GB1572305A – Method for storing pressurised fluid undergroud and a reservoir for effecting this method
– Google Patents
GB1572305A – Method for storing pressurised fluid undergroud and a reservoir for effecting this method
– Google Patents
Method for storing pressurised fluid undergroud and a reservoir for effecting this method
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Publication number
GB1572305A
GB1572305A
GB48815/77A
GB4881577A
GB1572305A
GB 1572305 A
GB1572305 A
GB 1572305A
GB 48815/77 A
GB48815/77 A
GB 48815/77A
GB 4881577 A
GB4881577 A
GB 4881577A
GB 1572305 A
GB1572305 A
GB 1572305A
Authority
GB
United Kingdom
Prior art keywords
anchoring
fluid
tank
casing
cavity
Prior art date
1976-12-02
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
Application number
GB48815/77A
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.)
Societe National Elf Aquitaine
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Original Assignee
Societe National Elf Aquitaine
Commissariat a lEnergie Atomique CEA
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.)
1976-12-02
Filing date
1977-11-23
Publication date
1980-07-30
1977-11-23
Application filed by Societe National Elf Aquitaine, Commissariat a lEnergie Atomique CEA
filed
Critical
Societe National Elf Aquitaine
1980-07-30
Publication of GB1572305A
publication
Critical
patent/GB1572305A/en
Status
Expired
legal-status
Critical
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Classifications
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28—HEAT EXCHANGE IN GENERAL
F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
F28D20/00—Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00
F28D20/0034—Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00 using liquid heat storage material
F28D20/0043—Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00 using liquid heat storage material specially adapted for long-term heat storage; Underground tanks; Floating reservoirs; Pools; Ponds
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
F17C3/00—Vessels not under pressure
F17C3/005—Underground or underwater containers or vessels
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
F17C2201/00—Vessel construction, in particular geometry, arrangement or size
F17C2201/05—Size
F17C2201/052—Size large (>1000 m3)
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
F17C2203/00—Vessel construction, in particular walls or details thereof
F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
F17C2203/0634—Materials for walls or layers thereof
F17C2203/0636—Metals
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
F17C2203/00—Vessel construction, in particular walls or details thereof
F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
F17C2203/068—Special properties of materials for vessel walls
F17C2203/0685—Special properties of materials for vessel walls flexible
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
F17C2209/00—Vessel construction, in particular methods of manufacturing
F17C2209/22—Assembling processes
F17C2209/221—Welding
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
F17C2270/00—Applications
F17C2270/01—Applications for fluid transport or storage
F17C2270/0142—Applications for fluid transport or storage placed underground
F17C2270/0144—Type of cavity
F17C2270/0149—Type of cavity by digging cavities
Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
Y02E60/14—Thermal energy storage
Description
PATENT SPECIFICATION
( 21) Application No 48815/77 ( 22) ( 31) Convention Application No.
7636283 ( 11) 1 572 305 Filed 23 Nov 1977 ( 32) Filed 2 Dec 1976 in ( 33) France (FR) ( 44) Complete Specification published 30 July 1980 ( 51) INT CL 3 B 65 G 5/00 ( 52) Index at acceptance El T SC 1 5 C 2 SD 1 8 B F 4 P AA ( 72) Inventors JACQUES DESPOIS FRANCIS NOUGAREDE ( 54) A METHOD OF STORING PRESSURIED FLUID UNDERGROUND AND A RESERVOIR FOR EFFECTING THIS METHOD ( 71) We, COMMMISSARIAT A L’ENERGIE ATOMIQUE, an organisation created in France by ordinance No 45-2563 of 18th October 1945, of 29 rue de la Federation, 75752 Paris Cedex 15, France, and SOCIETE NATIONALE ELF A Qui TAINE, a French Body Corporate, of Tour Aquitaine, Cedex 4, 92080 Paris La Defense, France, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: It is known to make underground tanks in which pressurized fluids can be left in transit or be stored until they are recovered later on The idea of an underground storage of heat through pressurized hot water was expounded, in particular, during the 8th World Conference on Energy (Bucarest, 28th June 1971).
Other modes of storage, e g compressed air, gas or radioactive waste, have already been contemplated or put into practice.
In the present state of the art, it is most often resorted to that the hydrostatic pressure of the water contained in the ground counterbalance the pressure within the cavity, in order that a lack of tightness, always to be feared in view of stresses already existing or generated on coatings, cannot give rise to important leakages.
Therefore, in the case of high pressures, the depth required soon becomes unrealistic.
By way of example, in the case of water to be stored at 300 C ( 570 ‘F), pressure being then of about 90 bars, the crown of the cavity would have to be at a depth of about 1000 meters ( 3300 ft).
Moreover, in the prior art, the fluid is usually in contact with the cavity walls as in French Patent 2,231,277 viz with the rock or a protective concrete, which induces chemical and thermal phenomena likely to alter both the cavity behaviour and the fluid composition In order to obviate such drawbacks, it has already been suggested to store a liquid, namely super 50 heated water, in a metal tank open in the upper portion thereof and built within the cavity under air, or gas pressure This solution has the double drawback of requiring a large investment of money for building 55 a whole tank underground and high operation expenses in view of the necessity to maintain the cavity atmosphere under constant pressure, in spite of the volume variations of the stored material due to 60 the temperature changes thereof (variations amounting to about 20 % in the case of water raised from 20 ‘C to 200 ‘C).
In other instances, lithostatic pressure is resorted to for balancing internal pressure 65 in various storage tanks, pressure-sustaining ducts or nuclear reactors (refer, in particular, to “Mdcanique des roches et ses applicaitons” published by Dunod, Paris 1967, pages 377 to 389) 70 In French Patent 2,286,260, it is suggested to store hot water in underground tanks situated at a depth that is sufficient to enable the weight of the rocks above the tank to generate a lithostatic pressure 75 adapted to counter-balance the pressure of the water to be stored In said patent, it is suggested, for achieving tightness, to use etiher a plastic material foil or a metal tank constituted by rings of U-shaped cross 80 section.
In either case, the solution advocated leads, in practice, to severe troubles, especially if the storage of hot fluids under high pressure is contemplated Indeed, a 85 plain foil of plastic material, in general, is not sufficiently resistent for sustaining the high pressure involved (e g of about bars and upwards) without being torn, when hot; as for the metal tank, since it 90 0 r 1 572 305 is made of rings and merely rests on the cavity floor, it is allowed but a longitudinal expansion (in only one direction), which therefore preludes the possibility, for said tank, to adhere by all its point to the cavity wall under the pressure of the contents thereof and, later on, to follow the various ” breathing ” movements of said wall due, in particular, to thermal stresses generated in the sub-soil formations.
One object of the present invention is a method for storing a fluid under a maximum superatmospheric pressure p underground, said method obviating the above drawbacks, while in addition providing a few extra advantages.
Said storage method essentially comprises the steps of digging, at a depth at which the lithostatic pressure resulting from the weight of the soil formations is at least p, an underground cavity in which is made a deformable tight casing, fixed to the cavity wall by a few points only while being free to expand or retract in every direction between said points in order to follow closely corresponding movements of the cavity wall, then injecting the pressurized fluid into said casing in order that the latter lie flat by all the points thereof against the wall of the cavity, all the possible movements of which it follows subsequently by sliding, the pressure of said fluid being thus counterbalanced, at every moment, by the lithostatic pressure of the cavity wall transferred to the fluid through the thus-expanded casing.
The use of a very special tight diaphragm endowed, as a matter of fact, with two degrees of expansibility, namely the possibility of sliding along the rock-wall between its points of attachment to that wall and the possibility of “breathing” at right angles to said wall, in particular, by following the movements of the latter resulting from thermal expansions or contractions, permits one to obtain the storage of pressurized fluid together with a uniform distribution of the pressure at every moment and over the whole area of the cavity.
In case of need, moreover, a smoothing coat can be inserted between the deformable casing and the cavity wall.
The present invention also relates to a tank for carrying out the above method, characterized in that it comprises, in an underground cavity dug at a depth at which the lithostatic pressure resulting from the weight of the soil formations is at least p, a deformable tight casing, fixed to the cavity-wall by a few points only while being free to expand or retract in every direction between said points in order to follow closely corresponding movements of the cavity wall, said casing being adapted to receive the pressurized fluid in order that said casing lie flat by all the points thereof against the wall of the cavity, all the possible movements of which it follows subsequently by sliding, the pressure of said fluid being thus counterbalanded, at 70 every moment, by the lithostatic pressure of the cavity wall transferred to the fluid through the thus-expanded casing.
The tank forming the object of the present invention advantageously turns to 75 profit the fact that the pressure within the cavity is distributed over the surrounding sub-soil formations against which the deformable tight wall is applied Accordingly, the internal pressure in said cavity 80 no longer needs to be counterbalanded by the surrounding hydrostatic pressure as in the prior art It is only sufficient that the lithostatic pressure, namely the pressure exerted by the sub-soil formations them 85 selves, counterbalances said internal pressure The minimum safety depth is thus divided by a coefficient that is at least equal to the mean specific weight of the above-jacent formations, viz by about 2 90 In the above mentioned example, relating to water at the temperature of 3000 C ( 570 ‘F) under a pressure of 90 bars, the crown of the cavity would have to be at a depth of about 500 meters ( 1650 ft) instead 95 of 1000 meters as in the prior art, and, in addition, the digging operation that required a lot of technical skill in the prior art and was moreover quite expensive although uncertain as to the results ob 100 tained, becomes, according to the present invention, a conventional application of the mining technique, provided geological conditions be normal Moreover in the case of smaller pressures the digging of the cavity 105 that would have required underground operations in the prior art, can now be carried out from the ground level, according to the so-called ” covered trenches” method or to any other appropriate method 110 Preferably, the tight deformable casing comprises a set of metal plates that are arc-welded or welded according to any suitable method capable of providing a very good tightness Said metal plates are pro 115 vided with a suitable number of appropriately shaped ribs ensuring a free play of the plates between the anchoring points.
Said metal plates are constituted by steel sheets, the thickness of which is determined 120 by the internal pressure and the radius of curvature of the corrugations forming said ribs, which permits said plates to withstand the pressure at the ribs Stresses on the flat portions applied against the sub 125 jacent material have not to be taken into account for determining the thickness, since the internal pressure is balanced bv the reaction of the sub-jacent material.
Another advantageous feature of the pre 130 1 572 305 sent invention is to be noted, resulting from the fact that it is possible to make use of relatively thin metal sheets, since the reduction of thicknesses is limited only by the fact that the corrugations, of necessity, must have feasible radiuses of curvature, providing a sufficient play of the coating, and that account must be taken of welding requirements as well as of resistance to corrosion and abrasion.
Other features of the invention will appear from the following description, given merely by way of example, of the tank according to the invention with respect to the accompanying drawings, in which:
-figs la, lb and lc show three possible embodiments, respectively, corresponding to various uses; -fig 2 is a general view of a deformable tight casing formed of welded ribbed metal plates; -fig 3 a is a detail view of a typical portion of said metal plates, and figs 3 b and 3 c represent the main fittings; -figs 4 to 6 are various cross-sections of the coatings, showing how the tight deformable casing is anchored; and -figs 7 a to 7 c are detail views relating to advantageous fittings forming part of the coating according to fig 6.
As shown in fig la the tank for pressurized fluids according to the invention comprises a cavity 1 dug underground via mineshaft 2 and galleries 3 Fig la shows the shape of cavity 1 and an arrangement of galleries 3 corresponding to the storage of a pressurized hot liquid according to the so called “balancing” conventional method, i e as follows:
The cavity being filled up to the top with hot liquid surmounting the cold liquid, of higher specific weight, filling the cavity-bottom, the whole unit operates through transfer of the cold liquid from the cavity lower portion towards transferand-heating means M, and transfer of the water heated by said means M towards the upper portion of cavity 1, in the storage step, on the one hand, and reverse flow through ducts 4 with absorption of heat by said means M, in the exhaust step.
Cavity 1, if necessary, is provided with a suitable coat 5; a tight deformable casing 6 spread over the cavity wall contains a liquid 7 The connection means M with a surface network providing the transfer of a coolant fluid from a source S to a station of use, is obtained through ducts 8 Fig lb shows a variant corresponding to lower pressures; the caving being dug directly from the ground-level according to the so-called ” covered trench ” method.
Cavity 1 is closed, at the upper portion thereof, by a veil of concrete or a metal structure 9, capable of withstanding the weight of filling earth 10 and leaning against moulded walls 11 Tight deformable casing 6 is applied against said moulded walls 11 and veil 9 and also against the bottom of the excavation, either 70 directly or through a suitable coat 5.
The above described means M of fig la are mounted in a hole 12 defined by a moulded wall 13.
Fig lc shows a possible embodiment of 75 tank for pressurized gas according to the invention A cavity 1 has been dug via a shaft 2 and a gallery 3 and is no more than a horizontal gallery of larger crosssection 80 Tight deformable casing 6 lines the wall of cavity 1, either directly or with a suitable intervening coat 5 Pressurized gas is fed into, and from, cavity 1 by means of a duct 14 connecting the tank to filling and 85 exhaust means M’ via shaft 2.
While figs la to lc comprise but a single cavity, quite obviously a tank according to the invention can comprise a plurality of cavities of various shapes and arranged 90 in a number of possible ways; in fact, the main feature of the tank according to the invention lies in the presence of tight deformable casing 6, whatever the use, shape and size of the thus defined space may be 95 In fig 2 is shown a possible embodiment o fa tight deformable casing, constituted by a plurality of metal sheets, arc-welded or welded according to any suitable method, comprising an appropriate number 100 of ribs of suitable shape adapted to provide the free-play of said plurality of plates between their anchoring points Preferably, said plurality of metal plates is constituted by an assembly of embossed metal sheets 105 provided with ribs that comprise one or several corrugations, said sheets being of two different types, viz anchoring sheets and connecting sheets 16, the latter being joined by means of welds 17, either 110 butt-welds or lap-welds, or by a metal strip (not shown).
Connecting sheets 16 are but plain flat sheets in which a median rib 18 has been embossed Said connecting sheets are sup 115 ported only by adjacent anchoring sheets and have no anchoring point whatever in the sub-jacent material.
Anchoring sheets 15 are provided with ribs 19 and 20 at right angles that meet 120 at the sheet center through a distributing rib 21 surrounding anchorage device 22.
The tight deformable casing according to the latter embodiment has a number of advantages: 125 -The metal sheets can be formed merely by an embossing operation, contrary to those sheets for liquid-gas tanks, the latter sheets having to be treated according to more intricate methods, in view of the 130 1 572 305 fact that they are subjected to temperatures at which the metal becomes brittle; -Since but now types of metal-sheets are used, the present invention allows an easy prefabrication of said sheets; -fig 2 corresponds to the coating of a developable surface, but it is easy matter to adjust a seet to the accurate dimensions of the cavity and to cover non-developable surfaces The anchoring sheets 15 are usually used in their entirely, but, in case of need, it is possible to tailor them, taking great care, however, not to cut distribution rib 21.
On the other hand, connecting sheets 16, being of simple structure with but a single rib, can be adjusted to the cavity dimensions By cutting out portions of, e g triangular shape, in said connecting sheets, it is possible to warp the whole metal-coating of the cavity and apply same on surfaces of spherical or ogival shape or the like.
In fig 3 a are shown distribution-rib 21 and anchorage device 22 more in detail.
Distribution-rib 21 is in the shape of a polygon or a closed curved line, e g a circle as shown in the figure It is substantially more portruding than adjoining perpendicular ribs 19 and 20.
At four places, in the vicinity of the intersections of distribution rib 21 with the bisectors of the angles defined by perpendicular ribs 19 and 20, said distribution rib 21 is provided with saddle-shaped carvings 23 adapted to lower the level of its ridge so as to give the latter substantially the same height as the tops of perpendicular ribs 19, 20.
Anchorage device 22 is constituted by a sleeve, or bushing, encircling anchorage hole 24.
For clearness sake, all the ribs of sheets and 16 including distribution rib 21, have been shown in the figure as comprising but a single corrugation, or wave; however, it is quite abvious that larger movements can be obtained without increasing either the thickness (and, therefore, the weight) of the tight deformable casing, or the cost and stiffness thereof, by using sheets with ribs comprising several concentric ribs.
Figs 3 b and 3 c show a possible embodiment of weldable fittings for rendering tight the deformable casing according to figs 2 and 3 a.
More precisely, fig 3 b shows a connecting member to be used for applying the tight deformable casing against the non developable surfaces, assuming ribs with only one corrugation (such as ribs 18, 19 and 20) are used Quite obviously connecting members with several corrugations might be contemplated This connecting member is used as follows: the cuttings of, e.g, triangular shape, made in connecting sheets 16 in the case of non developable surfaces obviously cause anchorage sheets to draw nearer to each other Whenever their spacing might become too narrow, 70 it is advisable to exchange some of them (as a rule, every second one) for connecting sheets 16 The latter are usually welded as an extension of anchorage sheets, except at interrupted rib 20 where, for en 75 suring tightness, it is necessary to provide a connecting member, such as that of fig.
3 b., welded astraddle both metal sheets.
Fig 3 c shows a cup shaped sealing cap of thick metal sheet, the diameter of 80 which is the same as that of anchoring sleeve, or bushing, 22 as shown in fig 3 a.
Once an anchoring sheet 15 has been fixed to the cavity wall (or to a suitable coat first applied to said wall), sealing cap 85 is welded to said sleeve of anchoring device 22 Fluid leakages through anchoring hole 24 are thus prevented.
It is to be noted that, in fig 3 c, an externally threaded pin 26, provided with a 90 nut, is welded to sealing cap 25; in fact, a ring or any other suitable fastening device might be used instead of said threeded pin.
Such an optimal arrangement permits to use sealing caps 25 as fastening means for 95 scaffolding or any devices used in the course of building the tank, or for maintenance operations or repairs.
As shown in fig 4, tight deformable casing 6 (which can with advantage be of 100 the type of figs 2 and 3 a) rests on a concrete lining 27 permitting to give a definitive shape to the cavity wall, applied before fixing tight deformable casing 6 by means of anchoring rods 28 passing through 105 anchoring holes 24; anchoring nuts 29 are screwed on the externally threaded ends of said rods 28 Sealing cap 25 is subsequently welded to the sleeve of anchoring device 22 110 Again in fig 4 are shown anchoring bolts provided with a distributing plate 31 and an anchoring device 32, the whole being arranged according to usual practice and constituting a paramount supporting 115 means for such cavities as those used as tanks according to the invention.
It can be contemplated to insert a lubricant substance 33 (or any other product likely to lessen friction forces at the 120 operating temperature involved) between tight metal casing 6 and the subjacent material.
Such an arrangement, which is to be found in figs 5 and 6, makes it possible 125 to restrict abrasion resulting from friction between the deformable casing and the subjacent material, and therefore proves to be favorable whatever the shape of said casing and of the subjacent material may be 130 1 572 305 Fig 5 shows another embodiment of the coat against which tight deformable casing 6 is applied As in the case of fig 4, anchoring bolts 30 are provided, with a distributing plate 31 and an anchoring device 32, said bolt still constituting a paramount supporting means The cavity walls are rendered smoother by means of a concrete lining 27 as above However, in the present instance, between tight deformable casing 6 and concrete lining 27, is sandwiched a thermally insulating material 34 of appropriate thickness, capable of withstanding the tank internal pressure transmitted through casing 6.
In fig 5, such thermally insulating medium, by way of example, is constituted by a concrete layer of low thermal conductivity, in which can be provided expansion joints 35 since tightness is ensured by casing 6 Said thermally insulating medium 34 is fastened to concrete lining 27 by means of hooks 36, whereas the tight deformable casing is fixed, as shown in fig.
4, by means of anchoring rods 28 inserted into the thermally insulating material Preferably, hooks 26 are not in alignment with anchoring bolts 30 and anchoring rods 30, nor in the immediate vicinity thereof, so as to avoid or restrict, thermal bridges.
Such an arrangement permits to limit the thermal flow between the fluid in the tank and the surrounding sub-soil formations.
Fig 6 shows a more elaborate embodiment of the coat against which deformable casing 6 is applied Generally of a structure similar to that shown in fig 5, the coat, between concrete lining 27 and thermally insulating material 34, additionally comprises a network of ducts 37 in which flows a coolant fluid With a view to restricting the number of ducts 37, it is preferable to provide a metal grid, a lattice of expanded metal or any other suitable thermally conductive material 38, thermally connected to ducts 37 and hooks 36, e g, by welding spots 39,40, respectively Such grid, lattice or thermally conductive material constitute a substantially isothermal surface at the average temperature of the colant fluid flowing in ducts 37 The circulation and cooling down of said fluid are obtained through pumping means and exchangers, e.g air coolants or means for exchanging heat with a heat sink (a river or the sea), such auxiliary means being outside the cavity and not shown.
The amount of heat thus dissipated varies only according to the temperature differential between coating 6 and the coolant fluid, to the thickness of thermally insulating medium 34 and to the thermal conductivity thereof A coherent selection of the values of these parameters will make it possible to restrict the dissipation of heat to a reasonable value In order to avoid troubles that might result from the thermal expansion of anchoring bolts 30, it is preferable to maintain said bolts at the same temperature as the coolant fluid To this 70 end is diagrammatically shown, in fig 6, a connecting box 41 connected to ducts 37 around the head of an anchoring bolt 30.
Thermal continuity between anchoring bolt and connecting box 41 is preferably ob 75 tained through the contact of the latter with distributing box 31, of usual design, used for maintaining anchoring bolt 30 in traction by means of nut 42 Connecting box 41 is maintained in position by means 80 of a counter-plate 43 contributing to ensure the requested thermal continuity, said counter-plate being attached to anchoring bolt 30 by means of an anchoring nut 44.
The type of cavity coat as shown in fig 6 85 is especially suited for high temperatures.
Inserting a thermally insulating medium, although restricting the flow of heat, is not sufficient however for preventing the temperature of adjacent sub-soil formations 90 from increasing gradually, which may give rise to troubles resulting from induced mechanical stresses.
While the calculation of such stresses is already intricate in the case of a well 95 known medium, it can lead to a severe disappointment when applied to a natural medium, the parameters of which are, of necessity, not very well known The rise of the soil temperature therefore leads to 100 hazards which, in practice, it is impossible to assess as regards the tank stability The arrangement of fig 6 permits one to delete, or at least lessen, the soil temperature increase Figs 7 a and 7 b shown details of a 105 possible embodiment of connecting box 41, in cross section and as seen from above, respectively In fig 7 a are shown in dotted line an anchoring bolt 30, with its distributing plate 31 and its anchoring nut 42 110 Such a bolt is fixed as follows: after having drilled a bore of suitable length in the cavity wall, the bolt is provisionally fixed to the bore end.
A flexible tube is forced into the an 115 nular space defined between the anchoring bolt and the soil; distribution plate 31 is then inserted and anchoring nut 42 is only partially screwed so as to allow the flexible tube to penetrate freely A yoke (not 120 shown) provided with two jacks applied against the sub-soil formations is previously screwed instead of anchoring nut 44, then anchoring bolt 30 is put in tension by means of said jacks Then concrete is 125 injected through the flexible tube, the latter being gradually extracted from the bore.
Once a sufficient amount of concrete has been injected, the flexible tube is with 130 1 572 305 drawn and plate 31 is locked by means of nut 42.
When the concrete is set, the jacks are released and the yoke is unscrewed It is then possible to mount box 41 and to lock the same by means of counter-plate 43 and anchoring nut 44 It is, then, only sufficient to make connections with ducts 37 by means of crooked fittings 45 (fig 7 a).
Figs 7 a and 7 b permit one to understand the principle of box 41 In these figures, said box 41 is assumed to be of circular shape and constituted by welded sheets; however, neither the shape of these boxes, nor the way they are manufactured, nor the material of which they are made, are specific features of the invention.
In the example reprsented in figs 7 a and 7 b, the box is made of thin metal sheet and it is all the thinner as thermally insulating material 34 is thicker and stiffer Box 41 is of annular shape and comprises several threaded ports in its upper surface.
Figs 7 a and 7 b represent a box with four ports, each of which is provided with a crooked fitting 45 (only one of which is shown in the figure).
Fig 7 c shows, seen from above, a set of two half boxes ( 41 a, 41 b) adapted to ensure the cooling of anchorage bolt 30 via two distinct circuits, which, in some cases, can be advantageous as regards the general tank safety.
Claims (1)
WHAT WE CLAIM IS: –
1 A method for storing fluid underground at maximum superatmospheric pressure p, comprising the steps of digging, at a depth at which the lithostatic pressure generated by the weight of the abovejacent soil formations is at least p, an underground cavity in which is made a tight deformable casing anchored to the cavity wall at some places only, while it can freely expand or contract in every direction between said anchoring places in order to follow closely corresponding movements of the cavity wall, then of injecting pressurized fluid into said casing in order that the latter be fully applied against the cavity wall, the possible movements of which said casing subsequently follows by sliding on the cavity wall, the pressure of said fluid being, at every moment, counterbalanced by the lithostatic pressure of the cavity walls transmitted to said fluid by the thus expanded casing.
2 A storing method according to claim 1, wherein a smoothing coat is inserted between said deformable casing and said cavity walls.
3 A tank for storing fluid underground at maximum superatmospheric pressure p, comprising, in an underground cavity dug at a depth at which the lithostatic pressure generated by the weight of the above jacent soil is at least p, a tight deformable casing anchored to the cavity wall at some places only while it can freely expand or contract in every direction between said anchoring places in order to follow closely 70 corresponding movements of the cavity wall, said casing being adapted to receive pressurized fluid so as to be fully applied against the cavity wall, the possible movements of which said casing 75 subsequently follows by sliding on the cavity wall, the pressure of said fluid being, at every moment, counterbalanced by the lithostatic pressure of the cavity wall transmitted to said fluid by the thus-expanded 80 casing.
4 A tank for storing pressurized fluids according to claim 1, wherein said tight deformable casing is constituted by a plurality of welded metal plates, said plates 85 being provided with an appropriate number of ribs of suitable shape allowing said plurality of plates to move freely between said anchoring places.
A tank for storing pressurized fluids 90 according to claim 4, wherein said plurality of metal plates is constituted by an assembly of embossed plates of metal sheet provided with ribs comprising only one corrugation or several parallel corrugations said plates 95 being of the following two types, viz:
-anchoring sheets comprising two ribs at right angles meeting at the sheet center through a distributing rib having the following features: said distributing rib forms 100 one or several corrugations substantially higher than said perpendicular ribs; it is provided, in the vicinity of the bisectors of the angles defined by said perpendicular ribs, with saddle shaped carvings that lower 105 the height of the ridge of said distributing rib to the level of the tops of said perpendicular ribs; it surrounds a hole of said anchoring sheet permitting the anchoring thereof to the cavity wall, said hole being 110 surrounded by a welded sleeve, or bushing, to which a sealing cap is fixed once said sheet has been fixed to the subjacent material; -connecting sheets without anchoring 115 points to the subjacent material, said sheets being provided with but one median rib, which permits one to cut said sheets, at will, in conformity with the dimensions and shape of the surface to be covered, said 120 sheets being welded to one another or to said anchoring sheets, either by causing the ribs to be without solution of continuity, or by using a connecting part of suitable shape so as to maintain tightness 125 wherever said ribs are interrupted.
6 A tank for storing pressurized fluids according to claim 5, wherein said sealing cap comprises a threaded rod, a ring or any other device capable of being used as 130 1 572 305 anchoring points for scaffoldings or various devices used when building said tank or for the maintenance thereof.
7.A tank for storing pressurized fluids according to any of claims 1 to 6, wherein, between said tight deformable casing and the subjacent material, is inserted a lubricant substance or any other substance likely to decrease friction at the operatng temperature involved.
8 A tank for storng pressurized fluids according to claim 2, wherein said smoothing coat contains a thermally insulating medium of appropriate thickness, capable of withstanding the fluid temperature and pressure.
9 A tank for storing pressurized fluids according to claim 8, wherein said thermally insulating medium is provided, on the face thereof opposite to said tight deformable casing, with a network of ducts in which flows a colant fluid maintained at suitable temperature by suitable auxiliary means.
10 A tank for storing pressurized fluids according to claim 9, wherein a metal grid, a lattice of expanded metal or any other casing of thermally conducting material is welded or thermally connected to said duct network.
11 A tank for storing pressurized fluids according to any of claims 9 or 10, wherein said network of ducts in which flows a coolant fluid comprises metal tubes and is provided with connecting boxes adapted to 35 distribute the flow of coolant fluid and thermally connected with the heads of anchoring bolts supported said cavity so as to ensure the cooling thereof.
12 A tank for storing pressurized fluids 40 according to claim 11, wherein, for each of said anchoring bolts, a counter plate locked by an achoring nut screwed on the free end of said anchoring bolt maintains said connecting box, or boxes, applied 45 against the distributing plate applied against said wall by means of said anchoring bolt, or bolts, or of said anchoring devices.
13 Application of the tanks for storing pressurized fluids according to any of the 50 above claims, to the underground storage of heat, compressed air, gas or radioactive waste.
14 A method for storing fluid underground substantially as described with 55 reference to the accompanying drawings.
A tank for storing fluid underground substantially as described and as shown in the accompanying drawings.
For the Applicants: F J CLEVELAND & COMPANY, Chartered Patent Agents, 40-43 Chancery Lane, London, WC 2 A 1 JQ.
Printed for Her Majesty’s Stationery Office by The Tweeddale Press Ltd, Berwick-upon-Tweed, 1980.
Published at the Patent Office, 25 Southampton Buildings, London, WC 2 A IAY, from which copies may be obtained
GB48815/77A
1976-12-02
1977-11-23
Method for storing pressurised fluid undergroud and a reservoir for effecting this method
Expired
GB1572305A
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
FR7636283A
FR2372751A1
(en)
1976-12-02
1976-12-02
UNDERGROUND TANK FOR PRESSURIZED FLUIDS
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GB1572305A
true
GB1572305A
(en)
1980-07-30
Family
ID=9180551
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Title
Priority Date
Filing Date
GB48815/77A
Expired
GB1572305A
(en)
1976-12-02
1977-11-23
Method for storing pressurised fluid undergroud and a reservoir for effecting this method
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Link
US
(1)
US4165945A
(en)
BE
(1)
BE861083A
(en)
CA
(1)
CA1091045A
(en)
DE
(1)
DE2753881A1
(en)
FR
(1)
FR2372751A1
(en)
GB
(1)
GB1572305A
(en)
SE
(1)
SE7713628L
(en)
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Title
FR2528811A1
(en)
*
1982-06-17
1983-12-23
Geostock
METHOD AND DEVICE FOR STORING GAS LIQUEFIED AT LOW TEMPERATURE IN A GROUND CAVITY
DE3340101A1
(en)
*
1983-11-05
1985-05-23
Deutsche Gesellschaft für Wiederaufarbeitung von Kernbrennstoffen mbH, 3000 Hannover
UNDERGROUND INTERMEDIATE STORAGE FOR COMBUSED CORE REACTOR FUEL ELEMENTS AND FOR GLAZED RADIOACTIVE WASTE
SE458443B
(en)
*
1985-07-03
1989-04-03
Torbjoern Hahn
SYSTEM FOR STORAGE OF LIQUID OR GAS IN A SPACE IN MOUNTAIN
AT392455B
(en)
*
1988-08-10
1991-04-10
Josef Auer
ARRANGEMENT FOR SUPPLYING WITH PRESSURE GAS
US7475791B2
(en)
*
2004-11-08
2009-01-13
Lee Jaslow
Toroidal tank
SE535370C2
(en)
*
2009-08-03
2012-07-10
Skanska Sverige Ab
Device and method for storing thermal energy
WO2013160897A1
(en)
*
2012-04-24
2013-10-31
Or Yogev
Hybrid system for electric power generation from solar-thermal energy and wind energy sources
KR20150133833A
(en)
2013-03-26
2015-11-30
코히러스 바이오사이언시즈, 인코포레이티드
Protein Production Method
JP6446773B2
(en)
*
2013-11-19
2019-01-09
株式会社Ihi
Low temperature tank
IL260175B
(en)
*
2018-06-20
2019-07-31
Or Yogev
System for storing compressed fluid
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Title
NL291792A
(en)
*
1962-06-09
US3557558A
(en)
*
1969-01-27
1971-01-26
Inst Gas Technology
Insulating and waterproofing system for storage tanks
GB1401915A
(en)
*
1973-01-31
1975-08-06
Carves Simon Ltd
Cryogenic storage tanks
SE380501B
(en)
*
1974-02-27
1975-11-10
Wp System Ab
PLANT FOR STORAGE OF LIQUID GAS, SPECIAL NATURAL GAS
1976
1976-12-02
FR
FR7636283A
patent/FR2372751A1/en
active
Granted
1977
1977-11-23
BE
BE182834A
patent/BE861083A/en
not_active
IP Right Cessation
1977-11-23
GB
GB48815/77A
patent/GB1572305A/en
not_active
Expired
1977-11-29
US
US05/855,641
patent/US4165945A/en
not_active
Expired – Lifetime
1977-11-29
CA
CA291,914A
patent/CA1091045A/en
not_active
Expired
1977-12-01
SE
SE7713628A
patent/SE7713628L/en
unknown
1977-12-02
DE
DE19772753881
patent/DE2753881A1/en
active
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Publication date
CA1091045A
(en)
1980-12-09
BE861083A
(en)
1978-03-16
FR2372751B1
(en)
1980-11-28
US4165945A
(en)
1979-08-28
FR2372751A1
(en)
1978-06-30
DE2753881A1
(en)
1978-06-08
SE7713628L
(en)
1978-06-03
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Legal Events
Date
Code
Title
Description
1980-10-15
PS
Patent sealed
1987-07-15
PCNP
Patent ceased through non-payment of renewal fee
