US20160356527A1 - Solar thermal absorber element - Google Patents
Solar thermal absorber element Download PDFInfo
- Publication number
- US20160356527A1 US20160356527A1 US15/174,388 US201615174388A US2016356527A1 US 20160356527 A1 US20160356527 A1 US 20160356527A1 US 201615174388 A US201615174388 A US 201615174388A US 2016356527 A1 US2016356527 A1 US 2016356527A1
- Authority
- US
- United States
- Prior art keywords
- absorber
- sealing
- fore
- insulation part
- cover glass
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000006096 absorbing agent Substances 0.000 title claims abstract description 104
- 238000007789 sealing Methods 0.000 claims abstract description 65
- 238000009413 insulation Methods 0.000 claims abstract description 38
- 239000006059 cover glass Substances 0.000 claims abstract description 23
- 239000011521 glass Substances 0.000 claims abstract description 23
- 229920001169 thermoplastic Polymers 0.000 claims abstract description 16
- 239000004416 thermosoftening plastic Substances 0.000 claims abstract description 16
- 239000007789 gas Substances 0.000 claims description 31
- 238000004519 manufacturing process Methods 0.000 claims description 14
- 239000011248 coating agent Substances 0.000 claims description 12
- 238000000576 coating method Methods 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 8
- 229910052786 argon Inorganic materials 0.000 claims description 4
- 229920000582 polyisocyanurate Polymers 0.000 claims description 3
- 239000011495 polyisocyanurate Substances 0.000 claims description 3
- 229920002635 polyurethane Polymers 0.000 claims description 3
- 239000004814 polyurethane Substances 0.000 claims description 3
- 238000001771 vacuum deposition Methods 0.000 claims description 2
- 241000238631 Hexapoda Species 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 6
- 239000010936 titanium Substances 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 5
- 239000000428 dust Substances 0.000 description 5
- 229910052710 silicon Inorganic materials 0.000 description 5
- 125000006850 spacer group Chemical group 0.000 description 5
- 229910052684 Cerium Inorganic materials 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910052727 yttrium Inorganic materials 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 239000004411 aluminium Substances 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 230000005855 radiation Effects 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 230000002528 anti-freeze Effects 0.000 description 2
- 125000000484 butyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 2
- 238000009833 condensation Methods 0.000 description 2
- 230000005494 condensation Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052756 noble gas Inorganic materials 0.000 description 2
- 238000005240 physical vapour deposition Methods 0.000 description 2
- 238000005334 plasma enhanced chemical vapour deposition Methods 0.000 description 2
- 238000000623 plasma-assisted chemical vapour deposition Methods 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- XDLMVUHYZWKMMD-UHFFFAOYSA-N 3-trimethoxysilylpropyl 2-methylprop-2-enoate Chemical compound CO[Si](OC)(OC)CCCOC(=O)C(C)=C XDLMVUHYZWKMMD-UHFFFAOYSA-N 0.000 description 1
- 108010053481 Antifreeze Proteins Proteins 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229920002522 Wood fibre Polymers 0.000 description 1
- 238000002835 absorbance Methods 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000003667 anti-reflective effect Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 229910052743 krypton Inorganic materials 0.000 description 1
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 description 1
- 239000002557 mineral fiber Substances 0.000 description 1
- 150000002835 noble gases Chemical class 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000005336 safety glass Substances 0.000 description 1
- 239000003566 sealing material Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
- 239000002025 wood fiber Substances 0.000 description 1
- 210000002268 wool Anatomy 0.000 description 1
- 229910052724 xenon Inorganic materials 0.000 description 1
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- 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
- F24S10/50—Solar heat collectors using working fluids the working fluids being conveyed between plates
-
- 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
- F24S80/70—Sealing means
-
- F24J2/465—
-
- 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
- F24S80/65—Thermal insulation characterised by the material
-
- F24J2/0488—
-
- F24J2/05—
-
- F24J2/507—
-
- 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
- F24S10/00—Solar heat collectors using working fluids
- F24S10/50—Solar heat collectors using working fluids the working fluids being conveyed between plates
- F24S10/504—Solar heat collectors using working fluids the working fluids being conveyed between plates having conduits formed by paired non-plane plates
-
- 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
- F24S10/50—Solar heat collectors using working fluids the working fluids being conveyed between plates
- F24S10/506—Solar heat collectors using working fluids the working fluids being conveyed between plates having conduits formed by inflation of portions of a pair of joined sheets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S25/00—Arrangement of stationary mountings or supports for solar heat collector modules
- F24S25/20—Peripheral frames for modules
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S70/00—Details of absorbing elements
- F24S70/20—Details of absorbing elements characterised by absorbing coatings; characterised by surface treatment for increasing absorption
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S70/00—Details of absorbing elements
- F24S70/20—Details of absorbing elements characterised by absorbing coatings; characterised by surface treatment for increasing absorption
- F24S70/225—Details of absorbing elements characterised by absorbing coatings; characterised by surface treatment for increasing absorption for spectrally selective absorption
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S70/00—Details of absorbing elements
- F24S70/20—Details of absorbing elements characterised by absorbing coatings; characterised by surface treatment for increasing absorption
- F24S70/25—Coatings made of metallic material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S70/00—Details of absorbing elements
- F24S70/30—Auxiliary coatings, e.g. anti-reflective coatings
-
- 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
- F24S80/50—Elements for transmitting incoming solar rays and preventing outgoing heat radiation; Transparent coverings
-
- 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
- F24S80/54—Elements for transmitting incoming solar rays and preventing outgoing heat radiation; Transparent coverings using evacuated elements
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S25/00—Arrangement of stationary mountings or supports for solar heat collector modules
- F24S2025/01—Special support components; Methods of use
- F24S2025/011—Arrangements for mounting elements inside solar collectors; Spacers inside solar collectors
-
- 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
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P80/00—Climate change mitigation technologies for sector-wide applications
- Y02P80/10—Efficient use of energy, e.g. using compressed air or pressurized fluid as energy carrier
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P80/00—Climate change mitigation technologies for sector-wide applications
- Y02P80/20—Climate change mitigation technologies for sector-wide applications using renewable energy
Definitions
- the application relates generally to a solar thermal absorber element.
- Sand, salt, and insects which have invaded inside a structure of solar thermal collectors along flowing air, cause damages decreasing a lifetime and an efficiency of the collectors.
- thermoplastic spacer (TPS) sealed absorber module wherein a cover glass is sealed with an absorber by a TPS.
- the TPS sealed module protects the absorber by preventing undesirable sand, salt, and insects to invade inside the absorber element.
- One object of the invention is to withdraw the above-mentioned drawback and provide a solar thermal absorber element, which comprises a TPS sealed back insulation that enables to manufacture elements in mass production by existing automatic production lines that are used for manufacturing of a TPS insulation glass.
- One object of the invention is fulfilled by providing a solar thermal absorber element of claim 1 , a solar thermal collector of claim 6 , and a method of claim 7 .
- One embodiment of the invention is a solar thermal absorber element that comprises a cover glass, a direct-flow absorber, a fore thermoplastic sealing for attaching the cover glass and the absorber to each other so that there is a distance therebetween, and a fore sealed space, which is formed by the cover glass, the absorber, and the fore sealing.
- the fore space is filled up with a first low thermal conductive gas.
- the element further comprises a back insulation part, a back thermoplastic sealing for attaching the insulation part and the absorber to each other so that there is a distance therebetween, and a back sealed space, which is formed by the insulation part, the absorber, and the back sealing.
- the back space is filled up with a second low thermal conductive gas.
- the direct-flow absorber refers to an absorber, wherein heat transport fluid, e.g. water, air, or antifreeze, circulates inside a structure of the absorber.
- heat transport fluid e.g. water, air, or antifreeze
- thermoplastic sealing refers to a sealing (spacer), which is made by a thermoplastic spacer (TPS) technology.
- TPS thermoplastic spacer
- the low thermal conductive gas refers to a gas, which has a low thermal conductivity, e.g. noble gases.
- the noble gas can be e.g. argon, krypton, or xenon.
- the roll-bond absorber refers to an absorber, which comprises at least one tube and which is provided by a roll-bond technology.
- the highly selective vacuum coating refers to e.g. a coating, which is deposited in vacuum and which forms a selective absorber coating with a solar absorbance more than 96% with low thermal emission by radiation in the infrared.
- One embodiment of the invention is a solar thermal collector that comprises an absorber element.
- the element comprises a cover glass, a direct-flow absorber, a fore thermoplastic sealing for attaching the cover glass and the absorber to each other so that there is a distance therebetween, and a fore sealed space, which is formed by the cover glass, the absorber, and the fore sealing.
- the fore space is filled up with a first low thermal conductive gas.
- the element further comprises a back insulation part, a back thermoplastic sealing for attaching the insulation part and the absorber to each other so that there is a distance therebetween, and a back sealed space, which is formed by the insulation part, the absorber, and the back sealing.
- the back space is filled up with a second low thermal conductive gas.
- One embodiment of the invention is a method for manufacturing a solar thermal absorber element.
- the element comprises a cover glass, a direct-flow absorber, a fore and back thermoplastic sealings, a fore sealed space, and a back insulation part.
- the method comprises attaching, by the fore sealing, the cover glass and the absorber to each other so that there is a distance therebetween, whereupon the cover glass, the absorber, and the fore sealing form the fore space, filling up the fore space with a first low thermal conductive gas.
- the method further comprises attaching, by the back sealing, the insulation part and the absorber to each other so that there is a distance therebetween, whereupon the insulation part, the absorber, and the back sealing form the back space, and filling up the back space with a second low thermal conductive gas.
- FIG. 1 a represents a cross-section of a solar thermal absorber element
- FIG. 1 b represents a cross-section of a solar thermal collector.
- FIG. 1 a represents a cross-section of solar thermal absorber element (module) 100 .
- the element 100 comprises a cover glass 110 and a direct-flow absorber 120 .
- the glass 110 covers the absorber 120 for mechanical damages, insects, and dust.
- the glass 110 may be e.g. a highly transparent antireflective safety glass that allows solar radiation to pass to the absorber 120 and reduces heat losses from the absorber 120 .
- the absorber 120 is configured to absorb the solar radiation.
- the absorber 120 comprises at least one heat transport tube 126 that forms a continuous heat transport channel, which has an inlet 127 a and an outlet 127 b.
- the channel is configured to circulate a heat transport fluid, e.g. water, air, or anti-freeze, inside the absorber 120 .
- the inlet 127 a and the outlet 127 b are possible to connect to external devices, e.g. a tubing of a solar thermal collector 190 or its adapter means.
- the absorber 120 which has a rigid structure, keeps a first distance h 1 between the glass 110 and the absorber 120 constant—i.e. prevents the absorber 120 to bend towards the glass 110 —in order to minimize thermal losses.
- the thermal losses are minimized when the distance h 1 is 10 mm. If the absorber 120 bends towards the glass 110 so that the distance h 1 is less than 10 mm, the thermal losses increase dramatically.
- the absorber 120 may be a roll-bond absorber that is formed from e.g. two aluminium plates by a roll-bond technology.
- a pattern and size of the tube(s) 126 are printed on an inner surface of one plate by a special silk screen and ink.
- the plates are bonded together by a rolling process, whereupon the printed pattern remains between inner surfaces of the bonded plates.
- the tube(s) 126 is formed between the plates by inflating compressed air through the printed pattern.
- the absorber 120 may be a direct-flow absorber that is formed from e.g. two steel, stainless steel, or copper plates.
- the tube(s) 126 is formed similarly as in the roll-bond absorber 120 except the bonding that is provided by welding the plates together.
- a design of tube(s) 126 may be e.g. a single twisting tube 126 and/or a multi-branched tube 126 , which is configured to decrease a flow resistant of the heat transport fluid.
- the absorber 120 may comprise a coating 150 , which is configured to absorb light.
- the coating 150 may be on a fore surface 122 of the absorber 120 , wherein it faces the glass 110 .
- the coating 150 may be deposited in vacuum on the entire and complete absorber 120 at once by a physical vapour deposition (PVD) process and/or a plasma-enhanced chemical vapour deposition (PECVD) process.
- PVD physical vapour deposition
- PECVD plasma-enhanced chemical vapour deposition
- the coating 150 may be a highly selective vacuum multilayer coating that comprises e.g. three deposited layers 152 , 154 , 156 .
- a first layer 152 on the fore surface 122 is configured to absorb light and to prevent a diffusion of elements from an absorber material that decreases a performance of the absorber 120 .
- a composition of the layer 152 may comprise titanium, aluminium, nitrogen, and one of following elements: silicon, yttrium, cerium, and chromium.
- the composition may be e.g. (Ti x Al y Si z )N a .
- at least one of Y, Ce, and Cr may be used additionally or instead of Si.
- Indices x, y, z, a, and b indicate a stoichiometric or non-stoichiometric composition of the layers 152 , 154 , 156 .
- Values of the layer 152 for x, y, z, and a may be e.g. 0.4; 0.5; 0.1; and 1.0 respectively. Typically, the values are 0.3-0.5; 0.3-0.6; 0.03-0.2; and 0.9-1.1 respectively.
- the layer 152 may have a layer thickness between e.g. 10-600 nm.
- a second intermediate layer 154 on the layer 152 is configured to absorb light and to increase an interference at selected wavelengths.
- a composition of the layer 154 may comprise Ti, Al, N, oxygen, and one of following elements: Si, Y, Ce, and Cr.
- the composition may be e.g. (Ti x Al y Si z )N a O b .
- at least one of Y, Ce, and Cr may be used additionally or instead of Si.
- Values of the layer 154 for x, y, z, a, and b may be e.g. 0.4; 0.5; 0.1; 0.8; and 0.3 respectively. Typically, the values are 0.3-0.5; 0.3-0.6; 0.03-0.2; 0.2-0.8; and 0.2-0.8 respectively.
- the layer 154 may have a layer thickness between e.g. 10-150 nm.
- a third top layer 156 on the layer 154 is configured to serve as an antireflection layer and to isolate the coating 150 from a surrounding gas 136 .
- a composition of the layer 156 may comprise Ti, Al, Si, N, and O.
- the composition may be e.g. (Ti x Al y Si z )N a O b .
- values of the layer 156 for x, y, z, a, and b may be e.g. 0-0.2; 0-0.2; 0-1; 0-2; and 0-2 respectively.
- the layer 156 may have a layer thickness between e.g. 50-250 nm.
- the coating 150 may be a selective absorber coating, e.g. a so-called MEMO multilayer coating, wherein the layer 152 is a TiAlSiN layer, the layer 154 is a TiAl—SiON layer, and the layer 156 is a SiO 2 layer.
- a selective absorber coating e.g. a so-called MEMO multilayer coating, wherein the layer 152 is a TiAlSiN layer, the layer 154 is a TiAl—SiON layer, and the layer 156 is a SiO 2 layer.
- the element 100 comprises a fore thermoplastic spacer (TPS) sealing 130 that attaches the glass 110 and the absorber 120 to each other so that there is a certain distance h 1 , e.g. 10, 15, or 20 mm, between the glass 110 and the absorber 120 .
- TPS thermoplastic spacer
- the attachment is made by a TPS technology in an automatic production line.
- the sealing 130 is injected on the glass 110 for achieving a desired sealing thickness and the distance h 1 .
- the glass 110 with the sealing 130 and the absorber 120 are pressed together so that a fore sealed space 134 is formed by the glass 110 , the absorber 120 , and the sealing 130 that surround the space 134 .
- the sealing 130 is a gas tight sealing that seals the space 134 hermetically.
- the sealing 130 may be a high temperature sealing material, e.g. a butyl sealing.
- a low thermal conductive gas 136 e.g. an argon gas, is injected into the space 134 so that it is filled up with the gas 136 .
- the glass 110 , the absorber 120 , and the sealing 130 keep the gas 136 in the space 134 and prevent the gas 136 to flow outside the element 100 .
- the gas 136 reduces thermal losses by convection.
- the element 100 comprises a fore secondary sealing 140 , which is attached to the sealing 130 , and between the glass 110 and the absorber 120 .
- the sealing 140 protects the sealing 130 and carries a weight of the absorber 120 .
- the sealing 140 may be e.g. a silicon sealing.
- the element 100 comprises a back insulation part 160 that covers the absorber 120 for mechanical damages and supports a heat insulation of the element 100 by reducing heat losses from the absorber 120 .
- the insulation part 160 covers the absorber 120 for mechanical damages, insects, and dust.
- the insulation part 160 may be e.g. a glass, a polyurethane (PUR) board, or a polyisocyanurate (PIR) board, whereupon it is a corrosion free.
- PUR polyurethane
- PIR polyisocyanurate
- the element 100 comprises a back TPS sealing 170 that attaches the insulation part 160 and the absorber 120 to each other so that there is a second distance h 2 , e.g. 10, 15, or 20 mm, therebetween.
- the attachment is made correspondingly in the automatic production line as the attachment of the glass 110 and the absorber 120 so that a back sealed space 174 is formed by the insulation part 160 , the absorber 120 , and the sealing 170 that surround the space 174 .
- the attachments of the glass 110 and the insulation part 160 may be made at the same time or successive production steps.
- the sealing 170 is a gas tight sealing that seals the space 174 hermetically and it may be e.g. a butyl sealing.
- the space 174 is filled up with a second low thermal conductive gas 176 , e.g. an argon gas, correspondingly as the space 134 .
- a second low thermal conductive gas 176 e.g. an argon gas
- the additions of the gases 136 , 176 may be made at the same time or successive production steps in accordance with the TPS technology.
- the insulation part 160 , the absorber 120 , and the sealing 170 keep the gas 176 in the space 174 and prevent the gas 136 to flow outside the element 100 .
- the gas 176 reduces thermal losses by convection.
- the element 100 comprises a back secondary sealing 180 , which is attached to the sealing 170 , and between the insulation part 160 and the absorber 120 .
- the sealing 180 which may be e.g. a silicon sealing, protects the sealing 170 and carries a weight of the absorber.
- the formations of the sealings 140 , 180 may be made at the same time or successive production steps in accordance with the TPS technology.
- the hermetically sealed space 134 preserves an efficiency of the absorber 120 , when it prevents dust or insects to let in it, whereupon there is no efficiency change during a lifetime of the absorber 120 because of the dust or insects.
- hermetically sealed space 134 prevents a water condensation on the glass 110 , whereupon the element 100 can start to produce energy earlier on a morning.
- FIG. 1 b represents a cross-section of a solar thermal collector 190 that comprises the element 100 represented in FIG. 1 a.
- the collector 190 is a flat-plate collector for e.g. high temperatures that may be used e.g. in solar cooling applications.
- the collector 190 may comprise a collector frame 192 that cover the collector 190 for mechanical damages, insects, and dust.
- the frame 192 may be made of e.g. an aluminium, composite plastic, or wood.
- the frame 192 comprising at least one support (insulation) element 194 on its inner surface.
- the support element(s) 194 supports the element 100 , when the element 100 is mounted into the frame 190 .
- the support element(s) 194 thermally insulates the element 100 and minimize environmental effects.
- the support element(s) 194 may be e.g. mineral or wood fiber wool.
- the element 100 is attached to the frame 192 by gluing edges of the glass 110 and the insulation part 160 with a high temperature and UV resistant glue 190 , which prevents water to penetrate inside the collector 190 , and spacer tapes.
- the element 100 enables to use cheaper materials for the support element(s) 194 , because there is no condensation of any evaporated components from the support element(s) 194 .
- the collector 190 may be without the frame 192 and the support element(s) 194 , whereupon its cross-section is in accordance with FIG. 1 a.
- the collector 190 may comprise adapter means and tubing means so that the the tube(s) 126 of the element 100 is possible to connect to the collector 190 by the inlet 127 a, the outlet 127 b, the adapter means, and the tubing means.
- the element 100 enables to build very effective modular large area collectors for process and district heating systems by connecting several collectors 190 .
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Thermal Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Securing Of Glass Panes Or The Like (AREA)
- Joining Of Glass To Other Materials (AREA)
- Photovoltaic Devices (AREA)
Abstract
Description
- The application relates generally to a solar thermal absorber element.
- Sand, salt, and insects, which have invaded inside a structure of solar thermal collectors along flowing air, cause damages decreasing a lifetime and an efficiency of the collectors.
- In order to eliminate these damages, it has been developed a thermoplastic spacer (TPS) sealed absorber module, wherein a cover glass is sealed with an absorber by a TPS.
- The TPS sealed module protects the absorber by preventing undesirable sand, salt, and insects to invade inside the absorber element.
- However, manufacturing costs of collectors, even if absorber modules would be TPS sealed modules, have been high, because manufacturing steps in series production comprise lots of manual work when an insulation is added and modules are mounted manually into a collector frame.
- One object of the invention is to withdraw the above-mentioned drawback and provide a solar thermal absorber element, which comprises a TPS sealed back insulation that enables to manufacture elements in mass production by existing automatic production lines that are used for manufacturing of a TPS insulation glass.
- One object of the invention is fulfilled by providing a solar thermal absorber element of claim 1, a solar thermal collector of claim 6, and a method of claim 7.
- One embodiment of the invention is a solar thermal absorber element that comprises a cover glass, a direct-flow absorber, a fore thermoplastic sealing for attaching the cover glass and the absorber to each other so that there is a distance therebetween, and a fore sealed space, which is formed by the cover glass, the absorber, and the fore sealing. The fore space is filled up with a first low thermal conductive gas. The element further comprises a back insulation part, a back thermoplastic sealing for attaching the insulation part and the absorber to each other so that there is a distance therebetween, and a back sealed space, which is formed by the insulation part, the absorber, and the back sealing. The back space is filled up with a second low thermal conductive gas.
- The direct-flow absorber refers to an absorber, wherein heat transport fluid, e.g. water, air, or antifreeze, circulates inside a structure of the absorber.
- The thermoplastic sealing refers to a sealing (spacer), which is made by a thermoplastic spacer (TPS) technology.
- The low thermal conductive gas refers to a gas, which has a low thermal conductivity, e.g. noble gases. The noble gas can be e.g. argon, krypton, or xenon.
- The roll-bond absorber refers to an absorber, which comprises at least one tube and which is provided by a roll-bond technology.
- The highly selective vacuum coating refers to e.g. a coating, which is deposited in vacuum and which forms a selective absorber coating with a solar absorbance more than 96% with low thermal emission by radiation in the infrared.
- One embodiment of the invention is a solar thermal collector that comprises an absorber element. The element comprises a cover glass, a direct-flow absorber, a fore thermoplastic sealing for attaching the cover glass and the absorber to each other so that there is a distance therebetween, and a fore sealed space, which is formed by the cover glass, the absorber, and the fore sealing. The fore space is filled up with a first low thermal conductive gas. The element further comprises a back insulation part, a back thermoplastic sealing for attaching the insulation part and the absorber to each other so that there is a distance therebetween, and a back sealed space, which is formed by the insulation part, the absorber, and the back sealing. The back space is filled up with a second low thermal conductive gas.
- One embodiment of the invention is a method for manufacturing a solar thermal absorber element. The element comprises a cover glass, a direct-flow absorber, a fore and back thermoplastic sealings, a fore sealed space, and a back insulation part. The method comprises attaching, by the fore sealing, the cover glass and the absorber to each other so that there is a distance therebetween, whereupon the cover glass, the absorber, and the fore sealing form the fore space, filling up the fore space with a first low thermal conductive gas. The method further comprises attaching, by the back sealing, the insulation part and the absorber to each other so that there is a distance therebetween, whereupon the insulation part, the absorber, and the back sealing form the back space, and filling up the back space with a second low thermal conductive gas.
- Further embodiments of the invention are defined in dependent claims.
- The features recited in depending claims are mutually freely combinable unless otherwise explicitly stated.
- The below definitions of verbs and terms shall be applied, unless a different definition is given in the claims or elsewhere in this description.
- The verb “to comprise” is used in this document as an open limitation that neither excludes nor requires the existence of also unrecited features. The verbs “to include” and “to have/has” are defined as to comprise.
- The terms “a”, “an”, and “at least one”, as used herein, are defined as one or more than one and the term “plurality” is defined as two or more than two.
- The term “another”, as used herein, is defined as at least a second or more.
- The term “or” is generally employed in its sense comprising “and/or” unless the content clearly dictates otherwise.
- The embodiments of the invention will be described with reference to the accompanying figures, in which
-
FIG. 1a represents a cross-section of a solar thermal absorber element and -
FIG. 1b represents a cross-section of a solar thermal collector. -
FIG. 1a represents a cross-section of solar thermal absorber element (module) 100. - The
element 100 comprises acover glass 110 and a direct-flow absorber 120. - The
glass 110 covers the absorber 120 for mechanical damages, insects, and dust. - The
glass 110 may be e.g. a highly transparent antireflective safety glass that allows solar radiation to pass to the absorber 120 and reduces heat losses from theabsorber 120. - The
absorber 120 is configured to absorb the solar radiation. - The
absorber 120 comprises at least oneheat transport tube 126 that forms a continuous heat transport channel, which has aninlet 127 a and anoutlet 127 b. The channel is configured to circulate a heat transport fluid, e.g. water, air, or anti-freeze, inside theabsorber 120. - The
inlet 127 a and theoutlet 127 b are possible to connect to external devices, e.g. a tubing of a solarthermal collector 190 or its adapter means. - The
absorber 120, which has a rigid structure, keeps a first distance h1 between theglass 110 and the absorber 120 constant—i.e. prevents theabsorber 120 to bend towards theglass 110—in order to minimize thermal losses. The thermal losses are minimized when the distance h1 is 10 mm. If the absorber 120 bends towards theglass 110 so that the distance h1 is less than 10 mm, the thermal losses increase dramatically. - The
absorber 120 may be a roll-bond absorber that is formed from e.g. two aluminium plates by a roll-bond technology. - A pattern and size of the tube(s) 126 are printed on an inner surface of one plate by a special silk screen and ink. The plates are bonded together by a rolling process, whereupon the printed pattern remains between inner surfaces of the bonded plates. The tube(s) 126 is formed between the plates by inflating compressed air through the printed pattern.
- Alternatively, the
absorber 120 may be a direct-flow absorber that is formed from e.g. two steel, stainless steel, or copper plates. - The tube(s) 126 is formed similarly as in the roll-bond absorber 120 except the bonding that is provided by welding the plates together.
- A design of tube(s) 126 may be e.g. a
single twisting tube 126 and/or amulti-branched tube 126, which is configured to decrease a flow resistant of the heat transport fluid. - In addition, the
absorber 120 may comprise acoating 150, which is configured to absorb light. - The
coating 150 may be on afore surface 122 of theabsorber 120, wherein it faces theglass 110. - The
coating 150 may be deposited in vacuum on the entire andcomplete absorber 120 at once by a physical vapour deposition (PVD) process and/or a plasma-enhanced chemical vapour deposition (PECVD) process. - The
coating 150 may be a highly selective vacuum multilayer coating that comprises e.g. three deposited 152, 154, 156.layers - A
first layer 152 on thefore surface 122 is configured to absorb light and to prevent a diffusion of elements from an absorber material that decreases a performance of theabsorber 120. - A composition of the
layer 152 may comprise titanium, aluminium, nitrogen, and one of following elements: silicon, yttrium, cerium, and chromium. - The composition may be e.g. (TixAlySiz)Na. Alternatively, at least one of Y, Ce, and Cr may be used additionally or instead of Si.
- Indices x, y, z, a, and b, indicate a stoichiometric or non-stoichiometric composition of the
152, 154, 156.layers - Values of the
layer 152 for x, y, z, and a may be e.g. 0.4; 0.5; 0.1; and 1.0 respectively. Typically, the values are 0.3-0.5; 0.3-0.6; 0.03-0.2; and 0.9-1.1 respectively. - The
layer 152 may have a layer thickness between e.g. 10-600 nm. - A second
intermediate layer 154 on thelayer 152 is configured to absorb light and to increase an interference at selected wavelengths. - A composition of the
layer 154 may comprise Ti, Al, N, oxygen, and one of following elements: Si, Y, Ce, and Cr. - The composition may be e.g. (TixAlySiz)NaOb. Alternatively, at least one of Y, Ce, and Cr may be used additionally or instead of Si.
- Values of the
layer 154 for x, y, z, a, and b may be e.g. 0.4; 0.5; 0.1; 0.8; and 0.3 respectively. Typically, the values are 0.3-0.5; 0.3-0.6; 0.03-0.2; 0.2-0.8; and 0.2-0.8 respectively. - The
layer 154 may have a layer thickness between e.g. 10-150 nm. - A third
top layer 156 on thelayer 154 is configured to serve as an antireflection layer and to isolate thecoating 150 from a surroundinggas 136. - A composition of the
layer 156 may comprise Ti, Al, Si, N, and O. - The composition may be e.g. (TixAlySiz)NaOb.
- Typically, values of the
layer 156 for x, y, z, a, and b may be e.g. 0-0.2; 0-0.2; 0-1; 0-2; and 0-2 respectively. - The
layer 156 may have a layer thickness between e.g. 50-250 nm. - The
coating 150 may be a selective absorber coating, e.g. a so-called MEMO multilayer coating, wherein thelayer 152 is a TiAlSiN layer, thelayer 154 is a TiAl—SiON layer, and thelayer 156 is a SiO2 layer. - In addition, the
element 100 comprises a fore thermoplastic spacer (TPS) sealing 130 that attaches theglass 110 and theabsorber 120 to each other so that there is a certain distance h1, e.g. 10, 15, or 20 mm, between theglass 110 and theabsorber 120. - The attachment is made by a TPS technology in an automatic production line. The sealing 130 is injected on the
glass 110 for achieving a desired sealing thickness and the distance h1. Theglass 110 with the sealing 130 and theabsorber 120 are pressed together so that a fore sealedspace 134 is formed by theglass 110, theabsorber 120, and the sealing 130 that surround thespace 134. - The sealing 130 is a gas tight sealing that seals the
space 134 hermetically. - The sealing 130 may be a high temperature sealing material, e.g. a butyl sealing.
- While the
glass 110 and theabsorber 120 are pressed together, a low thermalconductive gas 136, e.g. an argon gas, is injected into thespace 134 so that it is filled up with thegas 136. - The
glass 110, theabsorber 120, and the sealing 130 keep thegas 136 in thespace 134 and prevent thegas 136 to flow outside theelement 100. - The
gas 136 reduces thermal losses by convection. - In addition, the
element 100 comprises a fore secondary sealing 140, which is attached to the sealing 130, and between theglass 110 and theabsorber 120. - The sealing 140 protects the sealing 130 and carries a weight of the
absorber 120. - The sealing 140 may be e.g. a silicon sealing.
- In addition, the
element 100 comprises aback insulation part 160 that covers theabsorber 120 for mechanical damages and supports a heat insulation of theelement 100 by reducing heat losses from theabsorber 120. - In addition, the
insulation part 160 covers theabsorber 120 for mechanical damages, insects, and dust. - The
insulation part 160 may be e.g. a glass, a polyurethane (PUR) board, or a polyisocyanurate (PIR) board, whereupon it is a corrosion free. - In addition, the
element 100 comprises a back TPS sealing 170 that attaches theinsulation part 160 and theabsorber 120 to each other so that there is a second distance h2, e.g. 10, 15, or 20 mm, therebetween. - The attachment is made correspondingly in the automatic production line as the attachment of the
glass 110 and theabsorber 120 so that a back sealedspace 174 is formed by theinsulation part 160, theabsorber 120, and the sealing 170 that surround thespace 174. - The attachments of the
glass 110 and theinsulation part 160 may be made at the same time or successive production steps. - The sealing 170 is a gas tight sealing that seals the
space 174 hermetically and it may be e.g. a butyl sealing. - The
space 174 is filled up with a second low thermalconductive gas 176, e.g. an argon gas, correspondingly as thespace 134. - The additions of the
136, 176 may be made at the same time or successive production steps in accordance with the TPS technology.gases - The
insulation part 160, theabsorber 120, and the sealing 170 keep thegas 176 in thespace 174 and prevent thegas 136 to flow outside theelement 100. - The
gas 176 reduces thermal losses by convection. - In addition, the
element 100 comprises a backsecondary sealing 180, which is attached to the sealing 170, and between theinsulation part 160 and theabsorber 120. - The sealing 180, which may be e.g. a silicon sealing, protects the sealing 170 and carries a weight of the absorber.
- The formations of the
140, 180 may be made at the same time or successive production steps in accordance with the TPS technology.sealings - The hermetically sealed
space 134 preserves an efficiency of theabsorber 120, when it prevents dust or insects to let in it, whereupon there is no efficiency change during a lifetime of theabsorber 120 because of the dust or insects. - In addition, the hermetically sealed
space 134 prevents a water condensation on theglass 110, whereupon theelement 100 can start to produce energy earlier on a morning. -
FIG. 1b represents a cross-section of a solarthermal collector 190 that comprises theelement 100 represented inFIG. 1 a. - The
collector 190 is a flat-plate collector for e.g. high temperatures that may be used e.g. in solar cooling applications. - In addition, the
collector 190 may comprise acollector frame 192 that cover thecollector 190 for mechanical damages, insects, and dust. - The
frame 192 may be made of e.g. an aluminium, composite plastic, or wood. - The
frame 192 comprising at least one support (insulation)element 194 on its inner surface. - The support element(s) 194 supports the
element 100, when theelement 100 is mounted into theframe 190. - In addition, the support element(s) 194 thermally insulates the
element 100 and minimize environmental effects. - The support element(s) 194 may be e.g. mineral or wood fiber wool.
- The
element 100 is attached to theframe 192 by gluing edges of theglass 110 and theinsulation part 160 with a high temperature and UVresistant glue 190, which prevents water to penetrate inside thecollector 190, and spacer tapes. - The
element 100 enables to use cheaper materials for the support element(s) 194, because there is no condensation of any evaporated components from the support element(s) 194. - Alternatively, the
collector 190 may be without theframe 192 and the support element(s) 194, whereupon its cross-section is in accordance withFIG. 1 a. - In addition, the
collector 190 may comprise adapter means and tubing means so that the the tube(s) 126 of theelement 100 is possible to connect to thecollector 190 by theinlet 127 a, theoutlet 127 b, the adapter means, and the tubing means. - In addition, the
element 100 enables to build very effective modular large area collectors for process and district heating systems by connectingseveral collectors 190. - The invention has been now explained above with reference to the aforesaid embodiments and the several advantages of the invention have been demonstrated.
- It is clear that the invention is not only restricted to these embodiments, but comprises all possible embodiments within the scope of the invention thought and the following claims.
Claims (7)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FI20155432A FI20155432A (en) | 2015-06-08 | 2015-06-08 | Aurinkolämpökeräinelementti |
| FI20155432 | 2015-06-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20160356527A1 true US20160356527A1 (en) | 2016-12-08 |
Family
ID=56101322
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15/174,388 Abandoned US20160356527A1 (en) | 2015-06-08 | 2016-06-06 | Solar thermal absorber element |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20160356527A1 (en) |
| EP (2) | EP3104098A1 (en) |
| JP (1) | JP2017003259A (en) |
| CN (2) | CN114857785A (en) |
| FI (1) | FI20155432A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4153753A (en) * | 1976-08-20 | 1979-05-08 | Trevor P. Woodman | Spectrally selective surfaces and method of fabricating the same |
| US4185616A (en) * | 1976-08-03 | 1980-01-29 | Johnson Steven A | Solar energy absorber apparatus and method |
| US20100206303A1 (en) * | 2009-02-19 | 2010-08-19 | John Danhakl | Solar Concentrator Truss Assemblies |
| US20110265785A1 (en) * | 2009-01-18 | 2011-11-03 | Shimon Klier | Solar thermal collecting system |
| US20120234313A1 (en) * | 2011-03-18 | 2012-09-20 | ZYRUS Beteiligungsgesellschaft mbH & Co., Patente I KG | Solar collector and method for manufacturing such a solar collector |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2721964A1 (en) * | 1977-05-14 | 1978-11-23 | Platz | Solar energy collector with spaced cover, absorber and insulator - in airtight housing with relative movement accommodating spacers |
| DE7818687U1 (en) * | 1978-06-22 | 1978-09-28 | Brown, Boveri & Cie Ag, 6800 Mannheim | SOLAR COLLECTOR WITH A FLAT HOUSING |
| CA1331851C (en) * | 1987-12-14 | 1994-09-06 | Gerhard Reichert | Insulating multiple layer sealed units and insulating spacers therefor |
| DE4217060A1 (en) * | 1992-05-22 | 1993-11-25 | Interpane Entw & Beratungsges | Solar energy collector - has circulating fluid in pipe embedded in absorber plate contained hermetically between transparent faceplate and backplate |
| US6673997B2 (en) * | 1999-10-22 | 2004-01-06 | Saint-Gobain Glass France | Solar module with border sealing |
| CN100343413C (en) * | 2002-12-30 | 2007-10-17 | 北京欧科能太阳能技术有限公司 | Solar selective absorption coating and preparation method thereof |
| GB2429517B (en) * | 2005-07-15 | 2010-10-06 | Viridian Concepts Ltd | Solar collector devices |
| DE102006007472B4 (en) * | 2006-02-17 | 2018-03-22 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Photovoltaic concentrator module with multifunctional frame |
| US9115272B2 (en) * | 2007-09-20 | 2015-08-25 | Adco Products Llc | Edge sealants having balanced properties |
| DE102008064010A1 (en) * | 2008-12-19 | 2010-07-01 | Wirgastkeller Gastronomie Gmbh | Thermal solar collector for e.g. use in facade element in insulating glass compound, has gaseous or liquid heat transfer medium comprising thin films or sheets, which deform under pressure of fluid |
| FR2951811B1 (en) * | 2009-10-22 | 2012-09-28 | Saint Gobain | SOLAR COLLECTOR |
| DE102010047292B4 (en) * | 2010-09-27 | 2014-01-02 | Frado Immobilien Und Beteiligungsgbr (Vertretungsberechtigter Gesellschafter: Elmar Dohmann, 34466 Wolfhagen) | Solar collector assembly |
| EP2678617B1 (en) * | 2011-02-22 | 2019-06-12 | Savo-Solar OY | Method for manufacturing thermal absorber for solar thermal collector |
| JP5912279B2 (en) * | 2011-04-13 | 2016-04-27 | 矢崎エナジーシステム株式会社 | Solar collector |
| IL212303A (en) * | 2011-04-13 | 2013-09-30 | Magen Eco Energy A C S Ltd | Solar collector |
-
2015
- 2015-06-08 FI FI20155432A patent/FI20155432A/en not_active Application Discontinuation
-
2016
- 2016-05-24 CN CN202210611930.5A patent/CN114857785A/en active Pending
- 2016-05-24 CN CN201610349618.8A patent/CN106247644A/en active Pending
- 2016-06-02 EP EP16172584.1A patent/EP3104098A1/en not_active Ceased
- 2016-06-02 EP EP21163380.5A patent/EP3859229A1/en active Pending
- 2016-06-06 US US15/174,388 patent/US20160356527A1/en not_active Abandoned
- 2016-06-08 JP JP2016114272A patent/JP2017003259A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4185616A (en) * | 1976-08-03 | 1980-01-29 | Johnson Steven A | Solar energy absorber apparatus and method |
| US4153753A (en) * | 1976-08-20 | 1979-05-08 | Trevor P. Woodman | Spectrally selective surfaces and method of fabricating the same |
| US20110265785A1 (en) * | 2009-01-18 | 2011-11-03 | Shimon Klier | Solar thermal collecting system |
| US20100206303A1 (en) * | 2009-02-19 | 2010-08-19 | John Danhakl | Solar Concentrator Truss Assemblies |
| US20120234313A1 (en) * | 2011-03-18 | 2012-09-20 | ZYRUS Beteiligungsgesellschaft mbH & Co., Patente I KG | Solar collector and method for manufacturing such a solar collector |
Also Published As
| Publication number | Publication date |
|---|---|
| EP3859229A1 (en) | 2021-08-04 |
| JP2017003259A (en) | 2017-01-05 |
| CN106247644A (en) | 2016-12-21 |
| CN114857785A (en) | 2022-08-05 |
| FI20155432A7 (en) | 2016-12-09 |
| FI20155432A (en) | 2016-12-09 |
| EP3104098A1 (en) | 2016-12-14 |
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