US3863408A - Prestressed concrete tanks for liquid natural gas tankers - Google Patents

Prestressed concrete tanks for liquid natural gas tankers Download PDF

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US3863408A
US3863408A US292727A US29272772A US3863408A US 3863408 A US3863408 A US 3863408A US 292727 A US292727 A US 292727A US 29272772 A US29272772 A US 29272772A US 3863408 A US3863408 A US 3863408A
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United States
Prior art keywords
tank
wall
stiffening
steel
disks
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US292727A
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John J Closner
Tadeusz Josef Marchaj
Sven Hjalmar Wichman
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Preload Technology Inc
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Preload Technology Inc
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Priority to US292727A priority Critical patent/US3863408A/en
Priority to GB3528773A priority patent/GB1437411A/en
Priority to ES418215A priority patent/ES418215A1/en
Priority to IT28257/73A priority patent/IT1001534B/en
Priority to JP10256673A priority patent/JPS5345925B2/ja
Priority to SE7313106A priority patent/SE402438B/en
Priority to DE19732348656 priority patent/DE2348656A1/en
Priority to US532016A priority patent/US3926134A/en
Application granted granted Critical
Publication of US3863408A publication Critical patent/US3863408A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B25/00Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby
    • B63B25/02Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods
    • B63B25/08Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid
    • B63B25/12Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed
    • 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
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/025Bulk storage in barges or on ships
    • 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
    • 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/016Preventing slosh
    • 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
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/0105Ships
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S220/00Receptacles
    • Y10S220/901Liquified gas content, cryogenic

Definitions

  • the tank wall is made up of a series of concrete, modular tank wall sections which are circumferentially [22] Flled: Sept 271972 prestressed by steel tendons and which have holes [21] Appl. No.: 292,727 therein for through-passage of axial prestressing tendons.
  • a steel sheath anchored to the concrete wall provides a secondary barrier against leakage of the liq- [52] U.S. Cl 52/224, 52/227, 220/3 uid natural gas cargo within the tank.
  • the modular Cl- Wall Sections are separated co crete or Steel Stiffen [58] Fleld of Search 220/5 9 52/224 ing disks.
  • the tank is formed by alternately position- 52/227 137/357 ing a number,of modular wall sections and stiffening disks.
  • Flat, concrete, stiffening plates which are inte- References cued gral with the modular tank wall sections and are UNlTED STATES PATENTS radially-axially positioned within the tank further 2,360,391 10/1944 Birchall 220/3 stiffen the structure.
  • the walls and the stiffening 3,256,069 6/1966 Peterson 220/3 X plates are axially prestressed and the heads are at- Bellier X tached
  • the tank is upported on the annular stiffen- 3,329,297 7/1967 Jordan 220/5 A ing disks which are joined to the tank wall.
  • the tank Fl'Ohly makes efficient use of h Vessels cubic a d is p FOREIGN PATENTS OR APPLICATIONS sive to construct.
  • p FOREIGN PATENTS OR APPLICATIONS sive to construct By preforming and prestressing the 1,524,285 4/1968 France 52/227 modular units and thereafter erecting them p y at 214,461 8/1967 Sweden 52/224 the ship-building site or at a removed fitting out S Primary ExaminerAlfred C. Perham Attorney, Agent, or Firm-Curtis, Morris & Safford important economies are achieved.
  • Liquid natural gas is comprised of a mixture of primarily methane, with lesser amounts of ethane, propane and butane. Although the actual composition may vary according to source and with the degree of processing during liquefication, typical liquefied natural gas products have a boiling point, at atmospheric pressure of approximately 250F. The natural gas is transported at these temperatures and at atmospheric pressures and the cargo containment systems must be designed for service at these temperatures as well as for cool-down and warm-up cycles.
  • the prismatic free-standing tank has been used more than the others. Generally, they are comprised of 9% nickel steel, stainless steel or aluminum alloy and their configuration roughly follows the interior configuration of the vessel. They include a secondary barrier between the tank and the steel hull of the vessel. Among the advantages of such tanks is that they are relatively efficient in terms of utilizing the internal volume (cubic) of the vessel. The center of gravity of such tanks is generally fairly low so that the amount of ballast required to trim the vessel is not excessive.
  • a very substantial disadvantage of prismatic, freestanding tanks stems from their configuration. To follow the shape of the hull structure, three corner systems are used, and although such structures are analyzable, design problems are more difficult than in tanks of more simple configuration. The many structural details and welded connections involved and the unknown stresses which develop due to thermal contraction of the steel, torsion of the hull, impact on the hull, motion of the vessel in a seaway and movement of the liquid within the tank, lead to a variety of structural problems. If simpler configurations, such as vertical cylinders are used, there is an attendant sacrifice in the efficiency of space usage within the vessel. Due to these problems, prismatic free-standing tanks tend to have a relatively higher weight and cost than do other types of tanks now in use.
  • Spherical, free-standing tanks have a salient advantage in that they are most easily analyzed for stresses, and accordingly spherical tank systems can be constructed having no secondary barrier or only a partial secondary barrier.
  • a related advantage is that the spherical tanks can be relatively easily fabricated; there is no necessity for internal structural members to ensure the integrity of the tank; and there are no unforeseen problems of metal fatigue due to unforeseen stresses.
  • spherical tanks have certain disadvantages primary among which is their inefficiency in regard to use of the internal cubic of the marine vessel. There is a greater amount of waste space within the hull although this is partially offset by a greater availability of hull volume for carriage of ballast. They are also relatively difficult to support, have a relatively high vertical center of gravity and extend above the deck level causing operational problems.
  • Membrane tanks which generally include two thin, flexible membranes comprised of, for example, stainless steel, and at least two layers of insulation separating the barriers from one another and the outer barrier from the steel hull of the vessel, have certain very significant advantages. Their primary advantage is that their configuration most closely follows that of the outer steel hull of the vessel and they therefore are most efficient with respect to use of the internal cubic of the vessel.
  • the construction cost of membrane tanks is relatively less than that of free-standing systems be cause the thickness of the membranes is considerably less than that of the steel plate used in prismatic tanks. Thus, the total material cost is drastically lower than for prismatic tanks although the unit cost for the membrane material may be slightly higher.
  • the smaller mass of the membranes also results in a substantially shorter cool-down time as compared with prismatic tanks.
  • stallation costs for membrane tanks tend to be somewhat less than for prismatic tanks largely because the weight of the materials used is less.
  • the primary disadvantage of membrane tanks is that they are virtually impossible to analyze structurally. Unknown problems of fatigue and stress concentration lead to increased risks, including the risk of damage to the primary barrier in the event of a ship collision.
  • the free-standing tanks, particularly the spherical tanks are less subject to damage in the event of collision because they have greater structural integrity and are separated from the hull by additional space.
  • the relatively weak membrane is also subject to damage during construction and during maintenance operations. Membranes can be damaged by overpressurization of the vapor space behind the primary barrier, by movement of liquid within the tank and by development of fatigue cracks or stresses within the hull of the vessel. For these reasons, construction of membrane tanks is more closely supervised by the authorities and must be attended with more care than with free-standing tanks.
  • a tank for containment of cryogenic liquid for placement within a marine transportation vessel which comprises a cylindrical tank wall, of any suitable curved cross-section for tank service but preferably of circular or elliptical cross-section comprised of prestressed concrete, and end closure means such as heads attached thereto.
  • the cylindrical tank wall is prestressed by steel tendons positioned essentially circumferentially about its exterior surface and by other steel tendons, positioned within the tank wall itself, and oriented essentially parallel to the axis of the tank.
  • T0 provide stiffness
  • one or more annular stiffening disks are positioned coaxially within the wall of the tank and are attached thereto.
  • the stiffening disks are formed from steel or concrete and a portion thereof may extend past the exterior surface of the tank wall to provide support or retainer posts for the tank. Desirably a plurality of these stiffening disks are attached at intermediate locations between the heads of the tank.
  • a series of planar stiffening plates (or ribs) are positioned in a radial-axial orientation with respect to the tank wall and are connected to the stiffening disks and to the interior of the tank wall.
  • the stiffening plates are flat, prestressed concrete plates and they, as well as the cylindrical tank wall have essentially axially positioned pre stressing tendons therein.
  • a steel sheath may be anchored to the outer surface of the cylindrical wall. This sheath may be of carbon steel since it acts compositely with the prestressed concrete, and thus is not subject to tensile stresses when subjected to the low temperatures of the cryogenic liquid within the concrete container.
  • the tank wall is concrete and of circular cross-section.
  • a series of axial holes are located within the tank wall through which steel prestressing tendons are passed.
  • a carbon steel sheath is anchored to the exterior of the tank wall by studs and external to the sheath are prestressing tendons wrapped essentially circumferentially. Either one continuous tendon in a helical wind or a series of individual tendons can be used.
  • Annular concrete stiffening disks are positioned coaxially within the tank wall and are attached to the steel sheath. The disks have holes along an outer circle and along certain radii, for through-passage of axially oriented prestressing tendons.
  • stiffening plates Between the several stiffening disks and abutting their surfaces are a plurality of flat, concrete, stiffening plates which are positioned radially-axially with respect to the tank. These stiffening plates abut the interior of the tank wall at their radial outermost extension. Located within these stiffening plates are axially oriented holes for prestressing tendons. Defining the remainder of the tank structure are steel heads which are attached to the end-most stiffening disks. lnlet and outlet means are provided for the cryogenic liquid.
  • the tank In its erected configuration, the tank is prestressed both circumferentially and axially, the circumferential prestressing is by means of the tendons positioned around the circumference of the tank and the axial prestressing is by means of the tendons passing through the holes in the tank wall.
  • the stiffening plates are also prestressed by tendons which pass through an axial series of plates located between adjacent stiffening disks, the tendons passing through the radially located holes in those disks.
  • the head is attached to the end stiffening disks and the toroidal section of the head is further anchored to the cylindrical wall by the axial prestressing tendons and by tendons external to the tank which are oriented diagonally of the tank axis.
  • the advantages of the tank configuration of this invention are many.
  • the circular or elliptical crosssection, particularly in a horizontal orientation, makes very efficient use of the internal cubic of conventional ships or barges.
  • Prestressed concrete is markedly more economical than the expensive alloy plates of freestanding, prismatic tanks or the even more expensive materials and complicated construction techniques associated with membrane tanks.
  • Since the configuration of the tank is relatively simple, the structure is a fully determinant one, and does not require a secondary barrier to protect the ship hull and the cargo from one another. With the steel sheath a measure of secondary barrier is provided, nonetheless.
  • the tank configuration of the invention provides all of the advantages of a two barrier system while being fully determinant and thus subject to the less rigid design controls promulgated for determinant systems.
  • the structural integrity of the system provides a very substantial measure of safety for tank and cargo, should the vessel be involved in a collision and lends a stiffness to the ship structure.
  • the relatively high weight of the concrete is an advantage insofar as it substantially reduces the ballast requirements of the vessel and lowers the center of gravity.
  • Still a further advantage of the tank configuration is that it is relatively easily positioned within a supporting cradle in the ship structure and can be firmly positioned therein without requiring elaborate support systems.
  • a modular wall component is fabricated.
  • the component is comprised of a length of concrete, cylindrical tank wall of suitable curved cross-section having axially oriented holes passing through its length, a steel sheath anchored to its exterior surface and prestressing tendons wrapped essentially circumferentially about the exterior of the steel sheath.
  • the concrete stiffening plates are integrally cast with the modular tank wall, and axial holes are provided therein.
  • a tank having the configuration described above can be relatively easily constructed within a conventional steel or concrete vessel.
  • the vessel will include a grid-like cradle which comprises transverse and axial structural members positioned in registration with the lower stiffening disks and the lower stiffening plates respectively.
  • the transverse members are provided with a balsa wood support upon which the exterior portion of a stiffening disk is mounted.
  • the axial structural members are positioned beneath the lower stiffening plates within the tank.
  • the tank is fixed to its cradle at only one position along the axis of the tank, i.e., at one transverse structural member and is slidably supported on several other structural members.
  • the purpose of the fixed support is to preclude axial movement of the tank within the vessel and the purpose of the sliding supports is to permit axial contraction and expansion of the tank during cool-down and warm-up. Chocks may be provided at the sides and top of the tank to prevent it from rotating. However, the chocks should permit axial expansion and contraction of the tank.
  • the invention also embraces the method for forming the modular component for the cryogenic tank.
  • a length of concrete, cylindrical tank wall of circular or elliptical cross-section is cast with axially oriented holes extending through it and radial-axial stiffening plates extending inwardly from .its inner surface at spaced locations.
  • a steel sheath is anchored to its exterior surface. The steel sheath may be studded to the concrete, as it is poured, according to conventional techniques.
  • the tank wall is prestressed by wrapping one or more steel tendons, in tension, about the outer surface of the steel sheath.
  • the latter step may be carried out by mounting the cast wall on a turntable and rotating the turntable while tendons are wrapped about the tank wall.
  • a carriage may be supported from the tank wall and moved about the circumference thereof while wrapping a tendon thereabout, as is conventional procedure in the construction of stationary tanks.
  • a group of components positioned one above the other may be prestressed in a single operation.
  • Modular components may be formed by conventional techniques in the shipyard, but at a distance from the site of the ship construction, or at a remote location.
  • the erection of the tank is simplified because the modular components should be sized so as to be of such weight as will be within the lifting capacity of available lifting apparatus at ship building sites.
  • FIG. 1 is a simplified, side elevation view of a steel tanker containing five liquid natural gas tanks according to the present invention
  • FIG. 2 is a side elevation view of one of the tanks shown in FIG. 1;
  • FIG. 3 is a fore and aft elevation view, in section, of the tank of FIG. 2 taken along lines 3-3 of FIG. 2;
  • FIG. 4 is a partial section view of the tank shown in FIG. 2, showing details of the modular wall construction
  • FIG. 5 is a partial fore and aft elevation view of the portion of the modular wall construction of FIG. 4 taken along lines 5--5 of FIG. 4;
  • FIG. 6 is a simplified, exploded, view of the modular components of the tank, showing their juxtaposition prior to assembly;
  • FIG. 7 is a view of the tank in partially assembled state
  • FIG. 9 is a detailed elevation view of a sliding support pedestal for the tank of FIG. 2.
  • reference numeral 10 refers generally to a conventional tanker.
  • Reference numeral l2 refers to a hull and reference numeral 14 to a tanker super structure.
  • Reference numerals l6, 18, 20, 22 and 24 refer to five, horizontally oriented tanks for containment of cryogenic liquid having the configuration more fully described below.
  • tank 16 is comprised of a cylindrical tank wall of circular cross-section 26 and includes heads 28 and 30.
  • Head 28 comprises a central dome 32 and a torus 34.
  • this head design is optional and may be employed in large tanks to reduce the amount of expensive alloy metal required.
  • the heads may be elliptical or hemispherical.
  • Inlet and outlet means for the cryogenic liquid are not shown, however, they may be provided at suitable locations in the top of the tank or through the steel heads.
  • cylindrical tank 16 is supported within hull 12 on a cradle 36 which includes several parallel, transverse, partially circular support members 38 and three parallel, axial support members 40, 42 and 44.
  • the entire tank is surrounded by insulation 46 which may be minneral wool, perlite or other suitable insulating material.
  • the tank 16 is prevented from to tating within hull 12 by means of a chock 48 which includes a bracket 50 attached to the top of the tank having a recess section 52 in which is placed restraining member 54 attached to the hull or deck structure. Chocks may also be attached to the sides of the tank.
  • Tank 16 is comprised of a plurality of modular, concrete wall components 60a, 60b, 600, etc. Each of these modular wall components is cylindrical and of circular cross-section and has a plurality of axial holes passing therethrough designated by reference numeral 62. Located within axial holes 62 are prestressing tendons 64. Located externally of modular components 60a, 60b, 600, etc. are steel sheaths 65a, 65b and 650, etc. which pass circumferentially around the exterior surface of the concrete. The steel sheaths are anchored to the concrete wall by means of studs 66. Located on the FIG. 8 is a detailed view of a fixed support pedestal for the tank of FIG. 2; and
  • prestressing tendons 68 which pass circumferentially about the sheaths and are in tension causing the concrete and steel sheath to act compositely.
  • a series of discrete tendons may be used or helically wound tendons may be employed.
  • a layer of gunnite or other suitable bitumastic material or plastic coating such as epoxy serves as protective overcover for the circumferential prestressing tendons as designated by reference numeral 70.
  • stiffening plates 74 are provided. Each of these stiffening plates are positioned both radially and axially with respect to tank 16. They are integral with the inner surface of the cylindrical tank wall at their radial outermost extension 76 and abut, at their axial extensions 78 and 80, the two stiffening disks between which they are located, i.e., in FIG. 4, disks 72a and 72b. These stiffening plates have essentially axially oriented holes therein designated by reference numeral 82 through which prestressing tendons 84 are passed.
  • Suitable holes are provided in stiffening disks 72 for through-passage of tendons 64 through the holes 62 in modular wall components 60, and through an axial series of stiffening plates 74. Prestressing tendons 84 terminate in suitable tensioning heads 86 on the end most stiffening disk, 72a.
  • stiffening disks 72 are spaced from one another by uniform modular wall components 60 and the rows of stiffening plates 74 are positioned at a uniform angular distance from one another around the inner circumference of the tank.
  • These outer extensions of the disks may form support posts or positioning rails for the tank, and as seen in FIG. 3, these posts are received in cradle 36 in transverse structural member 38.
  • the tank configuration of this invention is most easily assembled by positioning modular wall components 100, comprised of cast concrete wall sections of circular cross-section having holes 102 therein and circumferential prestressing tendons 104, alternately with stiffening disks 106 which have circumferential holes 108 and radial holes 110 for through-passage of prestressing tendons.
  • the axial prestressing tendons which pass through the wall of the concrete tank are designated by reference numerals and the prestressing tendons which pass through the series of stiffening plates are designated by reference numerals 122.
  • the interior of the assembled tank has a partially compartmentalized configuration, which is of advantage in reducing sloshing when the tank is filled.
  • heads are fixed to either end of the assembled cylindrical structure as shown in FIG. 2.
  • the torus may be further anchored to the assembled cylindrical wall by prestressing tendons and 127 which are oriented diagonally of the tank volume enclosed by the torus.
  • FIG. 8 shows a fixed support for the tank.
  • Reference numeral 38 represents a transverse support member for the tank.
  • support member 38 Within support member 38 is a recess 39 containing balsa wood 41 which provides a support for the tank.
  • the lower extension of stiffening disk 72 on one end of the tank is thus fuxed with respect to the axis of the tank and accordingly the tank cannot move when affected by impacts due to waves or other disturbances encountered by the vessel.
  • reference numeral 138 refers to a transverse, cradle support member, of partial circular shape, having a recess at 139 filled with balsa 141.
  • the lower extension of the stiffening disk 172 sits on the upper surface 143 of balsa 141 and can slide across that surface under the influence of contraction and expansion forces encountered in the cool-down and warm-up of the tank.
  • a tank for cryogenic adapted for placement within a marine transportation vessel comprising:
  • a concrete, cylindrical tank wall having a plurality of steel prestressing tendons located therein in axial orientation;
  • stiffening plates positioned radiallyaxially with respect to said tank and abutting at both axial extensions thereof, said stiffening disks and at their radial outermost extension, the said cylindrical tank wall, said stiffening plates having essentially axially oriented prestressing tendons therein;
  • a modular component for construction of a tank for cryogenic liquids for placement within a marine transportation vessel comprising:
  • a. a plurality of prestressed concrete wall modules comprising:
  • annular stiffening disks positioned between adjacent wall modules, said disks having holes therein for through-passage of said axially oriented prestressing tendons;
  • a tank for cryogenic liquids comprising:
  • a tank as recited in claim 7 having a plurality of said stiffening disks attached intermediate to said end closures of said tank.
  • a tank as recited in claim 7 having a steel sheath anchored to the outer surface of said cylindrical wall.
  • a tank for cryogenic liquids comprising:
  • At least one annular stiffening disk positioned coaxially within the said cylindrical tank wall intermediate the said end closures and attached to said wall.

Abstract

A tank for cryogenic liquids, specifically liquid natural gas, adapted for placement within a conventional marine transportation vessel is shown. The tank is preferably cylindrical and of circular cross section and is comprised of prestressed concrete with steel heads. The tank wall is made up of a series of concrete, modular tank wall sections which are circumferentially prestressed by steel tendons and which have holes therein for through-passage of axial prestressing tendons. A steel sheath anchored to the concrete wall provides a secondary barrier against leakage of the liquid natural gas cargo within the tank. The modular wall sections are separated by concrete or steel stiffening disks. The tank is formed by alternately positioning a number of modular wall sections and stiffening disks. Flat, concrete, stiffening plates which are integral with the modular tank wall sections and are radially-axially positioned within the tank further stiffen the structure. The walls and the stiffening plates are axially prestressed and the heads are attached. The tank is supported on the annular stiffening disks which are joined to the tank wall. The tank makes efficient use of the vessels cubic and is inexpensive to construct. By preforming and prestressing the modular units and thereafter erecting them rapidly at the ship-building site or at a removed fitting out site, important economies are achieved.

Description

United States Patent Closner et al. Feb. 4, 1975 [54] PRESTRESSED CONCRETE TANKS FOR LIQUID NATURAL GAS TANKERS [57 ABSTRACT [75] Inventors: John Closner Dougiaston; A tank for cryogenic liquids, specifically liquid natural Tadeus? Josef Mail-ch31 New York gas, adapted for placement within a conventional ma- Sven Jalmar Yaphank rine transportation vessel is shown. The tank is preferably cylindrical and of circular cross section and is [73] Assignee: Preload Technology, Inc., Gard n comprised of prestressed concrete with steel heads.
City, NY. The tank wall is made up of a series of concrete, modular tank wall sections which are circumferentially [22] Flled: Sept 271972 prestressed by steel tendons and which have holes [21] Appl. No.: 292,727 therein for through-passage of axial prestressing tendons. A steel sheath anchored to the concrete wall provides a secondary barrier against leakage of the liq- [52] U.S. Cl 52/224, 52/227, 220/3 uid natural gas cargo within the tank. The modular Cl- Wall Sections are separated co crete or Steel Stiffen [58] Fleld of Search 220/5 9 52/224 ing disks. The tank is formed by alternately position- 52/227 137/357 ing a number,of modular wall sections and stiffening disks. Flat, concrete, stiffening plates which are inte- References cued gral with the modular tank wall sections and are UNlTED STATES PATENTS radially-axially positioned within the tank further 2,360,391 10/1944 Birchall 220/3 stiffen the structure. The walls and the stiffening 3,256,069 6/1966 Peterson 220/3 X plates are axially prestressed and the heads are at- Bellier X tached The tank is upported on the annular stiffen- 3,329,297 7/1967 Jordan 220/5 A ing disks which are joined to the tank wall. The tank Fl'Ohly makes efficient use of h Vessels cubic a d is p FOREIGN PATENTS OR APPLICATIONS sive to construct. By preforming and prestressing the 1,524,285 4/1968 France 52/227 modular units and thereafter erecting them p y at 214,461 8/1967 Sweden 52/224 the ship-building site or at a removed fitting out S Primary ExaminerAlfred C. Perham Attorney, Agent, or Firm-Curtis, Morris & Safford important economies are achieved.
14 Claims, 9 Drawing Figures PATENTED FEB U975 sum 3 or e Z I J PATENIED rm mars .SHEET t 0F 6 PAIENTED 4W5 3. 863 A08 sum 5 or e s Q s PATENTEDFEB mm SHEEI 8 OF 6 PRESTRESSED CONCRETE TANKS FOR LIQUID NATURAL GAS TANKERS This invention relates broadly to the transport of cryogenic liquids in marine vessels. More specifically, this invention relates to use of inexpensive prestressed concrete tanks in steel or concrete barges and ships for carrying liquefied natural gas. Even more specifically, this invention relates to a modular tank configuration for liquid natural gas tanks which provides exceptional safety features and economies in the design, construction and operation of marine transport vessels.
The art of transporting cryogenic liquids in ships and barges has developed rapidly in the past several years. The accelerating world-wide demand for liquid natural gas has resulted in development of ever larger barges and tankers and has given rise to several different types of cargo containment systems. World wide fuel shortages have now been foreseen and in view of the ecological acceptability of natural gas as a fuel, the demand for it will certainly increase. Thus, the art is faced with a need to develop safe and economical systems for liquid natural gas containment and transport.
BACKGROUND OF INVENTION AND PRIOR ART Liquid natural gas is comprised of a mixture of primarily methane, with lesser amounts of ethane, propane and butane. Although the actual composition may vary according to source and with the degree of processing during liquefication, typical liquefied natural gas products have a boiling point, at atmospheric pressure of approximately 250F. The natural gas is transported at these temperatures and at atmospheric pressures and the cargo containment systems must be designed for service at these temperatures as well as for cool-down and warm-up cycles.
It has long been recognized that carbon steels, which are used commonly in ship building are relatively weak at cryogenic temperatures. For this reason, the tanks are typically made of nickel steel or aluminum alloys which have superior strength characteristics at low temperatures and serve to safely contain the liquid natural gas cargo, protecting the hull of the vessel from exposure to extremely low temperatures. Several configurations of tanks, in ships and barges, have been developed, many of which provide a double barrier between the cargo and the external steel hull to protect the hull from exposure to low temperatures in the event of a rupture of the cargo containment system; and numerous intricate configurations have been developed for insulating the outer hull from the cryogenic temperatures. Configurations have also been developed to protect the cargo containment systems from rupture in the event of a collision which damages the external hull of the vessel.
Conventional liquid natural gas containment systems heretofore have fallen within three general catgeories: prismatic free-standing tanks. spherical free-standing tanks and membrane tanks. Although each of the several types of tanks and the several design variants thereof have been used with success in the past, and although each type of tank has certain advantages peculiar to it, each likewise has certain disadvantages. In evaluating each of the several alternative designs, many factors must be taken into consideration including the initial cost of the containment systems, the overall life of the system, operational safety, ease and time of construction, unit cost per cargo-mile and many other factors.
The prismatic free-standing tank has been used more than the others. Generally, they are comprised of 9% nickel steel, stainless steel or aluminum alloy and their configuration roughly follows the interior configuration of the vessel. They include a secondary barrier between the tank and the steel hull of the vessel. Among the advantages of such tanks is that they are relatively efficient in terms of utilizing the internal volume (cubic) of the vessel. The center of gravity of such tanks is generally fairly low so that the amount of ballast required to trim the vessel is not excessive.
A very substantial disadvantage of prismatic, freestanding tanks stems from their configuration. To follow the shape of the hull structure, three corner systems are used, and although such structures are analyzable, design problems are more difficult than in tanks of more simple configuration. The many structural details and welded connections involved and the unknown stresses which develop due to thermal contraction of the steel, torsion of the hull, impact on the hull, motion of the vessel in a seaway and movement of the liquid within the tank, lead to a variety of structural problems. If simpler configurations, such as vertical cylinders are used, there is an attendant sacrifice in the efficiency of space usage within the vessel. Due to these problems, prismatic free-standing tanks tend to have a relatively higher weight and cost than do other types of tanks now in use.
Spherical, free-standing tanks have a salient advantage in that they are most easily analyzed for stresses, and accordingly spherical tank systems can be constructed having no secondary barrier or only a partial secondary barrier. A related advantage is that the spherical tanks can be relatively easily fabricated; there is no necessity for internal structural members to ensure the integrity of the tank; and there are no unforeseen problems of metal fatigue due to unforeseen stresses.
On the other hand, spherical tanks have certain disadvantages primary among which is their inefficiency in regard to use of the internal cubic of the marine vessel. There is a greater amount of waste space within the hull although this is partially offset by a greater availability of hull volume for carriage of ballast. They are also relatively difficult to support, have a relatively high vertical center of gravity and extend above the deck level causing operational problems.
Membrane tanks, which generally include two thin, flexible membranes comprised of, for example, stainless steel, and at least two layers of insulation separating the barriers from one another and the outer barrier from the steel hull of the vessel, have certain very significant advantages. Their primary advantage is that their configuration most closely follows that of the outer steel hull of the vessel and they therefore are most efficient with respect to use of the internal cubic of the vessel. The construction cost of membrane tanks is relatively less than that of free-standing systems be cause the thickness of the membranes is considerably less than that of the steel plate used in prismatic tanks. Thus, the total material cost is drastically lower than for prismatic tanks although the unit cost for the membrane material may be slightly higher. The smaller mass of the membranes also results in a substantially shorter cool-down time as compared with prismatic tanks. In-
stallation costs for membrane tanks tend to be somewhat less than for prismatic tanks largely because the weight of the materials used is less.
The primary disadvantage of membrane tanks, is that they are virtually impossible to analyze structurally. Unknown problems of fatigue and stress concentration lead to increased risks, including the risk of damage to the primary barrier in the event of a ship collision. The free-standing tanks, particularly the spherical tanks are less subject to damage in the event of collision because they have greater structural integrity and are separated from the hull by additional space. The relatively weak membrane is also subject to damage during construction and during maintenance operations. Membranes can be damaged by overpressurization of the vapor space behind the primary barrier, by movement of liquid within the tank and by development of fatigue cracks or stresses within the hull of the vessel. For these reasons, construction of membrane tanks is more closely supervised by the authorities and must be attended with more care than with free-standing tanks.
In view of the many, and often conflicting, design, construction and operational factors which must be considered in the development of tanks for cryogenic liquids in marine vessels, there is considerable room for improvement over conventional containment systems. Several, but by no means all of the objectives facing the art are hereinafter set forth.
OBJECTIVES It is the primary object of this invention to provide a tank construction for marine transport vessels having a configuration which makes maximum use of the internal volume of the marine vessel.
It is another primary object of this invention to provide a construction for such tanks which requires relatively inexpensive materials and is relatively easy to fabricate and erect within a conventional concrete or steel ship or barge.
It is still a further primary object of this invention to provide a tank having a substantial structural integrity to protect the outer vessel from the cryogenic cargo and to protect the cargo from damage in the event the outer vessel is ruptured due to collision.
It is a further and important object of this invention to provide a fully determinate tank system wherein the stresses can be readily analyzed without excessive design or testing work and wherein excessive safety factors and redundant structural systems need not be employed.
It is a further related object of this invention to provide a tank configuration which does not require the structural and operational complexities of a double barrier system.
It is still a further object to provide a tank which because of its structural simplicity and reliability will enjoy the benefit of relaxed design requirements of the authorities having jurisdiction over the design and erection of these tanks.
It is still a further object of this invention to provide economies in construction and specifically to reduce or eliminate the use of expensive alloy steels in the construction of cryogenic tanks in marine vessels.
It is a further object of this invention to provide a tank which is simple to erect in a ship yard and whose construction does not grossly disturb other operations within that yard.
It is a further object of this invention to provide a modular construction for such tanks which simplifies the tank construction and reduces the time required to complete such construction.
It is still a further object of this invention to provide a simple method for constructing the modular components of the tank.
It is another object of this invention to provide compartments within the tank to reduce movement of the cryogenic liquid contained therein during ship movement.
It is another object of this invention to provide a tank in which the weight of both the tank and its contents are distributed along the tank so as to reduce the concentrated loads normally encountered at the ends of horizontal cylindrical tanks;
It is another and related object of this invention to provide a tank structure which cooperates with the ship structure to reduce the requirements of the ship structure.
It is yet another object of this invention to provide a tank which has a low vertical center of gravity.
SUMMARY OF THE INVENTION These and many other objectives of the invention are achieved in a tank for containment of cryogenic liquid, for placement within a marine transportation vessel which comprises a cylindrical tank wall, of any suitable curved cross-section for tank service but preferably of circular or elliptical cross-section comprised of prestressed concrete, and end closure means such as heads attached thereto. In order to withstand, the very considerable hydrostatic and vapor pressures which are developed within the tank, the cylindrical tank wall is prestressed by steel tendons positioned essentially circumferentially about its exterior surface and by other steel tendons, positioned within the tank wall itself, and oriented essentially parallel to the axis of the tank. T0 provide stiffness, one or more annular stiffening disks are positioned coaxially within the wall of the tank and are attached thereto. The stiffening disks are formed from steel or concrete and a portion thereof may extend past the exterior surface of the tank wall to provide support or retainer posts for the tank. Desirably a plurality of these stiffening disks are attached at intermediate locations between the heads of the tank. A series of planar stiffening plates (or ribs) are positioned in a radial-axial orientation with respect to the tank wall and are connected to the stiffening disks and to the interior of the tank wall. Desirably, the stiffening plates are flat, prestressed concrete plates and they, as well as the cylindrical tank wall have essentially axially positioned pre stressing tendons therein. To provide a secondary barrier, a steel sheath may be anchored to the outer surface of the cylindrical wall. This sheath may be of carbon steel since it acts compositely with the prestressed concrete, and thus is not subject to tensile stresses when subjected to the low temperatures of the cryogenic liquid within the concrete container.
In the preferred tank configuration, the tank wall is concrete and of circular cross-section. A series of axial holes are located within the tank wall through which steel prestressing tendons are passed. A carbon steel sheath is anchored to the exterior of the tank wall by studs and external to the sheath are prestressing tendons wrapped essentially circumferentially. Either one continuous tendon in a helical wind or a series of individual tendons can be used. Annular concrete stiffening disks are positioned coaxially within the tank wall and are attached to the steel sheath. The disks have holes along an outer circle and along certain radii, for through-passage of axially oriented prestressing tendons. Between the several stiffening disks and abutting their surfaces are a plurality of flat, concrete, stiffening plates which are positioned radially-axially with respect to the tank. These stiffening plates abut the interior of the tank wall at their radial outermost extension. Located within these stiffening plates are axially oriented holes for prestressing tendons. Defining the remainder of the tank structure are steel heads which are attached to the end-most stiffening disks. lnlet and outlet means are provided for the cryogenic liquid.
In its erected configuration, the tank is prestressed both circumferentially and axially, the circumferential prestressing is by means of the tendons positioned around the circumference of the tank and the axial prestressing is by means of the tendons passing through the holes in the tank wall. The stiffening plates are also prestressed by tendons which pass through an axial series of plates located between adjacent stiffening disks, the tendons passing through the radially located holes in those disks. Where the tank is of large diameter, it may be desirable to form the steel head from a central dome and a surrounding torus, in order to limit the amount of steel which is required. The head is attached to the end stiffening disks and the toroidal section of the head is further anchored to the cylindrical wall by the axial prestressing tendons and by tendons external to the tank which are oriented diagonally of the tank axis.
The advantages of the tank configuration of this invention are many. The circular or elliptical crosssection, particularly in a horizontal orientation, makes very efficient use of the internal cubic of conventional ships or barges. Prestressed concrete is markedly more economical than the expensive alloy plates of freestanding, prismatic tanks or the even more expensive materials and complicated construction techniques associated with membrane tanks. Since the configuration of the tank is relatively simple, the structure is a fully determinant one, and does not require a secondary barrier to protect the ship hull and the cargo from one another. With the steel sheath a measure of secondary barrier is provided, nonetheless. Thus, the tank configuration of the invention provides all of the advantages of a two barrier system while being fully determinant and thus subject to the less rigid design controls promulgated for determinant systems. The structural integrity of the system, by virtue of its circumferential and axial prestressing, provides a very substantial measure of safety for tank and cargo, should the vessel be involved in a collision and lends a stiffness to the ship structure. The compartments which are formed within the tank, due to the presence of stiffening disks and stiffening plates, reduce sloshing of the cargo within the tank and make the overall operation more safe. The relatively high weight of the concrete, is an advantage insofar as it substantially reduces the ballast requirements of the vessel and lowers the center of gravity. Still a further advantage of the tank configuration, is that it is relatively easily positioned within a supporting cradle in the ship structure and can be firmly positioned therein without requiring elaborate support systems.
To facilitate construction'of the tank, a modular wall component is fabricated. The component is comprised of a length of concrete, cylindrical tank wall of suitable curved cross-section having axially oriented holes passing through its length, a steel sheath anchored to its exterior surface and prestressing tendons wrapped essentially circumferentially about the exterior of the steel sheath. The concrete stiffening plates are integrally cast with the modular tank wall, and axial holes are provided therein. To erect the tank, from the modular components, it is necessary only to combine several of the wall modules, end to end and position, between them, annular, steel or concrete stiffening disks. The assembled tank is then prestressed axially as described above and the steel heads are attached to the end disks.
By providing a number of the modular components, together with the annular disks, a tank having the configuration described above can be relatively easily constructed within a conventional steel or concrete vessel. Desirably, the vessel will include a grid-like cradle which comprises transverse and axial structural members positioned in registration with the lower stiffening disks and the lower stiffening plates respectively. The transverse members are provided with a balsa wood support upon which the exterior portion of a stiffening disk is mounted. The axial structural members are positioned beneath the lower stiffening plates within the tank. Desirably, the tank is fixed to its cradle at only one position along the axis of the tank, i.e., at one transverse structural member and is slidably supported on several other structural members. The purpose of the fixed support is to preclude axial movement of the tank within the vessel and the purpose of the sliding supports is to permit axial contraction and expansion of the tank during cool-down and warm-up. Chocks may be provided at the sides and top of the tank to prevent it from rotating. However, the chocks should permit axial expansion and contraction of the tank.
The invention also embraces the method for forming the modular component for the cryogenic tank. A length of concrete, cylindrical tank wall of circular or elliptical cross-section is cast with axially oriented holes extending through it and radial-axial stiffening plates extending inwardly from .its inner surface at spaced locations. A steel sheath is anchored to its exterior surface. The steel sheath may be studded to the concrete, as it is poured, according to conventional techniques. After the concrete has set, the tank wall is prestressed by wrapping one or more steel tendons, in tension, about the outer surface of the steel sheath. The latter step may be carried out by mounting the cast wall on a turntable and rotating the turntable while tendons are wrapped about the tank wall. Alternatively, a carriage may be supported from the tank wall and moved about the circumference thereof while wrapping a tendon thereabout, as is conventional procedure in the construction of stationary tanks. A group of components positioned one above the other may be prestressed in a single operation.
The advantages in the methods of this invention are numerous. Modular components may be formed by conventional techniques in the shipyard, but at a distance from the site of the ship construction, or at a remote location. The erection of the tank is simplified because the modular components should be sized so as to be of such weight as will be within the lifting capacity of available lifting apparatus at ship building sites. The
axial tensioning of the modules andstiffening plates is performed with suitable jacks.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a simplified, side elevation view of a steel tanker containing five liquid natural gas tanks according to the present invention;
FIG. 2 is a side elevation view of one of the tanks shown in FIG. 1;
FIG. 3 is a fore and aft elevation view, in section, of the tank of FIG. 2 taken along lines 3-3 of FIG. 2;
FIG. 4 is a partial section view of the tank shown in FIG. 2, showing details of the modular wall construction;
FIG. 5 is a partial fore and aft elevation view of the portion of the modular wall construction of FIG. 4 taken along lines 5--5 of FIG. 4;
FIG. 6 is a simplified, exploded, view of the modular components of the tank, showing their juxtaposition prior to assembly;
FIG. 7 is a view of the tank in partially assembled state;
FIG. 9 is a detailed elevation view ofa sliding support pedestal for the tank of FIG. 2.
With reference to FIG. 1, reference numeral 10 refers generally to a conventional tanker. Reference numeral l2 refers to a hull and reference numeral 14 to a tanker super structure. Reference numerals l6, 18, 20, 22 and 24 refer to five, horizontally oriented tanks for containment of cryogenic liquid having the configuration more fully described below.
With reference to FIGS. 2, 3, 4 and 5, it can be seen that tank 16 is comprised of a cylindrical tank wall of circular cross-section 26 and includes heads 28 and 30. Head 28 comprises a central dome 32 and a torus 34. However, this head design is optional and may be employed in large tanks to reduce the amount of expensive alloy metal required. In smaller tanks, the heads may be elliptical or hemispherical. Inlet and outlet means for the cryogenic liquid are not shown, however, they may be provided at suitable locations in the top of the tank or through the steel heads.
As shown in FIG. 3, cylindrical tank 16 is supported within hull 12 on a cradle 36 which includes several parallel, transverse, partially circular support members 38 and three parallel, axial support members 40, 42 and 44. The entire tank is surrounded by insulation 46 which may be minneral wool, perlite or other suitable insulating material. The tank 16 is prevented from to tating within hull 12 by means of a chock 48 which includes a bracket 50 attached to the top of the tank having a recess section 52 in which is placed restraining member 54 attached to the hull or deck structure. Chocks may also be attached to the sides of the tank.
Tank 16 is comprised of a plurality of modular, concrete wall components 60a, 60b, 600, etc. Each of these modular wall components is cylindrical and of circular cross-section and has a plurality of axial holes passing therethrough designated by reference numeral 62. Located within axial holes 62 are prestressing tendons 64. Located externally of modular components 60a, 60b, 600, etc. are steel sheaths 65a, 65b and 650, etc. which pass circumferentially around the exterior surface of the concrete. The steel sheaths are anchored to the concrete wall by means of studs 66. Located on the FIG. 8 is a detailed view of a fixed support pedestal for the tank of FIG. 2; and
outer surface of steel sheaths 65 are prestressing tendons 68 which pass circumferentially about the sheaths and are in tension causing the concrete and steel sheath to act compositely. A series of discrete tendons may be used or helically wound tendons may be employed. A layer of gunnite or other suitable bitumastic material or plastic coating such as epoxy serves as protective overcover for the circumferential prestressing tendons as designated by reference numeral 70. Positioned at the right end of modular tank component 60a and between each of components 60a and 60b, 60b and 600, etc. are annular, concrete stiffening disks 72a, 72b, 720, etc. Each of these stiffening disks are positioned coaxially with respect to the tank. Head 28 is attached, by suitable connection to endmost stiffening disk 72a.
As seen best in FIGS. 4 and 5, a series of flat, concrete stiffening plates 74 are provided. Each of these stiffening plates are positioned both radially and axially with respect to tank 16. They are integral with the inner surface of the cylindrical tank wall at their radial outermost extension 76 and abut, at their axial extensions 78 and 80, the two stiffening disks between which they are located, i.e., in FIG. 4, disks 72a and 72b. These stiffening plates have essentially axially oriented holes therein designated by reference numeral 82 through which prestressing tendons 84 are passed. Suitable holes are provided in stiffening disks 72 for through-passage of tendons 64 through the holes 62 in modular wall components 60, and through an axial series of stiffening plates 74. Prestressing tendons 84 terminate in suitable tensioning heads 86 on the end most stiffening disk, 72a.
Desirably, stiffening disks 72 are spaced from one another by uniform modular wall components 60 and the rows of stiffening plates 74 are positioned at a uniform angular distance from one another around the inner circumference of the tank. These outer extensions of the disks may form support posts or positioning rails for the tank, and as seen in FIG. 3, these posts are received in cradle 36 in transverse structural member 38.
As shown in FIGS. 6 and 7, the tank configuration of this invention is most easily assembled by positioning modular wall components 100, comprised of cast concrete wall sections of circular cross-section having holes 102 therein and circumferential prestressing tendons 104, alternately with stiffening disks 106 which have circumferential holes 108 and radial holes 110 for through-passage of prestressing tendons. The axial prestressing tendons which pass through the wall of the concrete tank are designated by reference numerals and the prestressing tendons which pass through the series of stiffening plates are designated by reference numerals 122. As seen best in FIG. 7, the interior of the assembled tank has a partially compartmentalized configuration, which is of advantage in reducing sloshing when the tank is filled. To complete the overall tank structure, heads are fixed to either end of the assembled cylindrical structure as shown in FIG. 2. As further shown in FIG. 2, where the heads'are toroidal, the torus may be further anchored to the assembled cylindrical wall by prestressing tendons and 127 which are oriented diagonally of the tank volume enclosed by the torus.
FIG. 8 shows a fixed support for the tank. Reference numeral 38 represents a transverse support member for the tank. Within support member 38 is a recess 39 containing balsa wood 41 which provides a support for the tank. The lower extension of stiffening disk 72 on one end of the tank is thus fuxed with respect to the axis of the tank and accordingly the tank cannot move when affected by impacts due to waves or other disturbances encountered by the vessel.
in FIG. 9, reference numeral 138 refers to a transverse, cradle support member, of partial circular shape, having a recess at 139 filled with balsa 141. As shown, the lower extension of the stiffening disk 172 sits on the upper surface 143 of balsa 141 and can slide across that surface under the influence of contraction and expansion forces encountered in the cool-down and warm-up of the tank.
What is claimed is:
l. A tank for cryogenic adapted for placement within a marine transportation vessel comprising:
a. a concrete, cylindrical tank wall having a plurality of steel prestressing tendons located therein in axial orientation;
b. a steel sheath anchored to the exterior surface of said wall;
c. a prestressing tendon wrapped essentially circumferentially about the exterior of said steel sheath;
d. at least two, annular stiffening disks positioned coaxially within the said wall said disks having holes therein for through-passage of axially oriented prestressing tendons;
e. a plurality of stiffening plates positioned radiallyaxially with respect to said tank and abutting at both axial extensions thereof, said stiffening disks and at their radial outermost extension, the said cylindrical tank wall, said stiffening plates having essentially axially oriented prestressing tendons therein;
f. steel heads defining the ends of said cylindrical tank and attached to said stiffening disks; and
g. inlet and outlet means for said cryogenic liquid.
2. A tank for cryogenic liquids as recited in claim 1 wherein said tank includes a series of stiffening disks spaced along the axis of said tank and a series of stiffening plates spaced around the circumference of said tank, between each of said disks, the axial prestressing tendons associated with each of said stiffening plates passing through mating holes in. said disks and linking an axial series of stiffening plates.
3. A tank as recited in claim 2 wherein at least a portion of said stiffening disks extends past the exterior surface of the said steel sheath the protruding edge thereof forming a post for retention of said tank.
4. A tank as recited in claim 2 wherein said steel head comprises a central dome and torus attached to a said end stiffening disk, said torus being further anchored to said cylindrical wall by external prestressing tendons oriented diagonally of the tank volume enclosed by said torus.
5. A modular component for construction of a tank for cryogenic liquids for placement within a marine transportation vessel comprising:
a. a length of concrete, cylindrical tank wall having a plurality of axially oriented holes passing through the length thereof;
b. a plurality of radial-axial stiffening members, integral with the internal surface of said cylindrical tank wall and extending inwardly thereof in order to act as compartmental walls within said tank for reduction of liquid movement within said tank; 0. a steel sheath anchored to the exterior surface of said wall; and
d. a prestressing tendon wrapped essentially circumferentially about the exterior of said steel sheath.
6. A tank, of modular construction, for cryogenic liquids, adapted for placement within a marine transportation vessel, comprising:
a. a plurality of prestressed concrete wall modules comprising:
1. a length of concrete, cylindrical tank wall and a plurality of radial-axial stiffening members integral with the internal surface thereof, said walls and stiffening members having a plurality of axially oriented prestressing tendons passing through the lengths thereof;
2. a steel sheath anchored to the exterior surface of said wall;
3. a prestressing tendon wrapped essentially circumferentially about the exterior of said steel sheath, said wall modules being laid end to end;
b. annular stiffening disks positioned between adjacent wall modules, said disks having holes therein for through-passage of said axially oriented prestressing tendons;
c. steel heads defining the ends'of said cylindrical tank; and
d. inlet and outlet means for said cryogenic liquid.
7. A tank for cryogenic liquids comprising:
a. a cylindrical tank wall comprised of prestressed concrete;
b. end closure means attached to said cylindrical tank wall;
c. at least one annular stiffening disk positioned coaxially within the said cylindrical tank wall intermediate the said end closures, said stiffening disk being attached to said wall and extending into said tank, in order to compartmentalize said tank and reduce movement of liquid therein; and
d. inlet and outlet means for said cryogenic liquids.
8. A tank as recited in claim 7 having a plurality of said stiffening disks attached intermediate to said end closures of said tank.
9. A tank as recited in claim 7 wherein at least a portion of the said disk extends past an exterior surface of said wall, the protruding edge thereof forming a longitudinal restraint for said tank.
10. A tank as recited in claim 7 wherein said end closure means comprises a steel head.
11. A tank as recited in claim 7 wherein said end closure means comprises a steel head comprising a central dome and torus.
12. A tank as recited in claim 7 having a steel sheath anchored to the outer surface of said cylindrical wall.
13. A tank for cryogenic liquids comprising:
a. a cylindrical tank wall comprised of prestressed concrete;
b. end closure means attached to said cylindrical tank wall;
c. at least one annular stiffening disk positioned coaxially within the said cylindrical tank wall intermediate the said end closures and attached to said wall.
(1. at least one stiffening member positioned radiallyaxially with respect to said tank, the axial extension of said stiffening member abutting said stiffening disk and the radial outermost extension of said stiffening member abutting the said cylindrical tank wall.
14. A tank as recited in claim 13 wherein said stiffening member comprises a flat, prestressed concrete plate having essentially axially positioned prestressing tendons therein.
UNITED STATES PATENT OFFICE QERTIFICATE 0F CORRECTION Patent 3,863,408 Dated February 4, 1975 Inventor s John J. Closner, et al.
It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
IN THE CLAIMS:
Column 9, line 14, after "cryogenic" insert liquids Signed and Sealed this second Day Of September 1975 [SEAL] Arrest:
RUTH C. MASON C. MARSHALL DANN o Mlesring Officer ('mnmissiuncr nj'PaIentx and Trademarks FORM PO-105O (10-69) USCOMMQDC 037 2 9 A .5. GOVERNMENT PRINTING OFFICE 2 I959 "355-334

Claims (16)

1. A tank for cryogenic adapted for placement within a marine transportation vessel comprising: a. a concrete, cylindrical tank wall having a plurality of steel prestressing tendons located therein in axial orientation; b. a steel sheath anchored to the exterior surface of said wall; c. a prestressing tendon wrapped essentially circumferentially about the exterior of said steel sheath; d. at least two, annular stiffening disks positioned coaxially within the said wall said disks having holes therein for through-passage of axially oriented prestressing tendons; e. a plurality of stiffening plates positioned radially-axially with respect to said tank and abutting at both axial extensions thereof, said stiffening disks and at their radial outermost extension, the said cylindrical tank wall, said stiffening plates having essentially axially oriented prestressing tendons therein; f. steel heads defining the ends of said cylindrical tank and attached to said stiffening disks; and g. inlet and outlet means for said cryogenic liquid.
2. A tank for cryogenic liquids as recited in claim 1 wherein said tank includes a series of stiffening disks spaced along the axis of said tank and a series of stiffening plates spaced around the circumference of said tank, between each of said disks, the axial prestressing tendons associated with each of said stiffening plates passing through mating holes in said disks and linking an axial series of stiffening plates.
2. a steel sheath anchored to the exterior surface of said wall;
3. a prestressing tendon wrapped essentially circumferentially about the exterior of said steel sheath, said wall modules being laid end to end; b. annular stiffening disks positioned between adjacent wall modules, said disks having holes therein for through-passage of said axially oriented prestressing tendons; c. steel heads defining the ends of said cylindrical tank; and d. inlet and outlet means for said cryogenic liquid.
3. A tank as recited in claim 2 wherein at least a portion of said stiffening disks extends past the exterior surface of the said steel sheath the protruding edge thereof forming a post for retention of said tank.
4. A tank as recited in claim 2 wherein said steel head comprises a central dome and torus attached to a said end stiffening disk, said torus being further anchored to said cylindrical wall by external prestressing tendons oriented diagonally of the tank volume enclosed by said torus.
5. A modular component for construction of a tank for cryogenic liquids for placement within a marine transportation vessel comprising: a. a length of concrete, cylindrical tank wall having a plurality of axially oriented holes passing through the length thereof; b. a plurality of radial-axial stiffening members, integral with the internal surface of said cylindrical tank wall and extending inwardly thereof in order to act as compartmental walls within said tank for reduction of liquid movement within said tank; c. a steel sheath anchored to the exterior surface of said wall; and d. a prestressing tendon wrapped essentially circumferentially about the exterior of said steel sheath.
6. A tank, of modular construction, for cryogenic liquids, adapted for placement within a marine transportation vessel, comprising: a. a plurality of prestressed concrete wall modules comprising:
7. A tank for cryogenic liquids comprising: a. a cylindrical tank wall comprised of prestressed concrete; b. end closure means attached to said cylindrical tank wall; c. at least one annular stiffening disk positioned coaxially within the said cylindrical tank wall intermediate the said end closures, said stiffening disk being attached to said wall and extending into said tank, in order to compartmentalize said tank and reduce movement of liquid therein; and d. inlet and outlet means for said cryogenic liquids.
8. A tank as recited in claim 7 having a plurality of said stiffening disks attached intermediate to said end closures of said tank.
9. A tank as recited in claim 7 wherein at least a portion of the said disk extends past an exterior surface of said wall, the protruding edge thereof forming a longitudinal restraint for said tank.
10. A tank as recited in claim 7 wherein said end closure means comprises a steel head.
11. A tank as recited in claim 7 wherein said end closure means comprises a steel head comprising a central dome and torus.
12. A tank as recited in claim 7 having a steel sheath anchored to the outer surface of said cylindrical wall.
13. A tank for cryogenic liquids comprising: a. a cylindrical tank wall comprised of prestressed concrete; b. end closure means attached to said cylindrical tank wall; c. at least one annular stiffening disk positioned coaxially within the said cylindrical tank wall intermediate the said end closures and attached to said wall. d. at least one stiffening member positioned radially-axially with respect to said tank, the axial extension of said stiFfening member abutting said stiffening disk and the radial outermost extension of said stiffening member abutting the said cylindrical tank wall.
14. A tank as recited in claim 13 wherein said stiffening member comprises a flat, prestressed concrete plate having essentially axially positioned prestressing tendons therein.
US292727A 1972-09-27 1972-09-27 Prestressed concrete tanks for liquid natural gas tankers Expired - Lifetime US3863408A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US292727A US3863408A (en) 1972-09-27 1972-09-27 Prestressed concrete tanks for liquid natural gas tankers
GB3528773A GB1437411A (en) 1972-09-27 1973-07-24 Prestressed concrete cryogenic tanks for liquid natural gas tankers
ES418215A ES418215A1 (en) 1972-09-27 1973-08-25 Prestressed concrete tanks for liquid natural gas tankers
IT28257/73A IT1001534B (en) 1972-09-27 1973-08-27 PRECOMPRES SO CONCRETE TANKS FOR GISTERNA SHIPS USED TO TRANSPORT LIQUEFIED NATURAL GAS
JP10256673A JPS5345925B2 (en) 1972-09-27 1973-09-10
SE7313106A SE402438B (en) 1972-09-27 1973-09-26 TENSIONED CONCRETE TANK FOR TANKERS FOR THE TRANSPORT OF LIQUID NATURAL GAS
DE19732348656 DE2348656A1 (en) 1972-09-27 1973-09-27 TANK FOR ULTRA-TEMPERATURE LIQUIDS, INSTALLABLE IN TANKER
US532016A US3926134A (en) 1972-09-27 1974-12-12 Prestressed concrete tanks for liquid natural gas tankers

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US292727A US3863408A (en) 1972-09-27 1972-09-27 Prestressed concrete tanks for liquid natural gas tankers

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US (1) US3863408A (en)
JP (1) JPS5345925B2 (en)
DE (1) DE2348656A1 (en)
ES (1) ES418215A1 (en)
GB (1) GB1437411A (en)
IT (1) IT1001534B (en)
SE (1) SE402438B (en)

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US4410487A (en) * 1978-04-28 1983-10-18 Kraftwerk Union Aktiengesellschaft Core baffle or enclosure and method of fabricating the same
US5429268A (en) * 1993-03-05 1995-07-04 Tri-Fuels, Inc. & The Rosalind Hale Revocable Trust Tubular above ground gas storage vessel
US5431295A (en) * 1989-03-31 1995-07-11 Westinghouse Electric Corporation Storage module for nuclear waste with improved liner
US5908134A (en) * 1993-03-05 1999-06-01 The Rosalind Hale Revocable Trust, Uta George Carl Hale, Trustee Tubular above ground gas storage vessel
US20080016788A1 (en) * 2004-05-20 2008-01-24 Gulati Kailash C Lng Containment System And Method Of Assembling Lng Containment System
EP2035742A1 (en) * 2006-06-19 2009-03-18 Tanker Engineering AS An arrangement for a cylindrical tank for transportation of liquefied gases at low temperature in a ship
US20110100583A1 (en) * 2009-10-29 2011-05-05 Freund Sebastian W Reinforced thermal energy storage pressure vessel for an adiabatic compressed air energy storage system
CN103114752A (en) * 2013-03-05 2013-05-22 东北石油大学 Fiber reinforce plastic (FRP) spherical tank - transposition support combination column system and construction method thereof
US20140150359A1 (en) * 2011-07-18 2014-06-05 Rolf J. Werner Tower-shaped supporting structure
US20150014186A1 (en) * 2013-07-12 2015-01-15 Ut-Battelle, Llc Hydrogen storage container
US10317008B2 (en) * 2016-07-15 2019-06-11 IFP Energies Nouvelles Container for a system for storing and restoring heat, comprising at least two modules formed from concrete
KR102267787B1 (en) * 2020-01-10 2021-06-22 한국이미지시스템(주) Prestressed concrete pressure vessels

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JPS5545871U (en) * 1978-09-21 1980-03-25
JPS5589346U (en) * 1978-12-14 1980-06-20
JPS55122656U (en) * 1979-02-25 1980-09-01
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Cited By (17)

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Publication number Priority date Publication date Assignee Title
US4410487A (en) * 1978-04-28 1983-10-18 Kraftwerk Union Aktiengesellschaft Core baffle or enclosure and method of fabricating the same
US5431295A (en) * 1989-03-31 1995-07-11 Westinghouse Electric Corporation Storage module for nuclear waste with improved liner
US5429268A (en) * 1993-03-05 1995-07-04 Tri-Fuels, Inc. & The Rosalind Hale Revocable Trust Tubular above ground gas storage vessel
US5908134A (en) * 1993-03-05 1999-06-01 The Rosalind Hale Revocable Trust, Uta George Carl Hale, Trustee Tubular above ground gas storage vessel
US20110023408A1 (en) * 2004-05-20 2011-02-03 Gulati Kailash C LNG Containment System and Method of Assembling LNG Containment System
US7837055B2 (en) 2004-05-20 2010-11-23 Exxonmobil Upstream Research Company LNG containment system and method of assembling LNG containment system
US20080016788A1 (en) * 2004-05-20 2008-01-24 Gulati Kailash C Lng Containment System And Method Of Assembling Lng Containment System
US8387334B2 (en) 2004-05-20 2013-03-05 Exxonmobil Upstream Research Company LNG containment system and method of assembling LNG containment system
EP2035742A1 (en) * 2006-06-19 2009-03-18 Tanker Engineering AS An arrangement for a cylindrical tank for transportation of liquefied gases at low temperature in a ship
EP2035742A4 (en) * 2006-06-19 2010-01-06 Tanker Engineering As An arrangement for a cylindrical tank for transportation of liquefied gases at low temperature in a ship
US20110100583A1 (en) * 2009-10-29 2011-05-05 Freund Sebastian W Reinforced thermal energy storage pressure vessel for an adiabatic compressed air energy storage system
US20140150359A1 (en) * 2011-07-18 2014-06-05 Rolf J. Werner Tower-shaped supporting structure
CN103114752A (en) * 2013-03-05 2013-05-22 东北石油大学 Fiber reinforce plastic (FRP) spherical tank - transposition support combination column system and construction method thereof
US20150014186A1 (en) * 2013-07-12 2015-01-15 Ut-Battelle, Llc Hydrogen storage container
US9562646B2 (en) * 2013-07-12 2017-02-07 Ut-Battelle, Llc Hydrogen storage container
US10317008B2 (en) * 2016-07-15 2019-06-11 IFP Energies Nouvelles Container for a system for storing and restoring heat, comprising at least two modules formed from concrete
KR102267787B1 (en) * 2020-01-10 2021-06-22 한국이미지시스템(주) Prestressed concrete pressure vessels

Also Published As

Publication number Publication date
DE2348656A1 (en) 1974-04-11
IT1001534B (en) 1976-04-30
JPS4971512A (en) 1974-07-10
ES418215A1 (en) 1976-06-16
SE402438B (en) 1978-07-03
GB1437411A (en) 1976-05-26
JPS5345925B2 (en) 1978-12-09

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