US2940631A - Storage vessels for liquefied gases - Google Patents
Storage vessels for liquefied gases Download PDFInfo
- Publication number
- US2940631A US2940631A US665968A US66596857A US2940631A US 2940631 A US2940631 A US 2940631A US 665968 A US665968 A US 665968A US 66596857 A US66596857 A US 66596857A US 2940631 A US2940631 A US 2940631A
- Authority
- US
- United States
- Prior art keywords
- line
- vessel
- vapour
- container
- filling
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- 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
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
-
- 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
- F17C2201/03—Orientation
- F17C2201/035—Orientation with substantially horizontal main axis
-
- 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
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0325—Aerogel
-
- 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
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0337—Granular
-
- 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
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0345—Fibres
-
- 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
- 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
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
-
- 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
- F17C2205/0352—Pipes
- F17C2205/0355—Insulation thereof
-
- 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
- F17C2223/043—Localisation of the removal point in the gas
- F17C2223/045—Localisation of the removal point in the gas 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
- 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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/04—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by other properties of handled fluid after transfer
- F17C2225/042—Localisation of the filling point
- F17C2225/046—Localisation of the filling point in the liquid
- F17C2225/047—Localisation of the filling point in the liquid with a dip tube
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S62/00—Refrigeration
- Y10S62/13—Insulation
Definitions
- Liquefied gases the boiling points of which are substantially below ambient temperature at atmospheric pressure, for example liquid oxygen or liquid nitrogen, are normally stored in such a manner that the influx of heat into the storage vessel from the surrounding atomsphere is kept to a minimum Undensuch conditions the evaporation losses. of the stored liquefied gases would be small, thus making the storage efficient and economical.
- An eflicient method is to use a donblewall vessel, the interspace of which is filled with powder of 'a very small grain size and evacuated.
- the absolute pressure inside the evacuated space can vary between and 10' mm. Hg.
- opacised powders or anti-radiation shields may be used. .These prove to be very effective if a high degree of insulating efiiciency is required.
- the filling and delivery pipes are usually made of a poorly conducting metal, such as stainless steel or German silver, their wall thickness and diameter are kept to a practical minimum and their length increased as much as conveniently possible.
- the liquid filling line can be accommodated inside the vapour venting line.
- these lines can be located in the insulating space between the inner and the outer shell and run inside it for a considerable distance, parallel to the inner vessel. This results however in an increased thickness of the insulating space in order to accommodate the filling and emptying connections and still maintain the required thickness of insulation.
- an insulated storage vessel for liquefied gases of low boiling point is provided with long insulated liquid withdrawal and vapour venting lines, located for the greater part of their length within the liquid contents space of the vessel.
- the filling and withdrawal line may open at a point near to the bottom of the vessel and leave the vessel through or near the top.
- the vapour venting line similarly will open at a point within the vapour space at the top of the vessel and leave the vessel through or near the bottom.
- the liquid withdrawal and vapour venting lines are straight and are arranged at an equal Patented June 14, 1960 angle on either side of the vertical so as to cross within the vessel, thus ensuring the maximum length for both lines.
- liquid and vapour delivery valves may therefore be positioned close to the outer shell of the vessel.
- the insulation of the vessel may be of any conventional type; the space between the vessel and its outer shell may be filled with powder or fibre, it may be filled with powder and evacuated or it may simply be evacuated.
- the insulation of the filling and vapour venting lines preferably forms part of the insulation system of the vessel.
- the filling line may be joined to and pass through the outer shell of the vessel at one end and be joined to its own shell at the other. This shellis itself joined at. its other end to the inner wall of the vessel, so that the space between the line and its shell communicates with the space between the vessel and its shell.
- the distance between line and shell may be maintained if necessary by spacers made of a material of low thermal conductivity. With such an arrangement, the outer shell of the' filling line is maintained at a low temperature by theliquefied gas surrounding it and is separated from the inner line by the selected insulation.
- vapour When the tank is filled with liquid and the filling valve is closed, vapour will gradually accumulate within the tilling line owing to the heat inleak along the line from outside the vessel. Ultimately the whole length of the line will be filled with vapour, the temperature of which will vary from that of the boiling liquid under storage pressure up to the ambient temperature. Such a temperature gradient along 'tthe vapour in the line reduces very substantially the heat inleak along the line. Some of the vapour may be recondensed but anysurplus vapour which cannot be accommodated within the filling line will pass through the opening of the-line and will leave the tank through the venting line. This latter line is constructed in a similar manner to the filling line.
- the storage vessel 1 is of cylindrical shape and is proyided with anoutershell 2 surrounding and spaced from the ves'sel'to define an insulating space 3.
- the liquid filling and withdrawal line 4 opens at a point near to the bottom of the'vessel at one end and leads diagonally in a straight line to emerge through an orifice 5 of diameter greater than that of the line in the Wall of the vessel 1 at its opposite top corner, and then in gas-tight manner through the shell 2.
- Flow of liquid through'the line 4 is controlled by a valve 6 located close to the'outside of the leads diagonally downwards in ,a'straight line to pass through the orifice 10 in the opposite bottom corner of the vessel 1, and thence in gas tight mannerthrough the outer shell 2.
- Theline9 is provided ,witha shell 13 surrounding andspaced-therefrom to define an insulationspac'e '14, .the shell 13 being joined in gas tight manner to the openend of the line 9 and' to the periphery of the orificetltl, so that the insulationspaces '3fand l 4rcommunicate, r f I 7 Provision (not shown) is made for filling the combined insulation space 3, 8 and 14 with an insulating powder and for evacuating the space.
- the liquefied gas is supplied and'withr drawn through the line 4 whilst the vapour'is vented through the line 9.
- the unavoidable heat inleak into the vessel 1 along the withdrawalfline 4 will cause evaporation of the liquefied gas;
- the valve 6 When the valve 6 is closed, the line 4 will be filled with vapour which will maintain a temperature gradient along the line thus fur- 1 ther reducing the evaporation process Iclaim: Q 1.
- a thermally insulated storage vessel for liquefied gases of low boiling point comprising, an inner container 7 for the liquid, a first outer shell surrounding and spaced from said inner container, aliquid withdrawal line opening within said container at a point close to the bottom thereof and passing through a' first aperture formed in the wall of said container at the top thereof, the diameter of said first aperture being greater than the outer diameter "of said liquid withdrawal line and said liquid withdrawal line passing through said first aperture without touching the wall of said container," a second outer shell surrounding and spaced from the part of said liquid withdrawal line Within said container, said second outer shell being joined at one endto' said liquid withdrawal line" at the open end thereof and at the other-end'to said container at the periphery of said first aperture, a vapour venting line opening within said container at a point close to the top thereof and passing through a second, aperture formed in the wall of said container at the bottom thereof, the diameter of saidscond aperture'bei'ng' greater than the outer diameter of said vapour venting line and said vapour ventinglline passing through
- a thermally insulated storagetvesseI-for.liquefied gases of low boiling point according. to claim 1 wherein ,said single insulating fspace is filled with apowder of low thermal conductivity in admixture with small reflecting bodies.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
801,328. Storing liquified gases. BRITISH OXYGEN CO., Ltd. June 26, 1957 [July 3, 1956], No. 20582/56. Class 8(2). A heat insulated liquified gas container 1 has heat insulated liquid withdrawal and vapour venting ducts 4, 9 located substantially within the liquid content space of the container. The withdrawal duct 4 extends from its lower open end through the diagonally opposite corner of the container, whereas the venting duct 9 extends from its upper open end through the opposite comer.
Description
June 14, 1960 w. o. KEEPING 2,940,531
STORAGE VESSELS FOR LIQUEFIED GASES Filed June 17, 1957 Inventor United States Patent 2,940,631 STORAGE VESSELS FOR LIQUEFIED GASES William 0. Keeping, Surrey, England, assignor to The British Oxygen Company Limited, a British company Filed June 17, 1957, Ser. No. 665,968 Claims priority, application Great Britain July 3, 1956 3 Claims. (Cl. 22014) This invention relates to the design and construction of storage vessels for liquefied gases.
Liquefied gases, the boiling points of which are substantially below ambient temperature at atmospheric pressure, for example liquid oxygen or liquid nitrogen, are normally stored in such a manner that the influx of heat into the storage vessel from the surrounding atomsphere is kept to a minimum Undensuch conditions the evaporation losses. of the stored liquefied gases would be small, thus making the storage efficient and economical.
Storage losses are caused by the heat inleak in the first instance through the container wallsand secondly through the filling and emptying connections. The losses through the walls can be very substantially reduced by the choice of the right method of insulation. An eflicient method is to use a donblewall vessel, the interspace of which is filled with powder of 'a very small grain size and evacuated. The absolute pressure inside the evacuated space can vary between and 10' mm. Hg. In cases where the insulating layer is relatively thin, a significant amount of heat can be transmitted through the walls by radiation. In such cases opacised powders or anti-radiation shields may be used. .These prove to be very effective if a high degree of insulating efiiciency is required.
All these remedies, however, cannot reduce the second category. of cold losses mentioned above, caused by straightforward thermal conduction along the filling or emptying lines. In order to decrease these evaporation losses the filling and delivery pipes are usually made of a poorly conducting metal, such as stainless steel or German silver, their wall thickness and diameter are kept to a practical minimum and their length increased as much as conveniently possible. In one method of minimising the heat inleak along the supply and withdrawal lines, the liquid filling line can be accommodated inside the vapour venting line. Alternatively, these lines can be located in the insulating space between the inner and the outer shell and run inside it for a considerable distance, parallel to the inner vessel. This results however in an increased thickness of the insulating space in order to accommodate the filling and emptying connections and still maintain the required thickness of insulation.
It is an object of the present invention to provide a storage vessel for liquefied gases in which heat inleak along the filling and venting lines is minimised without increasing the thickness of the insulation of the vessel.
According to the present invention, an insulated storage vessel for liquefied gases of low boiling point is provided with long insulated liquid withdrawal and vapour venting lines, located for the greater part of their length within the liquid contents space of the vessel.
Conveniently, the filling and withdrawal line may open at a point near to the bottom of the vessel and leave the vessel through or near the top. The vapour venting line similarly will open at a point within the vapour space at the top of the vessel and leave the vessel through or near the bottom. Preferably, the liquid withdrawal and vapour venting lines are straight and are arranged at an equal Patented June 14, 1960 angle on either side of the vertical so as to cross within the vessel, thus ensuring the maximum length for both lines.
With such an arrangement, there is no need to provide long filling and emptying connections protruding from the storage vessel since the necessary length of line is provided within the vessel itself. The liquid and vapour delivery valves may therefore be positioned close to the outer shell of the vessel.
The insulation of the vessel may be of any conventional type; the space between the vessel and its outer shell may be filled with powder or fibre, it may be filled with powder and evacuated or it may simply be evacuated. The insulation of the filling and vapour venting lines preferably forms part of the insulation system of the vessel. Thus, the filling line may be joined to and pass through the outer shell of the vessel at one end and be joined to its own shell at the other. This shellis itself joined at. its other end to the inner wall of the vessel, so that the space between the line and its shell communicates with the space between the vessel and its shell. The distance between line and shell may be maintained if necessary by spacers made of a material of low thermal conductivity. With such an arrangement, the outer shell of the' filling line is maintained at a low temperature by theliquefied gas surrounding it and is separated from the inner line by the selected insulation. 1
When the tank is filled with liquid and the filling valve is closed, vapour will gradually accumulate within the tilling line owing to the heat inleak along the line from outside the vessel. Ultimately the whole length of the line will be filled with vapour, the temperature of which will vary from that of the boiling liquid under storage pressure up to the ambient temperature. Such a temperature gradient along 'tthe vapour in the line reduces very substantially the heat inleak along the line. Some of the vapour may be recondensed but anysurplus vapour which cannot be accommodated within the filling line will pass through the opening of the-line and will leave the tank through the venting line. This latter line is constructed in a similar manner to the filling line.
=It will be appreciated that provision will have to be made to allow for difierential thermal contraction or expansion of the filling and venting lines and their respective outer shells as the vessel is filled or emptied This may be efiected by using materials of construction which have a low thermal contraction coefi'icient, such as Invar (registered trademark), or if conventional materials of construction are used, stress-relieving elements, such as bellows or membranes, may be incorporated in the inner line or the outer shell.
An important application of this inventon is to vessels where the interspace between the inner and outer vessels, and the respective interspaces between the filling line and its outer jacket, and the vapour line and its outer jacket, are filled with a powder of low thermal conductivity, the interstices between the particles of powder being maintained at a gas pressure of less than 5X10" mm. of mercury absolute, but greater than the pressure normally employed when a vacuum space only is relied upon for insulating efiect.
When powders are employed under such conditions in a narrow layer (that is, of less than about 2 inches thickness) an important mechanism of heat transfer between the surroundings and the contents of the vessel is radiation. The heat transferred by this mechanism can be reduced by including with the insulating powder, and intimately mixed with it, a proportion of small reflecting bodies such as finely divided aluminium powder, finely divided copper or bronze powder and the like.
One embodiment of the invention will now be more particularly described with reference to the accompanying drawing which shows in longitudinal section a storage vessel according to'the invention. 7
The storage vessel 1 is of cylindrical shape and is proyided with anoutershell 2 surrounding and spaced from the ves'sel'to define an insulating space 3. The liquid filling and withdrawal line 4 opens at a point near to the bottom of the'vessel at one end and leads diagonally in a straight line to emerge through an orifice 5 of diameter greater than that of the line in the Wall of the vessel 1 at its opposite top corner, and then in gas-tight manner through the shell 2. Flow of liquid through'the line 4 is controlled by a valve 6 located close to the'outside of the leads diagonally downwards in ,a'straight line to pass through the orifice 10 in the opposite bottom corner of the vessel 1, and thence in gas tight mannerthrough the outer shell 2. ,Flow of vapour through the line 9 is' controlled by a valve 11 located close to the outside of the shelI Z. A safety valve 12 is provided between the valve ll and the'outside of thefshell, 2. [Theline9 is provided ,witha shell 13 surrounding andspaced-therefrom to define an insulationspac'e '14, .the shell 13 being joined in gas tight manner to the openend of the line 9 and' to the periphery of the orificetltl, so that the insulationspaces '3fand l 4rcommunicate, r f I 7 Provision (not shown) is made for filling the combined insulation space 3, 8 and 14 with an insulating powder and for evacuating the space.
, In operation, the liquefied gas is supplied and'withr drawn through the line 4 whilst the vapour'is vented through the line 9. During storage, the unavoidable heat inleak into the vessel 1 along the withdrawalfline 4 will cause evaporation of the liquefied gas; When the valve 6 is closed, the line 4 will be filled with vapour which will maintain a temperature gradient along the line thus fur- 1 ther reducing the evaporation process Iclaim: Q 1. A thermally insulated storage vessel for liquefied gases of low boiling point comprising, an inner container 7 for the liquid, a first outer shell surrounding and spaced from said inner container, aliquid withdrawal line opening within said container at a point close to the bottom thereof and passing through a' first aperture formed in the wall of said container at the top thereof, the diameter of said first aperture being greater than the outer diameter "of said liquid withdrawal line and said liquid withdrawal line passing through said first aperture without touching the wall of said container," a second outer shell surrounding and spaced from the part of said liquid withdrawal line Within said container, said second outer shell being joined at one endto' said liquid withdrawal line" at the open end thereof and at the other-end'to said container at the periphery of said first aperture, a vapour venting line opening within said container at a point close to the top thereof and passing through a second, aperture formed in the wall of said container at the bottom thereof, the diameter of saidscond aperture'bei'ng' greater than the outer diameter of said vapour venting line and said vapour ventinglline passing through ,said secondnaperture without touching the, wall of said container, a third outer shell surrounding and spaced from the part of said vapour venting line ,within said containenjsaidthird outer shell being joined at one endto tsaidvapourventingline and at theother end to said container atthe periphery of said 7 second aperture, the space formed between each of said liquid withdrawal and vapour venting. lines. and said sec ond and thirdouter shell respectively being in communication with the spaceiformed between said inner container and said first olitershelhtofonn a single insulation space,
e and means for evacuating said insulation'space.
2. ,A thermally insulated, storage vessel according to claim 1 wherein said single insulating. space. is filled with a powder offl'ow thermal conductivity, a
3 J 3. A thermally insulated storagetvesseI-for.liquefied gases of low boiling point according. to claim 1 wherein ,said single insulating fspace is filled with apowder of low thermal conductivity in admixture with small reflecting bodies. j-.- W
References Cited in thetfile patent" V UNITED STATES PATENTS 671078 Bobrick Q;Q;.. Q JAprQ BO, 1901 1,813,612 Du Pont July 7, 1931 2,000,882 Comstock May 7, 1935 2,579,035 Edelman Dec. 18, 1951 2,725,722 Ashlstrand et a1; V T Dec. .6, 1955 FOREIGN PATENTS G Germany in. 9, 1941
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB20582/56A GB801328A (en) | 1956-07-03 | 1956-07-03 | Storage vessels for liquefied gases |
Publications (1)
Publication Number | Publication Date |
---|---|
US2940631A true US2940631A (en) | 1960-06-14 |
Family
ID=10148296
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US665968A Expired - Lifetime US2940631A (en) | 1956-07-03 | 1957-06-17 | Storage vessels for liquefied gases |
Country Status (2)
Country | Link |
---|---|
US (1) | US2940631A (en) |
GB (1) | GB801328A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3207353A (en) * | 1961-10-20 | 1965-09-21 | Union Carbide Corp | Cryogenic liquid storage containers |
US3272375A (en) * | 1965-03-03 | 1966-09-13 | Union Carbide Corp | Apparatus for cryogenic liquid storage containers |
US3377813A (en) * | 1965-10-22 | 1968-04-16 | Cryogenic Eng Co | Storage container |
US20030136403A1 (en) * | 1999-10-29 | 2003-07-24 | Frye Mark Robert | Portable liquid oxygen unit with multiple operational orientations |
US20070068247A1 (en) * | 2005-09-26 | 2007-03-29 | Da Silva Jader M | Modular construction of a liquid hydrogen storage tank with a common-access tube and method of assembling same |
US20170336031A1 (en) * | 2016-05-17 | 2017-11-23 | Hexagon Technology As | Pressure vessel liner venting via nanotextured surface |
US20230107610A1 (en) * | 2021-10-05 | 2023-04-06 | General Electric Company | Onboard liquid hydrogen storage for a hydrogen aircraft |
EP4403472A1 (en) * | 2023-01-18 | 2024-07-24 | Airbus Operations Limited | Aircraft fuel storage system |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3241705A (en) * | 1963-08-19 | 1966-03-22 | Air Reduction | Container |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US673073A (en) * | 1900-11-08 | 1901-04-30 | Gabriel A Bobrick | Receptacle for containing liquid air or other gases. |
US1813612A (en) * | 1930-03-14 | 1931-07-07 | Pont Eleuthere Paul Du | Filler connection for tanks |
US2000882A (en) * | 1928-09-07 | 1935-05-07 | Stator Refrigeration Inc | Insulating housing |
DE701137C (en) * | 1939-10-27 | 1941-01-09 | Messer & Co G M B H | Storage of supercooled liquid oxygen |
US2579035A (en) * | 1948-10-11 | 1951-12-18 | Norman B Edelman | Insulation composition of resin-impregnated glass wool briquettes and feathers |
US2725722A (en) * | 1954-03-09 | 1955-12-06 | Union Carbide & Carbon Corp | Automatic apparatus for dispensing gas |
-
1956
- 1956-07-03 GB GB20582/56A patent/GB801328A/en not_active Expired
-
1957
- 1957-06-17 US US665968A patent/US2940631A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US673073A (en) * | 1900-11-08 | 1901-04-30 | Gabriel A Bobrick | Receptacle for containing liquid air or other gases. |
US2000882A (en) * | 1928-09-07 | 1935-05-07 | Stator Refrigeration Inc | Insulating housing |
US1813612A (en) * | 1930-03-14 | 1931-07-07 | Pont Eleuthere Paul Du | Filler connection for tanks |
DE701137C (en) * | 1939-10-27 | 1941-01-09 | Messer & Co G M B H | Storage of supercooled liquid oxygen |
US2579035A (en) * | 1948-10-11 | 1951-12-18 | Norman B Edelman | Insulation composition of resin-impregnated glass wool briquettes and feathers |
US2725722A (en) * | 1954-03-09 | 1955-12-06 | Union Carbide & Carbon Corp | Automatic apparatus for dispensing gas |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3207353A (en) * | 1961-10-20 | 1965-09-21 | Union Carbide Corp | Cryogenic liquid storage containers |
US3272375A (en) * | 1965-03-03 | 1966-09-13 | Union Carbide Corp | Apparatus for cryogenic liquid storage containers |
US3377813A (en) * | 1965-10-22 | 1968-04-16 | Cryogenic Eng Co | Storage container |
US20080066471A1 (en) * | 1999-10-29 | 2008-03-20 | Frye Mark R | Portable liquid oxygen unit with multiple operational orientations |
US6843247B2 (en) * | 1999-10-29 | 2005-01-18 | Mallinckrodt Inc. | Portable liquid oxygen unit with multiple operational orientations |
US20050098174A1 (en) * | 1999-10-29 | 2005-05-12 | Mallinckrodt Inc. | Portable liquid oxygen unit with multiple operational orientations |
US7296569B2 (en) * | 1999-10-29 | 2007-11-20 | Mallinckrodt, Inc. | Portable liquid oxygen unit with multiple operational orientations |
US20030136403A1 (en) * | 1999-10-29 | 2003-07-24 | Frye Mark Robert | Portable liquid oxygen unit with multiple operational orientations |
US7766009B2 (en) | 1999-10-29 | 2010-08-03 | Caire Inc. | Portable liquid oxygen unit with multiple operational orientations |
US20070068247A1 (en) * | 2005-09-26 | 2007-03-29 | Da Silva Jader M | Modular construction of a liquid hydrogen storage tank with a common-access tube and method of assembling same |
US8162167B2 (en) * | 2005-09-26 | 2012-04-24 | GM Global Technology Operations LLC | Modular construction of a liquid hydrogen storage tank with a common-access tube and method of assembling same |
US20170336031A1 (en) * | 2016-05-17 | 2017-11-23 | Hexagon Technology As | Pressure vessel liner venting via nanotextured surface |
US10088110B2 (en) * | 2016-05-17 | 2018-10-02 | Hexagon Technology As | Pressure vessel liner venting via nanotextured surface |
US20230107610A1 (en) * | 2021-10-05 | 2023-04-06 | General Electric Company | Onboard liquid hydrogen storage for a hydrogen aircraft |
US12017789B2 (en) * | 2021-10-05 | 2024-06-25 | General Electric Company | Onboard liquid hydrogen storage for a hydrogen aircraft |
EP4403472A1 (en) * | 2023-01-18 | 2024-07-24 | Airbus Operations Limited | Aircraft fuel storage system |
Also Published As
Publication number | Publication date |
---|---|
GB801328A (en) | 1958-09-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2396459A (en) | Insulated container for liquefied gases and the like | |
US3069042A (en) | Method and apparatus for storing liquefied gases | |
US3119238A (en) | Cryogenic dewar | |
US2863297A (en) | Method and apparatus for storing liquified gases | |
US3698200A (en) | Cryogenic storage dewar | |
US3069045A (en) | Thermally insulated storage container | |
US2776776A (en) | Liquefied gas container | |
US4175395A (en) | Distribution of gas under pressure | |
US2994452A (en) | Insulated tank for liquefied hydrocarbons and the like with loose membranous lining therefor | |
US2940631A (en) | Storage vessels for liquefied gases | |
US4218892A (en) | Low cost cryostat | |
US3087311A (en) | Container for liquefied gas | |
US3648018A (en) | Transfer device for cryogenic fluids | |
US2329765A (en) | Low temperature storage tank | |
US3134237A (en) | Container for low-boiling liquefied gases | |
US3097084A (en) | Liquefied gas container | |
US2986891A (en) | Low-temperature vessels | |
US3461678A (en) | Stationary,large-capacity storage container for the storage of liquefied gases | |
US3319433A (en) | Rectangular dewar | |
US20190145579A1 (en) | Transport container | |
GB1167902A (en) | Vacuum Insulated Vessels. | |
GB955320A (en) | Improvements in and relating to containers for refrigerating articles | |
GB914193A (en) | Cryogenic liquid storage tank | |
US2907177A (en) | Container and method of dispensing liquefied gases therefrom | |
JPH08295394A (en) | Cryogenic tank for cryogenic liquefied gas |