US3707850A - Cryogenic storage tank improvements - Google Patents

Cryogenic storage tank improvements Download PDF

Info

Publication number
US3707850A
US3707850A US00080117A US3707850DA US3707850A US 3707850 A US3707850 A US 3707850A US 00080117 A US00080117 A US 00080117A US 3707850D A US3707850D A US 3707850DA US 3707850 A US3707850 A US 3707850A
Authority
US
United States
Prior art keywords
opening
liner
wall
screening
thermal insulation
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
Application number
US00080117A
Inventor
J Connell
A Baranyi
P Laylander
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SYST CAPITOL CORP
Original Assignee
SYST CAPITOL CORP
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SYST CAPITOL CORP filed Critical SYST CAPITOL CORP
Application granted granted Critical
Publication of US3707850A publication Critical patent/US3707850A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/005Underground or underwater containers or vessels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0119Shape cylindrical with flat end-piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/03Orientation
    • F17C2201/032Orientation with substantially vertical main axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/052Size large (>1000 m3)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/014Suspension means
    • F17C2203/016Cords
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0337Granular
    • F17C2203/0341Perlite
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0391Thermal insulations by vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0604Liners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0626Multiple walls
    • F17C2203/0629Two walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0639Steels
    • F17C2203/0643Stainless steels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0646Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0663Synthetics in form of fibers or filaments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0663Synthetics in form of fibers or filaments
    • F17C2203/0673Polymers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0678Concrete
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0352Pipes
    • F17C2205/0367Arrangements in parallel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/228Assembling processes by screws, bolts or rivets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/033Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/04Handled 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
    • F17C2223/042Localisation of the removal point
    • F17C2223/046Localisation of the removal point in the liquid
    • F17C2223/047Localisation of the removal point in the liquid with a dip tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/01Propulsion of the fluid
    • F17C2227/0128Propulsion of the fluid with pumps or compressors
    • F17C2227/0135Pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/01Propulsion of the fluid
    • F17C2227/0128Propulsion of the fluid with pumps or compressors
    • F17C2227/0171Arrangement
    • F17C2227/0178Arrangement in the vessel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03Heat exchange with the fluid
    • F17C2227/0337Heat exchange with the fluid by cooling
    • F17C2227/0341Heat exchange with the fluid by cooling using another fluid
    • F17C2227/0353Heat exchange with the fluid by cooling using another fluid using cryocooler
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03Heat exchange with the fluid
    • F17C2227/0367Localisation of heat exchange
    • F17C2227/0388Localisation of heat exchange separate
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04Indicating or measuring of parameters as input values
    • F17C2250/0404Parameters indicated or measured
    • F17C2250/0439Temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/06Controlling or regulating of parameters as output values
    • F17C2250/0605Parameters
    • F17C2250/0631Temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0142Applications for fluid transport or storage placed underground
    • F17C2270/0144Type of cavity
    • F17C2270/0147Type of cavity by burying vessels

Definitions

  • a cooling system is pro- [56] References Cited vided for freezing the earth to aid in the excavation of the opening and this system is subsequently used to UNITED STATES PATENTS maintain the wall and floor of the opening frozen to a controlled thickness by cooling them in response to a 3 2 a a1 "61/5 X rise in the temperature of the'surrounding earth above 3'326'011 6/1967 ac en apredetermined temperature level. 3,360,941 1968 Also disclosed are various techniques for constructing 3.32.35: a storage tank of the type described. 3:5l6:568 6/1970 7 Claims, 9 Drawing Figures //0 4 n n m 5, a fix r If! g if; y; 417 1/!
  • the present invention relates to the storing of large quantities of liquified gas, most advantageously natural gas and in particular to the storing of such liquified gas underground.
  • the present invention is directed to certain structural features of an underground storage tank which was broadly conceived by Joseph A. Connell and Anthony J. Baranyi and which is described and claimed in a patent application entitled METHOD AND MEANS FOR THE UNDERGROUND STORAGE OF LIQUIFIED GAS Ser. No. 99,980 filed by the above joint inventors on Oct. 12, 1 970.
  • the aforesaid underground storage tank is constructed by first excavating a generally bucket-shaped opening in the earths surface and placing two bucket-shaped liners, one within the other, into the opening. Between the two liners thermal insulation packed in bags is distributed along the floor and wall of the opening.
  • the two liners have radially extending flanges which are sealed to one another so as to form, together with the thermal insulation between them, a double walled, moisture-impervious insulating bucket within the opening in the earth.
  • a diaphragm caps the top ofthe insulating bucket and forms with it a container for receiving cryogenic liquid such as liquid natural gas.
  • a thermally insulating ceiling is suspended above the diaphragm in order to form a completely thermally insulated container.
  • the present invention lies in certain methods and structural features for constructing an underground storage tank of the above type.
  • a layer of padding is placed over the wall of the opening and the outer liner of the insulating bucket is installed within that layer, thereby protecting the outer liner from puncture by sharp projections on the wall of the earthen opening.
  • a unique retaining structure is provided between the bags of insulation which are stacked along the wall of the opening and the inner liner.
  • This retaining structure has a dual purpose. First, it serves to prevent the bags which are stacked along the wall of the opening inside the outer liner from falling down. That this would otherwise be a problem will be appreciated when it is considered that a typical height for the wall of the opening, and hence for the stacked bags along that wall, is of the order of 60 feet.
  • the insulating bags or pillows are stacked inside the outer liner to a height which is a fraction of the total height of the wall of the excavated opening.
  • a screening is then installed along the floor of the opening on top of the inner liner, is brought up inside the stacked insulating pillows and is held in place by means of an expandable cryogenically stable retaining ring. Once that ring is installed, the height of the stacked bags is increased by piling additional insulating pillows to an additional height approximately equal to the height of the first set of pillows thus installed.
  • the screening is then extended further upward so as to cover the additionally stacked pillows and a second expandable retaining ring is put in place inside the screening near the top of the stacked pillows. This process continues, with the height of the pillows being successively increased along the wall of the opening and with the screening and additional retaining bands being installed all the way to the top of the opening.
  • the inner liner is installed inside the retaining structure which also serves to reinforce that inner liner when it is filled with cryogenic liquid.
  • the retaining structure and particularly the screening serve not only to hold the insulating pillows in place but also serve the important function of lending additional strength to the inner liner to prevent it from being ruptured by the fluid which is stored within it.
  • a concrete ring which is installed at the rim of the opening and which serves to support the inner and outer liners by means of a set of anchoring bolts distributed around its periphery.
  • a lightweight supporting structure is mounted upon this concrete ring to support the thermally insulating ceiling which is required above the top of the underground container.
  • the supporting structure is in the form of a net comprised of steel cables stretched across the concrete ring. On top of the cables a cryogenically sta ble screening, of the same type used to maintain the bags in the opening upright, is laid.
  • a liner similar to those used for the insulating bucket, is then laid on top of the cryogenically stable screening and insulating pillows, again of the same type used between the inner and outer liners, are installed in several layers over the liner.
  • a second liner is laid on top of the layers of insulating pillows and the top and bottom liners are sealed together at their edges so as to form a moisture-impervious enclosure or envelope for the thermally insulating pillows between them.
  • FIG. 1 is a plan view, partially cut away, of a storage tank incorporating features of the present invention
  • FIG. 2 is a cross section along line 2-2 of the storage tank illustrated in FIG. 1;
  • FIG. 3 is a sectional view of a wall of the storage tank illustrated in FIG. 2 taken along line 33;
  • FIG. 4 is a sectional view of the ceiling and roof of the storage tank illustrated in FIG. 2, taken through line 44;
  • FIG. 5 is an enlarged sectional view of the supporting concrete ring surrounding the mouth of the opening which houses the storage tank illustrated in FIG. 2;
  • FIG. 5a is an enlarged perspective cross-sectional view of a portion of the concrete ring of FIG. 5 showing more clearly the manner in which the several layers of the storage tank are anchored upon the ring;
  • FIG. 6 is a sectional view of the floor of the storage tank of FIG. 2, taken through line 6-6;
  • FIG. 7 is an enlargement of a portion of FIG. 2 to illustrate some of the details of the submerged pump used in the illustrated storage tank and the manner in which it is installed therein;
  • FIG. 8 is a side view of a few of the freeze pipes which are sunk into the earth in a circular array and through which a refrigerant is pumped to create a frozen shell of earth to provide structural support for the storage tank of FIGS. 1 and 2.
  • FIGS. 1, 2, and 5 An underground storage tank incorporating features of the present invention is illustrated in FIGS. 1, 2, and 5.
  • the exemplary storage is comprised principally of an opening 13 in the earths surface housing a double walled container 15.
  • the container is shown to be fabricated of a bucketshaped inner liner 17 capped by a diaphragm 19.
  • the inner liner 17 of the container is surrounded by insulating pillows 21 comprised of thermal insulation packed in bags, and the pillows 21 are in turn held within an outer bucket-shaped liner 23 which serves to prevent moisture from the earth from seeping into the thermal insulation.
  • a concrete ring 25 surrounds the lip of the opening 13 and serves as a structural support for the ceiling 27.
  • the latter includes a net 29 of cables upon which several layers of bags 31 packed with insulation are distributed. If desired, a roof 33 supported by an inert gas such as nitrogen may be anchored upon the ring 25 to prevent damage to the ceiling 27. Cryogenic fluid is pumped out of the storage tank by a submersible pumping system 37 which is suspended into the storage tank from a cantilever support structure 35.
  • a submersible pumping system 37 which is suspended into the storage tank from a cantilever support structure 35.
  • the storage tank may be either in an opening which is in a rock formation, in which case freezing of the ground is not required, or it may be formed in an opening in soil in which case it is desirable'that the ground be frozen both as an aid in construction and to provide structural strength during operation of the tank.
  • the tank which is illustrated in the figures is of the latter type.
  • the first step in constructing the subject storage tank is to investigate the soil conditions at the site thoroughly. The results of this investigation will help determine the exact construction methods which are to be employed, the required thickness of the soil that is to be frozen, as well as the amount of refrigeration that will be required.
  • the first step in ground freezing is the insertion of freeze pipes into the ground on a circle which will ultimately be the center of the frozen earthen wall.
  • Pipes 39 and 41 which are alternately long and short, as illustrated in FIG. 8, are preferably employed, with the long pipes 39 extending into the ground about -20 percent deeper than the bottom of the ultimate excavated hole.
  • the short pipes 41 extend into the ground approximately feet.
  • the staggered arrangement of pipes provides a greater transfer surface and hence cooling capacity near the ground level where the largest amount of heat must be removed from the soil.
  • two separate systems 43 and 45 for circulating refrigerant through the pipes are shown.
  • the first system 43 is connected to the long pipes 39 through a manifold 44 and the second system 45 is connected to the short pipes 41 through a second manifold 46.
  • the advantage of this arrangement derives from the fact that at times during normal tank operation heat leak from the ground into the insulated tank is not sufficient to maintain the frozen wall at the desired thickness. When this occurs, it is only necessary to pass refrigerant through the short pipes 41 since it is from the ground surface that the heat leak into the tank is the greatest.
  • the long freeze pipes 39 are comprised of coaxial pipes 390 and 39b, and the manifold 44 is comprised of an inlet manifold 44a and a return manifold 44b.
  • Refrigerant is circulated from the cooling unit 43 down through the inside freeze pipes 39a, up through the outside freeze pipes 39b and back to the cooling unit 43 through the return manifold 44b.
  • the short pipes 41 and their associated manifold 46 are similarly constructed.
  • temperature sensors 47 preferably of the type which produce an electrical indication of temperature on a pair of wires, are also inserted into the ground on radii extending out from the tank.
  • the sensors may be contained in pipes (not shown), sunk into the earth to the same length as the long freeze pipes 39, and containing temperature sensors throughout their length.
  • the wires of the sensors will, of course, be brought up through the pipes for connection to suitable controls or indicators.
  • the temperature sensors 49 in combination with additional sensors 49 and 50 which are inserted inside the excavation 13 and also beneath its floor also serve to monitor the temperature of the earth surrounding the excavation during operation of the tank.
  • one or both of the cooling systems 43 and 45 are kept running during the operation of the tank so as to keep the thickness of its frozen floor and wall within set limits, with the status of the floor and wall being determined by the sensors 49 and 50.
  • the ring 25 contains reinforcing steel rods whose number and thickness will depend upon the diameter of the opening and upon the loads which the ring is to carry. The necessary calculations for determining the number, thickness and distribution of the reinforcing steel rods are well known in the civil engineering art and will not be described herein. It might be noted that, before the concrete ring 25 is poured, it is desirable that some portion of the frozen earth be chipped out in order that the concrete may be poured directly against the frozen ground to eliminate the possibility of ice lens formation.
  • heat exchanger 51 consisting of a series of connected pipes is installed.
  • the heat exchanger 51 is connected to the manifold 44 which serves the long pipes 39.
  • Additional temperature sensors 49 and 50 are placed along the bottom of the opening and along its side. After the heat exchanger 51 and the additional temperature probes 49 have been installed on the bottom of the opening 13, they are covered with a layer of sand 52 to a depth of several feet, usually less than 4. Refrigerant is then pumped through the heat exchanger 51 until a bottom which is typically four feet thick is frozen.
  • the wall of the opening 13 is smoothed, preferably by spraying water upon it which freezes and produces a smooth surface.
  • padding is installed all around the opening over its wall and base. This may be done by fiberglass mats 53 in the form of vertically running strips attached to the wall of the opening and layed over its bottom, as shown in FIGS. 3 and 6.
  • the outer liner 23 is lowered into the opening.
  • it will be prefabricated to have a shape which conforms to the shape of the opening 13 and to have a size which is slightly larger than the opening. The latter will insure that when the outer liner 23 is put in place it will be slightly wrinkled so as to preclude the possibility of its being placed in tension when the tank is filled.
  • the outer liner 23 should be made of a cryogenically stable material.
  • a cryogenically stable material includes at least one multilayer laminate having layers of aluminum and polyester.
  • the outer, liner 23 is provided with a radially extending flange 23a by which it is anchored to the concrete ring 25.
  • a plurality of bolts 55 are anchored around the periphery of the concrete ring 25 and the rim 23a is fastened upon these bolts.
  • FIGS. 5 and 5a show a suitable arrangement wherein the bolts 55 are distributed around the periphery of the concrete ring in a channel 58.
  • a sealant paste is first applied in a layer 60 to the bottom of the channel 58 around the bolts 55, and the outer liner flange 23a is placed on top of the sealant layer 60.
  • the extreme portions of thescreening 61 and of the inner liner 17 are also extended into the channel 58, with additional layers 62 and 64 of sealant being applied under each of them.
  • the entire sandwich structure thus formed is clamped by meansof a series of arcuate retaining strips 56 made of a durable cryogenically stable material.
  • the strips 56 will be typically several feet long and will be predrilled to mate with approximately six bolts 55 for each strip, each bolt receiving a respective nut 66 to secure the strips 56 thereon.
  • the thermal insulation may now be installed upon the floor of the opening on top of the liner.
  • the insulation is preferably in the form of pillows 21 wherein particulated insulation is packed in bags 57 made of a cryogenically stable, porous material.
  • the material needs to be cryogenically stable since at least some of the bags will be exposed to the cryogenic temperatures of the liquid stored within the tank.
  • the advantage of making the bags out of porous material is that this allows trapped air to escape from within the bags when the tank is filled. Perlite has been found to be suitable for the insulating material.
  • the number of layers of insulating pillows 21 are a matter of choice, three being shown in the drawings.
  • the insulation of the wall of the opening 13 within the outer liner 23 may begin.
  • the use of insulating pillows 21 comprised of bagged Perlite is again preferred.
  • the insulating of the wall of the opening is best achieved by first stacking insulating pillows 21 along the wall of the opening 13 to a moderate height such as for example ten feet.
  • means are next installed to help retain the insulating pillows 21 which have been stacked next to the wall of the opening.
  • these means comprise a screening 61 combined with a series of expandable retaining bands 59.
  • the screening 61 is made up of a plurality of screen strips 63 which are laid upon the floor of the opening, with their edges slightly overlapping to make for a continuous, pie-shaped piece of screening. The screen strips 63 are brought up next to the stacked pillows along the wall of the opening 13.
  • a f rst retaining band 59 is installed and is expanded sufficiently to hold it, and the screen strips 63, in place.
  • the retaining bands are provided for this purpose with one or more ratcheted expanding joints 60 of conventional construction, which permit the retaining bands to expand, both during installation and subsequently, when the bands are further expanded, typically by several feet, by the pressure exerted upon them when the storage tank is filled.
  • the retaining bands 59 will contract at cryogenic temperatures but this is provided for in the expandable ratcheting connections 60.
  • the retaining bands will generally be of a semi-tubular shape, that is, their cross-section would be arcuate, to obtain structural strength and to present a smooth surface without abrupt corners to the inner liner 17.
  • the ratcheted expanding joints 60 would be in the hollow of the retaining bands and would have no contact with inner liner 17.
  • the ratcheting is so arranged that the retaining bands 59 can only expand and cannot contract even when the pressure which had caused them to expand in the first place is removed, as by emptying of the storage tank.
  • the screen strips 63 overlap not only along the floor of the opening but also along the wall so that a generally cylindrical screening is formed inside the insulating pillows 21 along the wall of the opening.
  • a lubricant such as a strip of polyester
  • the screening 61 is made capable of expanding under the pressure of liquid entering the tank. This is particularly important because the insulating pillows 21 are significantly compressed by the liquid, especially toward the bottom where they may be compressed by more than 6 inches.
  • the next step is to install the inner liner 17 which in the preferred embodiment has the same bucket shape as the outer liner 23, but which of course is made to be smaller.
  • the inner liner 17 is provided with a radially extending flange 17a at its top and the flange is fastened on top of the outer liner flange 230 by means ofthe bolts 55 and the washers 56.
  • the air between the inner and outer liners 17 and 23 is exhausted through an opening 69.
  • the resulting vacuum inside the space formed by the two liners 17 and 23 causes the inner liner 17 to press against the screening 61 so that both the screening and the inner liner conform generally to the shape of the pillows 21 which are stacked against the wall of the opening.
  • the inner liner 17 is designed, with a waffled surface configuration, to be slightly larger than the space inside the insulating pillows 21.
  • the screening 61 of the present invention serves a dual purpose. As noted earlier, it serves to hold the insulating pillows 21 flat against the wall of the opening in combination with the retaining rings 59.
  • the screening 61 also serves, however, as a reinforcement for the inner liner 17.
  • the screening is preferably made of some cryogenically stable material having good structural strength. It may be, for example, made of either fiberglass screening, aluminum screening, or stainless steel screening. Tests have proven that the strength of the laminate which makes up the inner liner 17 can be substantially increased by use of the screening 61.
  • the diaphragm preferably is made of the same laminate as the liners 17 and 23 and is sufficiently large so that it extends past their flanges 17a and 230. it is provided with a series of openings about its periphery which fit around a corresponding plurality of bolts 67.
  • retaining strips of the same type as the retaining strips 56 used for the liners 17 and 23 the edges of the diaphragm 19 are sealed to the top surface of the concrete ring 25 so that the ring provides a seal between the double walled insulating bucket formed by the inner and outer liners 17 and 23 on the one hand and the diaphragm 19 on the other hand.
  • a net 29 of steel cables is stretched across the concrete ring 25.
  • the net 29 is comprised of an outer steel l-beam ring 72, an inner steel ring 74, and a plurality of steel cables 73 stretched radially between them.
  • the entire net 29 can be assembled away from the tank and lowered in one piece by a crane to rest upon the horizontal ledge of the concrete ring 25, where it would then be bolted, to prevent it from rising thereafter.
  • Thermal insulation 76 in loose form is installed around the edge of the net 29 to prevent heat leaks between the ceiling insulation 31 and the wall insulation 21.
  • Suitable tensioning devices 79 are usually provided near the end of the cables 73 to give them a desired catenary.
  • a protective cushion 71 such as one inch thick fiberglass on top ofthe diaphragm 19 to prevent it from rubbing against the net.
  • a layer of screening 81 is installed on top of the net 29 to provide a continuous floor upon which the thermal insulating ceiling can be stacked.
  • a liner 85 which may be of the same construction as the liners 17 and 23 is next installed on top of the screening 79. Then, before the thermal insulation 31 is installed on top of the liner 85, a flange 87 is first formed through the liner 85, the screening 81, the fiberglass padding 71, and the diaphragm 19 below by cutting a hole 88 through them in order to accommodate the casing of the submersible pump 37.
  • a gasket 89 is placed and immediately on top of the hole opposite the gasket 89 a double-flanged collar 91 is laid.
  • the gasket 89 and the collar 91 are fastened together by a set of bolts 93, thereby forming a vapor sealing flange 87 and sandwiching between them the liner 85 and the diaphragm 19.
  • the next step is to lower the submersible pump system 37 through the flange 87just formed.
  • a suitable such pumping system is manufactured by the Carter Pump Company of Costa Mesa, California and is described in U.S. Pat. No. 3,369,715 issued to J. C. Carter. Since the pumping system is commercially available, it will not be described herein in detail. Suffice it to say that it includes a casing 95 having a bottom portion 95a and a top portion 95b having abutting flanges 99 and 100 which are clamped and sealed together.
  • the initial part in installing the pumping system 37 is to lower the casing 95 through the flange 87 by means of a crane.
  • the casing 95 is lowered to a depth sufficient to bring its bottom close to but not in contact with the bottom of the storage tank. It is then fixed in place upon the support structure 35, suitable brackets 102 being provided on the casing 95 for this purpose, and its flanges 99 and 100 are bolted to the top flange of the ceiling collar 91.
  • a submersible, electrically powered pump 105 is lowered in place to the bottom of the casing 95 to rest on top of a foot valve assembly 107 which automatically opens in response to the pump 105 being seated thereon.
  • Electric power is supplied to the pump 105 through an electric cable 109 fed from a conduit 108.
  • a connecting member 103 which may be either a pipe or a cable suspended from a cover plate 101 at the top of the casting 95, the pump 105 may be both lowered into place and subsequently lifted and removed from the casing 95 for repairs without unduly disrupting the operation of the storage tank.
  • the connecting member 103 is suspended from the cover plate 101 by means of a hand crank 104 which, when turned, is operative to lift or lower the pump 105.
  • the hand crank 104 is used only to lift the pump 105 sufficiently to close the valve assembly 107.
  • cryogenic fluid is pumped out of the storage tank through an inlet and outlet pipe flange 110 which extends from the upper casing portion 95b.
  • a fill and vent assembly 113 comprised of a flanged, vent pipe 114 and a fill pipe 116 supported within the vent pipe. This may be accomplished in a manner similar to the installation of the casing 95. ln particular, an opening 112 is cut through the ceiling material and receives a gasket 111 and a double flanged collar 118 which are fastened together by a set of bolts 117.
  • the vent pipe 114 extends up through the ceiling structure of the tank and is rigidly held in place by brackets 120 bolted to the support structure 35.
  • the liquid till pipe 116 also extends through the ceiling structure and has at its bottom a splash plate 122 to disperse the cryogenic fluid being fed therethrough.
  • the thermal ceiling insulation may be laid.
  • This thermal insulation may bein the same form as that used for insulating the floor and walls of the storage tank and is therefore shown in FIGS. 2 and 7 as several layers of thermally insulating pillows 31.
  • the insulating pillows 31 are laid over the entire ceiling on top of the liner 85 and are preferably packed to the edge of the concrete ring as shown in FIG. 5.
  • a second liner 121 which may be of the same material as the bottom ceiling liner 85 is then installed over the ceiling insulating pillows 119.
  • the ceiling screening 81, and the ceiling liners and 121 are anchored at their peripheries in a groove 82 which extends all around the top of the concrete ring 25.
  • the manner of attachment is similar to that used for the tank diaphragm 19.
  • the screening 81 and the liners 85 and 121 are sandwiched together in the groove 82 with a sealant being applied under each of them, and they are clamped in the groove 82 by means of long arcuate strips 83 fastened down by bolts 84 and nuts 86 distributed along the groove.
  • Additional vapor seals 124 are provided subsequently where the casing and the pipe 113 penetrate the upper liner 121 and the ceiling 33.
  • the two liners 85 and 121 together form a moisture-impervious barrier which fully encloses the ceiling insulating pillows 119.
  • the space between liners 85 and 121, filled with bagged Perlite insulation, is maintained in an inerted gas atmosphere, such as nitrogen.
  • a protective roof 33 This structure may be made of a flexible, airtight commercially available material, such as vinyl coated nylon fastened at its edges to the outer periphery of the concrete ring by a set of bolts 123 and washers 125.
  • the protective roof 33 may be inert gas supported by maintaining the pressure in the space 127 below it at slightly above atmospheric.
  • a purging of the inner vessel and insulated annular space between outer and inner liners 23 and 17 with inerting gas is accomplished by introducing inerting gas, such as nitrogen, into the inner vessel area first, and then into the annulus through the inlet 69, maintaining a higher pressure in the vessel than in the annulus to avoid displacement of the inner liner 17 from the insulated wall.
  • inerting gas such as nitrogen
  • the filling of the tank may now begin. It will usually be done through both the fill pipe 116 and the pump housing 95.
  • the pipe flange 110 of the housing 95 is connected to a source of cryogenic fluid as in the till pipe 116.
  • cryogenic fluid will then be fed through the pipes 110 and 116.
  • the feeding of the cryogenic fluid through the till pipe 116 has the advantage that the cryogenic fluid is dispersed by means of the splash plate 122 near the top of the tank, thus serving to condense some of the rising flash and vapor which is always generated when cryogenic fluids are transferred.
  • additional cryogenic fluid may be supplied through the till pipe 116. This may be done either while the submerged pump is inoperative or at the same time that cryogenic fluid is being withdrawn from the tank by means of the pump through the pipe 110.
  • the lateral pressure of the liquid being exerted upon the wall of the inner liner 17 will cause that liner to expand, this being made possible by the presence of waffling distributed over its entire surface.
  • the screening 61 will also expand by virtue of the sliding engagement of its individual strips 63, as will the retaining bands 59 by virtue of its ratchet joints 60.
  • the principal reason for this expansion is the compressibility of the insulating pillows 21 which line the wall of the opening 13.
  • the entire double walled insulating bucket which is comprised of the liners l7 and 23 and of the pillows 21 between them, is compressible, with its inner wall being made expandable for this purpose.
  • the tank assumes its final configuration upon being filled, it will retain that configuration even if the liquid is withdrawn therefrom.
  • the insulating pillows 21 do not spring back to their original shape, but remain in their compressed form and partly because the retaining bands maintain their expanded dimension as a result of their one-way ratcheted joints.
  • a liquid container is provided which can withstand very high liquid pressures by responding flexibly to them.
  • An underground storage tank for liquified gas comprising:
  • thermal insulation distributed between said screening and the floor and wall of said opening and a thermally insulated roof covering the top of said opening.
  • the storage tank of claim 1 characterized further by a plurality of expanding retention bands located within said screen at vertically spaced intervals between said screening and the side of said container and pressing said screening against said thermal insulation to hold said thermal insulation in place.
  • the storage tank of claim 2 characterized further by a moisture-impervious liner surrounding the thermal insulation which is distributed between said screening and the floor and wall of said opening and a layer of padding distributed between the wall of said opening and said liner to protect said liner from puncture.
  • a thermally insulated roof comprising:
  • thermal insulation packed in bags and distributed in several layers on top of said laminate.
  • thermally insulated container for use in storing liquified gas in a bucket-shaped opening in the earth's surface a thermally insulated container comprising:
  • thermal insulation distributed in a continuous layer above said diaphragm.
  • thermally insulated container for use in storing liquified gas in a bucket-shaped opening in the earth's surface a thermally insulated container comprising:
  • bracing means for maintaining said bags of insulation upright against the wall of said opening and for reinforcing the inner wall of said liner, said bracing means including,
  • thermal insulation distributed in a continuous layer above said diaphragm.
  • thermally insulated container for use in storing liquified gas in a bucket-shaped opening in the earths surface a thermally insulated container comprising in combination:
  • thermal insulation distributed in a continuous layer above said diaphragm, said container being characterized in that its inner liner, its retaining bands, and its screening all expand and said compressible pillows are compressed when said tank is initially filled.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

Liquified gas is stored underground in a large double walled container seated in an opening in the earth''s surface. Between the walls of the liner, thermal insulation is distributed in a continuous layer along the floor and wall of the opening. A diaphragm is supported across the top of the opening with a seal being provided between the diaphragm and the double walled liner to form a container for the liquified gas. Surrounding the lip of the opening is a concrete ring across which a net of cables is stretched to support a thermally insulating ceiling. A cooling system is provided for freezing the earth to aid in the excavation of the opening and this system is subsequently used to maintain the wall and floor of the opening frozen to a controlled thickness by cooling them in response to a rise in the temperature of the surrounding earth above a predetermined temperature level. Also disclosed are various techniques for constructing a storage tank of the type described.

Description

United States Patent i191 Connell et al.
[5-41 CRYOGENIC STORAGE TANK IMPROVEMENTS 11 3,707,850 1 Jan.2,19 73 Primary Examiner-Meyer Perlin v Assistant Examiner-Ronald C. Capossela' [75] Inventors: fi gr fi 3:12:32 i s Attorney-Fowler, Knobbe & Martens '7 2:11:f V. Laylander, Irvine, all of [57] ABSTRACT i Liquified gas is stored underground in a large double [73] Asslgnee gr ,Cqmol Cowl-mm walled container seated in an opening in the earths oemx' surface. Between the walls of the liner, thermal insula- [22] Filed: Oct. 12, 1970 tion is distributed in a continuous layer along the floor and wall of the opening. A diaphragm is supported [21] Appl 80417 across the top of the opening with a seal being provided between the diaphragm and the double walled 52 US. Cl. ..62/45,6ll.5, 62/260 liner to form a container for the liquified s [5i] lnt'.Cl. ..F17c 1/00 mmdins P P of the Owing is a concrete ring 58 Field of Search ..6l/.5; 62/45 which a cables Stretched PP a thermally insulating ceiling. A cooling system is pro- [56] References Cited vided for freezing the earth to aid in the excavation of the opening and this system is subsequently used to UNITED STATES PATENTS maintain the wall and floor of the opening frozen to a controlled thickness by cooling them in response to a 3 2 a a1 "61/5 X rise in the temperature of the'surrounding earth above 3'326'011 6/1967 ac en apredetermined temperature level. 3,360,941 1968 Also disclosed are various techniques for constructing 3.32.35: a storage tank of the type described. 3:5l6:568 6/1970 7 Claims, 9 Drawing Figures //0 4 n n m 5, a fix r If! g if; y; 417 1/! 2 J 1 *r u a 4 1- s Ma l W Aa a? 4/ J7) 3 21- :g [J7 *l a E r 1 i 1 5 4 1 I49 1 l i i" I o o o 0 0 0 0 o o o o o o o' o o o o dzo o o c oli o 0' Q/ a 17 PATENTEUJm ma SHEET 1 [IF 5 INVENTORS.
rA-rammmz ms SHEET 3 UF 5.
INVENTORS.
JOSEPH A. comm ANTHONY J. BARANYI BY PAUL V. LAYLANDER OWL 5?, KNOBEE a Mfl/QTENS ATTORNEYS.
PATENTED m 2 I975 I sum u 0F 5 INVENTORS.
JOSEPH A. CON'NELL ANTHONY J. BARANYI PAUL V. LAYLANDER CRYOGENIC STORAGE TANK IMPROVEMENTS The present invention relates to the storing of large quantities of liquified gas, most advantageously natural gas and in particular to the storing of such liquified gas underground.
More particularly, the present invention is directed to certain structural features of an underground storage tank which was broadly conceived by Joseph A. Connell and Anthony J. Baranyi and which is described and claimed in a patent application entitled METHOD AND MEANS FOR THE UNDERGROUND STORAGE OF LIQUIFIED GAS Ser. No. 99,980 filed by the above joint inventors on Oct. 12, 1 970. The aforesaid underground storage tank is constructed by first excavating a generally bucket-shaped opening in the earths surface and placing two bucket-shaped liners, one within the other, into the opening. Between the two liners thermal insulation packed in bags is distributed along the floor and wall of the opening. The two liners have radially extending flanges which are sealed to one another so as to form, together with the thermal insulation between them, a double walled, moisture-impervious insulating bucket within the opening in the earth. A diaphragm caps the top ofthe insulating bucket and forms with it a container for receiving cryogenic liquid such as liquid natural gas. A thermally insulating ceiling is suspended above the diaphragm in order to form a completely thermally insulated container.
The present invention lies in certain methods and structural features for constructing an underground storage tank of the above type. Thus, in accordance with one of these features, a layer of padding is placed over the wall of the opening and the outer liner of the insulating bucket is installed within that layer, thereby protecting the outer liner from puncture by sharp projections on the wall of the earthen opening.
In accordance with another aspect of the presentin vention, a unique retaining structure is provided between the bags of insulation which are stacked along the wall of the opening and the inner liner. This retaining structure has a dual purpose. First, it serves to prevent the bags which are stacked along the wall of the opening inside the outer liner from falling down. That this would otherwise be a problem will be appreciated when it is considered that a typical height for the wall of the opening, and hence for the stacked bags along that wall, is of the order of 60 feet. In carrying out this feature of the invention, the insulating bags or pillows are stacked inside the outer liner to a height which is a fraction of the total height of the wall of the excavated opening.
A screening is then installed along the floor of the opening on top of the inner liner, is brought up inside the stacked insulating pillows and is held in place by means of an expandable cryogenically stable retaining ring. Once that ring is installed, the height of the stacked bags is increased by piling additional insulating pillows to an additional height approximately equal to the height of the first set of pillows thus installed. The screening is then extended further upward so as to cover the additionally stacked pillows and a second expandable retaining ring is put in place inside the screening near the top of the stacked pillows. This process continues, with the height of the pillows being successively increased along the wall of the opening and with the screening and additional retaining bands being installed all the way to the top of the opening.
With the insulating pillows all held securely in place, the inner liner is installed inside the retaining structure which also serves to reinforce that inner liner when it is filled with cryogenic liquid. This is particularly important because the insulating pillows are by their nature compressible. Moreover, they present to the inner liner a surface having gaps which the liner must bridge. Both of these characteristics tend to cause the inner liner to balloon outward under the weight of the liquid within. Thus, the retaining structure and particularly the screening serve not only to hold the insulating pillows in place but also serve the important function of lending additional strength to the inner liner to prevent it from being ruptured by the fluid which is stored within it.
In the storage tank which is described in the abovereferenced patent application, there is described a concrete ring which is installed at the rim of the opening and which serves to support the inner and outer liners by means of a set of anchoring bolts distributed around its periphery. ln accordance with the present invention, a lightweight supporting structure is mounted upon this concrete ring to support the thermally insulating ceiling which is required above the top of the underground container. In keeping with this feature of the invention, the supporting structure is in the form of a net comprised of steel cables stretched across the concrete ring. On top of the cables a cryogenically sta ble screening, of the same type used to maintain the bags in the opening upright, is laid. A liner, similar to those used for the insulating bucket, is then laid on top of the cryogenically stable screening and insulating pillows, again of the same type used between the inner and outer liners, are installed in several layers over the liner. A second liner is laid on top of the layers of insulating pillows and the top and bottom liners are sealed together at their edges so as to form a moisture-impervious enclosure or envelope for the thermally insulating pillows between them.
The present invention and its advantages will be more clearly understood with reference to the following description of a preferred embodiment thereof taken in conjunction with the accompanying drawings wherein:
FIG. 1 is a plan view, partially cut away, of a storage tank incorporating features of the present invention;
FIG. 2 is a cross section along line 2-2 of the storage tank illustrated in FIG. 1;
FIG. 3 is a sectional view of a wall of the storage tank illustrated in FIG. 2 taken along line 33;
FIG. 4 is a sectional view of the ceiling and roof of the storage tank illustrated in FIG. 2, taken through line 44;
FIG. 5 is an enlarged sectional view of the supporting concrete ring surrounding the mouth of the opening which houses the storage tank illustrated in FIG. 2;
FIG. 5a is an enlarged perspective cross-sectional view of a portion of the concrete ring of FIG. 5 showing more clearly the manner in which the several layers of the storage tank are anchored upon the ring;
FIG. 6 is a sectional view of the floor of the storage tank of FIG. 2, taken through line 6-6;
FIG. 7 is an enlargement of a portion of FIG. 2 to illustrate some of the details of the submerged pump used in the illustrated storage tank and the manner in which it is installed therein; and
FIG. 8 is a side view of a few of the freeze pipes which are sunk into the earth in a circular array and through which a refrigerant is pumped to create a frozen shell of earth to provide structural support for the storage tank of FIGS. 1 and 2.
In the detailed description which follows, an exemplary storage tank incorporating features of the present invention is described in detail. It should be kept in mind that several of the structural features as well as several of the construction methods described herein are the joint inventions of Joseph A. Connell and Anthony J. Baranyi, are not claimed in the present application, but are claimed instead in the abovereferenced application ofthese joint inventors.
An underground storage tank incorporating features of the present invention is illustrated in FIGS. 1, 2, and 5. As best seen in FIGS. 1, 2, and 5, the exemplary storage is comprised principally of an opening 13 in the earths surface housing a double walled container 15. The container is shown to be fabricated of a bucketshaped inner liner 17 capped by a diaphragm 19. The inner liner 17 of the container is surrounded by insulating pillows 21 comprised of thermal insulation packed in bags, and the pillows 21 are in turn held within an outer bucket-shaped liner 23 which serves to prevent moisture from the earth from seeping into the thermal insulation. A concrete ring 25 surrounds the lip of the opening 13 and serves as a structural support for the ceiling 27. The latter includes a net 29 of cables upon which several layers of bags 31 packed with insulation are distributed. If desired, a roof 33 supported by an inert gas such as nitrogen may be anchored upon the ring 25 to prevent damage to the ceiling 27. Cryogenic fluid is pumped out of the storage tank by a submersible pumping system 37 which is suspended into the storage tank from a cantilever support structure 35.
The storage tank may be either in an opening which is in a rock formation, in which case freezing of the ground is not required, or it may be formed in an opening in soil in which case it is desirable'that the ground be frozen both as an aid in construction and to provide structural strength during operation of the tank. The tank which is illustrated in the figures is of the latter type. The first step in constructing the subject storage tank is to investigate the soil conditions at the site thoroughly. The results of this investigation will help determine the exact construction methods which are to be employed, the required thickness of the soil that is to be frozen, as well as the amount of refrigeration that will be required.
The first step in ground freezing is the insertion of freeze pipes into the ground on a circle which will ultimately be the center of the frozen earthen wall. Pipes 39 and 41 which are alternately long and short, as illustrated in FIG. 8, are preferably employed, with the long pipes 39 extending into the ground about -20 percent deeper than the bottom of the ultimate excavated hole. The short pipes 41 extend into the ground approximately feet. The staggered arrangement of pipes provides a greater transfer surface and hence cooling capacity near the ground level where the largest amount of heat must be removed from the soil. In order to permit close control of the rate of freezing, two separate systems 43 and 45 for circulating refrigerant through the pipes are shown. The first system 43 is connected to the long pipes 39 through a manifold 44 and the second system 45 is connected to the short pipes 41 through a second manifold 46. The advantage of this arrangement derives from the fact that at times during normal tank operation heat leak from the ground into the insulated tank is not sufficient to maintain the frozen wall at the desired thickness. When this occurs, it is only necessary to pass refrigerant through the short pipes 41 since it is from the ground surface that the heat leak into the tank is the greatest.
As shown in FIG. 2, the long freeze pipes 39 are comprised of coaxial pipes 390 and 39b, and the manifold 44 is comprised of an inlet manifold 44a and a return manifold 44b.
Refrigerant is circulated from the cooling unit 43 down through the inside freeze pipes 39a, up through the outside freeze pipes 39b and back to the cooling unit 43 through the return manifold 44b. The short pipes 41 and their associated manifold 46 are similarly constructed.
At the same time that the freeze pipes 39 and 41 are installed, several rows of temperature sensors 47, preferably of the type which produce an electrical indication of temperature on a pair of wires, are also inserted into the ground on radii extending out from the tank. The sensors may be contained in pipes (not shown), sunk into the earth to the same length as the long freeze pipes 39, and containing temperature sensors throughout their length. The wires of the sensors will, of course, be brought up through the pipes for connection to suitable controls or indicators. By sensing and monitoring the ground temperatures with the temperature sensors 47 the progress of ground freezing may be monitored and the time when excavation may begin can be determined. The temperature sensors 49 in combination with additional sensors 49 and 50 which are inserted inside the excavation 13 and also beneath its floor also serve to monitor the temperature of the earth surrounding the excavation during operation of the tank. As explained in the related Joseph A. Connell and Anthony J. Baranyi application, one or both of the cooling systems 43 and 45 are kept running during the operation of the tank so as to keep the thickness of its frozen floor and wall within set limits, with the status of the floor and wall being determined by the sensors 49 and 50.
After the walls have been frozen to the desired thickness, excavation of the unfrozen center of the frozen ring by any of several known methods may begin. After excavation has progressed to a depth which will represent the bottom of the concrete ring 25, the latter is installed. The ring 25 contains reinforcing steel rods whose number and thickness will depend upon the diameter of the opening and upon the loads which the ring is to carry. The necessary calculations for determining the number, thickness and distribution of the reinforcing steel rods are well known in the civil engineering art and will not be described herein. It might be noted that, before the concrete ring 25 is poured, it is desirable that some portion of the frozen earth be chipped out in order that the concrete may be poured directly against the frozen ground to eliminate the possibility of ice lens formation.
After the concrete ring 25 has been installed, the unfrozen earth within is excavated to a depth which is several feet greater than that ultimately required. In the over-excavated portion at the bottom of heat exchanger 51 consisting of a series of connected pipes is installed. The heat exchanger 51 is connected to the manifold 44 which serves the long pipes 39. Additional temperature sensors 49 and 50 are placed along the bottom of the opening and along its side. After the heat exchanger 51 and the additional temperature probes 49 have been installed on the bottom of the opening 13, they are covered with a layer of sand 52 to a depth of several feet, usually less than 4. Refrigerant is then pumped through the heat exchanger 51 until a bottom which is typically four feet thick is frozen.
The installation of the tank may now begin. First, the wall of the opening 13 is smoothed, preferably by spraying water upon it which freezes and produces a smooth surface. To further insure that no damage will be done to the outer liner 23, and in accordance with a feature of the present invention, padding is installed all around the opening over its wall and base. This may be done by fiberglass mats 53 in the form of vertically running strips attached to the wall of the opening and layed over its bottom, as shown in FIGS. 3 and 6. After the mats 53, which should be at least an inch thick, have been installed, the outer liner 23 is lowered into the opening. Preferably, it will be prefabricated to have a shape which conforms to the shape of the opening 13 and to have a size which is slightly larger than the opening. The latter will insure that when the outer liner 23 is put in place it will be slightly wrinkled so as to preclude the possibility of its being placed in tension when the tank is filled.
The outer liner 23 should be made of a cryogenically stable material. One which is believed will be found suitable includes at least one multilayer laminate having layers of aluminum and polyester. At its top the outer, liner 23 is provided with a radially extending flange 23a by which it is anchored to the concrete ring 25. For this purpose a plurality of bolts 55 are anchored around the periphery of the concrete ring 25 and the rim 23a is fastened upon these bolts. FIGS. 5 and 5a show a suitable arrangement wherein the bolts 55 are distributed around the periphery of the concrete ring in a channel 58. A sealant paste is first applied in a layer 60 to the bottom of the channel 58 around the bolts 55, and the outer liner flange 23a is placed on top of the sealant layer 60. At subsequent stages of construction the extreme portions of thescreening 61 and of the inner liner 17 are also extended into the channel 58, with additional layers 62 and 64 of sealant being applied under each of them. Finally, the entire sandwich structure thus formed is clamped by meansof a series of arcuate retaining strips 56 made of a durable cryogenically stable material. The strips 56 will be typically several feet long and will be predrilled to mate with approximately six bolts 55 for each strip, each bolt receiving a respective nut 66 to secure the strips 56 thereon.
Having installed the outer liner 23, the thermal insulation may now be installed upon the floor of the opening on top of the liner. The insulation is preferably in the form of pillows 21 wherein particulated insulation is packed in bags 57 made of a cryogenically stable, porous material. The material needs to be cryogenically stable since at least some of the bags will be exposed to the cryogenic temperatures of the liquid stored within the tank. The advantage of making the bags out of porous material is that this allows trapped air to escape from within the bags when the tank is filled. Perlite has been found to be suitable for the insulating material.
The number of layers of insulating pillows 21 are a matter of choice, three being shown in the drawings.
Once the floor of the opening has been covered with the desired number of layers of bagged thermal insulation, the insulation of the wall of the opening 13 within the outer liner 23 may begin. The use of insulating pillows 21 comprised of bagged Perlite is again preferred. The insulating of the wall of the opening is best achieved by first stacking insulating pillows 21 along the wall of the opening 13 to a moderate height such as for example ten feet. To prevent the inner liner 17 from having a sharp corner and thereby to reduce the chances of rupture when the tank is filled, it is desirable at this point to install all around the bottom corner of the opening 13 next to the pillows 21 a series of triangularly cross-sectioned corner pillows 65 which may be comprised of the same materials as those used for the pillows 21, forming a curved radial side wall-to-base configuration.
In keeping with a principal feature of the present invention, means are next installed to help retain the insulating pillows 21 which have been stacked next to the wall of the opening. In the exemplary embodiment illustrated in FIGS. 1 and 2, these means comprise a screening 61 combined with a series of expandable retaining bands 59. As best' seen in FIG. 1, the screening 61 is made up of a plurality of screen strips 63 which are laid upon the floor of the opening, with their edges slightly overlapping to make for a continuous, pie-shaped piece of screening. The screen strips 63 are brought up next to the stacked pillows along the wall of the opening 13. To hold the screen strips 63 in place against the bags 21, and in further keeping with the present invention, a f rst retaining band 59 is installed and is expanded sufficiently to hold it, and the screen strips 63, in place. The retaining bands are provided for this purpose with one or more ratcheted expanding joints 60 of conventional construction, which permit the retaining bands to expand, both during installation and subsequently, when the bands are further expanded, typically by several feet, by the pressure exerted upon them when the storage tank is filled. The retaining bands 59 will contract at cryogenic temperatures but this is provided for in the expandable ratcheting connections 60. The retaining bands will generally be of a semi-tubular shape, that is, their cross-section would be arcuate, to obtain structural strength and to present a smooth surface without abrupt corners to the inner liner 17. The ratcheted expanding joints 60 would be in the hollow of the retaining bands and would have no contact with inner liner 17. The ratcheting is so arranged that the retaining bands 59 can only expand and cannot contract even when the pressure which had caused them to expand in the first place is removed, as by emptying of the storage tank.
The screen strips 63 overlap not only along the floor of the opening but also along the wall so that a generally cylindrical screening is formed inside the insulating pillows 21 along the wall of the opening. In some instances it may be advisable to sandwich a lubricant, such as a strip of polyester, between the overlapping edges of adjacent screen strips 63 so as to allow them to slide relative to one another. In this way, the screening 61 is made capable of expanding under the pressure of liquid entering the tank. This is particularly important because the insulating pillows 21 are significantly compressed by the liquid, especially toward the bottom where they may be compressed by more than 6 inches.
Once the screen strips 63 have been fastened under the first retaining band 59, more insulating pillows 21 may be piled on top of those which had been initially placed next to the wall. As shown in FIG. 2, when the pillows 21 have been stacked along the wall to an additional height,- approximately the same as the initial height of pillows stacked there, another retaining band 59 is installed and the screen strips 63 are raised all around the wall of insulation and fastened under the second retaining band 59. This process continues, with additional pillows being piled on top of those stacked previously and with successive retaining bands 59 being installed, each time raising the screen strips just above the last retaining band 59 so installed. The process continues until the wall of insulating pillows and the screening 61 inside it reaches the top of the opening 13. At this point the screen strips 63 are brought over on top of the pillows 21 and are fastened upon the concrete ring 25 in the manner explained previously with reference to FIG. a.
The next step is to install the inner liner 17 which in the preferred embodiment has the same bucket shape as the outer liner 23, but which of course is made to be smaller. The inner liner 17 is provided with a radially extending flange 17a at its top and the flange is fastened on top of the outer liner flange 230 by means ofthe bolts 55 and the washers 56.
As an aid in the proper installation of the inner liner 17 the air between the inner and outer liners 17 and 23 is exhausted through an opening 69. The resulting vacuum inside the space formed by the two liners 17 and 23 causes the inner liner 17 to press against the screening 61 so that both the screening and the inner liner conform generally to the shape of the pillows 21 which are stacked against the wall of the opening. The inner liner 17 is designed, with a waffled surface configuration, to be slightly larger than the space inside the insulating pillows 21.
it may be seen at this point that the screening 61 of the present invention serves a dual purpose. As noted earlier, it serves to hold the insulating pillows 21 flat against the wall of the opening in combination with the retaining rings 59. The screening 61 also serves, however, as a reinforcement for the inner liner 17. Thus, where the liner bridges a gap between adjacent insulating pillows, and particularly where such a bag collapses under the weight of cryogenic liquid within the inner liner 17, the screening keeps the inner liner from ballooning into the resulting space. For this reason, the screening is preferably made of some cryogenically stable material having good structural strength. It may be, for example, made of either fiberglass screening, aluminum screening, or stainless steel screening. Tests have proven that the strength of the laminate which makes up the inner liner 17 can be substantially increased by use of the screening 61.
With the inner liner 17 in place the next step is to install the diaphragm 19. The diaphragm preferably is made of the same laminate as the liners 17 and 23 and is sufficiently large so that it extends past their flanges 17a and 230. it is provided with a series of openings about its periphery which fit around a corresponding plurality of bolts 67. By means of retaining strips of the same type as the retaining strips 56 used for the liners 17 and 23 the edges of the diaphragm 19 are sealed to the top surface of the concrete ring 25 so that the ring provides a seal between the double walled insulating bucket formed by the inner and outer liners 17 and 23 on the one hand and the diaphragm 19 on the other hand.
The provision at this point of a light yet strong, thermally insulating ceiling forms yet another feature of the present invention. Specifically, a net 29 of steel cables is stretched across the concrete ring 25. In the exemplary embodiment disclosed, particularly in FIGS. 1 and 5, the net 29 is comprised of an outer steel l-beam ring 72, an inner steel ring 74, and a plurality of steel cables 73 stretched radially between them. The entire net 29 can be assembled away from the tank and lowered in one piece by a crane to rest upon the horizontal ledge of the concrete ring 25, where it would then be bolted, to prevent it from rising thereafter. Thermal insulation 76 in loose form is installed around the edge of the net 29 to prevent heat leaks between the ceiling insulation 31 and the wall insulation 21. Suitable tensioning devices 79 are usually provided near the end of the cables 73 to give them a desired catenary.
Before installing the net 29, it is desirable first to lay a protective cushion 71, such as one inch thick fiberglass on top ofthe diaphragm 19 to prevent it from rubbing against the net.
A layer of screening 81 is installed on top of the net 29 to provide a continuous floor upon which the thermal insulating ceiling can be stacked. To provide a moisture-impervious protective layer for the thermal ceiling insulation 31, a liner 85 which may be of the same construction as the liners 17 and 23 is next installed on top of the screening 79. Then, before the thermal insulation 31 is installed on top of the liner 85, a flange 87 is first formed through the liner 85, the screening 81, the fiberglass padding 71, and the diaphragm 19 below by cutting a hole 88 through them in order to accommodate the casing of the submersible pump 37.
Under the hole 88 a gasket 89 is placed and immediately on top of the hole opposite the gasket 89 a double-flanged collar 91 is laid. The gasket 89 and the collar 91 are fastened together by a set of bolts 93, thereby forming a vapor sealing flange 87 and sandwiching between them the liner 85 and the diaphragm 19. The next step is to lower the submersible pump system 37 through the flange 87just formed. A suitable such pumping system is manufactured by the Carter Pump Company of Costa Mesa, California and is described in U.S. Pat. No. 3,369,715 issued to J. C. Carter. Since the pumping system is commercially available, it will not be described herein in detail. Suffice it to say that it includes a casing 95 having a bottom portion 95a and a top portion 95b having abutting flanges 99 and 100 which are clamped and sealed together.
The initial part in installing the pumping system 37 is to lower the casing 95 through the flange 87 by means of a crane. The casing 95 is lowered to a depth sufficient to bring its bottom close to but not in contact with the bottom of the storage tank. It is then fixed in place upon the support structure 35, suitable brackets 102 being provided on the casing 95 for this purpose, and its flanges 99 and 100 are bolted to the top flange of the ceiling collar 91. Next, a submersible, electrically powered pump 105 is lowered in place to the bottom of the casing 95 to rest on top of a foot valve assembly 107 which automatically opens in response to the pump 105 being seated thereon. Electric power is supplied to the pump 105 through an electric cable 109 fed from a conduit 108. By means of a connecting member 103, which may be either a pipe or a cable suspended from a cover plate 101 at the top of the casting 95, the pump 105 may be both lowered into place and subsequently lifted and removed from the casing 95 for repairs without unduly disrupting the operation of the storage tank. For this purpose the connecting member 103 is suspended from the cover plate 101 by means ofa hand crank 104 which, when turned, is operative to lift or lower the pump 105. The hand crank 104 is used only to lift the pump 105 sufficiently to close the valve assembly 107. When it is desired to entirely remove the pump 105 from the casing 95, the 'cover plate 101 is removed and other means, such as a crane are used to pull the pump 105 from the casing.
As described in greater detail in the referenced Carter patent, cryogenic fluid is pumped out of the storage tank through an inlet and outlet pipe flange 110 which extends from the upper casing portion 95b.
At the same time that the pump casing 95 is installed, there is also installed in the ceiling of the tank a fill and vent assembly 113 comprised of a flanged, vent pipe 114 and a fill pipe 116 supported within the vent pipe. This may be accomplished in a manner similar to the installation of the casing 95. ln particular, an opening 112 is cut through the ceiling material and receives a gasket 111 and a double flanged collar 118 which are fastened together by a set of bolts 117. The vent pipe 114 extends up through the ceiling structure of the tank and is rigidly held in place by brackets 120 bolted to the support structure 35. The liquid till pipe 116 also extends through the ceiling structure and has at its bottom a splash plate 122 to disperse the cryogenic fluid being fed therethrough.
Once the pump assembly 37 and the fill and vent assembly 113 have been installed through the ceiling structure, the thermal ceiling insulation may be laid. This thermal insulation may bein the same form as that used for insulating the floor and walls of the storage tank and is therefore shown in FIGS. 2 and 7 as several layers of thermally insulating pillows 31. The insulating pillows 31 are laid over the entire ceiling on top of the liner 85 and are preferably packed to the edge of the concrete ring as shown in FIG. 5. A second liner 121, which may be of the same material as the bottom ceiling liner 85 is then installed over the ceiling insulating pillows 119. The ceiling screening 81, and the ceiling liners and 121 are anchored at their peripheries in a groove 82 which extends all around the top of the concrete ring 25. As shown in FIG. 5, the manner of attachment is similar to that used for the tank diaphragm 19. In particular, the screening 81 and the liners 85 and 121 are sandwiched together in the groove 82 with a sealant being applied under each of them, and they are clamped in the groove 82 by means of long arcuate strips 83 fastened down by bolts 84 and nuts 86 distributed along the groove. Additional vapor seals 124 are provided subsequently where the casing and the pipe 113 penetrate the upper liner 121 and the ceiling 33. The two liners 85 and 121 together form a moisture-impervious barrier which fully encloses the ceiling insulating pillows 119. The space between liners 85 and 121, filled with bagged Perlite insulation, is maintained in an inerted gas atmosphere, such as nitrogen.
To protect the ceiling 27 from damage caused by the elements it is advisable to install a protective roof 33. This structure may be made of a flexible, airtight commercially available material, such as vinyl coated nylon fastened at its edges to the outer periphery of the concrete ring by a set of bolts 123 and washers 125. The protective roof 33 may be inert gas supported by maintaining the pressure in the space 127 below it at slightly above atmospheric.
Prior to filling the vessel with cryogenic fluid, a purging of the inner vessel and insulated annular space between outer and inner liners 23 and 17 with inerting gas is accomplished by introducing inerting gas, such as nitrogen, into the inner vessel area first, and then into the annulus through the inlet 69, maintaining a higher pressure in the vessel than in the annulus to avoid displacement of the inner liner 17 from the insulated wall.
The filling of the tank may now begin. It will usually be done through both the fill pipe 116 and the pump housing 95. For this purpose, the pipe flange 110 of the housing 95 is connected to a source of cryogenic fluid as in the till pipe 116. By means of suitable external pumps, cryogenic fluid will then be fed through the pipes 110 and 116. The feeding of the cryogenic fluid through the till pipe 116 has the advantage that the cryogenic fluid is dispersed by means of the splash plate 122 near the top of the tank, thus serving to condense some of the rising flash and vapor which is always generated when cryogenic fluids are transferred. At subsequent times when the level of the cryogenic fluid in the tank has diminished, additional cryogenic fluid may be supplied through the till pipe 116. This may be done either while the submerged pump is inoperative or at the same time that cryogenic fluid is being withdrawn from the tank by means of the pump through the pipe 110.
During the initial filling of the tank the lateral pressure of the liquid being exerted upon the wall of the inner liner 17 will cause that liner to expand, this being made possible by the presence of waffling distributed over its entire surface. The screening 61 will also expand by virtue of the sliding engagement of its individual strips 63, as will the retaining bands 59 by virtue of its ratchet joints 60. The principal reason for this expansion is the compressibility of the insulating pillows 21 which line the wall of the opening 13.
In essence, therefore, the entire double walled insulating bucket, which is comprised of the liners l7 and 23 and of the pillows 21 between them, is compressible, with its inner wall being made expandable for this purpose. However, once the tank assumes its final configuration upon being filled, it will retain that configuration even if the liquid is withdrawn therefrom. This is partly because the insulating pillows 21 do not spring back to their original shape, but remain in their compressed form and partly because the retaining bands maintain their expanded dimension as a result of their one-way ratcheted joints. Thus, by use of compressible insulation and expandable inner wall construction in the tank, a liquid container is provided which can withstand very high liquid pressures by responding flexibly to them.
We claim:
1. An underground storage tank for liquified gas comprising:
a. an opening in an earthen surface;
b. a container made of a laminate and conforming when filled to the shape of said opening;
c. porous reinforcing screening covering the floor and wall of said opening and serving to surround and gird said container; and
d. thermal insulation distributed between said screening and the floor and wall of said opening and a thermally insulated roof covering the top of said opening.
2. The storage tank of claim 1 characterized further by a plurality of expanding retention bands located within said screen at vertically spaced intervals between said screening and the side of said container and pressing said screening against said thermal insulation to hold said thermal insulation in place.
3. The storage tank of claim 2 characterized further by a moisture-impervious liner surrounding the thermal insulation which is distributed between said screening and the floor and wall of said opening and a layer of padding distributed between the wall of said opening and said liner to protect said liner from puncture.
4. In an underground storage tank for liquified gas of the type having an opening in the earths surface and a container in said opening, a thermally insulated roof comprising:
a. a concrete ring surrounding the lip of said opening;
b. a net of steel cables stretched across said opening and supported by said concrete ring;
0. screening of cryogenically stable material extending on top of said net;
d. a moisture-impervious laminate extending on top of said screening; and
e. thermal insulation packed in bags and distributed in several layers on top of said laminate.
5. For use in storing liquified gas in a bucket-shaped opening in the earth's surface a thermally insulated container comprising:
a. a sealed, double walled, liquid and gas impervious bucket-shaped liner covering the floor and wall of said opening;
b. thermal insulation packed in bags and distributed in a continuous layer between the inner and outer walls of said liner;
0. a porous reinforcing screen surrounding the inner wall of said liner; a liquid and gas impervious diaphragm stretched across the mouth of said opening and sealed to the rim of said liner; and
e. thermal insulation distributed in a continuous layer above said diaphragm.
6. For use in storing liquified gas in a bucket-shaped opening in the earth's surface a thermally insulated container comprising:
a. a sealed, double walled, liquid and gas impervious bucket-shaped liner covering the floor and wall of said opening;
b. thermal insulation packed in bags and distributed in a continuous layer between the inner and outer walls of said liner;
c. bracing means for maintaining said bags of insulation upright against the wall of said opening and for reinforcing the inner wall of said liner, said bracing means including,
1. cryogenically stable bucket-shaped screening surrounding the inner wall of said liner, and
2. a series of vertically spaced apart, expandable, cryogenically stable retainer bands between the upright portion of said screening and the upright portion of said inner wall for holding said screening against said insulation;
. a liquid and gas impervious diaphragm stretched across the mouth of said opening and sealed to the rim of said liner; and
e. thermal insulation distributed in a continuous layer above said diaphragm.
7. For use in storing liquified gas in a bucket-shaped opening in the earths surface a thermally insulated container comprising in combination:
a. a bucket-shaped liquid and gas impervious liner within said opening;
b. compressible pillows of thermal insulation distributed in a continuous layer inside said liner along its floor and wall;
c. a bucket-shaped expandable cryogenically stable reinforcing screening inside said layer of bags;
d. a series of vertically spaced apart, expandable, cryogenically stable retaining bands compressed inside said screening;
e. a bucket-shaped liquid and gas impervious liner within said series of retaining bands, made expandable by distributed folds;
f. a liquid and gas impervious diaphragm stretched across the mouth of said opening and sealed to the rim of said inner liner; and
g. thermal insulation distributed in a continuous layer above said diaphragm, said container being characterized in that its inner liner, its retaining bands, and its screening all expand and said compressible pillows are compressed when said tank is initially filled.

Claims (8)

1. An underground storage tank for liquified gas comprising: a. an opening in an earthen surface; b. a container made of a laminate and conforming when filled to the shape of said opening; c. porous reinforcing screening covering the floor and wall of said opening and serving to surround and gird said container; and d. thermal insulation distributed between said screening and the floor and wall of said opening and a thermally insulated roof covering the top of said opening.
2. The storage tank of claim 1 characterized further by a plurality of expanding retention bands located within said screen at vertically spaced intervals between said screening and the side of said container and pressing said screening against said thermal insulation to hold said thermal insulation in place.
2. a series of vErtically spaced apart, expandable, cryogenically stable retainer bands between the upright portion of said screening and the upright portion of said inner wall for holding said screening against said insulation; d. a liquid and gas impervious diaphragm stretched across the mouth of said opening and sealed to the rim of said liner; and e. thermal insulation distributed in a continuous layer above said diaphragm.
3. The storage tank of claim 2 characterized further by a moisture-impervious liner surrounding the thermal insulation which is distributed between said screening and the floor and wall of said opening and a layer of padding distributed between the wall of said opening and said liner to protect said liner from puncture.
4. In an underground storage tank for liquified gas of the type having an opening in the earth''s surface and a container in said opening, a thermally insulated roof comprising: a. a concrete ring surrounding the lip of said opening; b. a net of steel cables stretched across said opening and supported by said concrete ring; c. screening of cryogenically stable material extending on top of said net; d. a moisture-impervious laminate extending on top of said screening; and e. thermal insulation packed in bags and distributed in several layers on top of said laminate.
5. For use in storing liquified gas in a bucket-shaped opening in the earth''s surface a thermally insulated container comprising: a. a sealed, double walled, liquid and gas impervious bucket-shaped liner covering the floor and wall of said opening; b. thermal insulation packed in bags and distributed in a continuous layer between the inner and outer walls of said liner; c. a porous reinforcing screen surrounding the inner wall of said liner; d. a liquid and gas impervious diaphragm stretched across the mouth of said opening and sealed to the rim of said liner; and e. thermal insulation distributed in a continuous layer above said diaphragm.
6. For use in storing liquified gas in a bucket-shaped opening in the earth''s surface a thermally insulated container comprising: a. a sealed, double walled, liquid and gas impervious bucket-shaped liner covering the floor and wall of said opening; b. thermal insulation packed in bags and distributed in a continuous layer between the inner and outer walls of said liner; c. bracing means for maintaining said bags of insulation upright against the wall of said opening and for reinforcing the inner wall of said liner, said bracing means including,
7. For use in storing liquified gas in a bucket-shaped opening in the earth''s surface a thermally insulated container comprising in combination: a. a bucket-shaped liquid and gas impervious liner within said opening; b. compressible pillows of thermal insulation distributed in a continuous layer inside said liner along its floor and wall; c. a bucket-shaped expandable cryogenically stable reinforcing screening inside said layer of bags; d. a series of vertically spaced apart, expandable, cryogenically stable retaining bands compressed inside said screening; e. a bucket-shaped liquid and gas impervious liner within said series of retaining bands, made expandable by distributed folds; f. a liquid and gas impervious diaphragm stretched across the mouth of said opening and sealed to the rim of said inner liner; and g. thermal insulation distributed in a continuous layer above said diaphragm, said container being characterized in that its inner liner, its retaining bands, and its screening all expand and said compressible pillows are compressed when said tank is initially filled.
US00080117A 1970-10-12 1970-10-12 Cryogenic storage tank improvements Expired - Lifetime US3707850A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8011770A 1970-10-12 1970-10-12

Publications (1)

Publication Number Publication Date
US3707850A true US3707850A (en) 1973-01-02

Family

ID=22155368

Family Applications (1)

Application Number Title Priority Date Filing Date
US00080117A Expired - Lifetime US3707850A (en) 1970-10-12 1970-10-12 Cryogenic storage tank improvements

Country Status (1)

Country Link
US (1) US3707850A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3933628A (en) * 1974-07-10 1976-01-20 Bio-Gas Of Colorado, Inc. Method and apparatus for the anaerobic digestion of decomposable organic materials
US4041722A (en) * 1975-09-26 1977-08-16 Pittsburgh-Des Moines Steel Company Impact resistant tank for cryogenic fluids
US4860544A (en) * 1988-12-08 1989-08-29 Concept R.K.K. Limited Closed cryogenic barrier for containment of hazardous material migration in the earth
WO1990006480A1 (en) * 1988-12-08 1990-06-14 Concept R.K.K. Limited Closed cryogenic barrier for containment of hazardous material in the earth
US5050386A (en) * 1989-08-16 1991-09-24 Rkk, Limited Method and apparatus for containment of hazardous material migration in the earth
US5447389A (en) * 1993-01-15 1995-09-05 Abeltech Incorporated Insulation system for soil
US5833401A (en) * 1995-04-07 1998-11-10 Abeltech Geoinsulation blanket and system for soil
US6076313A (en) * 1998-07-06 2000-06-20 Earthsource Technologies, Inc. Facility for maintaining an item in a controlled environment
US6682259B1 (en) 2000-02-04 2004-01-27 Earthsource Technologies Structure having an insulated support assembly
US20060037278A1 (en) * 2003-04-10 2006-02-23 Crane Stephen D Fluid containment vessel, method of constructing fluid containment vessel, in particular chemical-resistant concrete liquid containment vessel
WO2007084007A1 (en) * 2006-01-18 2007-07-26 Norsk Hydro Asa Lng storage with the storage tank provided in a cavern
US20100187237A1 (en) * 2008-09-23 2010-07-29 Alec Nelson Brooks Cryogenic Liquid Tank
US20190107241A1 (en) * 2017-10-09 2019-04-11 Lmk Technologies Llc Grooved Sealing Member for Sealing Pipes and Other Underground Structures and Method of Using
US11359829B2 (en) 2018-07-03 2022-06-14 Rupert R. Thomas, Sr. Quasi-equilibrium atmospheric modular thermodynamic system and method

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3241274A (en) * 1963-05-24 1966-03-22 Conch Int Methane Ltd Roof structure for ground reservoir
US3249251A (en) * 1963-01-07 1966-05-03 Conch Int Methane Ltd Thermally insulated and counterweighted roof
US3326011A (en) * 1965-10-21 1967-06-20 Cryogenic Entpr Ltd Cryogenic storage facility
US3360941A (en) * 1964-12-15 1968-01-02 Conch Int Methane Ltd Reservoir with seal for liquefied gas storage
US3418812A (en) * 1966-02-14 1968-12-31 Inst Gas Technology Insulating means for underground storage system
US3504496A (en) * 1968-09-30 1970-04-07 Exxon Research Engineering Co Storage tank
US3516568A (en) * 1966-07-01 1970-06-23 Nat Res Dev Storage of liquids

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3249251A (en) * 1963-01-07 1966-05-03 Conch Int Methane Ltd Thermally insulated and counterweighted roof
US3241274A (en) * 1963-05-24 1966-03-22 Conch Int Methane Ltd Roof structure for ground reservoir
US3360941A (en) * 1964-12-15 1968-01-02 Conch Int Methane Ltd Reservoir with seal for liquefied gas storage
US3326011A (en) * 1965-10-21 1967-06-20 Cryogenic Entpr Ltd Cryogenic storage facility
US3418812A (en) * 1966-02-14 1968-12-31 Inst Gas Technology Insulating means for underground storage system
US3516568A (en) * 1966-07-01 1970-06-23 Nat Res Dev Storage of liquids
US3504496A (en) * 1968-09-30 1970-04-07 Exxon Research Engineering Co Storage tank

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3933628A (en) * 1974-07-10 1976-01-20 Bio-Gas Of Colorado, Inc. Method and apparatus for the anaerobic digestion of decomposable organic materials
US4041722A (en) * 1975-09-26 1977-08-16 Pittsburgh-Des Moines Steel Company Impact resistant tank for cryogenic fluids
US4860544A (en) * 1988-12-08 1989-08-29 Concept R.K.K. Limited Closed cryogenic barrier for containment of hazardous material migration in the earth
WO1990006480A1 (en) * 1988-12-08 1990-06-14 Concept R.K.K. Limited Closed cryogenic barrier for containment of hazardous material in the earth
US4974425A (en) * 1988-12-08 1990-12-04 Concept Rkk, Limited Closed cryogenic barrier for containment of hazardous material migration in the earth
US5050386A (en) * 1989-08-16 1991-09-24 Rkk, Limited Method and apparatus for containment of hazardous material migration in the earth
US5447389A (en) * 1993-01-15 1995-09-05 Abeltech Incorporated Insulation system for soil
US5833401A (en) * 1995-04-07 1998-11-10 Abeltech Geoinsulation blanket and system for soil
US6076313A (en) * 1998-07-06 2000-06-20 Earthsource Technologies, Inc. Facility for maintaining an item in a controlled environment
US6682259B1 (en) 2000-02-04 2004-01-27 Earthsource Technologies Structure having an insulated support assembly
US20060037278A1 (en) * 2003-04-10 2006-02-23 Crane Stephen D Fluid containment vessel, method of constructing fluid containment vessel, in particular chemical-resistant concrete liquid containment vessel
WO2007084007A1 (en) * 2006-01-18 2007-07-26 Norsk Hydro Asa Lng storage with the storage tank provided in a cavern
US20100187237A1 (en) * 2008-09-23 2010-07-29 Alec Nelson Brooks Cryogenic Liquid Tank
US8960482B2 (en) 2008-09-23 2015-02-24 Aerovironment Inc. Cryogenic liquid tank
US9829155B2 (en) 2008-09-23 2017-11-28 Aerovironment, Inc. Cryogenic liquid tank
US10584828B2 (en) 2008-09-23 2020-03-10 Aerovironment, Inc. Cryogenic liquid tank
US11346501B2 (en) 2008-09-23 2022-05-31 Aerovironment, Inc. Cryogenic liquid tank
US20190107241A1 (en) * 2017-10-09 2019-04-11 Lmk Technologies Llc Grooved Sealing Member for Sealing Pipes and Other Underground Structures and Method of Using
US10436374B2 (en) * 2017-10-09 2019-10-08 Lmk Technologies, Llc Grooved sealing member for sealing pipes and other underground structures and method of using
US11359829B2 (en) 2018-07-03 2022-06-14 Rupert R. Thomas, Sr. Quasi-equilibrium atmospheric modular thermodynamic system and method

Similar Documents

Publication Publication Date Title
US3701262A (en) Means for the underground storage of liquified gas
US3707850A (en) Cryogenic storage tank improvements
US3407606A (en) Underground cavern storage for liquefied gases near atmospheric pressure
US4041722A (en) Impact resistant tank for cryogenic fluids
US3092933A (en) Storage structure
US3196622A (en) Cryogenic storage tank
US3047184A (en) Storage tank
US4136493A (en) Supporting structure for containers used in storing liquefied gas
EP0192308B1 (en) A reservoir for placing in a fixed position on the ground and method for manufacturing same
US3195310A (en) Storage installation and sealing method therefor
EP2668440B1 (en) Gas accumulator
US3987925A (en) Insulated tank
WO2006046872A1 (en) Tank for storage of lng or other cryogenic fluids
US5058330A (en) Self-supporting membrane structure for use on the moon
US3361284A (en) Thermal insulation construction
US3854265A (en) Method for constructing an underground storage tank
US3326011A (en) Cryogenic storage facility
US4542626A (en) Method and apparatus for underground storage of ammonia and analogous products
US3175370A (en) Roofs for reservoirs
US4717285A (en) Cistern for liquid or gas, constructed of reinforced concrete
NO115803B (en)
US3241274A (en) Roof structure for ground reservoir
US4112690A (en) Method and construction of underground tank well
NO115397B (en)
US3300982A (en) Storage of volatile liquids