EP4295045A1 - Device for compressing a fluid stored in the form of a cryogenic liquid, and associated method of manufacture - Google Patents
Device for compressing a fluid stored in the form of a cryogenic liquid, and associated method of manufactureInfo
- Publication number
- EP4295045A1 EP4295045A1 EP22710681.2A EP22710681A EP4295045A1 EP 4295045 A1 EP4295045 A1 EP 4295045A1 EP 22710681 A EP22710681 A EP 22710681A EP 4295045 A1 EP4295045 A1 EP 4295045A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cryogenic
- enclosure
- pressure
- gas
- compression device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000007788 liquid Substances 0.000 title claims abstract description 59
- 239000012530 fluid Substances 0.000 title claims abstract description 45
- 238000004519 manufacturing process Methods 0.000 title claims description 36
- 238000000034 method Methods 0.000 title claims description 30
- 239000007789 gas Substances 0.000 claims abstract description 85
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims abstract description 14
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 7
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052786 argon Inorganic materials 0.000 claims abstract description 7
- 229910001882 dioxygen Inorganic materials 0.000 claims abstract description 7
- 238000007906 compression Methods 0.000 claims description 86
- 230000006835 compression Effects 0.000 claims description 83
- 238000003860 storage Methods 0.000 claims description 30
- 238000010438 heat treatment Methods 0.000 claims description 28
- 239000000463 material Substances 0.000 claims description 28
- 238000007493 shaping process Methods 0.000 claims description 24
- 230000001681 protective effect Effects 0.000 claims description 21
- 238000009834 vaporization Methods 0.000 claims description 16
- 230000008016 vaporization Effects 0.000 claims description 16
- 238000003780 insertion Methods 0.000 claims description 11
- 230000037431 insertion Effects 0.000 claims description 11
- 239000002131 composite material Substances 0.000 claims description 8
- 239000011810 insulating material Substances 0.000 claims description 8
- 239000011347 resin Substances 0.000 claims description 8
- 229920005989 resin Polymers 0.000 claims description 8
- 238000000605 extraction Methods 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 7
- 229910001873 dinitrogen Inorganic materials 0.000 claims description 6
- 238000005242 forging Methods 0.000 claims description 5
- 239000007769 metal material Substances 0.000 claims description 4
- 238000004804 winding Methods 0.000 claims description 4
- 239000000835 fiber Substances 0.000 claims description 3
- 239000008187 granular material Substances 0.000 claims description 3
- 239000013529 heat transfer fluid Substances 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 229920002493 poly(chlorotrifluoroethylene) Polymers 0.000 claims description 3
- -1 polychlorotrifluoroethylene Polymers 0.000 claims description 3
- 239000005023 polychlorotrifluoroethylene (PCTFE) polymer Substances 0.000 claims description 3
- 230000005855 radiation Effects 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 2
- 238000000576 coating method Methods 0.000 claims description 2
- 238000004090 dissolution Methods 0.000 claims description 2
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 238000003303 reheating Methods 0.000 abstract 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 9
- 238000009413 insulation Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 229920000049 Carbon (fiber) Polymers 0.000 description 3
- 239000004917 carbon fiber Substances 0.000 description 3
- 230000000295 complement effect Effects 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000005219 brazing Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 210000004907 gland Anatomy 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000010420 art technique Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
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- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/001—Thermal insulation specially adapted for cryogenic vessels
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- F17C9/00—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F17C2223/033—Small pressure, e.g. for liquefied gas
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/04—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
- F17C2223/042—Localisation of the removal point
- F17C2223/043—Localisation of the removal point in the gas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/04—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
- F17C2223/042—Localisation of the removal point
- F17C2223/046—Localisation of the removal point in the liquid
- F17C2223/047—Localisation of the removal point in the liquid with a dip tube
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/01—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
- F17C2225/0107—Single phase
- F17C2225/0123—Single phase gaseous, e.g. CNG, GNC
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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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/01—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
- F17C2225/0146—Two-phase
- F17C2225/0153—Liquefied gas, e.g. LPG, GPL
- F17C2225/0161—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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/03—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the pressure level
- F17C2225/036—Very high pressure, i.e. above 80 bars
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/04—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by other properties of handled fluid after transfer
- F17C2225/042—Localisation of the filling point
- F17C2225/046—Localisation of the filling point in the liquid
- F17C2225/047—Localisation of the filling point in the liquid with a dip tube
-
- 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/01—Propulsion of the fluid
- F17C2227/0107—Propulsion of the fluid by pressurising the ullage
-
- 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0304—Heat exchange with the fluid by heating using an electric heater
-
- 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another fluid
- F17C2227/0323—Heat exchange with the fluid by heating using another fluid in a closed loop
-
- 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
- F17C2250/06—Controlling or regulating of parameters as output values
- F17C2250/0605—Parameters
- F17C2250/0626—Pressure
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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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/02—Improving properties related to fluid or fluid transfer
-
- 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
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/06—Fluid distribution
- F17C2265/065—Fluid distribution for refuelling vehicle fuel tanks
-
- 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
- F17C2270/0139—Fuel stations
-
- 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
- Y02E60/30—Hydrogen technology
- Y02E60/32—Hydrogen storage
Definitions
- the field of the invention is that of gas storage.
- the invention relates to a device for compressing a fluid stored in the form of a cryogenic liquid and an associated method of manufacture.
- the invention finds applications in particular for the storage of dihydrogen with a view to powering an electric vehicle, or for the storage of other fluids such as dioxygen, dinitrogen, argon or methane.
- cryogenic techniques In order to reduce the bulk and transportation of the gas, techniques have been developed to store the gas in liquid form, usually at cryogenic temperatures. [8] Such techniques generally include a cryogenic tank whose insulation is carried out for a vacuum enclosure surrounding the internal enclosure of the tank.
- cryogenic enclosures are most often a metallic material offering mechanical characteristics suitable for low temperatures, i.e. temperatures below -20°C.
- reservoirs made of composite material, such as those comprising carbon fiber are poorly suited to low temperatures since they generally do not withstand the mechanical stresses associated with the pressure at these temperatures.
- the present invention aims to remedy all or part of the drawbacks of the state of the art mentioned above.
- the invention relates to a device for compressing a gas, such as dihydrogen, dioxygen, dinitrogen, or argon, comprising - a cryogenic enclosure, capable of containing the fluid in liquid form at a cryogenic temperature, and fluid in the form of gas originating from vaporization of the liquid in the cryogenic enclosure;
- a gas such as dihydrogen, dioxygen, dinitrogen, or argon
- a pressure enclosure including the cryogenic enclosure, configured to withstand internal pressure
- the balancing device comprising a pipe configured to transfer gas under overpressure in the cryogenic enclosure in a space comprised between the pressure enclosure and the cryogenic enclosure, the piping comprising a device for heating the pressurized gas coming from the cryogenic enclosure, to a predetermined temperature above the cryogenic temperature.
- the fluid can be compressed to a high pressure without the use of a complex mechanical device by reinjecting the pressurized gas resulting from the vaporization of the cryogenic liquid contained in the cryogenic enclosure.
- the cryogenic enclosure is advantageously immersed in a pressurized environment in which the pressure is balanced between the interior and the exterior of the cryogenic enclosure. The pressure stresses are thus transferred to the pressure enclosure which includes the cryogenic enclosure.
- the temperature of the pressure vessel in service is preferably greater than -20°C in order to guarantee the mechanical resistance of the pressure vessel at high pressures, the maximum value of which is for example order from 100 to 800 bar.
- the compression device is not intended to store the fluid over a long period but is rather intended to be inserted into a storage system comprising a cryogenic tank storing the fluid in liquid form and a final storage tank.
- the compression device corresponds to an intermediate stage making it possible to supply the final storage tank with a compressed gas resulting from the vaporization of part of the cryogenic liquid previously stored in the cryogenic tank.
- the compressed gas can then be used to supply, for example, a tank of a vehicle equipped with a fuel cell to generate electricity that powers an electric motor of the vehicle.
- the gas heating device is a heat exchanger placed outside the pressure vessel.
- the heat exchanger can be of the gas/gas or gas/fluid type in order to heat the gas extracted from the cryogenic enclosure to a temperature suitable for the pressure enclosure.
- a suitable temperature can be determined according to the stresses admissible by the pressure enclosure at the chosen operating pressure.
- the shape and type of the heat exchanger are determined according to the power to be extracted and the inlet and outlet temperatures of the exchanger.
- the heating device includes a thermal resistor inserted in the piping.
- the thermal resistance can be inside or outside the pressure enclosure.
- the compression device includes a conduit for introducing the fluid in liquid form into the cryogenic enclosure, the conduit passing through the walls of the pressure enclosure and of the cryogenic chamber, the piping of the balancing device comprising:
- balancing duct passing through the pressure enclosure and emerging between the pressure enclosure and the cryogenic enclosure, the balancing duct being connected to an outlet of the heating device.
- the compression device also comprises a heating device inside the cryogenic enclosure configured to vaporize the fluid in liquid form with a predetermined flow of energy.
- the heating device comprises an electrical resistor and/or a conduit for the circulation of a heat transfer fluid.
- the pressure vessel and the cryogenic vessel are generally cylindrical in shape around the same axis of revolution.
- the pressure enclosure is essentially formed from a metallic material, and configured to withstand a maximum internal pressure of between 100 and 800 bar.
- the cryogenic enclosure comprises a layer of a solid insulating material resistant to cryogenic temperatures and to the fluid.
- the solid insulating material is polychlorotrifluoroethylene (PTCFE).
- the invention also relates to a method of manufacturing a compression device according to any one of the preceding embodiments, the method of manufacturing comprising steps of:
- a reflective material is introduced before the step of shaping the constriction in order to protect the cryogenic enclosure from thermal radiation.
- the step of shaping a constriction is carried out by deforming the open end.
- the deformation is carried out by forging.
- the step of shaping a constriction is carried out by joining a part together.
- the manufacturing method comprises a step of inserting a plug before the step of shaping a constriction, the plug making it possible to close the enclosure of pressure tightly.
- the method of manufacture comprises a step of threading the narrowing of the open end of the pressure vessel, the thread being configured to mate with a thread of the cap.
- the shaping of the pressure vessel is carried out by forging.
- the manufacturing process includes a step of adding an outer reinforcing layer of composite material.
- This addition step can advantageously be carried out by winding at least one strip of fibre, preferably carbon, coated with resin around the pressure vessel.
- the protective material is a mixture of a granular material and a liquid resin.
- the invention also relates to an alternative method of manufacturing a compression device according to any one of the preceding embodiments, comprising the steps of:
- the invention also relates to a system for storing a fluid, such as dihydrogen, dioxygen, dinitrogen or argon, comprising:
- cryogenic tank storing the fluid in liquid form at a pressure below 10 bar and at a temperature below -150°C;
- a pressurized gas storage tank configured to withstand a maximum internal pressure of between 100 and 800 bar.
- the invention also relates to a process for compressing a fluid stored in liquid form in a cryogenic tank of said storage system, comprising the steps of:
- the compression method also comprises a step of bypassing the overpressure gas when the pressure inside the compression device is greater than a predetermined value, the bypass gas being transferred to the pressurized gas storage tank of the storage system.
- the compression method also comprises a step of emptying part of the gas from the compression device, in order to lower the internal pressure of the compression device to a value lower than the pressure of the cryogenic tank, prior to a new filling of the cryogenic enclosure of the compression device with fluid in liquid form at a cryogenic temperature coming from the cryogenic tank.
- FIG. 1 is a perspective view of a storage system comprising an exemplary embodiment of the compression device according to the invention
- FIG. 1 is a sectional view of the compression device of Figure 1;
- FIG. 3 is a block view of a mode of implementation of a method of manufacturing the compression device of Figure 1;
- Figure 4 comprises five successive views illustrating the manufacturing process of Figure 3;
- FIG. 5 is a block view of an implementation mode of a compression method implementing the system of Figure 1;
- FIG. 6 includes two sectional views of another example embodiment of a compression device that can be inserted into the storage system of Figure 1;
- FIG. 7 is a block view of an embodiment of a method of manufacturing the compression device of Figure 6.
- Figure 1 is a perspective view of a storage system 100 comprising a compression device 110 according to the invention.
- the compression device 110 corresponds to an intermediate stage between a cryogenic tank 120 storing a fluid in the form of a liquid and a second tank 130 storing the fluid in the form of a pressurized gas for example to feed a tank of a vehicle (not shown in Figure 1).
- the fluid is dihydrogen (H2) used to power a fuel cell of the vehicle whose engine is electric.
- H2 dihydrogen
- the present invention can also be applied to the storage of other types of fluid, such as dinitrogen (N2), dioxygen (O2), argon (Ar) or methane (ChL) by adapting the dimensions if necessary. and the operating conditions which are described below.
- the present invention applies to fluids whose liquid/gas phase change temperature is less than 120 K (that is to say approximately -150°C).
- cryogenic liquid fluid in liquid form
- gas in gaseous form fluid in gaseous form
- the compression device 110 makes it possible on the one hand to vaporize the cryogenic liquid coming from the cryogenic tank 120 where it is stored for example at 10 bar and at a temperature of 3 K (that is to say -270 ° C), and on the other hand to compress the gas obtained without the use of complex mechanical parts at pressures of the order of 300 to 800 bar.
- the compression device 110 is mainly composed of two chambers 210 formed by an internal cryogenic enclosure 220 and by an outer pressure enclosure 230 encompassing the enclosure cryogenic 220.
- the cryogenic enclosure 220 and the pressure enclosure 230 are generally cylindrical in shape around the same axis 235 of revolution.
- the cryogenic enclosure 220 is intended to contain a predetermined quantity of cryogenic liquid 225 which has been transferred from the cryogenic reservoir 120 through a conduit 240.
- the conduit 240 passes through the walls of the pressure enclosure 230 and of the enclosure cryogenic 220, through plugs 231 and 221, and opens into a lower part of the cryogenic enclosure 220 in order to limit the evaporation of the cryogenic liquid during the filling phase.
- part of the cryogenic liquid 225 vaporizes initially with a high flow rate, in particular in a phase of heating up the cryogenic enclosure 220, then with a lower flow rate when the temperature of the cryogenic chamber 220 has stabilized.
- the flow rate then corresponds to the energy flow E P passing through the cryogenic enclosure 220 by conduction, the structure of which is not optimized to store the cryogenic liquid over a long period of time but configured only to contain the cryogenic liquid 225 during its vaporization phase. .
- the compression device 110 comprises a device 250 for balancing the pressure between the chamber 210A inside the cryogenic enclosure 220 and the chamber 210B between the pressure enclosure 230 and the cryogenic enclosure 220 .
- the pressure equalization device 250 comprises piping configured to transfer gas under overpressure into the cryogenic enclosure 220 in a space between the pressure enclosure 230 and the cryogenic enclosure 220, namely here in the chamber 210B whose volume is equal to the interior volume of the pressure enclosure 230 from which is subtracted the volume of the cryogenic enclosure 220.
- the piping of the device 250 for balancing the pressure comprises a device 270 for heating the gas coming from the cryogenic enclosure 220, to a predetermined temperature above the cryogenic temperature.
- the predetermined temperature may for example be equal to 250 K (about -20°C), at room temperature, or at any other temperature between 250 K and room temperature.
- the device 270 for heating the gas is a heat exchanger placed outside the pressure enclosure 230, as shown in Figure 2.
- the heat exchanger is configured to allow the gas coming from of the cryogenic enclosure 220 on average at the predetermined temperature.
- the heat exchanger can be of the gas/gas or gas/liquid type, and is configured to withstand high pressures.
- the advantage of the heat exchanger is to have zero impact on the energy balance of the operation of the compression device 110, the gas moving naturally between the two enclosures of the compression device 110, crossing the heat exchanger.
- the heat exchanger can consist, for example, of projecting fins around the piping or of a more complex shape capable of withstanding the pressure, such as a tube exchanger.
- the device 270 for heating the gas can be a resistance heater.
- the piping of the device 250 for balancing the pressure comprises a pipe 251 for extracting gas under overpressure, passing through the pressure enclosure 230 and the cryogenic enclosure 220 towards an inlet of the device 270 for heating some gas.
- the piping of the pressure equalization device 250 also includes an equalization conduit 252 allowing the gas extracted from the cryogenic enclosure 220 to be returned to the chamber 210B.
- the balancing conduit 252 is connected to an outlet of the gas heating device 270, passes through the pressure enclosure 230 and emerges between the pressure enclosure 230 and the cryogenic enclosure 220.
- Chamber 210B thus stores gas under pressure at a temperature of around 250 K, while chamber 210A stores fluid at a cryogenic temperature.
- the flow of vaporization of the cryogenic liquid in the cryogenic enclosure 220 corresponds at least to the flow of thermal energy E P passing through the walls.
- the vaporization flow can be increased by an energy supply made for example by means of a heating device 280 inserted inside the cryogenic enclosure 220. This energy supply which can be varied automatically or manually by an operator makes it possible to adjust the flow of vaporization of the cryogenic liquid.
- the heating device 280 may for example be composed of an electrical resistor and/or a conduit for the circulation of a heat transfer fluid.
- the pressure enclosure 230 is essentially formed in a metallic material, thus allowing a configuration of the enclosure to withstand a maximum internal pressure of the order of 800 bar.
- the cryogenic enclosure 220 is essentially formed, in this non-limiting example of the invention, in a solid insulating material resistant to cryogenic temperatures.
- the solid insulating material used for the cryogenic enclosure 220 is inert to the fluid contained.
- the solid insulating material used is polychlorotrifluoroethylene (PTCFE), conferring good mechanical properties in terms of insulation and resistance of the materials to cryogenic temperatures.
- PTCFE polychlorotrifluoroethylene
- cryogenic enclosure 220 formed in such an insulating material tends to deteriorate when the internal pressure is greater than 5 or 10 bar compared to the external pressure. Its main role is then to provide a container suitable for the temporary storage of the cryogenic liquid coming from the cryogenic tank 120, during the phase of isochoric compression of the gas resulting from the vaporization of the cryogenic liquid, while minimizing the thermal losses in order to adjust to the better the quantity of gas produced by vaporization of the cryogenic liquid.
- a valve 290 is opened in order to transfer pressurized gas into the storage tank 130.
- a valve 295 for emptying the device 110 of compression can be included in the circuit in order to lower the internal pressure of the device 110 of compression to a value lower than the pressure of the cryogenic tank 120, prior to a new filling of the cryogenic enclosure 220 of the compression device 110 with cryogenic liquid coming from the cryogenic tank 120.
- Figure 3 is a block view of an example of implementation of a method 300 of manufacturing the device 110 of compression according to the invention.
- the figure 4 illustrates in schematic form the progress of the manufacture of the device 110 of compression.
- the manufacturing process 300 includes a first step 310 of shaping the pressure vessel 230 into the overall shape of a slender cylinder 400 closed at one end 410, the other open end 420 being left straight in a first time to allow the insertion of the cryogenic enclosure 220 during a second 320 of the manufacturing process 300, as illustrated by sub-figure a) of FIG. 4.
- the shaping of the first step 310 can be carried out by example by a classic boilermaking technique from a pipe or a disc deformed by a press.
- a protective material 430 is inserted in a liquid form into the chamber 210B between the pressure enclosure 230 and the cryogenic enclosure 220 during a third step 330 of manufacture, as illustrated by sub-figure b) of figure 4.
- the protective material which is for example a mixture of resin and of a granular material such as sand, will harden after its insertion in the chamber 210B .
- the protective material may have been previously heated to thin it, thus allowing its insertion into the chamber 210B. As it cools, the protective material will harden, taking on the shape of the chamber 210B.
- a shaping of a constriction 440 of the open end 420 of the pressure vessel 230 is then carried out during the fourth step 340 of the method 300 of manufacturing, after the protective material has hardened.
- This shaping can be done by deforming the open end 420, for example by a forging technique, or by securing a complementary piece of suitable shape.
- the joining of the complementary part can be done by brazing or welding.
- the pressure vessel 230 is locally heated to a temperature high enough to be likely to irreversibly damage the cryogenic vessel 220.
- the prior insertion of the protective material during the step 330 makes it possible to minimize the rise in temperature of the cryogenic enclosure 220 during the step 340 of shaping the narrowing of the open end of the enclosure under pressure 230.
- the thickness of the pipe used to shape the pressure vessel 230 generally corresponds to that defined by the "schedule 160" type so that the ratio between the thickness and the diameter is large enough to resist mechanical stresses due to the nominal pressure of 700 to 800 bar.
- reinforcement by adding an outer layer 460 of composite material can be considered during a optional step 345.
- the outer layer 460 of composite material can for example be produced by winding at least one strip 465 of carbon fiber coated with resin.
- a reflective material such as a screen can be introduced before the shaping step 340, in order to protect the cryogenic enclosure 220 from the thermal radiation induced during the shaping step. shaping.
- the protective material 430 is then dissolved and extracted from the compression device 110 during a fifth step 350 of the manufacturing process 300.
- the compression device 110 is finalized by closing the pressure vessel 230 in a sealed manner during a sixth step 360 of the manufacturing process 300, as illustrated in sub-figure d) of Figure 4.
- a plug 450 of frustoconical shape making it possible to close the pressure enclosure is inserted before the step 340 of shaping the constriction 440 during an optional step 325 of the manufacturing process 300, for example just after the insertion of the cryogenic chamber 220.
- the stopper 450 is threaded in a manner complementary to a thread of the constriction 440 of the open end 420, previously made.
- a cylindrical plug is inserted into the constriction 440 and secured to the constriction by a welding or brazing technique.
- the protective material 430 is advantageously retained, the steps 350 and 360 of the manufacturing process possibly being reversed.
- the plugs have through holes, preferably threaded in order to allow the various conduits 240, 251 and 252 to pass through cable glands previously installed.
- the protective material 430 can thus be extracted from the chamber 210B through the through hole provided for the duct 252 for balancing.
- the cryogenic enclosure 220 is held in position inside the pressure enclosure 230 by means of cable glands tightly clamping the conduits 240 and 251 when they pass through the plugs 221 and 450 of each enclosure.
- Figure 5 presents a block view of an implementation mode of a method 500 for compressing the fluid stored in the form of cryogenic liquid in the cryogenic tank 120.
- the compression method 500 includes a first step 510 of filling the cryogenic enclosure 220 of the compression device 110 with cryogenic liquid via the conduit 240 for introduction.
- the cryogenic liquid vaporizes inside the cryogenic enclosure during a third stage 530 of the compression process 500. This vaporization can be increased by adding an energy supply via the heating device 280 which preferentially immerses in the cryogenic liquid.
- the pressurized gas above the cryogenic liquid in the cryogenic enclosure 220 is then extracted from the cryogenic enclosure 220 via the extraction conduit 251 during a fourth step 540 of the process 500 of compression.
- the extracted gas is reheated to a temperature close to or greater than 250 K (approximately -20°C) during a fifth stage 550 before being reinjected into the pressure enclosure 230, more precisely into the chamber 210B between the pressure enclosure 230 and the cryogenic enclosure 220, during a sixth step 560 of the compression method 500.
- bypass can advantageously be carried out in the circuit of the balancing device 250 after the gas has passed through the heating device 270.
- the gas is diverted upstream of the heating device 270.
- an auxiliary heating device is preferably installed on the pipe connecting the bypass of the balancing device 250 to the storage tank 130.
- the method 500 may also include a step 580 of emptying part of the gas from the compression device 110, in order to lower the internal pressure of the compression device 110 to a value lower than the pressure of the cryogenic reservoir 120. The process 500 can then begin again.
- the cryogenic tank 120 has a volume of the order of 3000 to 10000 liters.
- the volume of the cryogenic enclosure 220 is for its part of the order of 100 to 300 liters.
- the volume of chamber 210B is generally between two and five times larger, preferably three times larger, than that of cryogenic enclosure 220 in order to provide a high compression ratio.
- the density of the gas is generally a thousand times lower than that of the liquid, the vaporization of the liquid in a given volume consequently leads to a natural increase in the pressure, which is allowed here thanks on the one hand to the presence of the pressure enclosure 230 and on the other hand thanks to the balancing circuit making it possible to transfer the gas between the two chambers 210 of the device 110 of compression while heating it to avoid a degradation of the mechanical resistance of the pressure enclosure 230.
- the volume of the storage tank 130 is generally three times greater than that of the chamber 210B, composed for example of three sub-tanks of the same volume as that of the chamber 210B. These three sub-tanks can be in different sub-circuits so that they can be filled or emptied individually.
- Figure 6 illustrates another example of a compression device 600 according to the invention which was produced according to an alternative manufacturing method 700 presented in the block diagram in Figure 7.
- the compression device 600 differs from the compression device 100 of the previous exemplary embodiment in that the pressure vessel 630 is composed of a metal skeleton 631 of generally cylindrical shape, replacing the pipe used during of the manufacturing process 300, as shown in subfigure a) of Figure 6.
- the metallic structure 631 is enveloped by an outer layer 632 of composite material maintaining the pressure, as shown in subfigure b) of Figure 6.
- the cryogenic enclosure 620 of the compression device 600 can advantageously comprise a plurality of legs 621 making it possible to hold the cryogenic enclosure 620 during the development of the compression device 600.
- the manufacturing process 700 thus comprises a first step 710 of producing the metal skeleton 631 surrounding the cryogenic enclosure 620 which can be positioned upstream or inserted when the metal skeleton 631 is produced.
- the skeleton 631 of the pressure vessel 630 is then wrapped by at least one strip of resin coated carbon fiber to form the outer layer 632.
- the thickness of the outer layer 632 is configured to resist the stresses mechanical due to the nominal pressure of 700 to 800 bar. It should be emphasized that any other type of composite material, responding to mechanical stresses, can be envisaged by those skilled in the art.
- the pressure enclosure 630 can then be closed by the plug 650, during a third step 730, similar to the manufacturing process 300, the plug 650 having been previously inserted inside the skeleton 631 .
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Separation By Low-Temperature Treatments (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2101698A FR3120097B1 (en) | 2021-02-22 | 2021-02-22 | Device for compressing a fluid stored in the form of a cryogenic liquid, and associated manufacturing method |
PCT/FR2022/050322 WO2022175636A1 (en) | 2021-02-22 | 2022-02-22 | Device for compressing a fluid stored in the form of a cryogenic liquid, and associated method of manufacture |
Publications (1)
Publication Number | Publication Date |
---|---|
EP4295045A1 true EP4295045A1 (en) | 2023-12-27 |
Family
ID=75108610
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP22710681.2A Pending EP4295045A1 (en) | 2021-02-22 | 2022-02-22 | Device for compressing a fluid stored in the form of a cryogenic liquid, and associated method of manufacture |
Country Status (8)
Country | Link |
---|---|
US (1) | US20240142057A1 (en) |
EP (1) | EP4295045A1 (en) |
JP (1) | JP2024506989A (en) |
KR (1) | KR20240019060A (en) |
CN (1) | CN117098914A (en) |
CA (1) | CA3215673A1 (en) |
FR (1) | FR3120097B1 (en) |
WO (1) | WO2022175636A1 (en) |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19544593C5 (en) * | 1995-11-30 | 2006-03-09 | Air Liquide Deutschland Gmbh | Vacuum-insulated cryocontainer |
US6430938B1 (en) * | 2001-10-18 | 2002-08-13 | Praxair Technology, Inc. | Cryogenic vessel system with pulse tube refrigeration |
US20140026597A1 (en) * | 2010-09-30 | 2014-01-30 | Michael Jay Epstein | Fuel storage system |
US9752728B2 (en) * | 2012-12-20 | 2017-09-05 | General Electric Company | Cryogenic tank assembly |
FR3033874B1 (en) * | 2015-03-20 | 2018-11-09 | Gaztransport Et Technigaz | METHOD FOR COOLING A LIQUEFIED GAS |
EP3181986A1 (en) * | 2015-12-17 | 2017-06-21 | Shell Internationale Research Maatschappij B.V. | Mitigating lng boiloff by application of peltier cooling |
FR3089600B1 (en) * | 2018-12-06 | 2021-03-19 | Air Liquide | Cryogenic fluid storage tank |
-
2021
- 2021-02-22 FR FR2101698A patent/FR3120097B1/en active Active
-
2022
- 2022-02-22 KR KR1020237031965A patent/KR20240019060A/en unknown
- 2022-02-22 US US18/547,177 patent/US20240142057A1/en active Pending
- 2022-02-22 CA CA3215673A patent/CA3215673A1/en active Pending
- 2022-02-22 EP EP22710681.2A patent/EP4295045A1/en active Pending
- 2022-02-22 WO PCT/FR2022/050322 patent/WO2022175636A1/en active Application Filing
- 2022-02-22 CN CN202280020680.6A patent/CN117098914A/en active Pending
- 2022-02-22 JP JP2023551102A patent/JP2024506989A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
WO2022175636A1 (en) | 2022-08-25 |
FR3120097B1 (en) | 2023-02-17 |
CA3215673A1 (en) | 2022-08-25 |
JP2024506989A (en) | 2024-02-15 |
KR20240019060A (en) | 2024-02-14 |
FR3120097A1 (en) | 2022-08-26 |
US20240142057A1 (en) | 2024-05-02 |
CN117098914A (en) | 2023-11-21 |
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