WO2023118713A1 - Système d'injection d'un gaz dans une cuve de stockage - Google Patents
Système d'injection d'un gaz dans une cuve de stockage Download PDFInfo
- Publication number
- WO2023118713A1 WO2023118713A1 PCT/FR2022/052414 FR2022052414W WO2023118713A1 WO 2023118713 A1 WO2023118713 A1 WO 2023118713A1 FR 2022052414 W FR2022052414 W FR 2022052414W WO 2023118713 A1 WO2023118713 A1 WO 2023118713A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- storage tank
- gas
- corrugated
- nozzle
- circular
- Prior art date
Links
- 239000012528 membrane Substances 0.000 claims abstract description 103
- 238000009413 insulation Methods 0.000 claims abstract description 74
- 238000002347 injection Methods 0.000 claims abstract description 57
- 239000007924 injection Substances 0.000 claims abstract description 57
- 230000004888 barrier function Effects 0.000 claims abstract description 46
- 239000012530 fluid Substances 0.000 claims abstract description 19
- 230000002093 peripheral effect Effects 0.000 claims description 49
- 238000000034 method Methods 0.000 claims description 35
- 238000007789 sealing Methods 0.000 claims description 9
- 239000007789 gas Substances 0.000 description 105
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 8
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 229910021529 ammonia Inorganic materials 0.000 description 4
- 238000004458 analytical method Methods 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 238000010408 sweeping Methods 0.000 description 3
- 230000000295 complement effect Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 239000003949 liquefied natural gas Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000000700 radioactive tracer Substances 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 238000004868 gas analysis Methods 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/022—Land-based bulk storage containers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0119—Shape cylindrical with flat end-piece
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/03—Orientation
- F17C2201/032—Orientation with substantially vertical main axis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- 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
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0375—Thermal insulations by gas
- F17C2203/0379—Inert
-
- 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
- F17C2203/0682—Special properties of materials for vessel walls with liquid or gas layer
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
- F17C2250/04—Indicating or measuring of parameters as input values
- F17C2250/0404—Parameters indicated or measured
- F17C2250/0447—Composition; Humidity
- F17C2250/0452—Concentration of a product
-
- 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
- F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
- F17C2250/04—Indicating or measuring of parameters as input values
- F17C2250/0486—Indicating or measuring characterised by the location
- F17C2250/0491—Parameters measured at or inside the vessel
-
- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/035—Dealing with losses of fluid
- F17C2260/037—Handling leaked fluid
-
- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/035—Dealing with losses of fluid
- F17C2260/038—Detecting leaked fluid
-
- 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
- F17C2270/0102—Applications for fluid transport or storage on or in the water
- F17C2270/0105—Ships
- F17C2270/0107—Wall panels
-
- 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
- F17C2270/0134—Applications for fluid transport or storage placed above the ground
- F17C2270/0136—Terminals
Definitions
- the present invention relates to a system for injecting a gas into a storage tank for a fluid whose liquefaction temperature is below -50° C. at atmospheric pressure, and in particular the injection of the gas into a space under a corrugated waterproof membrane of said storage tank, as well as a gas evacuation assembly.
- Fluid storage tanks whose liquefaction temperature is below -50°C at atmospheric pressure allow this fluid to be stored before, during or after its transport.
- Such storage tanks then usually comprise at least one thermal insulation barrier covered by the corrugated waterproof membrane comprising a plurality of corrugations.
- the at least one thermal insulation barrier as well as the corrugated sealed membrane participate in particular in delimiting an internal volume of the storage tank in which the fluid in question is placed.
- the thermal insulation barrier and the corrugated waterproof membrane also make it possible to store this fluid in optimal storage conditions both in terms of temperature and pressure.
- the corrugated sealed membrane being in direct contact with the fluid, it must retain its sealing properties in order to allow efficient storage of the fluid whose liquefaction temperature is lower than - 50° C. atmospheric pressure.
- gas injections can also be used in storage tank inerting processes, i.e. when the internal volume of the storage tank contains the fluid. The inerting process allows, among other things, to sweep the space under the corrugated waterproof membrane by means of an inerting gas in order to ensure, for example, the tightness of the corrugated waterproof membrane.
- the object of the present invention is therefore to propose an improvement and a simplification of the means allowing the control of the sealing of the corrugated sealed membrane and/or of inerting of the fluid storage tank whose liquefaction temperature is lower than - 50°C at atmospheric pressure.
- the invention therefore relates to a storage tank for a fluid whose liquefaction temperature is less than -50° C. at atmospheric pressure, the storage tank having a cylindrical shape around an axis of revolution with a bottom wall , an upper wall and a cylindrical peripheral wall connecting the bottom wall and the upper wall, said storage tank comprising at least one thermal insulation barrier covered by a corrugated waterproof membrane and such that the corrugated waterproof membrane delimits a volume internal of the storage tank, the corrugated sealed membrane comprising a plurality of corrugations which participate in delimiting a space between said corrugations and the at least one thermal insulation barrier, the storage tank comprising at least one injection system of a gas in space, characterized in that the gas injection system comprises at least one circular pipe which extends around the axis of revolution of the storage tank, the said circular pipe being located in the space delimited by the undulations of the corrugated sealed membrane of the bottom wall and the thermal insulation barrier (12), the gas injection system comprising at least one nozzle fluidly connected to the circular conduit and such that the
- the storage tank according to the invention makes it possible to store, for example and in a non-limiting manner, liquefied natural gas and is preferably an onshore tank.
- the circular pipe of the injection system extends around the axis of revolution of the storage tank, the axis of revolution thus passing inside a perimeter defined by the circular pipe.
- the injection of gas through the at least one nozzle into the space formed between the undulations of the corrugated sealed membrane and the thermal insulation barrier makes it possible to control the tightness of the corrugated waterproof membrane via complementary means, for example arranged in the internal volume and capable of detecting the presence of gas in said internal volume, revealing a leak through the corrugated waterproof membrane, in particular at the level of its welds.
- the gas injected can be a tracer gas, for example ammonia or helium.
- the injection of gas through the at least one nozzle into the space under the corrugations allows said gas to spread in an insulation volume of the storage tank.
- the insulation volume of the storage tank comprises the thermal insulation barrier as well as the space formed between the corrugated waterproof membrane and said thermal insulation barrier. It is then understood that the insulation volume comprises the space under the corrugations of the corrugated waterproof membrane mentioned above as well as the space between the thermal insulation barrier and flat portions of the corrugated waterproof membrane, added to the volume defined by the thickness of the thermal insulation barrier.
- the injection system of the invention makes it possible to fill the entire insulation volume of the storage tank, by means of at least one nozzle disposed in the space formed between the undulations of the sealed membrane. corrugated and the thermal insulation barrier.
- such injection of gas into space can be used in an inerting process, in the presence of the liquid whose liquefaction temperature is below -50° C at atmospheric pressure contained in the internal volume of the vessel.
- the gas injected called inerting or sweeping, may be nitrogen.
- the gas injection system comprises at least one assembly for supplying gas from the circular pipe, the supply assembly comprising at least one supply ring which extends around the axis of revolution.
- the gas injection system makes it possible to route the gas from a gas storage unit, external to the tank, to at least the circular pipe in such a way that said gas is injected by the at least one nozzle.
- the supply ring can be arranged in the peripheral wall of the storage tank.
- the ring supply can be arranged in the upper wall of the storage tank. More precisely, according to this second example of the invention, the supply ring can extend in a peripheral edge of the upper wall, the peripheral edge of the upper wall being the zone of the upper wall in contact with the wall peripheral.
- the role of the supply ring is to distribute the gas around the tank to supply the circular pipe, advantageously at at least two points.
- the storage tank can comprise a gas supply device disposed in the internal volume of the storage tank and fluidly connected to the circular pipe.
- a gas supply device can be complementary to the supply assembly comprising the supply ring, in particular during the process for checking the tightness of the corrugated waterproof membrane, for example to inject more gas into the pipe. circular.
- the supply assembly comprises at least one supply pipe which extends mainly in the space of the peripheral wall and in such a way that it fluidically connects the circular pipe with the power ring.
- the supply line extends at least in the peripheral wall and in the bottom wall of the storage tank.
- the supply assembly may comprise two supply lines which extend opposite to each other with respect to the axis of revolution of the storage tank.
- the bottom wall comprises a peripheral edge and a center aligned with the axis of revolution of the storage tank, the circular pipe being arranged closer to the center of the bottom wall than to its edge. peripheral.
- peripheral edge of the bottom wall corresponds to an area where the bottom wall and the peripheral wall are in contact with each other.
- the at least one nozzle injects the gas under the undulations of the corrugated sealed membrane of the bottom wall in the direction of its peripheral edge.
- the gas thus sweeps or fills the space and the insulation volume by moving towards the peripheral wall, so as to borrow it and reach the upper part of the storage tank.
- the corrugated sealed membrane is configured such that at least its corrugations formed at the level of the peripheral wall communicate fluidly with its corrugations formed at the level of the bottom wall.
- the entire insulation volume of the storage tank is configured such that it communicates fluidly at least between the insulation volume arranged at the level of the bottom wall and the insulation volume of the peripheral wall. It is thus possible, by the injection of gas into the space under the undulations of the corrugated sealed membrane of the bottom wall and in the direction of the peripheral edge, to sweep or fill with this gas the volume of insulation of the wall of the bottom and the peripheral wall, including in the thickness of the insulation space of these walls.
- the at least one nozzle is capable of reducing a gas pressure at the outlet of said nozzle relative to the gas pressure at the inlet of said nozzle.
- an inlet section of the at least one nozzle is strictly less than an outlet section of said nozzle.
- Such a characteristic of the invention makes it possible, for example and in a non-limiting manner, to obtain a gas pressure of 25mbar at the outlet of the nozzle when it was 200mbar at the inlet of said nozzle.
- the at least one nozzle is placed at a distance of between 200mm and 5000mm from the circular pipe.
- the at least one nozzle is arranged at a distance of between 400mm and 600mm.
- Such an arrangement of the nozzle relative to the circular pipe makes it possible to ensure a stable gas flow at least in the circular pipe and at the outlet of the nozzle.
- At least the corrugated sealed membrane arranged at the level of the bottom wall comprises circular corrugations which extend around the axis of revolution of the storage tank and radial corrugations, secant of the corrugations circular, and which extend in a radial direction of the storage tank, the circular pipe extending at least under one of the circular undulations of the corrugated sealed membrane.
- the circular undulations and the radial undulations communicate fluidly with each other.
- the corrugated waterproof membrane of the peripheral wall may comprise a similar distribution of its undulations, and in such a way that it comprises the circular undulations and axial undulations, secant from its circular undulations and which extend along a vertical direction of the storage tank, the axial corrugations of the corrugated waterproof membrane of the peripheral wall being aligned with the radial corrugations of the corrugated waterproof membrane of the bottom wall.
- the radial corrugations at the bottom wall and the axial corrugations at the peripheral wall communicate fluidly with each other.
- an injection axis of the at least one nozzle is aligned on a main axis of a radial corrugation of the corrugated sealed membrane arranged at the level of the bottom wall.
- the at least one supply pipe extends at least in the space under one of the radial undulations of the corrugated sealed membrane of the bottom wall.
- the at least one supply pipe can extend at least in the space delimited by an axial corrugation of the corrugated sealed membrane of the peripheral wall.
- the injection system comprises at least one injection device which extends inside a perimeter delimited by the circular pipe. More particularly, the injection device extends under a radial corrugation of the bottom wall, in the space delimited between said radial corrugation of the corrugated sealed membrane and the thermal insulation barrier.
- the at least one injection device comprises at least one additional nozzle disposed at one of its ends which extends in the perimeter delimited by the circular pipe, said additional nozzle injecting gas at least within the perimeter delimited by the circular pipe.
- the tank comprises a plurality of nozzles arranged around the circular pipe and such that each of the nozzles are spaced apart from each other by an angle of between 25° and 70° around the axis of revolution of the storage tank.
- an evacuation system provided with at least one circular evacuation pipe which extends around the axis of revolution of the storage tank, advantageously outside its internal volume, the system evacuation comprising at least one evacuation conduit which at least partially passes through the peripheral wall of the storage tank into the thermal insulation barrier, the evacuation conduit being fluidly connected to the circular evacuation conduit.
- the evacuation system comprises two evacuation ducts installed at 180° relative to each other.
- the circular evacuation pipe extends around the peripheral wall of the storage tank and is connected to a gas recovery and/or analysis device, in order to recover and/or analyze the gas evacuated at least the insulation volume of the storage tank.
- Such Evacuation system can be implemented within the framework of the sealing and/or inerting control process mentioned above.
- the invention also relates to a method for checking the tightness of a corrugated tight membrane of a storage tank according to any one of the preceding characteristics, the method implementing at least the gas injection system.
- the tightness control process is the one that aims to check the tightness, in particular the welds between the plates that make up the corrugated waterproof membrane.
- the invention also relates to a method for scanning an insulation volume of a storage tank according to any one of the preceding characteristics, the method implementing at least the gas injection system.
- the sweeping process otherwise called the inerting process, is the one that aims to renew the volume of gas present in the thermal insulation barrier, or between this barrier and the corrugated waterproof membrane, by sweeping this space by means of a inerting gas.
- Advantage is thus taken of the injection system of the invention in that it allows the gas injected by the at least one nozzle to sweep the entire insulation volume of the storage tank comprising the insulation barrier heat and the space between the corrugated waterproof membrane and said barrier.
- the invention finally proposes a method for injecting a gas into a space of a storage tank according to any one of the preceding characteristics, in which the gas is injected into the gas injection system so that 'it circulates at least in the circular conduit at a pressure of between 170mbar and 230mbar and in such a way that it emerges from the at least one nozzle at a pressure of between 20mbar and 30mbar.
- FIG 1 is a schematic general view of a storage tank comprising a gas injection system according to the invention
- FIG 2 is a close-up view of part of a bottom wall of the storage tank showing a circular pipe and at least one nozzle of the gas injection system of Figure 1;
- FIG. 3 is a schematic sectional view of a corrugation of a corrugated sealed membrane of the storage tank of FIG. 1 showing a space in which the gas injection system extends at least in part.
- FIG. 1 illustrates a storage tank 1 for a fluid whose liquefaction temperature is lower than -50° C. at atmospheric pressure, for example a liquefied natural gas or ammonia, the storage tank 1 being particularly used for the storage of such a fluid on a terrestrial space.
- the storage tank 1 according to the invention has a circular cylindrical shape around an axis of revolution R, with at least one bottom wall 2, an upper wall 4 and a peripheral wall 6 which connects them. More particularly, the bottom wall 2 and the upper wall 4 are opposite one another along the axis of revolution R of the storage tank 1 and the peripheral wall 6 extends in such a way that it connects a peripheral edge 8 of each of the bottom wall 2 and the top wall 4, one to the other.
- the bottom wall 2, the upper wall 4 and the peripheral wall 6 mentioned above then make it possible to delimit an internal volume 10 of the storage tank 2 in which can be contained the fluid whose liquefaction temperature is lower than -50° C. atmospheric pressure.
- the storage tank 2 comprises at least one thermal insulation barrier 12 covered by a corrugated waterproof membrane 14 and such that the corrugated waterproof membrane 14 is in contact with the internal volume 10 of the storage tank 1.
- An insulation volume 13 of the storage tank 1 is then defined comprising at least the thermal insulation barrier 12 and the space formed between the corrugated waterproof membrane 14 and said barrier.
- the storage tank 1 may comprise more than one thermal insulation barrier, for example a first thermal insulation barrier and a second thermal insulation barrier, and a secondary sealed membrane placed between this first barrier thermal insulation and this second thermal insulation barrier, such a set of barriers and secondary sealed membrane then forming part of the insulation volume of the storage tank.
- a thermal insulation barrier for example a first thermal insulation barrier and a second thermal insulation barrier
- a secondary sealed membrane placed between this first barrier thermal insulation and this second thermal insulation barrier, such a set of barriers and secondary sealed membrane then forming part of the insulation volume of the storage tank.
- the thermal insulation barrier 12 reduces heat loss from the storage tank 1 in order to guarantee optimum preservation of the fluid whose liquefaction temperature is below -50° C. at atmospheric pressure in the storage tank 1.
- the corrugated waterproof membrane 14 seals the storage tank by ensuring that this fluid is maintained in the internal volume 10 of the tank 2.
- the corrugated waterproof membrane 14 comprises flat portions 22 and a plurality of undulations 18 visible in Figures 2 and 3, which surrounds the flat portions.
- corrugation 18 is meant a deformation of the corrugated waterproof membrane 14 in a direction perpendicular to a main plane P of the corrugated waterproof membrane 14 in which the flat portions 22 are inscribed.
- the corrugations 18 of the corrugated waterproof membrane 14 correspond to a deformation in an axial direction A of the storage tank 1, parallel to the axis of revolution R.
- the undulations 18 of the corrugated waterproof membrane 14 then have a concave shape seen in a section perpendicular to the main plane P of the corrugated waterproof membrane 14.
- the thermal insulation barrier 12 and the corrugated sealed membrane 14 extend at least against the bottom wall 2 and the peripheral wall 6 of the storage tank 1.
- Such a configuration of the storage tank 1 provides it with greater resistance to the stresses generated by the storage of the fluid whose temperature of liquefaction is less than -50° C at atmospheric pressure, in particular thermal shrinkage when the storage tank is cooled or hydrostatic pressure due to the loading of the fluid in the liquid state.
- the plurality of undulations 18 participate in delimiting a space 20 between said undulations 18 and the at least one thermal insulation barrier 12, visible in FIG. 3. More precisely, the undeformed portions of the corrugated waterproof membrane 14 form the flat portions 22 which extend in the main plane P of the corrugated waterproof membrane 14 and which are in contact with the thermal insulation barrier 12.
- the corrugations 18 of the membrane corrugated seal 14 make it possible, among other things, to generate the space 20 between said corrugations 18 and the thermal insulation barrier 12.
- the corrugated sealed membrane 14 disposed at least at the level of the bottom wall 2 of the storage tank 1 comprises circular undulations 18a which extend around the axis of revolution R of the storage tank 1 and radial undulations 18b, secant of the circular undulations 18a, and which extend in a radial direction L of the storage tank 1. It is further understood that the radial undulations 18b and the circular undulations 18a of the membrane sealed corrugated 14 fluidly communicate with each other.
- Such an arrangement of the corrugated sealed membrane 14 at least at the level of the bottom wall 2 notably allows the latter to adapt to the particular shape of the cylindrical storage tank 1.
- the peripheral wall 6 of the storage tank 1, visible in FIG. 1, comprises the circular undulations 18d and axial undulations 18c, intersecting the circular undulations 18d and extending in the axial direction of the storage tank 1
- the corrugated waterproof membrane 14 is configured in such a way that the radial corrugations 18b at the level of the bottom wall 2 and the axial corrugations 18c at the level of the peripheral wall 6 are aligned with each other in such a way that they communicate fluidly.
- the space 20 formed between the corrugations 18 of the corrugated sealed membrane 14 and the thermal insulation barrier 12 is fluidically common for the whole of the storage tank 1 where the corrugated sealed membrane 14 is arranged.
- the insulation volume 13 of the storage tank 1, located at the level of the bottom wall 2 communicates fluidly with the insulation volume 13 located at the level of the peripheral wall 6.
- the storage tank 1 comprises at least one system 24 for injecting a gas into the space 20 described previously.
- a gas injection system 24 is notably used in processes for inerting the storage tank 1 or else in processes for checking the tightness of the corrugated sealed membrane 14.
- the gas injected by the injection system 24 can then be, in a non-limiting manner, nitrogen or even ammonia, or a tracer gas which can be detected in the event of a leak at the level of a weld.
- other means external to the injection system are implemented, such as a gas evacuation system which will be described later in the description.
- the gas injection system 24 comprises at least one circular pipe 26 which extends around the axis of revolution R of the storage tank 1. terms, the axis of revolution R of the storage tank 1 passes through a perimeter E defined by the circular pipe 26.
- the circular pipe 26 extends in the space 20 between the undulations 18 of the corrugated waterproof membrane 14 of the bottom wall 2 and the thermal insulation barrier 12. More precisely, the circular pipe 26 extends in the space 20 formed between one of the circular undulations 18a of the corrugated waterproof membrane 14 which extends at the level of the bottom wall 2 and the thermal insulation barrier 12.
- a center C of the bottom wall 2 is then defined which is aligned with the axis of revolution R of the storage tank 1.
- the circular pipe 26 is then arranged closer to the center C of the bottom wall 2 than to its peripheral edge 8 mentioned above.
- the circular pipe 26 extends in a radius of between 2m and 2.5m from the center C of the bottom wall 2. This arrangement closer to the center C than to the peripheral edge 8 guarantees the gas supply of a great length of the radial undulations 18b of the bottom wall 2.
- the gas injection system 24 comprises at least one nozzle 28 connected fluidically to the circular pipe 26 and so that the at least one nozzle 28 injects the gas under the corrugations 18 of the corrugated sealed membrane 14. More particularly, an injection axis I of the nozzle 28, visible in FIGS. or 2, is aligned on a main axis A of a radial corrugation 18b of the corrugated sealed membrane 14 arranged at the level of the bottom wall 2.
- the gas is injected through at least one nozzle 28 into the space 20 defined previously. More particularly, the at least one nozzle 28 injects the gas into the space 20 under the corrugations 18 of the corrugated sealed membrane 14 of the bottom wall 2 and in the direction of its peripheral edge 8.
- the at least one nozzle 28 injects the gas into the space 20 under the corrugations 18 of the corrugated sealed membrane 14 of the bottom wall 2 and in the direction of its peripheral edge 8.
- Such a characteristic of the au at least one nozzle 28 allows the injected gas to circulate at least in the space 20 formed under the corrugations 18 of the corrugated sealed membrane 14 which extends at least at the level of the bottom wall 2 and continues at the level of the wall device 6. It is also understood that such a characteristic of the at least one nozzle 28 allows the gas to sweep or fill the insulation volume 13 of the storage tank 1, at the level of the bottom wall 2 up to to the insulation volume 13 located at the level of the peripheral wall 6.
- the at least one nozzle 28 is capable of reducing a pressure of the gas at the outlet of said nozzle 28 with respect to the pressure of the gas at the inlet of said nozzle 28.
- an outlet section of the nozzle 28 is strictly greater than an inlet section of said nozzle 28, the inlet and the outlet of the nozzle 28 being defined with respect to a direction of circulation of the gas in the nozzle 28.
- the outlet of the at least one nozzle 28 is placed at a distance D, visible in FIG. 2, between 200mm and 5000mm, from the circular pipe 26.
- a distance D visible in FIG. 2, between 200mm and 5000mm, from the circular pipe 26.
- the gas pressure at the nozzle inlet 28 is 200 mbar and is nozzle 28.
- the gas injection system 24 comprises a plurality of nozzles 28, as detailed above, arranged around the circular pipe 26 and such that each nozzles 28 are separated from each other by an angle G, visible in Figure 2, between 25° and 70° around the axis of revolution R of the storage tank 1.
- each angular sector of the bottom wall 2 of the storage tank 1, representing between 25° and 70° around the axis of revolution R, is bordered by a nozzle 28.
- the gas injection system 24 comprises at least one assembly 30 for supplying gas to the circular pipe 26.
- Such an assembly includes the pipes and pipes necessary to supply the gas to the circular pipe 26 exposed more high.
- the feed assembly 30 comprises at least one feed ring 32, visible in FIG. 1, which extends around the axis of revolution R of the storage tank 1 so that it peripherally distributes the gas around said storage tank 1.
- the supply ring 32 extends in the peripheral wall 6 of the storage tank 1.
- the supply ring supply 32 can then be arranged at different heights in the peripheral wall 6, along the axial direction A of the storage tank 1, thus making it possible to adapt to different configurations of storage tank 1.
- the supply ring can extend into the peripheral edge of the upper wall mentioned above.
- the supply ring 32 is fluidically connected to a storage unit 33 for the gas to be injected, arranged outside the storage tank 1.
- Supply assembly 30 also includes at least one supply conduit 34 which extends into space 20 and such that it fluidly connects circular conduit 26 with supply ring 32.
- the supply line 34 extends at least in the space 20 under one of the radial undulations 18b of the corrugated sealed membrane 14 of the bottom wall 2, as can be seen in FIG. example of the invention illustrated in FIG. 1, the supply pipe 34 also extends in space under one of the axial corrugations 18c of the corrugated sealed membrane 14 of the peripheral wall 6 which extends in the extension of the aforementioned radial undulation.
- the supply assembly 30 may comprise two supply lines 34 arranged opposite each other with respect to each other. to the axis of revolution R of the storage tank 1.
- Such a configuration of the supply assembly 30 makes it possible, among other things, to improve the distribution of the gas to the circular pipe 26 by supplying it at two opposite points .
- the injection system 24 comprises at least one injection device 36 which extends inside the perimeter E defined by the circular pipe 26. precise, the injection device 36 extends from the circular pipe 26 and in the direction of the center C of the bottom wall 2 of the storage tank 1.
- the injection device 36 extends under one of the radial corrugations 18b of the corrugated sealed membrane 14 of the bottom wall 2.
- the injection device 36 can extend in the radial extension of a supply pipe 34 which travels under a radial corrugation 18b of the corrugated membrane which equips the bottom wall 8.
- the injection device 36 then comprises at least one additional nozzle 38 arranged at one of its ends which extends in the perimeter E delimited by the circular pipe 26 and opposite the latter.
- the additional nozzle 38 then makes it possible to inject gas at least into the perimeter E delimited by the circular pipe 26. This makes it possible to sweep or fill, with the injected gas, the entire space 20 formed between the corrugations 18 of the corrugated waterproof membrane 14 and the thermal insulation barrier 12 and therefore, the entire insulation volume 13 of the storage tank 1.
- a method of injecting gas into the storage tank 1 will now be described in relation to FIGS. 1 to 3. It is understood that the method of injecting gas can be used in the methods for checking the tightness of the membrane sealed corrugated or in the inerting processes of the storage tank 1.
- the gas stored in the gas storage unit is injected into the supply ring 32 at a pressure comprised for example between 170 mbar and 230 mbar.
- the gas injected into the supply ring 32 circulates vertically then radially in the at least one supply pipe 34 until it reaches the circular pipe 26.
- the latter is injected by the at least one nozzle 28 in the space 20 formed between the corrugations 18 of the corrugated waterproof membrane 14 and the barrier thermal insulation 12. More specifically, the gas is injected through at least one nozzle 28 such that it has a pressure of between 20 mbar and 30 mbar, at the outlet of said nozzle 28.
- Such a pressure at the outlet of at least one nozzle 28 then makes it possible to improve the diffusion of the gas in the whole of the space 20 of the storage tank 1 and in the insulation volume 13 of the storage tank 1.
- a gas evacuation process is implemented in order to recover the gas injected by the at least one nozzle 28 into the space 20 and the insulation volume 13 of storage tank 1.
- the gas evacuation method implements an evacuation system 40, visible in FIG. 1, comprising at least one circular evacuation pipe 42 which extends around the axis of revolution R of the storage tank. 1, and outside the internal volume 10 of the latter. More particularly, the circular discharge pipe 42 extends around the peripheral wall 6 of the storage tank 1.
- the evacuation system 40 also comprises at least one evacuation conduit 44 which passes through at least in part the peripheral wall 6 of the storage tank 1, the at least one evacuation conduit 44 being fluidly connected to the conduit circular evacuation pipe 42. More particularly, the evacuation conduit 44 extends into the thermal insulation barrier 12. It is then understood that the evacuation conduit 44 makes it possible to capture the gas injected into the insulation volume 13 of the storage tank 1. Thus, the gas collected by the at least one evacuation pipe 44 is directed into the circular evacuation pipe 42, the latter being fluidically connected to a recovery device and/or analysis 46 of the gas, in order to recover and/or analyze the gas evacuated at least from the isolation volume 13 of the storage tank 1.
- Gas analysis means in particular the analysis of its composition, for example in ammonia or helium within the framework of the process for checking the tightness of the membrane sealed corrugated membrane 14 or nitrogen during the process of inerting the storage tank 1.
- the presence of at least one gas other than those mentioned in the process for checking the tightness of the corrugated sealed membrane 14 is indicative of a leak of the latter.
- the evacuation system 40 comprises two evacuation ducts 44 arranged radially opposite one another with respect to the axis of revolution R of the storage tank 1
- Such a configuration of the evacuation system 40 makes it possible to optimize the capture of gas in the insulation volume 13 of the storage tank 1.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202280085702.7A CN118591706A (zh) | 2021-12-22 | 2022-12-19 | 将气体注入储罐的系统 |
EP22847576.0A EP4453466A1 (fr) | 2021-12-22 | 2022-12-19 | Système d'injection d'un gaz dans une cuve de stockage |
CA3240293A CA3240293A1 (fr) | 2021-12-22 | 2022-12-19 | Systeme d'injection d'un gaz dans une cuve de stockage |
MX2024007678A MX2024007678A (es) | 2021-12-22 | 2022-12-19 | Sistema de inyeccion de gas en un tanque de almacenamiento. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2114223A FR3130932B1 (fr) | 2021-12-22 | 2021-12-22 | Système d’injection d’un gaz dans une cuve de stockage |
FR2114223 | 2021-12-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2023118713A1 true WO2023118713A1 (fr) | 2023-06-29 |
Family
ID=80735846
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/FR2022/052414 WO2023118713A1 (fr) | 2021-12-22 | 2022-12-19 | Système d'injection d'un gaz dans une cuve de stockage |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP4453466A1 (fr) |
CN (1) | CN118591706A (fr) |
CA (1) | CA3240293A1 (fr) |
FR (1) | FR3130932B1 (fr) |
MX (1) | MX2024007678A (fr) |
WO (1) | WO2023118713A1 (fr) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2662800A1 (fr) * | 1990-06-05 | 1991-12-06 | Nippon Kokan Kk | Procede de detection d'un defaut dans un reservoir de gaz liquides liquefies. |
FR2739675A1 (fr) * | 1995-10-05 | 1997-04-11 | Gaztransport Et Technigaz | Cuve terrestre pour le stockage du liquide a basse temperature |
KR20170038233A (ko) * | 2015-09-30 | 2017-04-07 | 대우조선해양 주식회사 | 화물 저장탱크 및 그의 배관 시스템 |
KR20190081550A (ko) * | 2017-12-29 | 2019-07-09 | 대우조선해양 주식회사 | 액화천연가스 운반선 화물창의 불활성 가스 파이프 시스템 |
WO2019180372A1 (fr) * | 2018-03-21 | 2019-09-26 | Gaztransport Et Technigaz | Procede de diffusion d'un gaz traceur et procede de test de l'etancheite d'une membrane |
WO2019180373A1 (fr) * | 2018-03-21 | 2019-09-26 | Gaztransport Et Technigaz | Cloche de détection de fuite pour membrane d'étanchéité |
FR3084347A1 (fr) * | 2018-07-27 | 2020-01-31 | Gaztransport Et Technigaz | Paroi etanche a membrane ondulee renforcee |
WO2020229777A1 (fr) * | 2019-05-16 | 2020-11-19 | Gaztransport Et Technigaz | Cuve de transport et/ou de stockage pour gaz sous forme liquide |
-
2021
- 2021-12-22 FR FR2114223A patent/FR3130932B1/fr active Active
-
2022
- 2022-12-19 EP EP22847576.0A patent/EP4453466A1/fr active Pending
- 2022-12-19 CN CN202280085702.7A patent/CN118591706A/zh active Pending
- 2022-12-19 MX MX2024007678A patent/MX2024007678A/es unknown
- 2022-12-19 WO PCT/FR2022/052414 patent/WO2023118713A1/fr active Application Filing
- 2022-12-19 CA CA3240293A patent/CA3240293A1/fr active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2662800A1 (fr) * | 1990-06-05 | 1991-12-06 | Nippon Kokan Kk | Procede de detection d'un defaut dans un reservoir de gaz liquides liquefies. |
FR2739675A1 (fr) * | 1995-10-05 | 1997-04-11 | Gaztransport Et Technigaz | Cuve terrestre pour le stockage du liquide a basse temperature |
KR20170038233A (ko) * | 2015-09-30 | 2017-04-07 | 대우조선해양 주식회사 | 화물 저장탱크 및 그의 배관 시스템 |
KR20190081550A (ko) * | 2017-12-29 | 2019-07-09 | 대우조선해양 주식회사 | 액화천연가스 운반선 화물창의 불활성 가스 파이프 시스템 |
WO2019180372A1 (fr) * | 2018-03-21 | 2019-09-26 | Gaztransport Et Technigaz | Procede de diffusion d'un gaz traceur et procede de test de l'etancheite d'une membrane |
WO2019180373A1 (fr) * | 2018-03-21 | 2019-09-26 | Gaztransport Et Technigaz | Cloche de détection de fuite pour membrane d'étanchéité |
FR3084347A1 (fr) * | 2018-07-27 | 2020-01-31 | Gaztransport Et Technigaz | Paroi etanche a membrane ondulee renforcee |
WO2020229777A1 (fr) * | 2019-05-16 | 2020-11-19 | Gaztransport Et Technigaz | Cuve de transport et/ou de stockage pour gaz sous forme liquide |
Also Published As
Publication number | Publication date |
---|---|
CN118591706A (zh) | 2024-09-03 |
CA3240293A1 (fr) | 2023-06-29 |
FR3130932B1 (fr) | 2023-11-10 |
EP4453466A1 (fr) | 2024-10-30 |
FR3130932A1 (fr) | 2023-06-23 |
MX2024007678A (es) | 2024-07-09 |
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