• 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:
    A balloon (202) comprises an envelope (4) containing a carrier gas (6) and a solar generator (8) with solar radiation concentration. The solar generator (8) comprises a reflector (10), one or two sets (204) of photovoltaic solar cells forming a first active face (208) facing the reflector (10) and a second active face (36) facing the outside the envelope (4) of the balloon. The reflector (10), the first active face (208) and the second active face (210) of the set (204) of the photovoltaic cells (206) are configured to ensure a cooperative production of electrical energy between the first active face (208) and the second active face (210) of the assembly (204) as long as the roll solar misalignment of the reflector (10) is less than or equal to an absolute value of 10 degrees.
    公开号:FR3038880A1
    申请号:FR1501486
    申请日:2015-07-15
    公开日:2017-01-20
    发明作者:Bernard Boulanger；Jean Pierre Prost；Jean Philippe Chessel；Philippe Dargent
    申请人:Thales SA；
    IPC主号:
    专利说明:

    A balloon equipped with a concentrated solar generator and using an arrangement of solar cells optimized to supply said balloon with flight
    The present invention relates to a balloon equipped with a concentrating solar generator and using an arrangement of solar cells optimized to feed said balloon in flight. The invention particularly relates to a stratospheric balloon, intended to evolve in the stratosphere and carrying, fixed below, a nacelle with on board one or more payloads.
    In general, the balloons have a high potential of application not only because of their low costs compared to those of the satellites but also because of the altitudes at which said balloons evolve and that they can make use of, in particular the altitudes of the stratosphere extending between 12 and 45 km.
    While the stratosphere is inaccessible to satellites and crossed too quickly by sounding rockets, balloons, or aerostats according to scientific terminology, can evolve durably in this layer called "average" of the atmosphere, and are particularly promising to meet a number of applications, particularly in the telecommunications field.
    Conventionally, the stratospheric balloons must satisfy two requirements: on the one hand, a lift requirement satisfied by the provision of a suitable balloon envelope volume; on the other hand a propulsion requirement for driving and following the balloon a desired trajectory, which requires having a sufficient source of energy.
    Generally and conventionally, for a stratospheric balloon directed is autonomous for a period of several months, it is necessary that it produces its energy using photovoltaic cells. In stratospheric wind conditions, typically those of a wind with a speed greater than 10 m / s, and for a permanent and continuous mission, the electrical energy produced during the day is stored on board for use at night. Daytime electricity production rapidly reaches several tens of kilowatts and requires a large area of photovoltaic cells that significantly and unfavorably impacts the mass balance of the balloon.
    In order to reduce the number of photovoltaic cells necessary for the generation of a sufficient quantity of electrical energy for a given mission and thus to lighten the weight of the entire balloon, the patent application FR 2 982 840 describes a balloon , equipped with a concentrated solar generator. The balloon uses photovoltaic means having an active face intended to receive solar rays and comprises an envelope. The envelope comprises at least a first zone transparent to solar rays, a second reflecting zone for said solar rays, a third zone comprising said photovoltaic means. The second and third zones are positioned and cooperate to return sunlight to said third zone.
    Such a balloon equipped with a concentrated solar generator undergoes an increase in temperature at least locally, which induces risks of damage with respect to the envelope and / or the carrier gas that the envelope contains, in particular. especially when the carrier gas is flammable.
    In addition, the use of a concentrating solar generator requires a continuous control of the pointing of the concentrator or means reflecting towards the sun. In the event of a solar misalignment, dictated for example by particular mission requirements (pointing of antenna (s) or sensors) or weather conditions or limits of monitoring of the sun itself, it is necessary to overcome a rapidly decreasing the electric power delivered by the concentrating solar generator when the angle of incidence of solar radiation varies with respect to the balloon.
    In addition, the rise in the temperature of solar or photovoltaic cells, induced by the concentration of solar radiation, degrades the efficiency of solar cells, in terms of conversion of solar energy into electrical energy.
    A first technical problem is to reduce the temperature of the concentration system to reduce the risks vis-à-vis the envelope and the carrier gas contained in the envelope.
    A second technical problem is also to mitigate a rapid decline in the electrical power delivered by the solar panel as a function of the angle of incidence of solar radiation in the event of solar misalignment.
    A third technical problem is also to reduce the temperature of solar cells to make them work with greater efficiency. For this purpose, the subject of the invention is a flask equipped with a concentrated solar generator comprising an envelope containing a carrier gas and a solar generator with solar radiation concentration, the solar generator comprising: a solar-ray reflector, disposed within the envelope in a first zone of the envelope; a second zone of the envelope, transparent to the sun's rays, to allow the sun's rays to pass towards the reflector, and a first set of photovoltaic cells, arranged in a third zone of the envelope, having a first active face; directed to the reflector; the first set of photovoltaic cells and the reflector being configured so that the reflector concentrates the solar rays on the first active face of the first set of photovoltaic cells, when the reflector is placed in the solar pointing position; said balloon being characterized in that: the solar generator further comprises a second set of photovoltaic cells, arranged in a fourth zone of the envelope or in the third zone of the envelope, and having a second active face directed towards the outside of the envelope; or .- the solar cells of the first set are bifacial solar cells and the first set comprises a second active face directed towards the outside of the envelope; and the reflector, the first single set of bifacial photovoltaic cells or the first and second sets of photovoltaic cells are configured so as to ensure a cooperative production of electrical energy between the first active face and the second active face as long as the solar misalignment Reflective roll is less than or equal to 10 degrees absolute.
    According to particular embodiments, the balloon equipped with a concentrated solar generator comprises one or more of the following characteristics: the reflector, the first single set of bifacial photovoltaic cells or the first and second sets of photovoltaic cells are configured from so as to maintain an illumination of the second active face as the solar roll-off of the second active face is less than or equal to 80 degrees; the first and second sets of photovoltaic cells are separate and arranged respectively in third and fourth different areas; the first and second sets of photovoltaic cells are separate and each comprise single-faceted photovoltaic cells; and the first and second sets are disposed on and outside the envelope in the same area; and the first and second sets are mutually superimposed, the second set being disposed furthest outside the envelope and the active faces of the photovoltaic cells of the first and second sets being oriented in opposite directions; the first set and the second set are mechanically decoupled from the envelope in terms of deformations of the envelope and / or thermally of the envelope and the carrier gas that the envelope contains; the first set of photovoltaic cells is a set of bifacial photovoltaic cells located above the third zone of the envelope, each bifacial cell having a first face associated with a first electrical polarization and a second face associated with a second electric polarization; bifacial cell manufacturing technology (206) is a technology comprised in the group consisting of Passivated Emitter Rear Totally Diffused (PERT) silicon technology, HTJ (Heterojunction) heterojunction silicon technology, and IBC (Interdigitated Back) silicon technology. Contact) ; Bifacial cell manufacturing and connection technology is a technology for producing heterojunction bifacial photovoltaic cells combined with SmartWire or SWCT connection technology; the bifacial cells are heterojunction bifacial photovoltaic cells, arranged between them so as to produce one or more solar cell chains electrically connected in series and to allow a planar interconnection of the cells between them on the same face without having recourse to through interconnections the whole in thickness from one of its faces to the other; the set of photovoltaic cells comprises a plurality of electronic protection switches each having at least one diode junction to protect one or more photovoltaic cells to protect the cell or cells against a rise in temperature following defects in uniformity of illumination of the second active faces by the reflector; the set of bifacial photovoltaic cells is thermally decoupled from the envelope and the carrier gas that the envelope contains by a support structure and spacing of all the cells of the envelope, the support structure and spacing being fixed on the envelope in the third zone and the set of bifacial solar cells being fixed on the support structure and spacing, and the space bounded by the envelope, the structure and all the cells forming an air circulation channel for cooling the bifacial solar cells by natural or forced convection; the balloon further comprises one or more fans for circulating air in the channel and cooling all the photovoltaic cells; the support and spacing structure is deformable to absorb the thermomechanical deformations of the envelope and / or maintain a sufficient gap between the envelope and all the cells to allow cooling of the cells; the second zone of the envelope, transparent to the solar rays, partially or completely surrounds the third zone (26) of location of the first set of photovoltaic cells intended to receive the solar rays of the reflector, and the surface of the second zone (16 ) is adjusted to ensure sufficient illumination of the photovoltaic cells of the first set and to prevent excessive heating of the solar cells and / or the envelope and / or the carrier gas that the envelope contains. The invention will be better understood on reading the description of several embodiments which follows, given solely by way of example and with reference to the drawings in which: FIG. 1 is a view of a first embodiment of production of a balloon according to the invention equipped with a concentrating solar generator and two sets of monofacial solar cells, the balloon being placed in a first operating configuration for which the concentrator reflector has a slight solar misalignment angle. high less than or equal to 10 degrees; FIG. 2 is a view of the balloon according to the invention of FIG. 1 placed in a second operating configuration for which the active face of a second set of mono-faceted solar cells has a high solar misalignment angle strictly greater than 10. degrees and less than or equal to 80 degrees; FIG. 3 is a view of a second embodiment of a balloon according to the invention equipped with a concentrating solar generator and a single assembly with two opposite faces of bifacial solar cells, the balloon being placed in a first operating configuration for which the concentrator reflector has a low solar misalignment angle of less than or equal to 10 degrees; FIG. 4 is a view of the balloon according to the invention of FIG. 3 placed in a second operating configuration for which the second active face of the single set of bifacial solar cells has a high solar misalignment angle strictly greater than 10 degrees. and less than or equal to 80 degrees; Figure 5 is a schematic view of a bifacial solar or photovoltaic cell using a heterojunction silicon technology; Figure 6 is a view of a bifacial solar cell of Figure 5 using heterojunction silicon technology combined with SmartWire or SWCT connection technology; Figure 7 is a schematic view of the planar interconnection of the solar cells together, forming a chain of electrically connected photovoltaic sources in series, of the set of bifacial solar cells of Figures 3 and 4, here limited to said chain; Fig. 8 is a view of a partial section of the solar cell chain of Fig. 7 in the direction of solar cell thickness showing the arrangement of the cells and their interconnection pattern; Figure 9 is a real view of all the solar cells of Figure 7 interconnected with each other; Fig. 10 is a view of a protective device for protecting solar cells from sudden changes in illumination by concentrated radii.
    According to FIGS. 1 and 2 and a first embodiment, a balloon 2, here a stratospheric balloon, comprises an envelope 4 in inflated pressure and containing a carrier gas 6, for example helium, and comprises a solar generator 8 to concentration of solar radiation.
    The solar generator 8 comprises a reflector 10 of solar rays 12, disposed inside the envelope 4 in a first zone 14 of the envelope, a second zone 16 of the envelope 4, transparent to the solar rays, to let passing the solar rays 12 to the reflector 10. The envelope 4 is for example reinforced polyurethane complex. The second zone 16 of the envelope 4 may be made by using solar-transparent polyurethanes for the envelope and avoiding covering the second zone 16 of the envelope with a coating preventing the passage of solar radiation.
    The solar generator 8 also comprises a first set 22 of mono-faceted photovoltaic cells 24, disposed in a third zone 26 of the envelope 4, the active faces of the cells being directed and oriented in the same direction towards the reflector 10 and forming a first active face 28 of the first set 22.
    The shape of the reflective surface of the reflector 10 is adapted to concentrate the solar rays on the monofacial photovoltaic cells 24 of the first set 22 and conditions the flux angle of the reflected beam of solar rays to concentrate it on the active surface of the photovoltaic cells. mono-facial of the first set 22.
    The reflector 10 can be concentrated by a cloth coated with a reflective coating and plated on said polyurethane envelope in the first zone 14 of the envelope 4. The geometric concentration of the sun's rays on the photovoltaic cells 24 of the first set 22 thus makes it possible to reduce the area of the first set of photovoltaic cells 24 significantly and consequently the associated mass. The concentrated solar energy then passes through a second transparent portion of the envelope which corresponds to part or all of the third zone 26 of the envelope 4.
    The solar generator 8 also comprises a second set 32 of photovoltaic cells 34, disposed in the third zone 26 of the envelope 4 and above the first set 22. The photovoltaic active faces of the cells 34 of the second set 32 are directed and oriented outwardly of the casing 4 and form a second active face 36 of the second assembly 32.
    Alternatively, the second set of monofacial photovoltaic cells, is disposed in a fourth zone, separate from the third zone of the envelope, the photovoltaic active faces of the cells of the second set being directed and oriented towards the outside of the envelope.
    In general, the reflector 10, the second zone 16 of the envelope, the first set 22 of photovoltaic cells 24 and the second set 32 of photovoltaic cells 34 mono-facial are configured so as to ensure a cooperative production of electrical energy between the first set 22 and the second set 32 of photovoltaic cells as long as the roll solar deflection ΔΘ1 of the reflector 10 at concentration is less than or equal to 10 degrees in absolute value, an example of this illumination configuration being shown in FIG. 1.
    According to FIG. 1, the rolling solar misalignment Δ01 of the concentrating reflector 10 is the angle formed between the optical axis 37 of the reflector 10 and a direction of the current sun 38
    According to FIGS. 1 and 2, the balloon 2 is supposed to have an axis 39 of longitudinal direction 39 passing through the center of gravity G of the balloon 2, shown end in FIGS. 1 and 2 and oriented towards the front of the latter, and around which the balloon 2 can rotate at a roll angle Θ.
    According to FIGS. 1 and 2, the cap attitude of the balloon 2 is assumed to have been adjusted so that the optical axis 37 of the reflector 10 and the current pointing direction of the balloon 2 towards the sun form a plane having for normal longitudinal direction 39 of the balloon 2.
    In a further and particular manner, the concentric reflector 10, the second zone 16 of the envelope, the first set 22 and the second set 32 of mono-facial solar cells are configured so as to maintain illumination of the photovoltaic cells 34 of the second together 32 as the rolling solar misalignment ΑΘ2 of the second active face 36 of the second set 32 is less than or equal to 80 degrees, an example of this illumination configuration being shown in Figure 2.
    According to FIG. 2, the rolling solar misalignment ΔΘ2 of the second active face 36 of the second set 32 is the angle formed between the pointing normal 37 'of the second active face 36 of the second set 32 and a direction of the current sun 38 .
    The first and second assemblies 22, 32 are arranged above and outside the envelope in the same third zone 26.
    The first and second assemblies 22, 32 are both superimposed, the second assembly 32 being disposed furthest outside the envelope 4 and the first and second active faces 28, 36 of the first and second assemblies 22, 32 being oriented in opposite directions.
    The cooling of the photovoltaic cells 24, 34 of the first and second assemblies 22, 32 is favored since heating of the photovoltaic cells takes place outdoors and thus benefits from natural or forced ventilation.
    The thermal decoupling between on the one hand the first and second sets of photovoltaic cells 22, 32 and on the other hand the casing 4 and the carrier gas 6 that the casing 4 contains is made by a supporting and spacing structure. 40 of the assemblies 22, 32 of the solar cells 24, 34 of the envelope 4.
    Here in FIGS. 1 and 2, two posts 42, 44 partially represent this support and spacer structure 40. The support structure 40 is fixed on the envelope 4 in the third zone 26 and the first and second assemblies 22, 32 mono-facial photovoltaic cells 24, 34 are fixed on the support structure 40. A space 48, defined by the envelope 4, the structure 40 and all the cells 24, 34 forms an air circulation channel to cool the cells 24, 34 by natural or forced convection.
    Here, in Figures 1 and 2 the convection is forced and provided by four fans 52, 54, 56, 58
    In addition, the support structure and spacer 40 is deformable to absorb the thermomechanical deformations of the envelope and / or maintain a sufficient distance between the envelope and all cells to allow cooling of the cells.
    According to FIGS. 3 and 4 and a second embodiment of the balloon according to the invention, a balloon 202 equipped with a concentrating solar generator has an architecture similar to that of the balloon 2 of FIGS. 1 and 2. Attitude configurations of balloon 202 and illumination of the balloon by the sun with respect to FIGS. 3 and 4 are respectively the same as those of FIGS. 1 and 2.
    The ball 202 differs from the balloon 2 in that the first and second sets 22, 32 of photovoltaic cells form a single single assembly 204 of bifacial photovoltaic cells 206, located above the third zone 26 of the envelope. The set 204 of the bifacial solar cells 206 comprises a first active face 208, oriented towards the concentrator reflector 10, and a second active face 210, oriented towards the outside of the envelope 4 and having a pointing direction opposite to that of the first face 208.
    In general, the concentrating reflector 10, the second zone 16 of the envelope 4, the first active face 208 and the second active face 210 of the assembly 204 of the bifacial photovoltaic cells 206 are configured so as to ensure cooperative production. of electrical energy between the first and second active faces 208, 210 of the assembly 204 of bifacial photovoltaic cells as long as the solar roll-off ΔΘ1 of the reflector 10 at concentration is less than or equal to 10 degrees in absolute value, an example of this illumination configuration being represented in FIG. 3.
    In a further and particular manner, the concentrator reflector 10, the second zone 16 of the envelope, the first active face 208 and the second active face 210 of the set 204 of the bifacial solar cells are configured so as to maintain an illumination of the second active face 210 of the assembly 204 as the rolling solar misalignment ΑΘ2 of the second active face 210 of the assembly 204 is less than or equal to 80 degrees, an example of this illumination configuration being shown in FIG. 4 Like the balloon 2 of FIGS. 1 and 2, the assembly 204 of the bifacial solar cells 206 is thermally decoupled from the envelope 4 and the carrier gas 6 that the envelope 4 contains by the support structure and from spacing 40. The decoupling of the solar cells from the balloon envelope allows cooling of the bifacial solar cells by natural or forced convection, which results in a better ure efficiency of solar cells, the latter being higher at low temperature.
    According to Figures 3 and 4, the convection is here forced and provided by the four fans 52, 54, 56, 58
    In addition, the support and spacer structure 40 is deformable to absorb the thermomechanical deformations of the envelope 4 and / or maintain a sufficient gap between the envelope 4 and the assembly 204 of the bifacial solar cells 206 to allow the cooling cells.
    The bifacial cell technology 206 is a technology that is comprised of Passivated Emitter Rear Totally Diffused (PERT) silicon technology, HTJ (Heterojunction) heterojunction silicon technology, and IBC (Interdigitated Back Contact) silicon technology. .
    According to Figure 5 and a conventional bifacial solar cell structure using a heterojunction silicon technology, a bifacial solar or photovoltaic cell 302 has a plurality of superimposed layers.
    The solar cell 302 comprises a central layer 304 forming a monocrystalline silicon substrate type (n) of high quality on which are deposited amorphous silicon layers 306, 308 of nanometric thickness in a first face 310 and a second face 312 to create the junction and thus ensure excellent surface passivation. On the amorphous silicon layers 306, 308 are deposited transparent oxide layers 314, 316 which ensure the lateral conduction of the charges and allow better optical confinement. On the faces 318, 320 are deposited a metal compound 322 respectively forming a first electrode comb 324 (in English gridfingers) and a second electrode comb 326 to ensure efficient collection of generated charges.
    Thus this symmetrical structure of the solar cell 302 allows illumination by the two faces or sides and an electrical activity of the two faces.
    In a preferred manner, the manufacturing and connecting technology of the bifacial cells is a technology for producing heterojunction bifacial photovoltaic cells combined with the SmartWire or SWCT connection technology.
    According to the SWCT method, metal wires are embedded in a polymer sheet which is applied directly to the metallized surface of the solar cell. Then, the assembly formed by the solar cell and the polymer sheet encrusted by the metallized son is laminated. The metal wires are thus fixed on the metallized layer of the cell and form an electrical contact.
    By increasing the number of busbars passing through the bifacial solar cell on each of its faces and reducing the thickness of said busbars, a better compromise is found between the reduction of the ohmic losses of the electrode combs. and the decrease of the shading of the surface of the solar cell. The use of SmartWire or SWCT connection technology is the ultimate result of this evolution by distributing the metallization over the entire surface of the solar cell as illustrated by a typical cell 352 in Figure 6.
    Advantageously, the use of the SWCT technology which is compatible with HTJ heterojunction silicon technology, reduces the resistance and shading of the solar cell, distributes the mechanical stresses over the entire surface of the cell, and increases the holding connections after thermal cycles compared to a technology using bus bars.
    Preferably, the solar cells of the type of the solar cell 352 are interconnected with each other on the same active face of the assembly, while avoiding that bushings of connections between the face of a first cell located on the same side as the first face of the assembly and the face of a second cell, adjacent to the first cell, located on the same side as the second face of the assembly is performed.
    A so-called planar interconnection method of heterojunction bifacial solar cells comprises a first step and a second step.
    In the first step, the heterojunction bifacial cells of the same chain of cells intended to be electrically connected in series are arranged between them so as to produce on the first active face of the assembly a first alternating distribution of a first polarity. and a second polarity, each bifacial cell having a first face associated with the first polarity and a second face having a second polarity. Complementarily in terms of polarities, for the same solar cell chain a second alternating distribution of the second polarity and the first polarity is performed on the second active face of the assembly.
    Then, in the second step, for each face of the set of bifacial cells, a planar interconnection of the cells between them on the same face is performed according to the arrangement of the cells provided to form one or more chains without resorting to interconnections crossing the whole in thickness from one of its active faces to the other.
    Planar interconnections reduce the risk of damage during thermal cycling and simplify the manufacturing process for all bifacial solar cells
    Advantageously, the planar interconnection method and the method of implementing the SWCT technology can be combined by performing the rolling step of the SWCT technology and the second interconnection step itself of the interconnection process. same time during a shared cooking phase.
    According to FIG. 7 and an exemplary interconnection diagram of cells, a set 402 of bifacial solar cells comprises a certain number of bifacial solar cells, here six solar cells 404, 406, 408, 410, 412, 414, connected to each other. by metal strips 422, 424, 426, 428, 430, 432, 434 to form here a series of photovoltaic cells electrically connected in series between a first electrical terminal 442 at a first polarity, here positive, and a second electrical terminal 444 at a second polarity, here negative.
    Each bifacial solar cell 404, 406, 408, 410, 412, 414 respectively has a first face 454, 456, 458, 460, 462, 464 at the first polarity and a second face 474, 476, 478, 480, 482, 484. at the second polarity.
    The ribbons 422, 424, 426, 428, 430, 432, 434 respectively connect the first electrical terminal 422, the second face 474, the second face 476, the second face 478, the second face 480, the second face 482, the second face 482. face 484 to the first face 454, the first face 456, the first face 458, the first face 460, the first face 462, the first face 464 and the second electrical terminal 444.
    Thus, the electromotive force generated by placing the solar cells in series between the first electrical terminal and the second electrical terminal is equal to the sum of the electromotive forces of the solar cells 404, 406, 408, 410, 412 and 414. The assembly 402 solar cells form a panel or sheet of solar cells having radii of curvature significantly larger than the size of a solar cell, the panel or the web having a first face 492 intended to be oriented towards the outside of the balloon and illuminated directly by the sun, and a second face 494 intended to be oriented towards the inside of the balloon and illuminated by the focusing reflector.
    According to FIG. 8, the interconnection diagram of the solar cells 410, 412 and 414 forming part of the single chain of the assembly 402 of FIG. 7 is represented and highlighted by a partial section of the assembly 402. .
    It is clear in this Figure 8 the absence of interconnections between cells traversing the whole in thickness from one active face to the other.
    According to FIG. 9, a real top view shows the assembly 402 of the solar cells 404, 406, 408, 410, 412, 414 interconnected according to the interconnection diagram described in FIGS. 7 and 8.
    It should be noted that in general the set of bifacial solar cells is not limited to a single solar cell chain.
    According to Figure 10 and an exemplary set of bifacial solar cells, a set 502 of the photovoltaic cells includes a plurality 504 of electronic protection switches 506, 508, 510 each having at least one diode junction.
    The plurality 504 of electronic protection switches 506, 508, 510 are configured to protect one or more photovoltaic cells 522, 524, 526 against a rise in temperature following illumination uniformity defects of the first active face of the 502 assembly by the concentrator reflector.
    Electronic switches are for example discrete diodes or transistors or combinations of diodes and / or transistors.
    It should be noted that in addition to the moderating effect on warming provided by the use of a second set of mono-facial solar cells or a second active face of a single set of bifacial solar cells due to its contribution to the supply of electrical energy iso-power according to a nominal reference pointing, it can be provided in an alternative embodiment described above, a second skin to protect the envelope, to the extent that it receives a concentrated beam of solar rays. Particular polyurethane films can be used for this purpose.
    Whatever the variant used, the reflective zone of the second zone of the envelope may have the shape of the envelope: in this case the shape of the envelope is chosen so as to optimize both the lift of the balloon and the optical convergence of solar rays to photovoltaic cells.
    According to a variant of the invention, the envelope may comprise a first skin and a second skin comprising the reflecting zone of the reflector, so as to have a shape different from that of the envelope. In this case, the shape of the envelope and that of the reflective surface of the reflector can be chosen independently. The shape of the envelope can be adapted to optimize the lift, the shape of the reflective surface being chosen for optical reasons only. In this case and advantageously, the reflective zone may be deformable, so as to optimize its shape also taking into account the angle of incidence of solar rays. This angle may vary depending on the time of day, the season, the altitude and the geographical position of the balloon.
    In general, the shape of the envelope is preferably of revolution. An ellipsoid shape for the envelope is adapted to provide satisfactory lift and optical performance, particularly if the reflective surface is the same as that of the envelope. Alternatively the envelope can be parabolic.
    The usual shapes of balloons that can be both spherical and parabolic, can be used, especially if the shape of the reflective zone is independent of the shape of the envelope.
    The shape of the reflective zone is preferably parabolic.
    In general, the configuration of the envelope leads to confer on the reflecting zone which is part of it a power of concentration of solar rays in the direction of photovoltaic cells. The concentration factor can be adjustable, typically it can be greater than 1 and less than 5, varying with the time of day, since the angle Θ of solar rays varies with the time of day.
    In general, for all the embodiments of the balloon according to the invention, in the case of a nominal score, the solar cells are illuminated by concentration from the inside of the balloon and from outside the balloon by the direct radiation of the Sun. electrical iso-power produced compared to a solution using a concentrator alone limits the radiant power of the concentrator which is a potential source of risk of damage to the balloon due to possible heating of the envelope and / or carrier gas contained in the envelope.
    In case of sufficient misalignment in roll, that is to say beyond about 10 degrees, the solar cells configured to receive the radiation of the concentrator will no longer be illuminated by the interior of the balloon but those oriented towards the outside of the balloon will always be illuminated directly by the sun as long as the ball roll misalignment remains below 80 degrees, which limits the use of the energy storage system on board, for example a fuel cell . In addition, this system is more robust to any yaw misalignment, that is to say a change of course. The advantage of this solution is that in case of misalignment, even if the concentration is not operational the face oriented directly to the sun is still operational, especially during the transition phases, balloon maneuvers.
    To obtain the same results and performances, the bifacial cells can be replaced by a pair of monofascial solar cells, or even the two functions of the solar generator, with internal concentration and without external concentration can be dissociated by being arranged on different locations.
    These solutions are sub-optimal compared to the solution using bifacial cells because in these cases the total number of solar cells forming the two networks is almost doubled, resulting in a larger mass and an increase in complexity.
    In general, the stratospheric balloon described above can be replaced by any other type of balloon evolving in other layers of the atmosphere, keeping identically the characteristics of the invention.
    权利要求:
    Claims (14)
    [1" id="c-fr-0001]
    CLAIMS .1 balloon equipped with a concentrated solar generator comprising an envelope (4) containing a carrier gas (6) and a solar generator (8) with solar radiation concentration, the solar generator (8) comprising a reflector (10). of solar rays, disposed inside the envelope (4) in a first zone (14) of the envelope (4), A second zone (16) of the envelope (4), transparent to the solar rays, for passing solar rays to the reflector (10), and a first set (22; 204) of photovoltaic cells (24; 206) disposed in a third zone (26) of the envelope having a first active face ( 28; 208) directed towards the reflector (10); The first set (22; 204) of photovoltaic cells (24; 206) and the reflector (10) being configured so that the reflector (10) concentrates the sun rays on the first active face (28; 208) of the first set ( 22; 204) of photovoltaic cells (24; 206) when the reflector (10) is placed in the sun pointing position; characterized in that the solar generator (8) further comprises a second set (32) of photovoltaic cells, arranged in a fourth zone of the envelope or in the third zone (26) of the envelope, and having a second face active towards the outside of the envelope (4); or the solar cells of the first set (204) are bifacial solar cells and the first set (204) has a second active face (36) directed outwardly of the envelope (4); and the reflector (10), the first set (204) of the bifacial photovoltaic cells (206) or the first and second sets (22, 32) of the photovoltaic cells (24, 34) are configured to ensure a cooperative production of electrical energy between the first active face (28; 208) and the second active face (36; 210) as long as the solar roll deflection of the reflector (10) is less than or equal to 10 degrees absolute value.
    [2" id="c-fr-0002]
    A solar concentrator-equipped balloon according to claim 1, wherein the reflector (10), the first set (204) of bifacial photovoltaic cells (206) alone or the first and second sets (22, 32) of photovoltaic cells (24, 34) are configured to maintain illumination of the second active face (36; 210) as long as the roll solar misalignment of the second active face (36; 210) is less than or equal to 80 degrees.
    [3" id="c-fr-0003]
    3. Balloon equipped with a solar concentrator according to any one of claims 1 to 2 wherein the first and second sets of photovoltaic cells (22, 32) are separate and arranged respectively in third and fourth different areas.
    [4" id="c-fr-0004]
    4. Balloon equipped with a solar concentrator according to any one of claims 1 to 2, wherein the first and second sets of photovoltaic cells (22, 32) are separate and each comprise mono-faceted photovoltaic cells; and the first and second sets are disposed on and outside the envelope in the same area (26); The first and second assemblies (22, 32) are mutually superposed, the second set (32) being disposed furthest outside the envelope (4) and the active faces of the photovoltaic cells of the first and second sets (22, 32) being oriented in opposite directions.
    [5" id="c-fr-0005]
    5. A solar concentrator pump ball according to any one of claims 1 to 4, wherein the first set (22) and the second set (32) are mechanically decoupled from the envelope in terms of deformations of the envelope and / or thermally envelope and carrier gas that the envelope contains.
    [6" id="c-fr-0006]
    A solar concentrator-equipped balloon according to any one of claims 1 to 2, wherein the first set (204) of photovoltaic cells is a set of bifacial photovoltaic cells (206) located above the third zone. (26) of the envelope (4), each bifacial cell (206) having a first face associated with a first electrical polarization and a second face associated with a second electric polarization.
    [7" id="c-fr-0007]
    A solar concentrator-equipped balloon according to claim 6, wherein the bifacial cell manufacturing technology (206) is a technology comprised in the group consisting of Passivated Emitter Rear Totally Diffused (PERT) silicon technology. HTJ (Heterojunction) heterojunction silicon technology, and IBC (Interdigitated Back Contact) silicon technology.
    [8" id="c-fr-0008]
    A solar concentrator-equipped balloon according to claim 7, wherein the bifacial cell manufacturing and connecting technology (206) is a heterojunction bifacial photovoltaic cell manufacturing technology combined with SmartWire connection technology or SWCT.
    [9" id="c-fr-0009]
    9. Balloon equipped with a solar concentration generator according to any one of claims 7 to 8, wherein the bifacial cells (206) are heterojunction bifacial photovoltaic cells, arranged between them so as to produce one or more string of solar cells electrically connected in series and to allow a planar interconnection of the cells with each other on the same face without having recourse to interconnections passing through the assembly (204) in thickness from one of its faces (208, 210) to the other .
    [10" id="c-fr-0010]
    A solar concentrator-equipped balloon according to any one of claims 6 to 9, wherein the photovoltaic cell assembly (502) comprises a plurality (504) of electronic protection switches (506, 508, 510) each having at least one diode junction for protecting one or more photovoltaic cells to protect the cell or cells against a rise in temperature consecutive to illumination uniformity defects of the second active faces by the reflector.
    [11" id="c-fr-0011]
    A solar concentrator-equipped balloon according to any one of claims 6 to 10, wherein the set (204) of the bifacial photovoltaic cells (206) is thermally decoupled from the shell (4) and the gas carrier (6) that the casing (4) contains a supporting and spacing structure (40) of all the cells of the casing, the supporting and spacing structure (40) being attached to the casing envelope in the third zone (26) and the assembly (204) of the bifacial solar cells (206) being fixed on the supporting and spacing structure (40), and the space (48) delimited by the envelope (4), the structure (40) and the set (204) of the cells forming an airflow channel for cooling the bifacial solar cells (206) by natural or forced convection.
    [12" id="c-fr-0012]
    A solar concentrator balloon according to claim 11, including one or more fans (52, 54, 56, 58) for circulating air through the channel and cooling the cell assembly (204). photovoltaic (206).
    [13" id="c-fr-0013]
    13. Balloon equipped with a solar concentrator according to any one of claims 11 to 12, wherein the support structure and spacer (40) is deformable to absorb the thermomechanical deformations of the envelope and / or maintain a sufficient gap between the envelope and all the cells to allow cooling of the cells.
    [14" id="c-fr-0014]
    14. Balloon equipped with a solar concentration generator according to any one of claims 1 to 13, wherein the second zone (16) of the envelope, transparent to the sun's rays, partially or completely surrounds the third zone (26). locating the first set of photovoltaic cells for receiving the sun's rays from the reflector, and the surface of the second area (16) is adjusted to provide sufficient illumination of the photovoltaic cells of the first set and to prevent excessive heating of the solar cells and / or the envelope (4) and / or the carrier gas (6) that the envelope (4) contains.
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    同族专利:
    公开号 | 公开日
    EP3118103B1|2020-04-22|
    CN106347621A|2017-01-25|
    JP2017024708A|2017-02-02|
    FR3038880B1|2018-03-23|
    CA2936127A1|2017-01-15|
    EP3118103A1|2017-01-18|
    US20170019055A1|2017-01-19|
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    法律状态:
    2016-06-28| PLFP| Fee payment|Year of fee payment: 2 |
    2017-01-20| PLSC| Publication of the preliminary search report|Effective date: 20170120 |
    2017-06-28| PLFP| Fee payment|Year of fee payment: 3 |
    2018-06-28| PLFP| Fee payment|Year of fee payment: 4 |
    2020-06-25| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1501486A|FR3038880B1|2015-07-15|2015-07-15|BALLO EQUIPPED WITH A CONCENTRATED SOLAR GENERATOR USING A SOLAR CELL ARRANGEMENT OPTIMIZED TO FEED IN FLIGHT OF THIS BALLOON|
    FR1501486|2015-07-15|FR1501486A| FR3038880B1|2015-07-15|2015-07-15|BALLO EQUIPPED WITH A CONCENTRATED SOLAR GENERATOR USING A SOLAR CELL ARRANGEMENT OPTIMIZED TO FEED IN FLIGHT OF THIS BALLOON|
    EP16179146.2A| EP3118103B1|2015-07-15|2016-07-13|Balloon equipped with a concentrated solar generator and employing an optimised arrangement of solar cells to power said balloon in flight|
    US15/209,691| US20170019055A1|2015-07-15|2016-07-13|Balloon equipped with a concentrated solar generator and employing an optimised arrangement of solar cells to power said balloon in flight|
    JP2016139376A| JP2017024708A|2015-07-15|2016-07-14|Balloon comprising light concentration type photovoltaic power generator and using solar battery cell arrangement optimized for power supply to the balloon in flight|
    CA2936127A| CA2936127A1|2015-07-15|2016-07-14|Balloon equipped with a concentrated solar generator and employing an optimised arrangement of solar cells to power said balloon in flight|
    CN201610736419.2A| CN106347621A|2015-07-15|2016-07-15|Balloon equipped with a concentrated solar generator and employing an optimised arrangement of solar cells to power said balloon in flight|
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