Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S60/00—Arrangements for storing heat collected by solar heat collectors
  • F24S60/10—Arrangements for storing heat collected by solar heat collectors using latent heat
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S10/00—Solar heat collectors using working fluids
  • F24S10/70—Solar heat collectors using working fluids the working fluids being conveyed through tubular absorbing conduits
  • F24S10/74—Solar heat collectors using working fluids the working fluids being conveyed through tubular absorbing conduits the tubular conduits are not fixed to heat absorbing plates and are not touching each other
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S10/00—Solar heat collectors using working fluids
  • F24S10/70—Solar heat collectors using working fluids the working fluids being conveyed through tubular absorbing conduits
  • F24S10/75—Solar heat collectors using working fluids the working fluids being conveyed through tubular absorbing conduits with enlarged surfaces, e.g. with protrusions or corrugations
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S23/74—Arrangements for concentrating solar-rays for solar heat collectors with reflectors with trough-shaped or cylindro-parabolic reflective surfaces
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S23/77—Arrangements for concentrating solar-rays for solar heat collectors with reflectors with flat reflective plates
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S23/79—Arrangements for concentrating solar-rays for solar heat collectors with reflectors with spaced and opposed interacting reflective surfaces
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S70/00—Details of absorbing elements
  • F24S70/60—Details of absorbing elements characterised by the structure or construction
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S80/00—Details, accessories or component parts of solar heat collectors not provided for in groups F24S10/00-F24S70/00
  • F24S80/60—Thermal insulation
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B19/00—Condensers, e.g. light collectors or similar non-imaging optics
  • G02B19/0004—Condensers, e.g. light collectors or similar non-imaging optics characterised by the optical means employed
  • G02B19/0019—Condensers, e.g. light collectors or similar non-imaging optics characterised by the optical means employed having reflective surfaces only (e.g. louvre systems, systems with multiple planar reflectors)
  • G02B19/0023—Condensers, e.g. light collectors or similar non-imaging optics characterised by the optical means employed having reflective surfaces only (e.g. louvre systems, systems with multiple planar reflectors) at least one surface having optical power
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B19/00—Condensers, e.g. light collectors or similar non-imaging optics
  • G02B19/0033—Condensers, e.g. light collectors or similar non-imaging optics characterised by the use
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B19/00—Condensers, e.g. light collectors or similar non-imaging optics
  • G02B19/0033—Condensers, e.g. light collectors or similar non-imaging optics characterised by the use
  • G02B19/0038—Condensers, e.g. light collectors or similar non-imaging optics characterised by the use for use with ambient light
  • G02B19/0042—Condensers, e.g. light collectors or similar non-imaging optics characterised by the use for use with ambient light for use with direct solar radiation
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S10/00—Solar heat collectors using working fluids
  • F24S10/40—Solar heat collectors using working fluids in absorbing elements surrounded by transparent enclosures, e.g. evacuated solar collectors
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S2023/84—Reflective elements inside solar collector casings
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S2023/86—Arrangements for concentrating solar-rays for solar heat collectors with reflectors in the form of reflective coatings
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S2023/87—Reflectors layout
  • F24S2023/872—Assemblies of spaced reflective elements on common support, e.g. Fresnel reflectors
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S2023/87—Reflectors layout
  • F24S2023/878—Assemblies of spaced reflective elements in the form of grids, e.g. vertical or inclined reflective elements extending over heat absorbing elements
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S2023/88—Multi reflective traps
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S23/00—Arrangements for concentrating solar-rays for solar heat collectors
  • F24S23/70—Arrangements for concentrating solar-rays for solar heat collectors with reflectors
  • F24S23/82—Arrangements for concentrating solar-rays for solar heat collectors with reflectors characterised by the material or the construction of the reflector
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F24—HEATING; RANGES; VENTILATING
  • F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
  • F24S80/00—Details, accessories or component parts of solar heat collectors not provided for in groups F24S10/00-F24S70/00
  • F24S80/50—Elements for transmitting incoming solar rays and preventing outgoing heat radiation; Transparent coverings
  • F24S80/52—Elements for transmitting incoming solar rays and preventing outgoing heat radiation; Transparent coverings characterised by the material
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
  • F28D20/00—Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00
  • F28D20/02—Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00 using latent heat
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
  • Y02B10/00—Integration of renewable energy sources in buildings
  • Y02B10/20—Solar thermal
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
  • Y02E10/00—Energy generation through renewable energy sources
  • Y02E10/40—Solar thermal energy, e.g. solar towers
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
  • Y02E10/00—Energy generation through renewable energy sources
  • Y02E10/40—Solar thermal energy, e.g. solar towers
  • Y02E10/44—Heat exchange systems

Definitions

• the present invention relates to a solar thermal panel for storing and returning solar thermal energy.
• a solar thermal panel of the type comprising at least one thermal collection element for receiving solar rays.
• a solar panel is for example intended to be coupled to a thermal machine, for the transformation of solar thermal energy into electrical or mechanical energy.
• the solar thermal energy can also be recovered to produce heat or cold, for example for a heating or refrigeration plant.
• the thermal collection element has a generally tubular shape, and it is arranged in a vacuum glass tube, coaxially with this glass tube.
• the solar panel further includes reflective elements, arranged to focus received solar rays toward the thermal collection element.
• the thermal energy of the solar rays is then restored by means of a heat transfer fluid, circulating in the heart of the thermal collection element, by thermal transfer between the collection element and the heat transfer fluid.
• thermal efficiency of such a solar panel is generally limited by thermal losses, due to thermal radiation emitted by the thermal collection element. This thermal radiation is particularly important when the temperature and the surface of the collection element are important.
• such a solar panel generally has a low efficiency at high temperature, for example at a temperature above 400 ° C.
• the present invention is intended to overcome this disadvantage, providing a solar thermal panel with a satisfactory performance, even at high temperature.
• the invention particularly relates to a solar thermal panel, of the type comprising at least one thermal collection element for receiving solar rays, characterized in that the panel comprises:
• a housing for the thermal collection element this housing being delimited by walls surrounding the thermal collection element, at least one wall of the housing comprising at least one slot for passing sunlight, preferably a plurality of slots,
• At least one reflecting zone arranged facing the thermal collection element, this reflecting zone being able to reflect a thermal radiation emitted by the thermal collection element
• each reflecting strip being arranged opposite a respective slot so as to focus a received radiation towards this slot
• each elongate reflective element having a planar base and two concave surfaces, so that the elongated reflective element has a substantially triangular cross section, the elongate reflective elements being arranged side by side so that their planar bases are coplanar and together form the slotted housing wall, each slit being formed by a gap between two adjacent elongated reflective elements, and each concave surface being arranged facing a reflective strip, so that reflected radiation by a concave surface is focused towards the corresponding reflective strip.
• the thermal radiation is not lost in full. In other words, the thermal losses are limited, and the thermal efficiency of the solar panel is increased.
• the focusing of the thermal radiation by mirrors has a better efficiency than a lens focusing known in the state of the art.
• a lens focusing device has undesirable achromatic effects, because the angle of refraction of the light rays by the lenses depends on their wavelength, which leads to an enlargement of the image which can only be corrected by adding a corrective lens.
• a lens focusing device is relatively complex, and allows a lower solar radiation transmission efficiency than a mirror focusing device.
• a solar thermal panel according to the invention comprises one or more of the following characteristics, taken alone or in any technically possible combination.
• Each pair of adjacent reflective elements forms a parabolic primary mirror, having a slot at its center
• the reflective strip arranged opposite this pair of reflecting elements forms a convex hyperbolic secondary mirror
• the reflecting elements and the reflecting strip are arranged so that the optical axes of the primary and secondary mirrors coincide, and that the focal point of the parabolic primary mirror coincides with one of the focal points of the hyperbolic mirror.
• Each pair of adjacent reflective elements forms a parabolic primary mirror, having a slot at its center
• the reflective strip arranged opposite this pair of reflecting elements forms a concave elliptical secondary mirror
• the reflecting elements and the reflecting band are arranged so that the optical axes of the primary and secondary mirrors coincide, and that the focal point of the parabolic primary mirror coincides with one of the focal points of the elliptical mirror.
• Each wall of the housing comprises at least one reflecting zone arranged facing the thermal collection element, this reflecting zone extending preferably over the entire wall.
• the housing comprises thermal insulation spacers, arranged between the thermal collection element and at least one wall of the housing.
• the solar thermal panel has a parallelepipedal general shape defined by side faces, a lower face and an upper face, defining together an interior space in which the housing is arranged, so that the housing has a bottom wall formed by the underside.
• the housing comprises lateral walls formed by the lateral faces, the housing comprises an upper wall, arranged between the upper and lower faces of the panel, parallel to these faces, comprising the at least one slot, and the upper face is formed by a transparent plate, preferably glass.
• the solar thermal panel comprises thermal transport means, comprising: a heat exchanger between the thermal collection element and a heat transfer fluid, housed in the thermal collection element, at least one tubular heat transfer fluid transfer element, connecting the heat exchanger with the outside of the solar panel, passing through a hole in a wall of the housing, and at least one seal and thermally insulating, interposed between the tubular element and the orifice.
• the thermal collection element comprises a shell capable of absorbing solar radiation and / or thermal, preferably metallic, enveloping a phase change material.
• the phase change material is selected from anthraquinone, or aluminum.
• the thermal collection element is formed by a tubular element, in which circulates a heat transfer fluid, this tubular element preferably being provided with an outer coating highly heat-absorbing and having a low thermal emissivity.
• a reflective zone is formed by a tubular reflection element, coaxially surrounding the tubular thermal collection element, this tubular reflection element being formed by an insulating material whose inner surface is treated, for example metallized, to make it reflective to residual thermal radiation emitted by the tubular heat collection element, and comprising on its upper generatrix a slot for passing the incident thermal radiation.
• the solar thermal panel comprises at least one element for introducing or discharging the thermal fluid, connected to all of the thermal collection elements, housed in a chamber laterally extending the panel, delimited by walls of thermally insulating material.
• FIG. 1 is a perspective view of a solar panel, cut transversely, according to a first exemplary embodiment of the invention
• FIG. 2 is a perspective view of the solar panel of FIG. 1 as a whole
• FIGS. 3 and 4 are perspective views of reflecting elements equipping the solar panel of FIG. 1;
• FIG. 5 is a perspective view of a thermal radiation focusing device, comprising reflecting elements such as that of FIG. 3;
• FIG. 6 is a view similar to Figure 5, a thermal radiation focusing device according to an alternative embodiment
• FIG. 7 is a perspective view of a thermal collection element fitted to the solar panel of FIG. 1;
• FIG. 8 is a cross-sectional view of a solar panel according to a second exemplary embodiment of the invention.
• FIG. 9 is a cross-sectional view of a thermal collection element equipping the solar panel of FIG. 8
• FIG. 10 is a view from above of a thermal storage element equipping the solar panel of FIG. 8.
• FIGS. 1 and 2 show a solar thermal panel 10 according to a first exemplary embodiment of the invention.
• the solar panel 10 has a parallelepipedal general shape, bounded by an upper face 12 intended to be turned towards the sun in order to receive solar rays, a lower face 14, opposite to the upper face 12 and longitudinal side faces, respectively longitudinal 16A and transverse 16B, joining the upper faces 12 and lower 14 between them.
• the solar panel 10 has lengths and widths, defined by the top 12 and bottom 14 faces, of about 1 m each, and a thickness, defined by the side faces 16A, 16B, of between 8 and 20 cm.
• the upper, lower, and lateral faces 16A and 16B together define a closed internal space 17 and are connected in a sealed manner to each other, for example by gluing, so that this internal space 17 is airtightly insulated. relative to the outside of the solar panel 10.
• the air is extracted from the internal space 17 in order to evacuate it.
• the elements arranged inside this internal space 17, which will be described later, are not subject to oxidative degradation on contact with air.
• the upper face 12 is formed by a transparent plate capable of allowing the sun's rays to pass through.
• this transparent plate 12 is made of glass, preferably of low iron content, so as to have an optimum coefficient of transmission of solar rays.
• the outer surface of the transparent plate 12 comprises an anti-reflection coating, intended to optimize its solar radiation transmittance.
• the transparent plate 12 has a substantially flat shape, so as not to deflect the solar rays passing through this transparent plate 12.
• the transparent plate 12 has length and width of about 1 m each, and a thickness between 1 and 2 cm.
• the transparent plate 12 is provided curved during the manufacture of the solar panel 10, so that the deformation of this transparent plate 12, by gravity and by the vacuum realized in the solar panel 10, opposes this bulging so as to lead to its flatness.
• side faces 16A, 16B and the lower face 14 are preferably formed by sun-opaque plates.
• the solar thermal panel 10 comprises at least one thermal collection element 18, intended to receive the solar rays, housed in a housing 20 formed in the internal space 17.
• this thermal collection element 18 has a parallelepipedal general shape, so as to have an optimal volume in the solar panel 10.
• the housing 20 is delimited by a bottom wall 22, side walls 24 and an upper wall 26.
• the bottom wall 22 is formed by the opaque plate forming the bottom face 14.
• the side walls 24 are formed by the side plates forming the side faces 16A, 16B.
• the upper wall 26 is arranged between the upper and lower faces 14 of the panel 10, parallel to these faces 12, 14, and has slots 28 for passing sunlight into the housing 20.
• the thermal panel 10 comprises at least one reflecting zone arranged facing the thermal collection element 18. Such a reflecting zone is able to reflect a thermal radiation emitted by the thermal collection element 18.
• At least one wall among the bottom wall 22, the side walls 24 and the upper wall 26, comprises such a reflecting zone.
• each wall 22, 24 and 26 of the housing 20 comprises such a reflecting zone, and each of these reflecting zones extends over the entire corresponding wall.
• each reflective zone is formed by a reflective coating, for example an aluminum coating, applied to the corresponding wall 22, 24, 26.
• each reflecting band is arranged between the housing 20 and the upper face 12 of the solar panel 10, extending parallel to the longitudinal side faces 16A, facing a respective slot 28.
• each reflecting band 30 is arranged on an inner face of the transparent plate 12, and its width is substantially identical to the width of the slot 28 opposite which it extends.
• the reflective strips 30 are for example made by depositing a reflective layer, for example aluminum or silver, on the inner face of the transparent plate 12.
• the solar panel 10 comprises a plurality of reflecting elements 32, as shown in FIG. in detail in Figure 3.
• Each reflective element 32 has a generally elongate shape extending along a dimension, for example over the entire length, of the solar panel 10. These elongated elements 32 are further juxtaposed along another dimension, for example over the entire width of this solar panel 10.
• each reflecting element 32 has a planar base 34 and two parabolic concave surfaces 36 so as to have a substantially triangular curvilinear cross section.
• the reflective elements 32 are juxtaposed so that their bases 34 are coplanar, and so that these bases 34 together form the upper wall 26 of the housing 20.
• Each slot 28 of this upper wall 26 is then formed by a space left between two adjacent reflective elements 32.
• each reflecting element 32 is covered with a reflective coating, for example aluminum, so as to form the reflecting zone of the upper wall 26.
• Each parabolic surface 36 is arranged facing a reflective strip 30, so that the solar rays reflected by each parabolic surface 36 are focused towards the corresponding reflective strip 30, which in turn focuses these solar rays towards the collection element. 18, through the slots 28.
• each pair of adjacent reflective elements 32 forms a parabolic primary mirror 36, having a slot 28 at its center, and the reflecting strip 30, arranged opposite this pair of reflecting elements 32, forms a convex hyperbolic secondary mirror, as shown in FIG. 5.
• Such a convex hyperbolic reflecting strip 30 is preferably attached, for example by gluing, to the inside of the transparent plate 12.
• the reflective strip 30 forms a concave elliptical secondary mirror.
• Such an elliptical reflective strip is preferably made by digging the inner face of the transparent plate 12 so as to obtain this concave elliptical shape, then by depositing a reflective layer.
• the reflective elements 32 and the reflective band 30 are arranged so that the optical axes of the primary 36 and secondary 30 mirrors coincide, and the focus of the parabolic primary mirror 36 coincides with a first focus of the hyperbolic secondary mirror or elliptical.
• the solar rays are reflected on the parabolic primary mirror 36 towards the focus of this parabolic mirror. Since this focus is also the first focus of the hyperbolic or elliptical secondary mirror 30, the rays are then reflected to a second focus of this secondary mirror 30.
• the solar panel 10 also comprises two lateral elongated reflective elements 38, shown in greater detail in FIG. 4.
• These lateral elements 38 each comprise a flat base 40, arranged coplanar with the bases 34 reflective elements 32, a concave face 42 arranged facing a corresponding reflective strip 30, and a flat face 44 intended to be fixed in abutment on the side plates forming the longitudinal side faces 16A.
• each elongated reflective element 32, 38 is fixed by its longitudinal ends to the transverse side faces 16B of the solar panel 10.
• a flange (not shown) is provided on each of the transverse side faces 16B, the longitudinal ends of each elongated reflective element 32, 38 resting and being glued on a respective flange.
• each elongate reflective element 32, 38 are for example made of glass, by molding or by extrusion, and covered with a reflective coating, for example aluminum, to give them their reflective function.
• each elongate reflective element 32 (respectively 38), has a length of 1 m, a width of 10 cm (respectively 5 cm), and a height of 2 cm.
• the housing 20 advantageously comprises spacers 46 of thermal insulation, arranged between the thermal collection element 18 and the wall
• the thermal collection element 18 does not rest directly on the lower wall 22, and therefore does not exchange heat by conduction with this lower wall 22.
• FIG. 7 shows an example of a thermal collection element 18.
• This thermal collection element 18 comprises an envelope 48, capable of absorbing solar and / or thermal radiation, enveloping a phase-change material 50.
• the envelope 48 is preferably metallic, and made of a material chosen according to the temperature to be reached by the thermal collection element 18.
• the surface of this envelope 48 is treated, by conventional means, so as to him to confer an optimum absorption capacity of the thermal energy received.
• the envelope 48 is covered with a black color coating.
• phase change material is a material capable of accumulating or yielding thermal energy at a constant temperature by a change of physical state at this temperature.
• the height used to quantify the energy involved in a phase change is latent heat.
• the thermal collection element 18 has a thermal accumulator function in addition to its thermal collection function.
• the phase change material 50 is chosen as a function of the working temperature of the thermal collection element 18.
• the phase change material 50 is selected from paraffin or stearic acid.
• the phase change material 50 is, for example, aluminum (whose melting point is 658 ° C and the latent heat of fusion 395 kJ / kg).
• the phase-change material 50 is, for example, anthraquinone (whose melting temperature is 286 ° C. and the latent heat of fusion is 157 kJ / kg).
• the latent heat of fusion of this material is sufficiently high that a reasonable quantity thereof (between 40 and 100 kg per m 2 of panel) can make it possible to achieve a 24-hour thermal recovery at a constant temperature equal to melting temperature mentioned above.
• the safety of anthraquinone makes it possible to handle it safely during the manufacture of the solar panel 10.
• anthraquinone being a pure body, has the advantage of not being subject to thermal decomposition as this is the case for some materials implemented in the state of the art.
• the thermal collection element 18 also comprises a heat exchanger 52, housed in the casing 48, for exchanging heat between the phase change material 50 and a heat transfer fluid 54 flowing in this heat exchanger.
• the heat exchanger 52 preferably comprises fins 56 immersed in the phase-change material 50.
• the heat transfer fluid 54 circulates in the casing 48 in a circulation tube 58, around which the fins 56 extend.
• the circulation tube 58 extends in the thermal collection element 18, for example in boustrophedon.
• This circulation tube 58 is connected to a conventional type of thermal machine (not shown), external to the solar panel 20, via a tubular input element 60 and a tubular outlet element 62 for transferring heat.
• heat transfer fluid 54 is adapted to convert thermal energy into mechanical or electrical energy.
• the thermal energy could also be recovered to produce heat or cold, for example for a heating or refrigeration plant, industrial or domestic.
• tubular inlet 60 and outlet 62 members pass through respective orifices 63 formed in a lateral face of the housing 20, for example a transverse lateral face 16B, as shown in FIG. 2, in the direction of the thermal machine. .
• a seal 64 is arranged between the tubular member 60 and the corresponding orifice. This seal 64 is sealed so as to allow the vacuum to remain in the solar panel 20, and this seal 64 is thermally insulating so as not to cause heat loss.
• the solar panel is oriented, during its construction, towards the south.
• the solar panel 10 is operated by an orientation device of this solar panel 10, intended to maintain the upper face 12 of the solar panel 10 in a direction perpendicular to the plane of the ecliptic, to ensure a significant amount of sunshine .
• the solar rays pass through the transparent upper face 12. These solar rays are reflected on the concave faces 36, 42 of the reflecting elements 32, 38, so as to focus these rays on the reflective strips 30 .
• Each reflective band 30 then focuses the solar rays received, through the corresponding slot 28, towards the thermal collection element 18.
• the solar panel 10 according to the invention makes it possible to reduce the thermal losses emitted by the thermal collection element 18.
• the evacuation of air from the inside of the solar panel 10 limits the convection around the thermal collection element 18.
• the spacers 46 of thermal insulation arranged between the thermal collection element 18 and the lower wall 22 of the housing 20, limit the conduction between this thermal collection element 18 and the bottom wall 22.
• the thermal radiation emitted by the thermal collection element 18 is confined within the solar panel 18 because the walls of the housing 20 are treated to reflect this thermal radiation.
• the outer surface of the envelope 48 of the thermal collection element 18 is treated to absorb as much as possible the solar radiation transmitted by the reflective strips 30 and the thermal radiation reflected by the faces of the housing 20.
• FIG. 8 shows a solar panel 10 according to a second exemplary embodiment of the invention.
• elements similar to those of the preceding figures are designated by identical references.
• the solar panel 10 comprises a plurality of thermal collection elements 18, in particular a thermal collection element 18 by a set of primary 36 and secondary 30 mirror assemblies.
• Each of these thermal collection elements 18 has a thermal transfer function towards a thermal storage element arranged for example outside the thermal panel 10, which will be described later with reference to FIG. 10.
• the solar thermal panel 10 comprises spacers 65, arranged between two adjacent thermal collection elements 18, and extending between the flat base 34 of a reflecting element 32 and the lower face 14 of the panel 10, so as to delimit respective dwellings for the thermal collection elements.
• these spacers 65 comprise a reflective coating.
• thermal collection element 18 An example of thermal collection element 18 is shown in FIG. 8.
• This heat collection element 18 is formed by a tubular heat transfer element in which circulates a heat transfer fluid 66, ensuring the heat transfer.
• this tubular heat collection element 18 is provided with a highly absorbent outer coating (ensuring a thermal absorption as close as possible to 100%) and having a low thermal emissivity so that the tubular element 18 emits a minimum of heat radiation, even when worn high temperature.
• the tubular heat-collecting element 18 is arranged so that the reflective elements 32 and the reflective strips 30 focus the solar rays on the upper generatrix of this tubular element 18.
• this upper generatrix coincides with the focal line hyperbolic or elliptical secondary mirror 30.
• a reflecting zone is carried by a tubular reflection element 70, coaxially surrounding the tubular heat-collecting element 18.
• This tubular reflection element 70 is preferably formed by an insulating material whose inner surface is metallized to make it reflective of the residual heat radiation emitted by the tubular heat transfer element 18, and comprising on its upper generatrix a slot 72 intended to let the incident solar rays pass.
• this tubular reflection element 70 is interspersed with centering rings, preferably made of the same insulating material as the tubular element 70, and provided with spikes. 74.
• These internal tips 74 allow in particular to maintain fixed the position of the upper generatrix of the tubular heat collection element 18, regardless of the temperature of the heat transfer fluid 66.
• the tips 74 are made of an insulating material, and have a conical shape whose apex cooperates with the tubular heat collection element 18 to minimize the contact between these points 74 and the thermal collection element 18. , thermal losses are minimized by contact of the thermal collection element 18 with these tips 74.
• FIG. 10 shows an element 76 for introducing or evacuating the thermal fluid, arranged inside the panel 10.
• Such elements 76 for introduction on the one hand, and for evacuation on the other hand are respectively arranged on either side of the panel 10, inside this panel 10.
• the introduction and evacuation elements are identical, and respectively provide the introduction of the thermal fluid to be heated, and the evacuation of the heated thermal fluid.
• Each element 76 is connected to the thermal collection elements 18 in order to introduce or evacuate the thermal fluid circulating in these thermal collection elements 18.
• the element 76 comprises bellows-shaped portions 78, allowing longitudinal thermal expansion of this element 76.
• the element 76 is housed in an enclosure laterally extending the panel 10, delimited by walls 80 made of thermally insulating material, and by a closure element 81.
• these walls 80 are provided with a reflective inner surface. It will be noted that this enclosure is sufficiently spacious to allow radial thermal expansion of the element 76.
• At least one of the walls 80 is provided with openings 82 for the passage of the thermal collection elements 18 from the panel 10 to the element 76.
• each opening 82 is completed with a thermal insulating seal, intended to prevent heat loss through this opening, similarly to the openings 63 and the seals and insulators 64 described above with reference to Figure 2.
• this wall 80 provided with an opening generally forms a side wall 16B of the sign.
• the enclosure in which the element for introducing the thermal fluid to be heated is arranged forms a bottom part of the panel, and the enclosure in which the element for discharging the heated thermal fluid is arranged forms an upper part of the panel.
• the side walls of adjacent panels may have openings, so that the internal spaces of these adjacent solar panels communicate with each other, all of these interior spaces remaining watertight relative to the outside. It is thus possible to evacuate these adjacent solar panels in a single operation.
• the heat transfer fluid circuit 54 can pass through several solar panels while remaining in a vacuum environment.

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• 2010
  • 2010-02-23 FR FR1051289A patent/FR2956727B1/fr not_active Expired - Fee Related
• 2011
  • 2011-02-23 WO PCT/FR2011/050376 patent/WO2011104479A1/fr active Application Filing
  • 2011-02-23 US US13/580,506 patent/US8656906B2/en not_active Expired - Fee Related
  • 2011-02-23 EP EP11712628A patent/EP2539644A1/de not_active Withdrawn

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