in the direction of luggage-space-shaped flat containers. In the case of a flat design, however, both the inner and outer containers are subjected to high loadings on account of the large planar and free surfaces, which loadings can only be absorbed by means of massive supports. This results in an increased weight (particularly negative in road vehicles and aircraft) and an increased introduction of heat into the interior of the container.
- It is therefore an object of the invention to develop a container which utilizes space effectively while simultaneously having a low weight.
- By definition, a longitudinal axis direction is to be understood to mean a direction substantially parallel to the direction of the longitudinal axes of the adjacent inner containers. Here, small deviations from a parallel alignment fall within the scope of protection.
- According to the invention, the container is a tank of flat design, but with certain deviations within the context of a slight curvature of the top, base and/or side surfaces of the outer tank being permitted and falling within the scope of protection.
- According to the invention, a plurality of inner containers are arranged in the outer container, with the longitudinal axes being arranged substantially parallel and in a plane. Slight deviations with regard to the parallel alignment of the longitudinal axes, or a slight axial offset of an inner container from a common plane, are however permitted and encompassed by the scope of protection.
- The expressions “substantially parallel” and “substantially in a plane” thereby encompass “parallel” and “in a plane” and insignificant deviations from these (for example as a result of production or design tolerances).
- By means of the support proposed according to the invention, the outer container can be stabilized against occurring compressive and tensile loadings from the inside and from the outside. Such compressive and tensile loadings may for example be brought about by an evacuation of the outer tank or by mechanical external loads on the outer tank.
- According to the invention, a design of a flat container is proposed which does not have the discussed disadvantages known from the prior art. Said design is intended to be as light and simple as possible while providing the best possible thermal insulation. According to one embodiment of the invention, this is achieved in that the inner containers are cylinders which are arranged adjacent to one another and have a base at both sides, and in that the planar wall parts of the outer container are supported with respect to one another by means of supports which are arranged between the cylinders. Thanks to the arrangement of a plurality of inner containers adjacent to one another (wherein it is not necessary for all the inner containers to be arranged strictly in a plane adjacent to one another), the cylindrical shape, which is particularly expedient in the case of an internal pressure, can be maintained. This makes it possible to store the cryogenic liquid under high pressure even in the case of a relatively small wall thickness. There is also the advantage that the cylinders can be used in a modular fashion, in different numbers and different configurations, for containers with different outer dimensions.
- According to one embodiment of the invention, the support is a compressive support, that is to say a support for providing support of/against compressive forces, and/or a tension support, for providing support of/against tensile forces.
- According to one embodiment of the invention, the inner containers are provided as separate containers, for example as structurally separate cylindrical tank containers which are filled and/or emptied by means of a suitable device, if appropriate together or separately.
- The support of the planar wall parts with respect to one another makes it possible for a plurality of inner containers to be surrounded by a common outer container, because atmospheric pressure which acts on the planar surfaces which are thereby created can be absorbed without subjecting the inner containers to any loading. Said support makes it possible to considerably reduce the wall thickness of the outer container, and permits a corresponding weight reduction
- According to one embodiment of the invention, the support has, as viewed in the section of the support with the plane of the longitudinal axes of the adjacent inner container, a maximum length extent measured in the longitudinal axis direction, and normally with respect thereto, a maximum width extent measured between the adjacent inner tanks. According to one particular embodiment of the invention, the ratio of maximum length extent to maximum width extent is at least 1.25:1. This results in particularly good stability of the container according to the invention.
- If the support between two inner containers is composed of a plurality of support elements arranged along the longitudinal axis, then the maximum length extents or maximum width extents of the support elements are added in order to determine the effective overall length extent or overall width extent of the support which acts between the inner containers. Here, overlaps of two or more compressive support elements in the longitudinal or width direction are counted only once in the determination of the effective overall length or the effective overall width of the support. The effective overall length or overall width of the support elements determined in this way is considered to be the dimension (length extent, width extent) of the support.
- According to a further embodiment of the invention, it is particularly advantageous if the support elements are arranged symmetrically or at approximately uniform intervals with respect to one another in the direction of the longitudinal axis of the inner container. In this way, it is ensured that the introduction of force via the outer container takes place uniformly without distortion of the container structure.
- According to a further embodiment of the invention, the ratio of maximum length extent to maximum width extent is at least 2:1.
- According to a further embodiment of the invention, the ratio of maximum length extent to maximum width extent is at least 5:1.
- According to a further embodiment of the invention, the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 10% of the length of the outer container by the support.
- According to a further embodiment of the invention, the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 25% of the length of the outer container by the support.
- According to a further embodiment of the invention, the compressive support has a minimum length of at least 10%, in particular of at least 25%, of the longitudinal dimension of the outer container.
- According to one particular embodiment, the compressive support has a minimum length of at least 10%, in particular of at least 25%, of the longitudinal dimension of the inner container.
- According to a further embodiment of the invention, the support which is arranged longitudinally between the at least two inner containers has a plurality of separate support elements.
- According to a further embodiment of the invention, the support extends over the entire length of the at least two inner containers.
- According to a further embodiment of the invention, the at least two inner containers are of cylindrical design.
- According to a further embodiment of the invention, the at least two inner containers are suspended at their ends on the side walls of the outer containers, such that thermal expansions in the longitudinal direction are absorbed.
- According to a further embodiment of the invention, the inner containers are composed of high-grade steel.
- According to a further embodiment of the invention, the inner containers are surrounded by carbon fibers embedded in a plastics matrix.
- According to a further embodiment of the invention, the inner containers are suspended at their bases, at both sides, on end walls of the outer containers, such that thermal expansions in the longitudinal direction are absorbed.
- According to a further embodiment of the invention, the inner containers are fixedly connected at one end to an end wall of the outer container, and at the other end are freely movable in the longitudinal direction.
- According to a further embodiment of the invention, the outer container is composed of thin sheet metal and is wrapped in fibers embedded in a plastics matrix.
- According to a further embodiment of the invention, the support may also be formed such that it at least partially supports the inner container transversely (that is to say transversely with respect to the longitudinal axis direction) either in the direction of the width of the outer container and/or in the direction of the height of the outer container, or at least partially holds the inner container in position in said directions.
- The invention is described and explained below on the basis of exemplary schematic figures, in which:
-
FIG. 1 shows an axonometric view of a container according to the invention, -
FIG. 2 shows a plan view of the same, -
FIG. 3 shows a side view of the same, -
FIG. 4 shows a section according to C-C inFIG. 3 , -
FIG. 5 shows an alternative embodiment toFIG. 4 , -
FIG. 6 shows a longitudinal section according to VI-VI inFIG. 5 , -
FIG. 7 shows an alternative embodiment toFIG. 2 , in section according to VII-VII inFIG. 8 , and -
FIG. 8 shows a section according to VIII-VIII inFIG. 7 . - In
FIGS. 1 to 4 , the outer container is denoted generally by 1, and the inner containers which are arranged adjacent to one another in parallel in said outer container 1 are denoted by 2, 3 and 4. The inner containers are cylindrical tubes, preferably composed of high-grade steel. The outer container 1 which surrounds said inner containers with a spacing can thereby have a flat design. Said outer container 1 is substantially a flat cuboid whose side surfaces may be rounded. In any case, however, said outer container has twoplanar wall parts space 5 between theinner containers space 5, theplanar wall parts inner containers inner containers bases inner containers - To absorb the compressive forces acting on the
planar wall parts wall parts supports FIG. 4 , said supports 12, 13 connect the twoplanar wall parts supports inner containers FIG. 2 , thesupports inner containers side walls suspension arrangements - The modified embodiment of
FIGS. 5 and 6 differs from this in that thesupports inner containers inner containers feet 32, to anend wall 33 of the outer container 1, and are freely movable with their other end. As can be seen inFIG. 5 , thesupports foot parts planar walls reinforcement ribs 26 in order to increase their buckling resistance. With theinner containers inner containers carbon fibers 30 embedded in a plastics matrix in order to withstand high internal pressures while having the lowest possible weight. In a similar way, the outer container 1 may also be composed of a very thin metal sheet if it is likewise provided with fiber-reinforcedwrapping 31. -
FIG. 7 andFIG. 8 illustrate a further possible embodiment of a container according to the invention for cryogenic liquid. Here, the container has anouter container 40 with a length L, a width B and a structural height H. - The further possible embodiment according to
FIG. 7 andFIG. 8 differs from other embodiments in that thesupport 34 has two separate,elongate support elements longitudinal axes 37 of theinner container 38, that is to say in the longitudinal axis direction. Here,FIG. 7 shows a section of the support along the plane through the twolongitudinal axes 37 of theinner containers 38. By adding the lengths of the cross sections of thesupport elements outer container 40 is supported between itsbase wall 41 and itstop wall 42 over more than 50% of its longitudinal extent by thesupport 34. It can also be seen that the longitudinal extent (along the longitudinal axis of the cylindrical inner container) of the support is, in cross section, a multiple of the width extent of said support. To determine the length extent or the width extent, the maximum length dimensions or maximum width dimensions of the cross section of the individual support elements, arranged in each case between two inner containers, are added. Portions of the cross section of the support elements which overlap in the direction of the longitudinal axis or in the direction of the width (section with the plane through the two longitudinal axes 37) are counted only once in said addition. - In
FIG. 8 , it can be seen that thesupport 34 has anadditional reinforcement 39 in the region of the base wall and of the top wall of theouter container 40. In this way, the mutual introduction of force between the outer tank and the support can be improved. InFIG. 7 andFIG. 8 , it can be seen that, in the illustrated embodiment, the cumulative extent of the cross-sectional area of thesupport 34 in the direction of the longitudinal axis is significantly greater than in the direction between the inner containers and at right angles to the longitudinal axis, that is to say in the direction of the width of theouter container 40. Theouter container 40 is illustrated in each case only schematically inFIG. 7 andFIG. 8 .
Claims (13)
1-11. (canceled)
12. A container for cryogenic liquids, comprising an evacuable outer container of flat design, the outer container comprising a substantially planar base wall, a substantially planar top wall and side walls, at least two inner containers which are arranged in the outer container, each of the inner containers having a longitudinal axis and the at least two inner containers being arranged, with their longitudinal axes arranged substantially parallel and adjacent to one another substantially in a plane, and having a support for supporting the base wall with respect to the top wall of the outer container, the support being arranged longitudinally between the at least two inner containers, and the support having, as viewed in a section of the support with the plane of the longitudinal axes of the adjacent inner container, a greater dimension in the longitudinal axis direction than in a direction at right angles to the longitudinal axis direction.
13. The container as claimed in claim 12 , wherein the support has, as viewed in the section of the support with the plane of the longitudinal axes of the adjacent inner container, a maximum length extent measured in the longitudinal axis direction, and a maximum width extent measured between the adjacent inner containers, wherein the ratio of maximum length extent to maximum width extent is at least 1.25:1.
14. The container as claimed in claim 13 , wherein the ratio of maximum length extent to maximum width extent is at least 2:1.
15. The container as claimed in claim 13 , wherein the ratio of maximum length extent to maximum width extent is at least 5:1.
16. The container as claimed in claim 12 , wherein the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 10% of the length of the outer container by the support.
17. The container as claimed in claim 16 , wherein the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 25% of the length of the outer container by the support.
18. The container as claimed in claim 16 , wherein the top wall is supported with respect to the base wall between the at least two inner containers, in the longitudinal axis direction, over at least 50% of the length of the outer container by the support.
19. The container as claimed in claim 12 , wherein the support which is arranged longitudinally between the at least two inner containers has a plurality of separate support elements.
20. The container as claimed in claim 19 , wherein the support extends over the entire length of the at least two inner containers.
21. The container as claimed in claim 12 , wherein the at least two inner containers each being of substantially cylindrical design.
22. The container as claimed in claim 12 , wherein the at least two inner containers are suspended at their ends on the side walls of the outer containers by means for absorbing thermal expansions in the longitudinal direction.
23. The container as claimed in claim 12 , wherein the support is composed at least partially of carbon fiber.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT0030606U AT9456U1 (en) | 2006-04-14 | 2006-04-14 | CONTAINER FOR CRYOGENEOUS LIQUIDS |
ATGM306/2006 | 2006-04-14 | ||
PCT/EP2007/003330 WO2007118695A1 (en) | 2006-04-14 | 2007-04-16 | Container for cryogenic liquids |
Publications (1)
Publication Number | Publication Date |
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US20090301104A1 true US20090301104A1 (en) | 2009-12-10 |
Family
ID=40935160
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US12/297,006 Abandoned US20090301104A1 (en) | 2006-04-14 | 2007-04-16 | Container for cryogenic liquids |
Country Status (6)
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US (1) | US20090301104A1 (en) |
EP (1) | EP2008014B1 (en) |
JP (1) | JP2009533637A (en) |
AT (2) | AT9456U1 (en) |
DE (1) | DE502007001200D1 (en) |
WO (1) | WO2007118695A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103353061A (en) * | 2013-06-24 | 2013-10-16 | 江苏荣成特种装备工程有限公司 | Low temperature storage tank |
CN105715942A (en) * | 2014-12-05 | 2016-06-29 | 刘建华 | Glass reinforced plastic storage tank internally provided with CNG cylinders |
CN110958956A (en) * | 2017-07-20 | 2020-04-03 | 罗伯特·博世有限公司 | Device for storing compressed fluid |
CN111503508A (en) * | 2020-05-03 | 2020-08-07 | 江苏枂硕电子科技有限公司 | Industrial gas safe transportation device and transportation method |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE202010001299U1 (en) | 2010-01-23 | 2010-05-06 | Moser, Peter | Metallic cylinder-like pressure vessel with flat surface elements |
KR101349456B1 (en) | 2011-12-09 | 2014-01-09 | 현대자동차주식회사 | Carrier for CNG tank |
Citations (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2792962A (en) * | 1955-10-21 | 1957-05-21 | Ernest H Granfelt | Multi-cellular rocket package |
US3528582A (en) * | 1967-08-31 | 1970-09-15 | Georges Alfred Rigollot | Fluid-tight metal tank |
US3537416A (en) * | 1969-01-02 | 1970-11-03 | Exxon Research Engineering Co | Shipping container and method for transporting hydrocarbon fluids and the like |
US3804292A (en) * | 1970-08-06 | 1974-04-16 | C Chiti | Fire-preventing fuel tank for motor vehicles and/or boats |
US4013190A (en) * | 1972-05-10 | 1977-03-22 | Mcdonnell Douglas Corporation | Flame arresting and explosion attenuating system |
US4187092A (en) * | 1978-05-15 | 1980-02-05 | Billings Energy Corporation | Method and apparatus for providing increased thermal conductivity and heat capacity to a pressure vessel containing a hydride-forming metal material |
US4496073A (en) * | 1983-02-24 | 1985-01-29 | The Johns Hopkins University | Cryogenic tank support system |
US4782892A (en) * | 1983-08-26 | 1988-11-08 | Oestbo Karl | Heat exchanger |
US5558214A (en) * | 1995-05-03 | 1996-09-24 | Brundidge; Jackie L. | Baby bottle carrier |
US5577630A (en) * | 1995-02-02 | 1996-11-26 | Thiokol Corporation | Composite conformable pressure vessel |
US5651474A (en) * | 1994-12-22 | 1997-07-29 | The United States Of America As Represented By The Secretary Of The Air Force | Cryogenic structures |
US5944215A (en) * | 1995-03-29 | 1999-08-31 | Perstorp Ab | Vessel for a pressurized fluid |
US6354321B1 (en) * | 1998-08-20 | 2002-03-12 | Linde Aktiengesellschaft | Storage container for cryogenic liquids |
US6796453B2 (en) * | 2002-11-13 | 2004-09-28 | Stan A. Sanders | Cellular reservoir flexible pressure vessel, apparatus and method for making same |
US20040195246A1 (en) * | 2003-04-03 | 2004-10-07 | Rainer Immel | Construction for multi-layered vacuum super insulated cryogenic tank |
US20060169704A1 (en) * | 2003-02-18 | 2006-08-03 | Klaus Brunnhofer | Double-walled container for cryogenic liquids |
US7112239B2 (en) * | 2003-05-20 | 2006-09-26 | Toyota Jidosha Kabushiki Kaisha | Gas storage apparatus |
US7159738B2 (en) * | 2001-08-20 | 2007-01-09 | Sida Engineering -S.R.L. | Multi-cell tank for pressurised gas |
US20080237240A1 (en) * | 2005-04-13 | 2008-10-02 | Magna Steyr Fahrzeugtechnik Ag & Co Kg | Modular Container for Cryogenic Liquids |
US7431756B2 (en) * | 2002-05-09 | 2008-10-07 | Ovonic Hydrogen Systems Llc | Modular metal hydride hydrogen storage system |
US7455723B2 (en) * | 2005-12-22 | 2008-11-25 | Modine Manufacturing Company | Hydrogen storage and release device |
US7637386B2 (en) * | 2006-01-06 | 2009-12-29 | Manfred Roth | Plastic underground tank |
US7708161B2 (en) * | 2006-12-05 | 2010-05-04 | Florida State University Research Foundation | Light-weight vacuum chamber and applications thereof |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2089014A (en) * | 1980-12-06 | 1982-06-16 | Ocean Phoenix Holdings Nv | Liquefied gas storage tanks |
DE19524681A1 (en) * | 1995-07-06 | 1997-01-09 | Linde Ag | Storage vessel for cryogenic media - comprising polygonal tube or tube-like assembly with apertures in walls for communication and contained in insulated vessel |
FR2766906B1 (en) * | 1997-07-30 | 1999-10-01 | Renault | TANK FOR PRESSURE FLUID |
MY125147A (en) * | 1998-10-27 | 2006-07-31 | Univ Johns Hopkins | Compressed gas manifold |
DE10008985A1 (en) * | 2000-02-25 | 2001-08-30 | Linde Ag | Reservoir container for cryogenic fluids; has insulation space between inner and outer containers with reinforcement webs may be formed on walls or support plates may be welded in inner container |
DE102004042001B4 (en) * | 2004-08-31 | 2006-10-19 | Daimlerchrysler Ag | Storage container for storing cryogenic liquids |
-
2006
- 2006-04-14 AT AT0030606U patent/AT9456U1/en not_active IP Right Cessation
-
2007
- 2007-04-16 JP JP2009508155A patent/JP2009533637A/en active Pending
- 2007-04-16 DE DE502007001200T patent/DE502007001200D1/en active Active
- 2007-04-16 AT AT07724268T patent/ATE438062T1/en active
- 2007-04-16 US US12/297,006 patent/US20090301104A1/en not_active Abandoned
- 2007-04-16 WO PCT/EP2007/003330 patent/WO2007118695A1/en active Application Filing
- 2007-04-16 EP EP07724268A patent/EP2008014B1/en not_active Not-in-force
Patent Citations (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2792962A (en) * | 1955-10-21 | 1957-05-21 | Ernest H Granfelt | Multi-cellular rocket package |
US3528582A (en) * | 1967-08-31 | 1970-09-15 | Georges Alfred Rigollot | Fluid-tight metal tank |
US3537416A (en) * | 1969-01-02 | 1970-11-03 | Exxon Research Engineering Co | Shipping container and method for transporting hydrocarbon fluids and the like |
US3804292A (en) * | 1970-08-06 | 1974-04-16 | C Chiti | Fire-preventing fuel tank for motor vehicles and/or boats |
US4013190A (en) * | 1972-05-10 | 1977-03-22 | Mcdonnell Douglas Corporation | Flame arresting and explosion attenuating system |
US4187092A (en) * | 1978-05-15 | 1980-02-05 | Billings Energy Corporation | Method and apparatus for providing increased thermal conductivity and heat capacity to a pressure vessel containing a hydride-forming metal material |
US4496073A (en) * | 1983-02-24 | 1985-01-29 | The Johns Hopkins University | Cryogenic tank support system |
US4782892A (en) * | 1983-08-26 | 1988-11-08 | Oestbo Karl | Heat exchanger |
US5651474A (en) * | 1994-12-22 | 1997-07-29 | The United States Of America As Represented By The Secretary Of The Air Force | Cryogenic structures |
US6095367A (en) * | 1995-02-02 | 2000-08-01 | Cordant Technologies Inc. | Composite conformable pressure vessel |
US5577630A (en) * | 1995-02-02 | 1996-11-26 | Thiokol Corporation | Composite conformable pressure vessel |
US5944215A (en) * | 1995-03-29 | 1999-08-31 | Perstorp Ab | Vessel for a pressurized fluid |
US5558214A (en) * | 1995-05-03 | 1996-09-24 | Brundidge; Jackie L. | Baby bottle carrier |
US6354321B1 (en) * | 1998-08-20 | 2002-03-12 | Linde Aktiengesellschaft | Storage container for cryogenic liquids |
US7159738B2 (en) * | 2001-08-20 | 2007-01-09 | Sida Engineering -S.R.L. | Multi-cell tank for pressurised gas |
US7431756B2 (en) * | 2002-05-09 | 2008-10-07 | Ovonic Hydrogen Systems Llc | Modular metal hydride hydrogen storage system |
US6796453B2 (en) * | 2002-11-13 | 2004-09-28 | Stan A. Sanders | Cellular reservoir flexible pressure vessel, apparatus and method for making same |
US20060169704A1 (en) * | 2003-02-18 | 2006-08-03 | Klaus Brunnhofer | Double-walled container for cryogenic liquids |
US20040195246A1 (en) * | 2003-04-03 | 2004-10-07 | Rainer Immel | Construction for multi-layered vacuum super insulated cryogenic tank |
US7112239B2 (en) * | 2003-05-20 | 2006-09-26 | Toyota Jidosha Kabushiki Kaisha | Gas storage apparatus |
US20080237240A1 (en) * | 2005-04-13 | 2008-10-02 | Magna Steyr Fahrzeugtechnik Ag & Co Kg | Modular Container for Cryogenic Liquids |
US7455723B2 (en) * | 2005-12-22 | 2008-11-25 | Modine Manufacturing Company | Hydrogen storage and release device |
US7637386B2 (en) * | 2006-01-06 | 2009-12-29 | Manfred Roth | Plastic underground tank |
US7708161B2 (en) * | 2006-12-05 | 2010-05-04 | Florida State University Research Foundation | Light-weight vacuum chamber and applications thereof |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103353061A (en) * | 2013-06-24 | 2013-10-16 | 江苏荣成特种装备工程有限公司 | Low temperature storage tank |
CN105715942A (en) * | 2014-12-05 | 2016-06-29 | 刘建华 | Glass reinforced plastic storage tank internally provided with CNG cylinders |
CN110958956A (en) * | 2017-07-20 | 2020-04-03 | 罗伯特·博世有限公司 | Device for storing compressed fluid |
CN111503508A (en) * | 2020-05-03 | 2020-08-07 | 江苏枂硕电子科技有限公司 | Industrial gas safe transportation device and transportation method |
Also Published As
Publication number | Publication date |
---|---|
WO2007118695A1 (en) | 2007-10-25 |
EP2008014A1 (en) | 2008-12-31 |
JP2009533637A (en) | 2009-09-17 |
DE502007001200D1 (en) | 2009-09-10 |
EP2008014B1 (en) | 2009-07-29 |
ATE438062T1 (en) | 2009-08-15 |
AT9456U1 (en) | 2007-10-15 |
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