• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a tank for the storage of liquid or gaseous media under pressure and its manufacturing process. Such a tank ensures a healthy mode of rupture and an optimized ratio between the mass of gas stored and the mass of the tank, for a fixed operating pressure. The present reservoir has applications in the fields implementing pressurized storage tanks such as automobiles, aeronautics, etc.
    公开号:FR3021726A1
    申请号:FR1454834
    申请日:2014-05-28
    公开日:2015-12-04
    发明作者:Guillaume Fourage；Laurent Lagunegrand
    申请人:EADS Composites Aquitaine；
    IPC主号:
    专利说明:

    [0001] BACKGROUND OF THE INVENTION Field of the Invention The present invention relates to a reservoir for the storage of liquid or gaseous media under pressure and to a process for the manufacture of liquid or gaseous media under pressure. such a tank. BACKGROUND ART Composite tanks are known for the storage of gas under high pressure (between 200 and 1000 bar, for example). Such tanks are used in various technical fields including compressed air storage for breathing apparatus, natural gas for vehicles or hydrogen for fuel cells. These tanks are usually cylindrical and closed by domes each with or without a nozzle. To resist the high pressures of the gases thus stored, these tanks comprise a liner defining a sealed storage chamber, placed in a mechanical reinforcing structure made of composite material. The tanks can thus be of several types, either with a metal liner covered with a layer of composite on its central part (Type II), or with a metal liner entirely covered with composite (Type III), or with a plastic liner covered with composite (Type IV). The main advantages of thermoplastic liners over metal liners lie in their lower weight and greater mechanical resistance to cyclic stresses. The mechanical reinforcing structure is typically made by winding layers of fibers around the liner, these fibers preferably being pre-impregnated with a thermosetting resin. One or more additional layers of protection may be added after completion of the reinforcing structure. The choice of the angle and the arrangement of the different winding layers depends on the technical constraints of the winding means, the geometry of the reservoir, the targeted performances and the possible sliding of the fibers at the beginning of the winding. . Nevertheless, it can be seen that the angles formed by the fibers deposited with respect to the longitudinal axis of the reservoir and the arrangement of the layers have a direct impact on the pressure and the mode of rupture of the reservoirs thus produced. It is known that the theoretical winding angle to achieve the highest bursting pressure on a resilient tubular structure with bottom effect, under the sole effect of the internal pressure, is 54.7 °. However, reinforcing structures which in parallel implement angles of between 50 ° and 58 ° are widely known for their mechanical strength. Tanks are also known using winding combinations of polar type (angle between 10 and 30 °) and circumferential (angle of the order of 90 °), to maintain a healthy mode of rupture, that is to say to say a rupture of the tank in one piece without generating projectiles. Some tanks still use helical and circumferential winding combinations, the angle of the helical winding being determined by the minimum polar aperture diameter (s) of the liner. However, the associated rupture pressure and the performance of these tanks, in particular the ratio between the mass of gas stored and the mass of the tank, are largely insufficient.
    [0002] In addition, the manufacture of these tanks which implements a relatively large number of deposited layers is long and expensive.
    [0003] The present invention aims at overcoming these various disadvantages of the prior art by proposing a pressurized gas storage tank and its manufacturing method, simple in their design and in their operating mode, ensuring a healthy mode of rupture of this reservoir, while minimizing the mass of the filament winding and optimizing the ratio mass of gas stored on tank mass, for a given operating pressure. BRIEF DESCRIPTION OF THE INVENTION To this end, the invention relates to a tank for storing liquid or gaseous media under pressure, comprising an inner envelope defining a storage chamber and a mechanical reinforcing envelope surrounding at least said inner envelope, said inner casing comprising an opening at at least one of its ends, a cylindrical central portion and two end portions of which at least one is outwardly curved, said inner casing defining a longitudinal axis. According to the invention, this mechanical reinforcing envelope comprises successively starting from the inner envelope to the outside: a first filament winding comprising a layer or a stack of layers each having fibers arranged so that the angle formed between the longitudinal direction of each fiber and said longitudinal axis is between +/- 45 ° and +/- 85 °, the absolute value of the angle α 1 formed by the fibers of each layer superimposed on another layer of this the stack being greater than the absolute value of the angle α 1 formed by the fibers of the immediately lower layer in this stack; a second filament winding comprising one or more intermediate layers placed under a single layer called the outermost layer of said second layer; said intermediate layers being superposed by defining a stack, said layer or each intermediate layer of this stack having fibers arranged so that the absolute value of the angle β 1 formed between the longitudinal direction of each fiber of the corresponding intermediate layer and said longitudinal axis is: θ 2 * equal to or greater than the maximum absolute value of the angle α1 for the first winding, and equal to or greater than the absolute value of the angle θ1 formed by the fibers of the immediately lower intermediate layer 5, when said corresponding intermediate layer is superimposed on another intermediate layer, less than the smallest absolute value of the angle ai for said first winding, and equal to or less than the absolute value of the angle aj formed by the fibers of the immediately lower intermediate layer 10 when said corresponding intermediate layer is superimposed on another intermediate layer, said outermost layer of said second winding being a the closed helicoidal layer having fibers arranged so that for said or each opening of said inner envelope, the polar aperture diameter of said closing helicoidal layer is equal to or substantially equal to the diameter of the aperture of the inner envelope considered at least one circumferential layer having fibers arranged with respect to said longitudinal axis at an angle ak between +/- 80 ° and +/- 90 °, and / or at least one helical layer having fibers arranged with respect to said axis longitudinally at an angle ak of between +/- 5 ° and +/- 45 ° and / or at least one closed helicoidal layer having fibers arranged so that for said or each opening of said inner envelope, the polar opening diameter of said closing helicoidal layer is equal to or substantially equal to the diameter of the opening of the inner casing 25 considered, to complete the number of layers of the assembly. formed by the first and second filament windings so as to obtain the total thickness of the mechanical reinforcing envelope in said cylindrical central portion. Advantageously, such a reservoir provides a one-piece reservoir rupture mode and an optimized ratio between the stored gas mass and the reservoir mass, for a fixed operating pressure. The ratio between the burst pressure and the mass of the reservoir is thus maximized, demonstrating the optimization of the number of layers deposited on the inner storage envelope, in order to produce the mechanical reinforcing envelope.
    [0004] It will be appreciated that the diameter of the aperture or at least one of the apertures of the inner envelope may not be constant, the opening diameter to the right of the area where the closing helicoidal layer is to be considered. this layer ends. As a purely illustrative example, the opening or one of the openings of the inner casing may have a section of frustoconical shape. The purpose of arranging the different layers of the first filament winding, i.e. the manner in which the inclination angle α formed between the longitudinal axis defined by the inner envelope and the longitudinal direction of each fiber of the different layers of this winding, increases with the distance separating the layer considered from the inner envelope, is to use the maximum potential of recovery of the efforts of each fiber to minimize the amount of fibers deposited at iso- Performance, i.e. for a given burst pressure value. In other words, the value of the angle of inclination α 1 of the fibers of the successive layers of the first filament winding is increased with the distance separating these layers from the inner envelope so as to increase the stress in the fibers of each of the fibers. layers until it is equal to, or substantially equal to that exerted on the fibers of the first layer in direct contact with the inner envelope. By putting the reservoir under pressure, a stress is obtained on the fibers in all the layers of the first filament winding, equal or substantially equal.
    [0005] The contribution of the second filament winding is twofold: on the one hand, the layers whose value of the angle of inclination aj of the fibers relative to the longitudinal axis is greater than the maximum value of the angle in the first stack, provide a continuity of what has been achieved on the first filament winding. It is again sought to have equal or substantially equal stress in each layer. This is true until the angle reaches 90 °, because then the value of the maximum angle for the recovery of forces by the fibers of the considered layer was reached. Moreover, the layers for which the value of the angle of inclination of the fibers is less than the minimum value of the angle α 1 of the first filament winding, are there to progressively cover the bottom of the tank, and avoid significant jumps of rigidity. The angle of inclination α1 then decreases for the same reason as recalled above, that is to say that it is always sought to use the maximum potential of each layer so as to minimize the number of layers. . The reservoir may in particular be used for storing a gas or a mixture of gases. For purely illustrative purposes, this gas may be air, nitrogen, helium, hydrogen or the like.
    [0006] The present reservoir has applications in the fields using pressurized storage tanks such as automobiles, aeronautics, etc. In various particular embodiments of this tank, each having its particular advantages and likely to many possible technical combinations: the thickness of said first filament winding represents between 15 and 35% of the thickness of the mechanical reinforcing envelope in said central cylindrical part, the thickness of the assembly formed by the first and second filament windings with the exception of said closing helicoidal layer, represents at most 45% of the thickness of the mechanical reinforcing envelope in said central cylindrical portion. Preferably, the thickness of the assembly formed by the first and second filament windings with the exception of said closed helicoidal layer, represents between 23 and 45% of the thickness of the mechanical reinforcing envelope in said central portion. cylindrical. the outermost layer of the mechanical reinforcing envelope is a circumferential type layer having fibers arranged with respect to said longitudinal axis at an angle α between 30 +/- 80 ° and +/- 90 °. the mechanical reinforcing envelope has a mass fraction of fibers of between 65% and 85%. Preferably, the mechanical reinforcing envelope has a mass fraction of fibers of between 75% and 81%. The fibers are selected from the group consisting of carbon, glass, aramid fibers, vegetable organic fibers, animal organic fibers, mineral fibers and combinations thereof. As a purely illustrative example, the reservoir can be made using so-called natural fibers such as organic plant fibers (cellulosics such as hemp, linen, or bamboo, for example) or organic animal fibers (proteins such as silk). for example), mineral fibers or a combination of several types of fibers. the inner envelope has an opening at its two ends, each of its ends receiving a base. As a purely illustrative example, a first of these bases comprises a connection such as a valve, the other end comprising a member selected from the group comprising a valve, a pressure sensor and / or temperature and / or humidity, an accelerometer, a safety device, a safety device of the PRD type ("Pressure Relief Device"), a safety device of the TPRD ("Thermal Pressure Relief Device" - "Device thermal expansion ") and combinations of these elements. Alternatively, the inner casing has at one of its ends an opening, the other end being closed and the open end receiving a base. The mechanical reinforcing envelope is disposed on at least a portion of the inner envelope advantageously surrounding this or these bases.
    [0007] By way of example, each base comprises a hollow cylindrical neck portion defining an inner channel and an annular portion. This base may be entirely metal or alloy, or comprise a metal insert or alloy covered at least in part with a plastic interface to facilitate the assembly of the inner casing and the base.
    [0008] Alternatively, this base can be made of plastic or reinforced plastic. As a purely illustrative example, the plastic is reinforced with short or long fibers or crushed, or with beads. These fibers and beads may be glass or carbon. The fibers are embedded in a cured matrix made from a thermosetting or thermoplastic resin.
    [0009] The resin used may be of the thermosetting type, such as a vinylester, polyester or epoxy resin, or of thermoplastic type such as a polyamide or polypropylene resin. Said inner casing is made of metal or plastic. The present invention also relates to a transport means equipped with at least one reservoir as described above. This means of transport may be an aircraft or a vehicle such as a truck or an automobile. The present invention also relates to the use of the tank as described above as a gas or fuel supply source. Such a tank can be used as a stationary power source or onboard a transport means.
    [0010] As a purely illustrative example, such a tank may be used as a power source for a fuel cell or in a filling or distribution plant such as a service station. The present invention further relates to the use of the tank as previously described as energy storage.
    [0011] The present invention further relates to a method of manufacturing a reservoir for storing liquid or gaseous media under pressure, said reservoir comprising an inner envelope defining a storage chamber and a mechanical reinforcing envelope surrounding at least said inner envelope, said envelope inner housing comprising an opening at at least one of its ends, a cylindrical central portion and two end portions of which at least one is outwardly curved, said inner envelope defining a longitudinal axis. According to the invention, the following steps are carried out to produce said mechanical reinforcing envelope: firstly, forming a first filament winding comprising a layer or a stack of layers having fibers arranged so that the angle α formed between the longitudinal direction of each fiber and said longitudinal axis is between +/- 45 ° and +/- 85 °, the absolute value of the angle α 1 formed by the fibers of each layer superimposed on another layer of this stack being greater than at the absolute value of the angle α 1 formed by the fibers of the immediately lower layer in this stack, forming a second filament winding comprising one or more intermediate layers placed under a single layer called the outermost layer of said second winding , said intermediate layers being superimposed by defining a stack, said layer or each intermediate layer of this emulsion. a pile having fibers arranged so that the absolute value of the angle α 1 formed between the longitudinal direction of each fiber of the corresponding intermediate layer and said longitudinal axis is: 10 * equal to or greater than the maximum absolute value of the angle ai for the first winding, and equal to or greater than the absolute value of the angle aj formed by the fibers of the immediately lower intermediate layer when said corresponding intermediate layer is superimposed on another intermediate layer, 15 * is equal to or less than the the smallest absolute value of the angle ai for said first winding, and equal to or less than the absolute value of the angle aj formed by the fibers of the immediately lower intermediate layer when said corresponding intermediate layer is superimposed on another intermediate layer Said outermost layer of said second winding being a helical layer oidale fermante having fibers arranged so that, for said or each opening of said inner envelope, the polar aperture diameter of said closing helical layer is equal to or substantially equal to the diameter of the aperture of the inner envelope considered, 25 - Then complete these first and second filament windings with the removal of at least one circumferential layer having fibers arranged with respect to said longitudinal axis at an angle ak between +/- 80 ° and +/- 90 °, and / or at least one helical layer having fibers arranged with respect to said longitudinal axis at an angle ak of between +/- 5 ° and +/- 45 °, and / or at least one closed helicoidal layer having fibers arranged so that, for said or each opening of said inner envelope, the polar aperture diameter of said closing helical layer is equal to or substantially equal to the diameter of the aperture of the inner envelope 35 considered, to obtain the total thickness of the mechanical reinforcing envelope in said central cylindrical portion.
    [0012] The reservoir can be made using one of the following methods: a filament winding method with direct wet impregnation, a filament winding process with indirect dry impregnation (winding of pre-impregnated fibers), a process automatic fiber removal (AFP), manual fiber removal, filament winding of dry fibers and indirect impregnation by a RTM (Resin Transfer Molding) process, a braiding process .
    [0013] It is observed here that the strict respect of the sequence of removal of the different layers is necessary to achieve the objective of the present invention. In various particular embodiments of this method, each having its particular advantages and capable of many possible technical combinations: the last deposited layer and thus forming the outermost layer of the mechanical reinforcing envelope is a circumferential type layer having fibers arranged with respect to said longitudinal axis at an angle α between +/- 80 ° and +/- 90 °, the fibers are impregnated in a thermosetting or thermoplastic resin before being wound on said envelope; The thickness of said first filament winding represents between 15 and 35% of the thickness of the mechanical reinforcing envelope in said central cylindrical portion, the thickness of the assembly formed by the first and second filament windings with the exception of of said closing helicoidal layer, represents between 23 and 45% of the thickness of the mechanical reinforcing envelope in said cylindrical central portion, prior to the removal of the first filament winding, the outer surface of at least a portion of the inner casing is treated to increase the adhesive and wetting properties of the material constituting said inner casing, the mechanical reinforcing envelope has a mass fraction of fibers of between 65% and 85%, and more preferably between 75% and 81%.
    [0014] BRIEF DESCRIPTION OF THE DRAWINGS Other advantages, aims and particular characteristics of the present invention will emerge from the description which follows, for explanatory and non-limiting purposes, with reference to the appended drawings, in which: FIG. 1 schematically represents a reservoir for the storage of gas under pressure according to a first embodiment of the present invention, this reservoir comprising two identical bases; FIG. 2 shows the inner storage shell of the tank of FIG. 1 on which is placed a layer of reinforcing fibers of a helicoidal type layer; FIG. 3 shows the internal storage envelope of the reservoir of FIG. 1 on which is placed a layer of reinforcing fibers of a closed helicoidal type layer; FIG. 4 shows the inner storage envelope of the reservoir of FIG. 1 on which is placed a layer of reinforcing fibers of a circumferential type layer; FIG. 5 shows the inner storage envelope of a storage tank according to a second embodiment of the invention on which is placed a layer of reinforcing fibers of a closed helicoidal type layer, the envelope internal having only one opening receiving a base; FIG. 6 shows the inner storage envelope of a storage tank according to a third embodiment of the invention on which a layer of reinforcing fibers of a closed helicoidal layer is placed, the envelope internal having an opening at each of its ends, each opening having a different diameter; FIG. 7 is a fragmentary sectional and exploded view of the reinforcing envelope of the reservoir of FIG. 1 showing the different layers of this envelope; DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION Firstly, it is noted that the figures are not to scale.
    [0015] Figures 1-4 describe a tank for storing pressurized gas according to a first embodiment of the present invention.
    [0016] This tank 10 comprises a cylindrical central portion 11 of radius Rv, which is closed at its two ends by domes 12, 13. The tank 10 defines a main axis 14, or axis of revolution of the tank, extending in the longitudinal direction of this reservoir 10. Each dome 12, 13 of curved shape, is provided with a base 15, 16, one of these bases 15 being used to ensure the internal / external connection of the reservoir, and therefore the filling in gas and dump. For this purpose, this base 15 is in particular intended to receive a fitting such as a tap, a valve or a pipe. The other base 16 placed at the opposite end of the tank 10 receives a valve, a pressure sensor and / or temperature and / or humidity. The reservoir 10 comprises a sealed inner envelope 17, also called a liner, defining a storage chamber in which a pressurized gas is intended to be stored. This liner 17 has at each of its ends a polar opening centered on the main axis 14 of the tank 10. Each polar opening which is circular radius Rf, receives a base 15, 16 corresponding. These polar openings are of identical diameter. The liner 17 here consists of a polymer such as polyamide, high density polyethylene (HDPE), polyurethane (PU), etc. The liner 17 is also surrounded by a mechanical reinforcement envelope intended to reinforce mechanically the tank to withstand the pressure of the gas stored in the storage chamber. This reinforcing envelope is here made of a composite material obtained by filament winding of unidirectional fibers impregnated with resin. Long fibers are preferably used which provide better resistance to successive and repetitive deformations, for example glass or carbon fibers bonded together by a resin such as an epoxy resin. Each layer is oriented with respect to the main axis 14 of the reservoir of a winding angle. The reinforcing fibers deposited on the liner 17 to form the mechanical reinforcing envelope forming a web defined by a width W, three types of layers will be distinguished: - layer of helicoidal type: the fibers 18 follow a helical path relative to the axis of rotation of the mandrel and the mean angle α of the layer is determined so that the radius R of the circular polar aperture of the layer is greater than the polar aperture Rf + 1 / 2 x W of the liner (FIG 2), - layer of helicoidal closing type: it is a helicoidal type layer having fibers 19 arranged with respect to the main axis 14 of the reservoir at a determined angle α means in such a way that the radius R of the circular polar aperture of the layer is between the circular polar opening radius Rf of the liner and a circular polar opening radius equal to Rf + 1/2 x W (FIG. 3), - circumferential type layer the fibers 20 of this layer follow a spiral path with respect to the axis of rotation of the mandrel and this layer has fibers 20 arranged with respect to the main axis 14 of the reservoir 15 at an average angle a of between 80 ° and 90 ° (Fig. 4). The reservoir is made by preferentially using the filament winding method with direct wet impregnation. Preferably, the reservoir also comprises a closing helicoidal layer 21 and a protective circumferential layer preferably made of glass fibers and epoxy resin. As shown in FIGS. 5 and 6, the liner 17 may also comprise two openings 22, 23 for the passage of the gas having radii of different polar openings (FIG 6), or a single opening 24 for the passage of the gas, the opposite bottom being a closed bottom (Fig. 7). In both cases, the liner is defined by two radii of different polar apertures Rf1 and Rf2. The closing helicoidal type layer 21 is then defined by two radii of different polar openings between Rf1 and Rf1 + W, and between Rf2 and Rf2 + W. The winding angle considered is the average angle between the angle of the ply at the beginning of the cylindrical portion and the angle of the ply at the end of the cylindrical portion. Figure 7 shows a reservoir according to a particular embodiment of the present invention. Only the structure of the envelope 26 of mechanical reinforcement protecting the liner 27 will be described below. Starting from the liner 27 towards the outside of the reservoir, this mechanical reinforcing envelope 26 comprises a first filament winding comprising two superimposed layers of fiber plies whose value of the angle α formed between the longitudinal direction of each fiber. of a given layer and the longitudinal axis 28 defined by the liner 26 is between +/- 55 ° and +/- 85 °. This first winding represents twenty percent (20%) of the total thickness of the mechanical reinforcing shell in its central cylindrical portion. It is noted that the absolute value of the angle α 1 formed by the fibers of the second layer of this first filament winding, that is to say seventy (70), is greater than that, fifty-five (55) from the first layer. On this first filament winding has been formed a second filament winding comprising a stack of three layers. The outermost layer, layer numbered five (5), of this second filament winding is a closed helicoidal layer whose angle aj formed between the longitudinal direction of each of its fibers and the longitudinal axis 28 is ten degrees ( 10 °). The two layers, numbered three (3) and four (4), placed under this last layer are such that: - the base layer of this winding, the layer numbered 3, which is placed directly on the outermost layer of the first filament winding, has an angle whose absolute value (35) is smaller than the smallest absolute value of the angle ai for the first winding, and - the layer placed above this base layer, ie the layer numbered 4, for its part presents an angle of inclination of the fibers relative to the longitudinal axis 28 whose absolute value (85) is greater than the maximum absolute value of the angle ai for the first winding. The assembly formed by these two filament windings with the exception of the closed helicoidal layer, represents forty percent (40%) of the total thickness of the mechanical reinforcing envelope in its central cylindrical portion.
    [0017] On these first two filament windings is placed an alternation of circumferential layers having fibers arranged with respect to said longitudinal axis 28 at an angle αk = 90 ° and closed helicoidal layers whose angle ak formed between the longitudinal direction of each fiber and the longitudinal axis 28 is ten degrees (10 °).
    [0018] The total number of layers constituting this mechanical reinforcing envelope is only ten (10) layers.
    [0019] In order to demonstrate the technical advantages provided by the present invention, comparative tests have been conducted between a tank according to an embodiment of the present invention with commercial tanks. The table shows the results obtained during these tests in which the tank according to an embodiment of the present invention is called tank 1 while the two separate commercial tanks are respectively called tank 2 and tank 3. The volumes of water and the masses of these tanks are comparable.
    [0020] On the other hand, the mass of gas stored is different because the operating pressure is different. Tank Type Diameter Length mm Capacity Weight at Pressure Coef. Type Weight Mass of mm in Water Empty of gas / Mass Liters Kg Service Safety gas tank gas harq cp 4 545 1030 143 77 525 3 H2 4.696 6.1G / 0 RA rvnir 1 ReAcunir 9 3 551 972 154 82 350 2.35 H2 3.73 4.5% Reservoir 3 4 403 1820 156 79 350 2.35 H2 3.81 4.81: Table 1: Comparative performance of the reservoir according to an embodiment with test reservoirs 15 It can be seen that, although that having both a higher service pressure and a safety factor (of the order of thirty percent (30%) higher) than those of commercial tanks 2 and 3, which requires a strengthening of the As a mechanical reinforcement with respect to tanks operating at lower pressures, the reservoir 1 according to an embodiment of the present invention advantageously provides a higher storage capacity with a comparable reservoir mass. Furthermore, the safety factor applied to the commercial tanks 2 and 3 being lower, one could theoretically: either increase the operating pressure of the tank 1 obtained according to one embodiment of the invention more induces an increase in the mass of gas stored, - or further reduce the amount of fiber used, that is to say, reduce the mass of the tank 1.
    [0021] In both cases, it would lead to an increase in the ratio of stored gas mass to tank mass.
    权利要求:
    Claims (18)
    [0001]
    REVENDICATIONS1. A tank for storing liquid or gaseous media under pressure, comprising an inner envelope (17) defining a storage chamber and a mechanical reinforcing envelope surrounding at least said inner envelope (17), said inner envelope (17) comprising an opening at least one of its ends, a cylindrical central portion (11) and two end portions (12, 13) of which at least one is outwardly curved, said inner envelope (17) defining a longitudinal axis (14), characterized in that said mechanical reinforcing envelope comprises successively starting from the inner casing (17) towards the outside: a first filament winding comprising a layer or a stack of layers each having fibers arranged so that the angle formed between the longitudinal direction of each fiber and said longitudinal axis (14) is between +/- 45 ° and +/- 85 °, the absolute value of the angle α formed by the fibers of each layer superimposed on another layer of this stack being greater than the absolute value of the angle α 1 formed by the fibers of the immediately lower layer in this stack, - a second filament winding comprising one or more so-called intermediate layers placed under a single layer called the outermost layer of said second winding, said intermediate layers being superposed by defining a stack, said layer or each intermediate layer of this stack having fibers arranged so that the absolute value of the angle aj formed between the longitudinal direction of each fiber of the corresponding intermediate layer and said longitudinal axis (14) is: * equal to or greater than the maximum absolute value of the angle ai for the first winding, and equal to or greater than the value absolute of the angle aj formed by the fibers of the immediate intermediate layer lower when said corresponding intermediate layer is superimposed on another intermediate layer, * is equal to or smaller than the smallest absolute value of the angle ai for said first winding, and equal to or less than the absolute value of the angle aj formed by the fibers of the immediately lower intermediate layer 3021726 17 when said corresponding intermediate layer is superimposed on another intermediate layer, said outermost layer of said second winding being a closed helical layer having fibers arranged so that for said or each opening of said inner casing (17), the polar opening diameter of said closing helicoidal layer (21) is equal to or substantially equal to the diameter of the opening of the inner casing (17) considered, - at least one circumferential layer having fibers arranged with respect to said longitudinal axis (14) according to a angle ak between +/- 80 ° and +/- 90 °, and / or at least one helical layer having fibers arranged with respect to said longitudinal axis (14) at an angle ak of between +/- 5 ° and +/- 45 °, and / or at least one closing helicoidal layer to complete the number of layers of the assembly formed by the first and second filament windings so as to obtain the total thickness of the mechanical reinforcing envelope in said central portion (11) cylindrical.
    [0002]
    2. Tank according to claim 1, characterized in that the thickness of said first filament winding represents between 15 and 35% of the thickness of the mechanical reinforcing envelope in said cylindrical central portion (11).
    [0003]
    3. Tank according to claim 1 or 2, characterized in that the thickness of the assembly formed by the first and second filament windings with the exception of said closing helicoidal layer (21), represents at most 45% of the thickness of the mechanical reinforcing envelope in said cylindrical central portion (11).
    [0004]
    4. Tank according to claim 3, characterized in that the thickness of the assembly formed by the first and second filament windings with the exception of said closed helicoidal layer (21), represents between 23 30 and 45% of the thickness of the mechanical reinforcing envelope in said cylindrical central portion (11).
    [0005]
    A tank according to any one of claims 1 to 4, characterized in that the outermost layer of the mechanical reinforcing shell is a circumferential type layer having fibers arranged with respect to said longitudinal axis (14) according to an angle α between +/- 80 ° and +/- 90 °. 3021726 18
    [0006]
    6. Tank according to any one of claims 1 to 5, characterized in that the mechanical reinforcing envelope has a mass fraction of fibers between 65% and 85%. 5
    [0007]
    7. Tank according to claim 6, characterized in that the mechanical reinforcing envelope has a mass fraction of fibers between 75% and 81%.
    [0008]
    8. Tank according to any one of claims 1 to 7, characterized in that the fibers are selected from the group consisting of carbon, glass, aramid fibers, vegetable organic fibers, animal organic fibers, mineral fibers and combinations of these elements.
    [0009]
    9. A method of manufacturing a reservoir for storing liquid or gaseous media under pressure, said reservoir comprising an inner casing (17) defining a storage chamber and a mechanical reinforcing envelope surrounding at least said inner casing (17). said inner casing (17) comprising an opening at at least one of its ends, a cylindrical central portion (11) and two end portions (12, 13) of which at least one is outwardly curved, said casing (17) inner defining a longitudinal axis (14), characterized in that the following steps are carried out to achieve said mechanical reinforcement envelope: - firstly form a first filament winding comprising a layer or a stack of layers having fibers arranged so that the angle α formed between the longitudinal direction of each fiber and said longitudinal axis (14) is between +/- 45 ° and +/- 85 °, the absolute value of the angle α formed by the fibers of each layer superimposed on another layer of this stack being greater than the absolute value of the angle α formed by the fibers of the layer immediately below in this stack, Forming a second filament winding comprising one or more intermediate layers placed under a single layer called the outermost layer of said second winding, said intermediate layers being superposed by defining a stack, said layer or each intermediate layer of this stack having fibers; arranged so that the absolute value of the angle α1 formed between the longitudinal direction of each fiber of the corresponding intermediate layer and said longitudinal axis (14) is: * equal to or greater than the maximum absolute value of the angle ai for the first winding, and equal to or greater than the absolute value of the angle aj form by the fibers of the immediately lower intermediate layer when said corresponding intermediate layer is superimposed on another intermediate layer, * is equal to or smaller than the smallest absolute value of the angle ai for said first winding, and equal to or less than to the absolute value of the angle α formed by the fibers of the immediately lower intermediate layer when said corresponding intermediate layer is superimposed on another intermediate layer, said outermost layer of said second winding being a closed helical layer having fibers arranged so that, for said or each opening of said inner casing (17), the polar aperture diameter of said closing helicoidal layer (21) is equal to or substantially equal to the diameter of the opening of the inner casing (17) considered, - then complete these first and second filament windings with the removal of at least one circumferential layer having fibers arranged with respect to said longitudinal axis (14) at an angle αk of between +/- 80 ° and +/- 90 °, and / or at least a helicoidal layer having fibers arranged with respect to said longitudinal axis (14) at an angle ak of between +/- 5 ° and +/- 45 ° and / or at least one closed helicoidal layer, to obtain the thickness total of the mechanical reinforcement envelope in said central portion (11) cylindrical.
    [0010]
    A method according to claim 9, characterized in that the last deposited layer and thus forming the outermost layer of the mechanical reinforcing envelope is a circumferential type layer having fibers arranged with respect to said longitudinal axis (14). at an angle α between +/- 80 ° and +/- 90 °.
    [0011]
    11. The method of claim 9 or 10, characterized in that the fibers are impregnated in a thermosetting or thermoplastic resin before being wound on said envelope. 3021726 20
    [0012]
    12. Method according to any one of claims 9 to 11, characterized in that the thickness of said first filament winding represents between 15 and 35% of the thickness of the mechanical reinforcement envelope 5 in said central portion (11). cylindrical.
    [0013]
    13. Method according to any one of claims 9 to 12, characterized in that the thickness of the assembly formed by the first and second filament windings with the exception of said closing helicoidal layer (21), represents between 23 and 45% of the thickness of the mechanical reinforcing shell in said cylindrical central portion (11).
    [0014]
    14. A method according to any one of claims 9 to 13, characterized in that prior to the removal of the first filament winding is treated the outer surface of at least a portion of the inner casing (17) to increase the adhesive and wetting properties of the material constituting said inner envelope (17).
    [0015]
    15. Method according to any one of claims 9 to 14, characterized in that the mechanical reinforcing envelope has a mass fraction of fibers between 65% and 85%. 20
    [0016]
    16. Transport means equipped with at least one tank according to any one of claims 1 to 8.
    [0017]
    17. Use of the tank according to any one of claims 1 to 8 as a source of gas or fuel.
    [0018]
    18. Use of the reservoir according to any one of claims 1 to 8 as an energy store.
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    同族专利:
    公开号 | 公开日
    EP2949449B1|2017-11-15|
    ES2659585T3|2018-03-16|
    NO2949449T3|2018-04-14|
    FR3021726B1|2016-07-01|
    EP2949449A1|2015-12-02|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    EP0580535A1|1992-07-23|1994-01-26|AEROSPATIALE Société Nationale Industrielle|Storage vessel for a fluid under pressure, being able to burst without disintegration|
    US5499739A|1994-01-19|1996-03-19|Atlantic Research Corporation|Thermoplastic liner for and method of overwrapping high pressure vessels|
    DE102010017413A1|2010-06-17|2011-12-22|Xperion Gmbh|Pressure vessel for storing a fluid|
    US20130299505A1|2011-02-02|2013-11-14|Toyota Jidosha Kabushiki Kaisha|Manufacturing method for high-pressure tank, and high-pressure tank|
    JP6448605B2|2016-11-21|2019-01-09|株式会社有沢製作所|Pressure vessel|
    FR3071765B1|2017-10-03|2020-11-20|Safran Ceram|COMPOSITE MATERIAL REALIZATION OF A FLOW MIXER LOBE STRUCTURE|
    FR3106185A1|2020-01-14|2021-07-16|Plastic Omnium Advanced Innovation And Research|Nipple for a pressurized fluid reservoir|
    WO2021144335A1|2020-01-14|2021-07-22|Plastic Omnium Advanced Innovation And Research|End fitting for a pressurised fluid reservoir|
    FR3109425A1|2020-04-15|2021-10-22|Centre Technique des Industries Mécaniques|Method of making a composite storage tank|
    FR3109426A1|2020-04-15|2021-10-22|Centre Technique des Industries Mécaniques|Reinforced pressurized fluid storage tank|
    法律状态:
    2015-05-29| PLFP| Fee payment|Year of fee payment: 2 |
    2015-12-04| PLSC| Publication of the preliminary search report|Effective date: 20151204 |
    2016-05-31| PLFP| Fee payment|Year of fee payment: 3 |
    2016-06-17| CD| Change of name or company name|Owner name: STELIA AEROSPACE COMPOSITES, FR Effective date: 20160513 |
    2017-05-30| PLFP| Fee payment|Year of fee payment: 4 |
    2018-05-31| PLFP| Fee payment|Year of fee payment: 5 |
    2019-05-31| PLFP| Fee payment|Year of fee payment: 6 |
    2020-05-29| PLFP| Fee payment|Year of fee payment: 7 |
    2022-02-11| ST| Notification of lapse|Effective date: 20220105 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1454834A|FR3021726B1|2014-05-28|2014-05-28|RESERVOIR FOR STORING PRESSURIZED LIQUID OR GASEOUS MEDIA AND METHOD OF MANUFACTURING THE SAME|FR1454834A| FR3021726B1|2014-05-28|2014-05-28|RESERVOIR FOR STORING PRESSURIZED LIQUID OR GASEOUS MEDIA AND METHOD OF MANUFACTURING THE SAME|
    ES15169192.0T| ES2659585T3|2014-05-28|2015-05-26|Tank for storing liquid or gaseous media under pressure and its manufacturing method|
    EP15169192.0A| EP2949449B1|2014-05-28|2015-05-26|Tank for storing liquid or gaseous media under pressure and method for manufacturing same|
    NO15169192A| NO2949449T3|2014-05-28|2015-05-26|
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