• 专利附录
  • 专利说明
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    • 专利摘要:
    The invention relates to a container (200) for a heat storage and recovery system comprising an enclosure in which a gas circulates for cooling or heating. The enclosure is bounded by a first concrete envelope (203) surrounded by a thermally insulating layer (206), itself surrounded by a steel shell (204). The enclosure comprises at least two modules (210), each having a double concrete wall and a perforated bottom (205) delimiting at least two volumes (217 and 216) each capable of containing a fixed bed of particles of a material of storage and heat recovery (207). The modules are arranged one above the other centrally such that the double concrete wall forms the first concrete shell (203) and a second concrete shell (215).
    公开号:FR3054028A1
    申请号:FR1656804
    申请日:2016-07-15
    公开日:2018-01-19
    发明作者:Fabrice Deleau；Florence Richard；David Teixeira
    申请人:IFP Energies Nouvelles IFPEN；
    IPC主号:
    专利说明:

    Field of the invention
    The present invention relates to the field of heat storage, in particular containers for the storage of large volume heat, as used for energy storage by compressed air (CAES from English “Compressed Air Energy Storage”). , in particular for the storage of energy by compressed air of the AACAES type (from the English “Advanced Adiabatic Compressed Air Energy Storage”) in which the air storage and the storage of the heat generated independently are provided.
    General context
    The majority of primary energy sources, such as gas, oil, coal, can be stored easily, and thus allow production of electricity on demand, unlike the production of electricity from energy sources. renewable energies such as wind or solar energy. To supply electricity on demand, produced by this type of renewable energy, it is necessary to store electricity. However, it is very difficult to store electricity in large quantities. It is nevertheless possible to convert electricity into so-called intermediate energies, and to store it in the form of potential energy, kinetic, chemical or thermal.
    Electricity can for example be stored in the form of compressed air. This is what is achieved in CAES systems in which energy, typically electricity, which one wishes to use at another time, is stored in the form of compressed air. For storage, electrical energy drives air compressors, and for destocking, compressed air drives turbines which are connected to an electric generator. Compressed air is typically stored in a basement cavity, a porous rock formation, an exhausted oil or gas reservoir, or any other compressed air reservoir, which can be a pressure vessel. The performance of this solution is not optimal because part of the energy of the compressed air is found in the form of heat which is not used: the heat produced during the compression of the air is rejected. On the other hand, the stored air is heated to achieve expansion of the air, which again penalizes the energy efficiency of the system.
    Several variants currently exist to this CAES system. Mention may in particular be made of the systems and processes:
    • ACAES (from the English "Adiabatic Compressed Air Energy Storage") in which air is stored at high temperature due to compression. However, this type of system requires a specific, bulky and expensive storage system (adiabatic storage).
    • AACAES (from the English "Advanced Adiabatic Compressed Air Energy Storage") in which air is stored at room temperature, and the heat due to compression is also stored, separately, in a TES heat storage system (from the English "Thermal Energy Storage"). The heat stored in the TES system is used to heat the air before it expands.
    According to some envisaged designs of the AACAES, the heat is stored using a heat transfer fluid making it possible to store the heat resulting from the compression of the air and to return it to the air before its expansion by means of heat exchangers. For example, patent application EP 2447501 describes an AACAES system in which oil, used as a heat transfer fluid, circulates in a closed circuit to exchange heat with air.
    According to other proposed designs of AACAES, heat is stored by means of static solids contained in one or more containers. For example, the heat is stored in a material in the form of particles in a fixed bed placed in one or more containers, and traversed by the air to be cooled. This heat is returned to the cold air which crosses the fixed bed in the opposite direction during a discharge phase (air decompression).
    The present invention relates to a container of the latter type, capable of receiving a heat storage material in the form of particles in a fixed bed.
    The container is advantageously used for storing energy in the form of compressed air of the AACAES type, but is not limited to this application. Thus, the container can be suitable for any application implementing a heat storage and return system requiring a large heat storage capacity, and which may require resistance to high temperatures and pressures. By way of example, mention may be made of other fields of application than that of energy storage in the form of compressed air, such as the field of metallurgy, for example in the context of recovery and restitution of the heat from blast furnace fumes, the field of marine energy storage, etc.
    A major difficulty consists in designing containers for heat storage systems which can be operated at high pressures, of the order of several tens of bars, typically pressures up to 65-85 bars, and which can operate at high temperatures, typically several hundred degrees C, up to 750 ° C.
    To withstand high temperatures and high pressures, TES generally include large cylindrical concrete tanks filled with heat storage material, which have thick walls of prestressed concrete that can be reinforced with steel, and which can have various wall reinforcement structures, for example of the spacer type, to resist the stresses exerted on the walls due to internal pressure.
    For example, a TES is known in the context of the storage of adiabatic compressed air capable of operating at very high temperature, for example up to 650 ° C., and at pressures up to 65 bar, as described in patent EP1857614B. This storage system comprises a double structure formed by two capsules nested one inside the other, with an external pressure capsule made of prestressed concrete, and an internal capsule made of heat-resistant concrete and containing the heat storage material. , for example stacked ceramic elements. This system relies on a mechanical contribution from the concrete wall to contain the internal pressure. This imposes on-site production with the production of prestressed concrete, without possible production in the workshop. In addition, such systems, involving the construction of cylindrical concrete walls of great thicknesses (more than 1 m for example) pose engineering difficulties, and are expensive and complex to produce. Finally, this system does not make it possible to respond to the pressure constraints targeted today in TES systems, which are rather of the order of 125 bars, or even 300 bars.
    There is also known a heat storage system which can store heat at pressures greater than 3-4 bars, which can be used in quasi-adiabatic compressed air storage systems, as described in patent FR2998556A1. Such a container has refractory concrete walls surrounded by a steel shell, a thermal insulator being provided between the steel shell and the concrete walls. The sandwich structure formed by the set of refractory concrete walls / insulation / steel shell makes it possible to reduce heat losses by insulating the thermal storage material, makes it possible to reduce the temperature of the steel wall thus limiting the degradation of the characteristics of the latter makes it possible to limit the skin temperature of the steel shell improving safety, and makes it possible to contain the pressure prevailing in the container depending on the thickness of the steel shell. The container according to FR2998556A1 also includes grids for holding the heat storage material which can be arranged at different heights in the container, which also play the role of spacers limiting the stress exerted on the walls. This configuration makes it possible to maintain the storage material at different heights in the container, thus helping to limit the stress exerted on the walls, and also allows a better distribution of the material in the tank which improves the interaction of the air. with the storage material.
    During air loading and unloading operations, the structure undergoes thermal expansion, in particular at the level of the grids. In order to absorb these expansions, the heat storage system according to FR2998556A1 provides that the grids are fixed to the concrete walls by rings associated with chains, avoiding the generation of mechanical stresses during thermal expansion.
    However, due to the significant efforts involved in the storage of the material, it is difficult to implement such a container comprising grids fixed by a system of rings and chains poorly suited to the quantity and the weight of the material used. , in particular in AACAES type applications in which several hundred tonnes of material in the form of particles are stored in tanks with a capacity of between approximately 200 m 3 and 1000 m 3 . In addition, such a fastening system is bulky.
    Objectives and summary of the invention
    The present invention provides a new embodiment of heat storage systems adapted to high pressure conditions, which can typically operate up to pressures of the order of 300 bars, and adapted to moderate temperature conditions, typically maximum temperatures. of the order of 300 ° C.
    In particular, the present invention aims to provide a TES container which can both withstand high internal pressures linked to pressurized gas which can be greater than 100 bars and even go up to 300 bars, and both withstand the stresses exerted by the heat storage material arranged in the form of a fixed bed of particles in the container.
    The present invention also aims to limit the problems associated with thermal expansion during heat storage and return operations, to reduce the costs of manufacturing the container, and to facilitate assembly of the container.
    Thus, to achieve at least one of the abovementioned objectives, among others, and to at least partially overcome the drawbacks of the prior art set out above, the present invention proposes, according to a first aspect, a container for a heat storage and return system, comprising an enclosure comprising means for injecting and withdrawing a gas to be cooled or heated, said enclosure being delimited by a first concrete envelope surrounded by a thermally insulating layer, said insulating layer being surrounded by a steel shell, and said enclosure comprising at least two modules each module comprising at least:
    - a first volume delimited by a first concrete side wall and a perforated bottom;
    - A second volume surrounding said first volume and delimited by the first side wall, by a second concrete side wall, and by the perforated bottom;
    said first and second volumes being each capable of containing a fixed bed of particles of a material for storage and of restitution of heat, and said modules being arranged one above the other in a centered manner such that the second walls lateral form the first concrete envelope and the first side walls form a second concrete envelope, the first and second concrete envelopes and the insulating layer being non-pressure tight.
    According to a first embodiment, the perforated bottom is made of metal.
    According to this first embodiment, the perforated bottom of each module may include a single metal grid bounded by the second concrete side wall, and supporting the first concrete side wall.
    Alternatively, the perforated bottom of each module may include a first metal grid bounded by the first concrete side wall and a second metal grid bounded by the first and second concrete side walls.
    According to a second embodiment, the perforated bottom of each module is made of concrete.
    According to this second embodiment, the modules can advantageously be one-piece concrete modules.
    Advantageously, the heat storage and restitution material is in the form of concrete particles.
    Preferably, the container is in the form of a column, the first and second concrete side walls of the modules being cylindrical.
    Preferably, the container has pressure holes in the first and second concrete casings.
    Each module may also include a gas homogenization zone placed under the perforated bottom and empty of any heat storage material.
    Advantageously, the thermal conductivity is between:
    - 0.1 and 2 W.m ' 1 .K' 1 for concrete envelopes,
    - 0.01 and 0.17 Wm 1 .K 1 for the insulating layer, and
    - 20 and 250 Wm 1 .K 1 for the steel hull.
    Advantageously, the thickness of the insulating layer is such that, when using heat storage, the temperature of the steel shell is less than or equal to 50 ° C., and in which the insulating layer is preferably chosen from a layer rock wool, perlite, glass wool, cellular glass, an air layer, and more preferably is a layer of rock wool.
    The container can contain between 2 and 12 concrete modules.
    The enclosure preferably has a volume of between 200 m 3 and 1000 m 3 .
    The container may include several speakers mounted in series and / or in parallel.
    According to a second aspect, the invention relates to a heat storage and return system comprising at least one container according to the invention.
    According to a third aspect, the invention relates to an energy storage installation by compressed air of the AACAES type comprising:
    - a compression system to compress air during a compression phase;
    - a heat storage and return system according to the invention for storing the heat of the compressed air during the compression phase and for restoring the heat to the compressed air during an expansion phase;
    - a final storage tank for air compressed by the compression system and cooled by the heat storage and return system;
    - a device for expanding the compressed air from the final storage tank during the expansion phase.
    According to one embodiment, the final tank has a volume of between 1000 m 3 and 7000 m 3 and the enclosure of said at least one container of the heat storage and return system has a volume of between 200 m 3 and 1000 m 3 , the heat storage and return system preferably comprising at least three containers.
    According to a fourth aspect, the invention relates to a method of mounting a container according to the invention, comprising:
    - the installation of the steel hull without a cover cap on the container assembly site, the steel hull being placed on a support;
    - the assembly of the modules, the installation of the insulating layer and the filling of the modules with the heat storage material, by successive insertion of the modules in the steel shell in a centered manner to form the first concrete envelope and the second concrete shell;
    - closing the container by assembling the steel shell with a steel cover previously thermally insulated, preferably by welding.
    According to one embodiment, the first volume and the second volume of the module are filled with the heat storage material so as to create two fixed beds of particles once said module is inserted into the steel shell.
    Alternatively, the first volume and the second volume of the module can be filled with the heat storage material so as to create two fixed beds of particles before the said module is inserted into the steel shell.
    Other objects and advantages of the invention will appear on reading the following description of examples of particular embodiments of the invention, given by way of non-limiting examples, the description being given with reference to the appended figures described below. -after.
    Brief description of the figures
    FIG. 1 is a diagram illustrating the principle of an AACAES process in which a heat storage and restitution (TES) system is implemented according to a nonlimiting embodiment of the invention.
    Figure 2 is a diagram of a TES container according to a first embodiment of the invention in which the concrete modules of the container have a perforated metal bottom.
    Figure 3 is a diagram of a TES container according to a variant of the first embodiment of the invention.
    Figure 4 is a diagram of a TES container according to a second embodiment of the invention in which the container modules have a perforated concrete bottom.
    FIG. 5A is a diagram of a module of the TES container according to the first embodiment illustrated in FIG. 2. FIGS. 5B and 5C illustrate a detail of said module.
    FIG. 6 is a diagram of a module of the TES container according to the variant of the first embodiment illustrated in FIG. 3.
    FIG. 7 is a diagram of a concrete module of the TES container according to the second embodiment illustrated in FIG. 4.
    Figures 8A and 8B are 3D views of the concrete module illustrated in Figure 7.
    FIG. 9 is a diagram of a concrete module of the TES container according to a variant of the second embodiment illustrated in FIG. 4.
    FIG. 10 is a diagram of a part of a TES container according to a variant of the first embodiment with modules comprising gas homogenization spaces.
    FIG. 11 is a diagram illustrating an example of assembly of the TES container shown in FIG. 4.
    FIG. 12 is a graph illustrating the evolution of the temperature through the multilayer wall of the TES container illustrated in FIG. 2.
    FIG. 13 is a 3D view of a first example of a steel shell of a TES container according to the invention.
    FIG. 14 is a 3D view of a second example of a steel shell of a TES container according to the invention.
    FIG. 15 is a 3D view of a third example of a steel shell of a TES container according to the invention.
    In the figures, the same references designate identical or analogous elements.
    Detailed description of the invention
    The present invention relates to a container of a heat storage and return system (TES) which has a structure reinforced by the presence of a double concrete shell.
    FIG. 1 schematically illustrates the operating principle of an AACAES installation comprising a heat storage and return system (TES) according to the invention. The features of the TES container according to the invention are not shown in this figure, and are described below, in particular in relation to Figures 2 to 15.
    In FIG. 1, the AACAES installation 100 comprises an air compression system 20, an air expansion system 30, a system for storing and returning the heat of the air called TES 40, and a final tank 10 for storing the compressed air.
    The TES according to the invention is suitable for all types of gas, in particular air. In this case, the inlet air used for compression can be taken from the ambient air, and the outlet air after expansion can be released into the ambient air. In the following description, only the variant embodiment with compressed air will be described. However, any gas other than air can be used in the TES container according to the invention.
    The compression train 20 has three compression stages, each stage comprising a compressor (21, 22, 23). The number of compression stages depends on the technologies and performance of the compressors and preferably comprises from one to six compressors. The compression train is necessary to obtain the desired pressure of the air which is stored in the tank 10. Preferably, the pressure of the compressed air in the final tank 10 is between 50 bars and 300 bars. The compressors are for example driven by a motor M, in particular an electric motor.
    The air expansion system 30 has three stages of turbines. The three turbines 31, 32, and 33 are used to relax the air and generate electrical power. The turbines are typically connected to an electricity generator G. The number of expansion stages is preferably identical to that of the compression train.
    Typically, the number of turbines is equal to the number of TES containers, and the number of compressors is equal to or greater than the number of TES containers.
    One TES container per compression stage is required. Thus the TES 40 has three containers (41, 42, 43). Each container includes an enclosure defining a volume having at least one fixed bed of particles of heat storage material, and is designed to withstand high pressures and moderate temperatures. The heat storage material is able to store the calories of the air which passes through the container and which is brought into contact with said material, and to restore this heat to the air which passes through the container at another time. These containers are described in detail later in the description.
    During the compression phase, also called the storage phase or the loading phase, hot air, produced by compression in a compressor (21, 22, 23), is admitted into a container of the TES (41, 42, 43) and comes out at low temperature to undergo the next compression stage or to be stored in the final tank 10. Thus, the air 1 enters at a temperature T o and a pressure P o in the compressor 21, for example at 25 ° C. (room temperature) and at atmospheric pressure. The air is compressed in the compressor 21, and heated due to the compression, and comes out at a temperature and a pressure P, higher than initially (T o , P o ), for example at about 260 ° C and about 6 bars. The compressed and heated air then enters the container 41 and passes through the heat storage material with which it exchanges calories, to come out cooled to a temperature T 2 , for example at about 100 ° C. This cooled air can possibly be further cooled in a ventilation device 51 placed at the outlet of the TES container 41, to reach a temperature T 3 lower than the temperature T 2 , approaching ambient temperature. The temperature T 3 is for example equal to around 50 ° C. The AACAES installation can thus include at least one additional air cooling device, different from the TES containers, for example of the fan type, in order to lower the temperature of the air leaving each TES container, and preferably comprises as many additional cooling devices, for example of the fan type, as there are TES containers, each being positioned on the line of air leaving the TES container and entering the compressor of a compression stage or entering the final tank 10. The air possibly cooled in the fan 51 is then sent to the compressor 22, to undergo a new compression and temperature increase accompanying it, and comes out at a pressure P 2 greater than the pressure P 1; for example at a pressure of around 30 bars, and at the temperature T v The air at the temperature h and pressure P 2 is then sent to the TES container 42 where it is cooled in the same way as in the container 41 The air leaves the container 42 at the temperature T 2 , is optionally further cooled in the fan 52 to the temperature T 3 , before being sent to the last compressor 23. The compressed air at the outlet of the compressor 23 has a pressure P 3 higher than the pressure P 2 , for example is about 125 bars, and is at the temperature Τ υ II is sent to the TES container 43, then possibly to a fan 53, to finally be sent (air 2) and stored in the final air storage tank 10, at a storage temperature T fj which is substantially equal to the temperature at the outlet of the last container TES 43 or possibly at the temperature T 3 at the outlet of the last fan 53, for example equal to about 50 ° C and preferably equal to the ambient temperature, and a storage pressure P f , which is substantially equal to the pressure P 3 at the outlet of the last compressor 23 (modulo the pressure drop at the end of the passage in the TES container and possibly in the fan), for example around 125 bars.
    During the expansion phase, also called the destocking phase or the discharge phase, the cold air produced during expansion in a turbine is admitted into the TES container (41, 42, 43) to transfer the heat to it. stored. Thus, the air 3 leaving the reservoir 10 at the storage temperature T, and the storage pressure P f , enters the TES container 43 where it is heated in contact with the heat storage material which releases the collected heat during the storage phase. The heated air is then sent to the turbine 31, it undergoes expansion, and therefore also cooling. Leaving the turbine 31, the cooled air is sent to the TES container 42 to be heated there, as in the container 43, then again undergoes expansion and cooling by its passage in the turbine 32. Before its entry into the third expansion stage by the turbine 33, the air leaving the turbine 32 is sent to the TES container 41 in order to undergo a final heating.
    Thanks to TES, the heat formed during the air compression phase is advantageously stored in the TES containers and returned during the expansion phase of the compressed air, thus ensuring optimal installation efficiency by limitation of the loss of calories during the process. In order to maximize efficiency and guarantee an adiabatic system, the TES container must minimize heat transfer to the outside. Each container of the TES preferably has a volume of between 200 m 3 and 1000 m 3 , typically chosen according to the energy to be stored. The TES container according to the invention can be used regardless of the size of the AACAES installation. The volume of the container and the number of containers are chosen according to the size of the targeted AACAES system. The air flow entering and leaving the TES container depends on the floor where the container is located, in particular depends on the pressure, and is preferably between 20 and 200 m 3 / h. The temperature of the storage material is preferably between room temperature, ie about 25 ° C, and 300 ° C, and preferably between room temperature and 260 ° C.
    In the installation shown in FIG. 1, the TES container 43, that is to say the TES container from which air is sent to the final tank 10, is the heat storage device which requires the most constraints for sizing the TES. In fact, it is the one that supports the strongest constraints related to air compression. In the example given and illustrated in FIG. 1, the container of TES 43 has the following characteristics:
    it is able to contain air having a temperature of about 260 ° C maximum; it is able to be operated at a maximum pressure of 125 bars; it contains 336 m 3 of heat storage material; the heat storage material it contains has a density of 2400 kg / m 3 , which leads for example to an apparent density of 1200 kg / m 3 considering a void rate of 50%;
    the storage material it contains is in the form of 10 mm diameter beads.
    Several compressed air storage units are shown in Figure 1 as forming the final air storage tank 10, without this being a limitation. The compressed air storage tank 10 can in fact be composed of one or more air storage units, for example one or more tanks, a pipe system, or one or more underground cavities. The total volume of the reservoir 10 can be between 1000 m 3 and 7000 m 3 in the case of AACAES installations of modest size, and can go up to 100,000 m 3 depending on the envisaged applications.
    The AACAES system comprising a TES container according to the invention is not limited to the example in FIG. 1. Other configurations can be envisaged: a different number of compression and / or expansion stages, the use of reversible means ensuring compression and expansion making it possible to limit the number of devices used in the system and thus ensure a gain in weight and volume of the system, etc.
    FIG. 2 represents a schematic longitudinal section of a TES container according to a first embodiment of the invention. Only half of the container is shown, the other part being symmetrical.
    The container 200 of the TES is an enclosure, typically having the shape of a column arranged substantially vertically, for example on a support 208 such as the ground, a concrete slab or any support suitable for the weight of the container, preferably comprising at its top and at its base, means for injecting and withdrawing 201/202 of a gas to be cooled or heated, typically air. In the figure, the arrows illustrate the circulation of the gas in the TES container during two distinct phases of operation of the container, typically a charging phase (gas compression phase with heat storage in the TES) and a discharge phase. (gas expansion with return of heat to gas) in an AACAES process. The TES container is not limited to a cylindrical geometry of the enclosure, but may also have another shape such as a parallelepiped shape. A piping system (not shown) is provided for fluidly connecting the container to the other devices of the AACAES installation (compressors, turbines, etc.), which may be partly located in the basement.
    The container 200 comprises at least two modules 210 arranged one above the other, and preferably a succession of several modules 210 arranged one above the other as shown in FIG. 2. For example, the container according to the invention comprises between 2 and 12 modules 210, preferably between 3 and 5 modules 210. The modules 210 are positioned centrally. The center of each module is on the main axis of elongation of the enclosure (shown in dotted lines in FIG. 2), and all the modules are substantially identical. FIG. 5A schematically illustrates in section such a module 210. As for FIG. 2, only half of the module is shown, the other half being identical by symmetry. Each module 210 has two concrete side walls 218 and 211 and a perforated bottom 205. The first concrete side wall 218 defines with the perforated bottom a first volume 217 of the module 210, and the second concrete side wall 211 delimits with the first concrete side wall 218 and the perforated bottom 205 a second volume 216 of the module 210. The module 210 thus comprises two volumes, the second volume 216 surrounding the first volume 217, 14 which are capable of receiving a material for storing heat and of rendering 207 in the form of particles forming a fixed bed of particles in each volume 217 and 216 of the module 210 (not shown in FIG. 5A). The presence of a double concrete envelope makes it possible to distribute the forces within the structure of the container.
    The perforated bottom 205 of the module 210 is made of metal according to this first embodiment. It can be made of concrete according to other embodiments described below. According to this first embodiment, the perforated bottom 205 is typically a metal plate having openings 212 whose size is smaller than that of the particles of the storage material. heat to retain the heat storage material while letting the gas pass through the container. This metal grid 205 is bounded by the second concrete side wall 211, and serves as a support for the first concrete side wall 218. The second concrete side wall 211 can be poured onto the periphery of the metal grid 205 in order to 'ensure a built-in link 221 (Figure 5B). Alternatively, the metal grid 205 can rest on a shoulder 222 of the second concrete side wall 211 (FIG. 5C), which facilitates maintenance operations.
    Preferably, the concrete side walls (218, 211) of the modules have a thickness of between 50 mm and 500 mm. Preferably, the perforated metal bottom 205 has a thickness of between 100 and 300 mm.
    Each module 210 preferably has a cylindrical shape, leading to a column-shaped container. In this case, the concrete side walls 218 and 211 are cylindrical. However, the module may have another form, for example parallelepiped.
    The container 200 thus comprises a plurality of fixed beds (at least four) of particles of heat storage and restitution materials 207, two beds being arranged in a module 210. By fixed bed of particles is meant a set of particles arranged randomly, which is neither mobile nor fluidized.
    The modules 210 form a first concrete envelope 203 of the container 200, as well as a second concrete envelope 215, internal to the first envelope 203, that is to say included in the interior space of the enclosure formed by the first casing 203. More specifically, the first concrete casing 203 is formed by all of the side walls 211 of the modules 210, and the second concrete casing 215 is formed by all of the side walls 218 of the modules 210. The first concrete shell 203 is surrounded by a thermally insulating layer 206, itself surrounded by a steel shell 204. The concrete shell 203 is in contact with the insulating layer 206, itself in contact with the steel shell 204.
    The concrete shell 203 preferably has a thickness of 50 mm and 500 mm, for example a thickness of 100 mm. The concrete casing 203 is capable of containing the storage material which can be at a temperature of up to 300 ° C, for example a temperature between room temperature (20 ° C) and 300 ° C, preferably between between 20 ° C and 260 ° C. The concrete 203 envelope can also withstand the stresses exerted by the heat storage material, in particular the stresses linked to the weight of the storage material which can represent a few hundred tonnes. The storage material and the first concrete envelope 203 are contained in a steel shell 204, separated from the first envelope 203 by the thermally insulating layer 206. The concrete envelopes (203, 215) and the insulating layer 206 are not pressure-tight, that is to say that there is no difference in pressure on either side of each concrete envelope, and of the insulating layer. Thus, it is the steel shell which takes up the internal pressure of the container. By internal pressure of the container is meant the air pressure in operation. In this way, the first envelope 203 is under pressure and the steel hull is only subjected to the force due to this internal pressure. The container 200 preferably comprises at least one equipression hole 209, which is an opening in the envelope 203 forming a passage between the interior of the enclosure and the insulating layer 206, making it possible to transmit the internal pressure of the enclosure towards the steel hull 204. Preferably the container 200 comprises several equipression holes 209, for example arranged in the side walls of each concrete module 210.
    The first concrete envelope 203 is mainly subjected to compression forces under moderate temperature conditions, typically up to about 300 ° C. The side walls of the modules 210 can be made of ordinary or high performance concrete (BHP), which can be subjected to this type of stress without significant degradation of their mechanical performance at the target operating temperatures. Refractory and reinforced concrete can also be used. The thermal conductivity of the concrete envelopes 203 is preferably between 0.1 and 2 Wm 1 .K 1 .
    The presence of a double concrete envelope (215 and 203) allows the forces to be distributed within the structure of the container. The double concrete envelope in fact allows the container to better resist the mechanical stresses exerted by the heat storage material 207. The positioning of the envelope 215 can be achieved by a stop carried by the plate 205.
    The insulating layer 206 makes it possible to limit the operating temperature of the steel shell by limiting the heat transfer. The insulating layer 206 also makes it possible to facilitate the dimensioning of the steel shell by allowing a low constraint on the temperature, in particular a dimensioning with a temperature which may be less than or equal to 50 ° G or even close to ambient temperature instead of dimensioning at maximum service temperature which is 300 ° C. The thickness of the insulating layer is preferably such that, in use, the temperature of the steel shell is less than or equal to 50 ° C. The insulating layer 206 is not pressure tight. This permeability to pressure allows operation under equipression thanks to the transmission of pressure to the steel shell 204. Preferably the insulating layer has a porosity such that it is not pressure tight. The thermal conductivity of the insulating layer 206 is preferably between 0.01 and 0.17 Wm 1 .K 1 . The insulating layer 206 preferably has a thickness of 50 mm and 400 mm, for example a thickness of 100 mm. The thickness of the insulating layer 206 can be reduced by choosing a refractory concrete to form the concrete modules 210 (reduced thermal conductivity of a refractory concrete, typically halved compared to an ordinary reinforced concrete). The thickness of the insulating layer also depends on the nature of the material chosen to form this layer. The insulating layer is preferably a layer of rock wool. Other materials can also be used to form the insulating layer 206, such as perlite, glass wool, cellular glass, an air space.
    The steel shell 204, which constitutes the outer envelope of the container 200, makes it possible to withstand the internal pressure of the container. Its thickness is dependent on the pressure stress. Preferably, the thickness of the steel shell does not exceed 300 mm in order to be compatible with the manufacturing means known to date (forging, rolling and welding). The thermal conductivity of the steel shell 204 is preferably between 20 and 250 Wm 1 .K 1 . Various steels can be used to make the hull 204. Typically, the hull is made of non-alloy steel of general use, such as steel P355GH.
    The sandwich structure formed by the succession, from the inside to the outside of the container 200, of the first concrete envelope 203, of the insulating layer 206 and of the steel shell 204, allows:
    - to decouple the constraints of weight recovery of the storage material and internal pressure. A clean structure is dedicated to each request: the weight of the storage material is supported by the first concrete shell 203 (helped by the second concrete shell 215), and the internal pressure is supported by the steel shell 204;
    - to carry out a dimensioning of the steel shell at room temperature thanks to the insulating layer, thus making it possible to reduce the thickness of the steel shell, which results in a significant gain on the mass of steel used, and consequently a reduction in costs compared to sizing for a temperature of the order of 300 ° C, but also which makes it possible to obtain thicknesses compatible with the means of production of the steel shell. Indeed, producing a TES container comprising a steel enclosure having an operating temperature much higher than 50 ° C., for example 260 ° C., for the high pressures targeted, represents a technological challenge, in particular for a larger tank diameter. at 1 m. Typically, by taking a steel such as those commonly used to form pressure devices (ESP), for example a P355GH type steel, the thickness of the steel wall reaches a thickness of at least 150 mm. This constitutes a manufacturing limit which complicates the shaping of the steel, the assembly by welding but also the transport, because the mass of the tanks can reach a few hundred tonnes;
    - to make larger diameter tanks, typically of the order of 4 m.
    Advantageously, the modules 210 comprising concrete side walls (218, 211) which is a material capable of storing the heat of the gas passing through the container, the modules 210 as such actively participate in the storage of the heat in the TES container . Thus, it is possible to increase the heat storage capacity of the TES container initially linked to the sole heat storage material in the form of particles in fixed beds and / or to reduce the mass of storage material within the container for the same heat storage capacity.
    The module 210 therefore has several functions, in particular those of forming the enclosure of the container, of participating in the storage and the restitution of the heat, of serving as a support for the granular heat storage material, and of ensuring a good distribution granular heat storage material in the container which improves the heat exchange between the gas and the particles of the storage material with the gas and which avoids the compaction at the bottom of the container which can weaken the structure of the container.
    The heat storage material is in the form of particles arranged so as to form two fixed beds in each module 210, ie a fixed bed in each of the volumes 217 and 216 formed in the module 210. The heat storage material is thus a granular material capable of storing and restoring heat, which can be, without being limiting, concrete, ceramic, asbestos, gravel.
    The shape and size of the particles may vary, and these parameters are chosen so as to guarantee the passage of air through the bed, and to ensure effective contact between the gas and the particles in order to optimize the heat exchanges. . Preferably, the particles are substantially spherical, and have an average diameter of between 1 and 20 mm
    In one configuration, the particles of the heat storage material are concrete. The use of the same material for the particles and for at least part of the modules 210 (the side walls) makes it possible to minimize the problems linked to the differences in thermal expansion between the heat storage material and the modules 210 containing said material.
    The particles, typically beads, of the heat storage material are preferably dimensioned so as to take into account the thermal expansion of the particles and that of the modules during the operation of the container, in particular in order to avoid any blocking phenomenon. As the temperature in the enclosure increases, the modules expand and therefore the granular heat storage material can fill the increase in volume. When a cooling phase occurs, the modules reduce in diameter and can compress the granular material and thus generate stresses harmful to the structure.
    For example, the heat storage material is concrete and in the form of balls with a diameter greater than or equal to 10 mm.
    The container 200 according to the invention makes it possible to store the heat coming from a hot gas, the storage being carried out by the particles of heat storage material 207. The container also makes it possible to restore the heat stored in the particles to a gas cold. The gas enters or leaves the container 200 by its ends, at the level of the injection and withdrawal means 201/202, and exchanges heat with the particles of the heat storage and restitution material 207 which are arranged under shape of beds allowing gas to pass through them. The passage of the fluid in the fixed bed of particles is substantially axial, that is to say that the fluid circulates generally along the main axis defined between the points of entry and exit of the gas in the container 200, typically located at two opposite ends of the container 200. Typically the passage of gas takes place substantially along the vertical. According to this configuration, during charging, the fluid enters hot, at a temperature T 1; from the top of the container, and comes out cold (cooled by the particles which store part of the heat of the gas), at a temperature T 2 (T ^ T ^, through the bottom of the container. For discharge, the gas enters cold , at a temperature T 2 , from the bottom of the container, and leaves hot (heated by the particles which restore part of the heat of the particles), at a temperature from the top of the container. The configuration described constitutes a preferred configuration in which the container includes a hot zone in its upper part, due to the entry of hot gas during the charging phase and the exit of the heated gas during discharge, and a cold zone in the lower part due to the exit of the gas cooled during the charging phase and the entry of cold gas during the discharging phase. A hot zone in the upper part makes it possible in particular to minimize the movement of air during a waiting phase before the however, the container can be used elon an inverted configuration in which the hot zone is located in its lower part and the cold zone in the upper part. In this case, during the charging phase, the hot gas to be cooled arrives at a temperature T 1; from the bottom of the container and leaves cold, at a temperature T 2 (T ^ Tq, from the top of the container, and during the discharge, the gas enters cold, at a temperature T 2 , from the top of the container, and leaves hot to a temperature T b from the bottom of the container.
    Advantageously, the TES container according to the invention is capable of operating at pressures between 1 bar and 300 bars, in particular between 100 bars and 300 bars, and more particularly between 100 and 150 bars, and at temperatures between room temperature, generally from 20 ° C to 300 ° C, preferably between room temperature and 260 ° C.
    According to a particular configuration, the TES container does not form a single reservoir but comprises several enclosures each defined as previously described for the enclosure of the TES container illustrated in FIG. 2, that is to say comprising, preferably at its top and base, gas injection and withdrawal means, each enclosure being delimited by a first concrete envelope surrounded by a thermally insulating layer, itself being surrounded by a steel shell. Each enclosure comprises at least two concrete modules arranged one above the other in a centered manner to form the first concrete envelope and a second concrete envelope. Each concrete module comprises at least a first volume delimited by a first concrete side wall and a perforated bottom and a second surrounding the first volume and delimited by the first side wall, by a second concrete side wall, and by the perforated bottom . The first and second volumes each contain a fixed bed of particles of heat storage and release material. The different enclosures communicate fluidly and are mounted in series and / or in parallel to form a TES container made up of elements of reduced size and weight. The series and / or parallel connection is understood relative to the gas sent into the enclosures of the TES container: in a series connection, the gas passes successively through the various enclosures of the TES container, while in a parallel connection, the The gas stream to be cooled / heated is divided into several sub-streams, each injected into an enclosure of the TES container.
    The present invention also covers a configuration in which each module comprises more than two volumes, for example three or four volumes, capable of receiving a fixed bed of particles of a material for storage and return of heat. In this case each volume is defined between two concrete side walls, one of the walls surrounding the other. The module then comprises at least three concrete side walls, preferably cylindrical side walls.
    The TES container according to the invention is preferably used in an AACAES system as described in relation to FIG. 1. However, the use of the TES container according to the invention is not limited to energy storage by compressed air type AACAES. The TES container according to the invention can also be used in other applications where storage and return of the heat of a gas are required, under conditions of high pressures, for example for use in heating networks. , or in concentrated solar thermal power plants. These different applications require energy storage means if the latter is not consumed during its production. Consequently, the energy available in the form of heat flow can be stored in a heat storage and return system (TES) according to the invention comprising at least one container as described.
    A variant of the first embodiment of the TES container according to the invention is illustrated in FIG. 3. Only the modules differ between the first embodiment and this variant. According to this variant, the modules 310, also illustrated in FIG. 6, each have a perforated metal bottom comprising:
    - a first metal grid 319 bounded by the first concrete side wall
    318, and
    - a second metal grid 320 bounded by the first and second concrete side walls 318 and 311.
    In the case of cylindrical modules with cylindrical side walls, the first metal grid 319 has a disc shape, and the second metal grid has a ring shape.
    The superimposition of the modules 310, in a centered manner, then makes it possible to obtain the first envelope 303 and the second envelope 315 of the container 300, as in the first embodiment. The second envelope 315 differs from the envelope 215 of the container 200 according to the first embodiment illustrated in FIG. 2 in that it is formed over its entire height by the concrete of the side walls 318 of the modules 310, while in the case of the container 200 illustrated in FIG. 2, the second concrete casing 215 is in some ways discontinuous because interrupted at different levels over its entire height by the presence of the single grid of each module 210 which serves to support the side wall in concrete 217 of module 210.
    According to this variant, the weight of the side walls 318 of the modules is advantageously not supported by the perforated bottom 305.
    The other elements of the container 300 illustrated in FIGS. 3 and 6 are identical to those of the container 200 illustrated in FIGS. 2 and 5, as well as the associated advantages, and their description is not repeated here. It will be understood in particular that the references 301,302, 304, 306, 307, 308, 309, 311, 312, 316, 317 designate elements identical to those referenced 201,202, 203, 204, 206 to 209, 211,212, 216 and 217.
    A second embodiment of the TES container according to the invention is illustrated in Figure 4. Only the modules differ between this second embodiment and the first embodiment (and its variant). According to this second embodiment, the modules 410, also illustrated in FIGS. 7, 8A and 8B, each have a perforated bottom in concrete 405. The concretes used are of the same nature as those of the side walls of the modules.
    The bottom 405 of the module 410 is typically a concrete plate having openings 412 whose size is smaller than that of the particles of the heat storage material in order to retain the heat storage material, while letting the gas pass through. the container. The perforated concrete bottom 405 and the concrete side walls 411 and 418 form three distinct entities, formed by a material of the same kind, i.e. concrete. The walls 411 and 418 rest on the concrete plate 405. The parts of the plate 405 supporting the walls 411 and 418 are preferably unperforated in order to ensure a thickness of solid concrete for the envelopes 403 and 415 at least equal to those walls 411 and 418 respectively. Alternatively to the configuration where the side wall 411 rests on the concrete plate 405, the side wall 411 may include a groove in which the periphery of the concrete plate 405 is housed constituting the bottom of the module 410 (configuration visible on the partial 3D view of module 410 in FIG. 8A). In this case, the part of the plate 405 fitting into the groove of the wall 411 is preferably unperforated in order to ensure a thickness of solid concrete at least equal to that of the wall 411 at the wall / bottom junction of the module. .
    In the case of cylindrical modules with cylindrical side walls, the concrete plate has a disc shape.
    The modules 410 being formed from side walls and bottoms made of the same material, i.e. concrete, this prevents the problems of differential thermal expansion known in the devices of the prior art.
    In addition, the modules 410 comprising not only concrete side walls (418, 411) but also a perforated concrete bottom 405, the modules 410 as such actively participate in the storage of heat in the TES container, the concrete being in fact a material capable of storing the heat of the gas passing through the container. Thus, it is possible to increase all the more the heat storage capacity of the TES container initially linked to the sole heat storage material in the form of particles in fixed beds and / or to reduce the mass of material of storage within the container for the same heat storage capacity.
    In addition, in the case where the particles of the heat storage material are made of concrete, the use of the same material for the particles and for the concrete modules 410 makes it possible to guarantee a substantially identical thermal expansion of the particles and of the modules hosting particles, thus avoiding any additional mechanical stress in the container.
    The other elements of the container 400 illustrated in FIGS. 4 and 7, 8A and 8B are identical to those of the container 200 illustrated in FIGS. 2 and 5, as well as the associated advantages, and their description is not repeated here. It will be understood in particular that the references 401, 402, 404, 406, 407, 408, 409, 411, 412, 416, 417 designate elements identical to those referenced 201, 202, 203, 204, 206 to 209, 211, 212, 216 and 217.
    According to a variant of the second embodiment of the TES container according to the invention, the modules are one-piece concrete modules. Such a one-piece concrete module is illustrated in FIG. 9. The concrete module 510 is formed from a single piece of concrete, more precisely the concrete side wall 511 and the perforated concrete bottom 505 form a single piece of concrete. The concrete module 510 has a side wall 511 extending by a perforated bottom 505, the openings 512 of which allow the gas to pass through the container. Preferably, the side wall 518 is also unitary with the assembly formed by the perforated bottom 505 and the side wall 511. As for the concrete module 410, the problems of differential expansion are reduced due to the same nature of material for the bottom and the walls of the module 510, and the module 510 as such participates in the storage and the restitution of the heat of the gas passing through the container.
    This configuration is also particularly advantageous for the manufacture of the TES container. Indeed, the entire modules can be prefabricated and thus facilitate the mounting of the container by stacking the modules in one piece. The modules can also be pre-filled with the heat storage material before they are assembled to form the container.
    According to another variant of the first and second embodiments of the container according to the invention, the modules include gas homogenization spaces located under the perforated bottoms. Such a configuration is illustrated in FIG. 10, for the case of a TES container according to the variant of the first embodiment comprising modules with two metal grids as a perforated bottom. In Figure 10, two successive modules of the container are shown. The elements referenced 1003, 1004, 1005, 1006, 1007, 1009, 1015, 1016, 1017 denote elements identical to those referenced 303, 304, 305, 306, 307, 309, 315, 316, 317. Their description, and that associated benefits, are not repeated here.
    According to this alternative embodiment, each module 1010 of the TES container has a gas homogenization zone 1020 placed under the perforated bottom 1005 and empty of any heat storage material 1007. Such a zone ensures homogenization of the gas temperature on each stage (module) in the container.
    FIG. 11 illustrates a nonlimiting example of mounting the TES container according to the invention. The diagrams (A) to (E) illustrate the succession of steps for mounting the TES container according to the invention. The example of a TES container according to the second embodiment illustrated in FIG. 4 is chosen to illustrate the mounting method, the latter applying to the other embodiments of the TES according to the invention. According to this mounting example, the steps below are carried out.
    A first step (diagram (A)) of on-site installation of the steel shell 404 without its cover cap 414, and the insulating layer 406 is carried out. The steel shell can also be referred to as a ferrule. The steel shell 404 is placed on a support 408, e.g. the ground.
    Advantageously, the steel hull is prefabricated, that is to say that the boilermaking of the hull is carried out in the workshop, and is conveyed in a single block to the place of assembly. In this case, only the welding or the assembly of the cover 414 is carried out on the assembly site after having inserted the concrete modules 410 and the heat storage material in the steel shell and placed the insulation between the modules. concrete and steel hull.
    Alternatively, the 404 steel hull is partitioned into several elements which are transported to the assembly site and assembled by welding on site.
    A second step (diagrams (B) to (C)) of mounting the concrete modules, placing the insulating layer 406, and filling the modules with the heat storage material 407 is carried out.
    Once the 404 steel hull is installed, each stage of the container comprising a module is preferably mounted as follows, in this order:
    installation of the concrete module. In particular, the bottom 405 and the external wall 418 are put in place, then the internal wall 418;
    installation of the insulation between the external concrete wall 418 and the steel shell 404. The insulation can typically be rock wool in bulk or in rolls;
    filling the concrete module with the chosen 407 storage material.
    The first concrete module 410 inserted into the steel shell by the open top of the shell 404, comes to rest on the bottom of the shell previously thermally insulated.
    During the mounting of the successive modules, the modules are centered on each other during their stacking, in order to create a continuous wall of the first concrete casing 203 and to create the concrete casing 415.
    According to an alternative, the concrete modules 410 can be filled with the heat storage material 207 before the installation of the insulator 206 between the external concrete wall 418 and the steel shell 404.
    According to another alternative, the concrete modules 410 can be filled with the heat storage material 407 before their insertion into the steel shell 404.
    A third step of closing the container 400 is carried out by assembling the shell 404 with its steel cover 414 previously thermally insulated, preferably by welding the cover 414 with the steel wall of the shell 404.
    The installation of other devices, such as the means for injecting and withdrawing gas is not detailed, this being easily designed by a person skilled in the art.
    The manufacturing of the 404 steel shell can be carried out using different techniques:
    - the steel shell can be assembled by welding curved sheets of a single thickness. FIG. 13 illustrates such a shell 1304, composed of sheets of a single thickness 1323 welded. The initially flat sheets are bent to obtain the radius of the enclosure, and are then assembled by welding to form the steel shell which has a monolayer wall.
    - the steel shell can also be assembled by welding curved multi-layer sheets in order to work with unitary sheet thicknesses smaller than the thickness of a sheet used to form a single-layer shell. Part of such a shell is illustrated in FIG. 14 where we can see several layers 1424 of sheets which are superimposed to form the wall 1423 of the steel shell. This technique facilitates the work of shaping the sheet. According to this manufacturing technique, the upper layers can be assembled with pretension in order to produce a multilayer shell with hooping on the outer layers. Compression of the lower layers allows them to withstand greater stresses or to withstand a similar stress while being thinner, which has the advantage of optimizing the quantity of steel necessary for construction.
    - The steel shell can also be manufactured from the assembly, preferably by welding, of curved sheets of a single thickness, such as the monolayer shell illustrated in FIG. 13, which are reinforced by circumferential rings. This technique makes it possible to obtain a shell with a thin wall and resistant to high pressure stresses. Figure 15 is a 3D drawing illustrating such a stiffened steel shell 1504 by the presence of circumferential rings 1525. The steel shell has a cylindrical shape, and comprises a plurality of circumferential reinforcement rings 1525 (12 in number in Figure 13). The circumferential rings 1525 are preferably made of metal, in particular steel.
    Example
    An encrypted example of a TES container according to the invention, used in an AACAES system as shown in FIG. 1 as the last container 43 before the gas passes into the final tank 10 (or first container when the gas leaves the tank 10), is given below.
    A TES container according to the invention comprises, for example, an enclosure comprising two volumes formed by two concrete envelopes 415 and 403, as shown in FIG. 4, having a respective internal diameter of 1.8 m and 3.5 m, and a thickness of 100 mm, and able to withstand a high temperature of the order of 260 ° C. These concrete walls are under pressure thanks to the holes 409 which they comprise. An insulating layer 406 of rock wool, 100 mm thick, is placed between the outer concrete shell 403 and the steel shell 404, making it possible to limit the temperature of the steel wall of the shell to 50 °. vs. The steel shell has an internal diameter of 3.9 m, and is 146 mm thick. Such a TES container develops an internal volume of 672 m 3 , making it possible to contain 806 tonnes of storage material having for example a density of 2400 kg / m 3 with a porosity of 50% (apparent density of 1200 kg / m 3 ). Five floors formed by the stacking of five concrete 410 modules, 14 m high each, can be provided to form the container with a total height of around 70 m (this height does not take into account the dimensions of the bottom and top of the container).
    FIG. 12 illustrates the evolution of the temperature (ordinate temperature in ° C.) within the multilayer wall (radius of the container on the abscissa in meters) of this example of TES container according to the invention, the wall being formed by the concrete envelope 403, the insulating layer 406 and the steel shell 404. The total thickness e of the wall of the TES container is 346 mm, with a thickness of the first concrete envelope 403 of 100 mm respectively, a thickness of the insulating layer 406 of 100 mm, and a thickness of the steel shell 404 of 146 mm. We see that with a temperature of 260 ° C in the enclosure of the container, we go to a temperature below 50 ° C in the steel shell 404.
    To manufacture such a TES container, 270 tonnes of concrete and 1000 tonnes of steel are required.
    权利要求:
    Claims (21)
    [1" id="c-fr-0001]
    1. Container (200, 300, 400) of a heat storage and return system (40), comprising an enclosure comprising injection and withdrawal means (201/202, 301/302, 401/402 ) of a gas to be cooled or reheated, said enclosure being delimited by a first concrete envelope (203, 303, 403, 1003) surrounded by a thermally insulating layer (206, 306, 406, 1006), said insulating layer (206 , 306, 406, 1006) being surrounded by a steel shell (204, 304, 404,1004), and said enclosure comprising at least two modules (210, 310, 410, 510,1010) each module (210, 310 , 410, 510, 1010) comprising at least:
    - a first volume (217, 317, 417, 517, 1017) delimited by a first concrete side wall (218, 318, 418, 518) and a perforated bottom (205, 305, 405, 505, 1005);
    - a second volume (216, 316, 416, 516, 1016) surrounding said first volume (217, 317, 417, 517, 1017) and delimited by the first side wall (218, 318, 418, 518), by a second concrete side wall (211, 311, 411, 511, 1011), and through the perforated bottom (205, 305, 405, 505, 1005);
    said first and second volumes being each capable of containing a fixed bed of particles of a heat storage and restitution material (207, 307, 407, 507, 1007), and said modules (210, 310, 410, 510, 1010) being arranged one above the other in a centered manner such that the second side walls (211, 311, 411, 511, 1011) form the first concrete envelope (203, 303, 403, 1003) and the first side walls (218, 318, 418, 518) form a second concrete casing (215, 315, 415, 1015), the first and second concrete casings and the insulating layer (206) being non-pressure-tight.
    [2" id="c-fr-0002]
    2. Container according to claim 1, in which the perforated bottom (205, 305) is made of metal.
    [3" id="c-fr-0003]
    3. Container according to claim 2, wherein the perforated bottom (205) of each module (210) comprises a single metal grid bounded by the second concrete side wall (211), and supporting the first concrete side wall (218 ).
    29
    [4" id="c-fr-0004]
    4. Container according to claim 2, in which the perforated bottom (305) of each module (310) comprises a first metal grid (319) bounded by the first concrete side wall (318) and a second metal grid (320 ) bounded by the first and second concrete side walls (318, 311).
    [5" id="c-fr-0005]
    5. Container according to claim 1, in which the perforated bottom of each module (410, 510) is made of concrete (405, 505).
    [6" id="c-fr-0006]
    6. Container according to claim 5, in which the modules (510) are monoblock concrete modules.
    [7" id="c-fr-0007]
    7. Container according to one of the preceding claims, wherein the heat storage and restitution material (207) is in the form of concrete particles.
    [8" id="c-fr-0008]
    8. Container according to one of the preceding claims in the form of a column, in which the first (218, 318, 418, 518) and second (211, 311, 411, 511, 1011) concrete side walls of the modules (210, 310, 410, 510.1010) are cylindrical,
    [9" id="c-fr-0009]
    9. Container according to one of the preceding claims, comprising equipression holes (209, 309, 409, 509, 1029) in the first and second concrete envelopes (203, 303, 403, 1003/215, 315,415, 1015 ).
    [10" id="c-fr-0010]
    10. Container according to one of the preceding claims, in which each module (1010) further comprises a gas homogenization zone (1020) placed under the perforated bottom (1005) and empty of any heat storage material ( 1007).
    [11" id="c-fr-0011]
    11. Container according to one of the preceding claims, in which the thermal conductivity is between:
    - 0.1 and 2 W.rn'ÎK ' 1 for concrete envelopes (203,215,303,315,403,415,1003,1015),
    - 0.01 and 0.17 Wm ÎK ' 1 for the insulating layer (206, 306,406,1006), and
    - 20 and 250 W.m ' 1 .K' 1 for the steel shell (204, 304, 404, 1004).
    [12" id="c-fr-0012]
    12. Container according to one of the preceding claims, in which the thickness of the insulating layer (206, 306, 406, 1006) is such that, in use, the temperature of the steel shell (204, 304, 404, 1004) is less than or equal to 50 ° C., and in which the insulating layer is preferably chosen from a layer of rock wool, perlite, glass wool, cellular glass, an air layer, and more preferably is a layer of rock wool.
    [13" id="c-fr-0013]
    13. Container according to one of the preceding claims, comprising between 2 and 12 concrete modules (210, 310, 410, 510,1010).
    [14" id="c-fr-0014]
    14. Container according to one of the preceding claims, in which the enclosure has a volume of between 200 m 3 and 1000 m 3 .
    [15" id="c-fr-0015]
    15. Container according to one of the preceding claims, comprising several enclosures mounted in series and / or in parallel.
    [16" id="c-fr-0016]
    16. Heat storage and return system (40) comprising at least one container (200, 300, 400) according to one of claims 1 to 15.
    [17" id="c-fr-0017]
    17. AACAES (100) compressed air energy storage installation, comprising:
    - a compression system (20) for compressing air during a compression phase;
    - a heat storage and return system (40) according to claim 16 for storing the heat of the compressed air during the compression phase and for restoring said heat to the compressed air during an expansion phase ;
    - a final tank (10) for storing the compressed air by the compression system and cooled by the heat storage and return system;
    - a device for expanding the compressed air from the final storage tank (30) during the expansion phase.
    [18" id="c-fr-0018]
    18. Installation according to claim 17, in which the final tank (10) has a volume of between 1000 m 3 and 7000 m 3 and the enclosure of said at least one container (200, 300, 400) of the storage and heat return (40) has a volume of between 200 m 3 and 1000 m 3 , said heat storage and return system (40) preferably comprising at least three containers (200).
    [19" id="c-fr-0019]
    19. Method of mounting a container according to one of claims 1 to 15, comprising:
    - Installation of the steel shell (404) without a cover cap (414) on the container mounting site, said steel shell (404) being arranged on a support (408);
    - mounting the modules (410), installing the insulating layer (406) and filling the said modules (410) with the heat storage material (407), by successive insertion of the said modules into the steel shell (404) centered to form the first concrete shell (403) and the second concrete shell (415);
    closing the container (400) by assembling the steel shell (404) with a steel cover (414) previously thermally insulated, preferably by welding.
    [20" id="c-fr-0020]
    20. Assembly method according to the preceding claim, in which the first volume (417) and the second volume (416) of the module (410) are filled with the heat storage material (407) so as to create two fixed beds of particles once said
    15 module (410) inserted in the steel shell (404).
    [21" id="c-fr-0021]
    21. The mounting method according to claim 19, in which the first volume (417) and the second volume (416) of the module (410) are filled with the heat storage material (407) so as to create two fixed beds. of particles before the insertion of said
    20 module (410) in the steel shell (404).
    1/10
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    同族专利:
    公开号 | 公开日
    PT3270087T|2019-06-06|
    US10240530B2|2019-03-26|
    EP3270087A1|2018-01-17|
    CN107621185A|2018-01-23|
    ES2726997T3|2019-10-11|
    TR201907413T4|2019-06-21|
    CN107621185B|2020-10-20|
    US20180016984A1|2018-01-18|
    EP3270087B1|2019-02-27|
    FR3054028B1|2018-07-27|
    引用文献:
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    优先权:
    申请号 | 申请日 | 专利标题
    FR1656804|2016-07-15|
    FR1656804A|FR3054028B1|2016-07-15|2016-07-15|CONTAINER OF A HEAT STORAGE AND RESTITUTION SYSTEM COMPRISING A DOUBLE CONCRETE WALL|FR1656804A| FR3054028B1|2016-07-15|2016-07-15|CONTAINER OF A HEAT STORAGE AND RESTITUTION SYSTEM COMPRISING A DOUBLE CONCRETE WALL|
    PT17180717T| PT3270087T|2016-07-15|2017-07-11|Container of a system for storing and restoring heat comprising a double concrete wall|
    TR2019/07413T| TR201907413T4|2016-07-15|2017-07-11|Container for a heat storage and recovery system including a pair of concrete walls.|
    ES17180717T| ES2726997T3|2016-07-15|2017-07-11|Container of storage and heat restitution system comprising a double concrete wall|
    EP17180717.5A| EP3270087B1|2016-07-15|2017-07-11|Container of a system for storing and restoring heat comprising a double concrete wall|
    CN201710575260.5A| CN107621185B|2016-07-15|2017-07-14|Container, system, energy storage facility and assembly method for a heat storage and recovery system|
    US15/650,552| US10240530B2|2016-07-15|2017-07-14|Container for a system for storing and restoring heat, comprising a double wall formed from concrete|
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