WO1982000510A1 - Solar energy collector having semiconductive coating formed from metal and dielectric - Google Patents
Solar energy collector having semiconductive coating formed from metal and dielectric Download PDFInfo
- Publication number
- WO1982000510A1 WO1982000510A1 PCT/US1980/000987 US8000987W WO8200510A1 WO 1982000510 A1 WO1982000510 A1 WO 1982000510A1 US 8000987 W US8000987 W US 8000987W WO 8200510 A1 WO8200510 A1 WO 8200510A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- coating
- metal
- dielectric material
- solar energy
- energy collector
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/027—Graded interfaces
-
- 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
- F24S10/45—Solar heat collectors using working fluids in absorbing elements surrounded by transparent enclosures, e.g. evacuated solar collectors the enclosure being cylindrical
-
- 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
-
- 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 energy collector having a semiconductive coating formed by the co-deposition of a metal and a dielectric material and having a relatively high solar absorptivity and low infrared emissivity.
- Solar energy is an extensive, constant energy source whose economic feasibility depends on efficient collection, retention, and utilization.
- the efficiency of some solar collecting systems has been low due to excessive heat losses.
- One area in which improvement has been sought is in solar selective absorber coatings, that is, coatings which absorb energy particularly well in the solar spectrum.
- coatings are designed to collect thermal energy from exposure to solar radiation and then transmit the collected energy through other media either to heat or cool homes and buildings through heat exchangers .
- heat exchangers In general, when radiant energy from the sun impinges on a cooler object, part of the energy is reflected and lost and the balance either absorbed or transmitted away. The absorbed energy may be re-radiated at a longer wavelength.
- a coating which absorbs in the range of solar radiation becomes heated, provided the surface does not reradiate or emit most or all of the energy collected.
- Solar radiation reaching the surface of the earth is almost entirely confined to the range of 0.3 to 2.5 microns. It is estimated that about 90% of solar radiation is at wavelengths of about 0.4 micron to about 1.5 microns. The amount of radiation above 2.5 microns is negligible.
- Solar energy selective coatings therefore, are designed to differentiate in their absorption, reflection or transmission characteristics between wavelengths above about 2.5 microns and wavelengths below about 2.5 microns. Thus, solar energy can be collected at wavelengths below about 2.5 microns and the collected energy then transferred to useful application at wavelengths above about 2.5 microns .
- a solar collector should absorb strongly at wavelengths below about 2.5 microns and not radiate at wavelengths greater than 2.5 microns .
- a coating which has a high absorptivity, usually termed alpha, in the solar spectrum but a low emissivity, epsilon, at the temperature at which the collector operates may be called a solar selective coating. Even though a high alpha to epsilon ratio is desirable, it is essential that the alpha value be near one to collect as much of the available energy as possible.
- Solar selective coatings are one important way to increase the efficiency of solar energy collectors, primarily by maximizing the absorption of solar energy and minimizing the energy lost by radiation.
- Metals These are materials in which the highest occupied energy band is only partially filled with electrons. The electrons are highly mobile and the energy gap between the valence band and the conduction band is less than about 0.1 electron volts (eV) . Metals have low emissivities in the infrared.
- Semiconductors These are materials in which the highest energy band is only partially filled at absolute zero.
- the energy gap for semiconductors is of the order of 0.1 eV to about 5 eV.
- Semiconductors are characterized by high solar absorptivity and, especially in thin layers high infrared transmissivity.
- Dielectrics or Insulators These are materials in which the highest occupied energy band is completely filled. Such materials have energy gaps larger than 4 eV.
- the prior art describes a number of solar selective coatings in which a semiconductor is deposited over a substrate. Typical semiconductors are silicon, germanium, copper oxide, and lead sulfide. Unfortunately, semiconductors have high indicies of refraction which provide high reflectivities at an air or vacuum interface. Disclosure of Invention
- An object of the invention is to provide an improved solar energy collector. Another object is to provide a solar element for a collector comprising an improved semiconductive coating. A related object is to provide a semiconductive coating for a solar energy collector that comprises a solid solution of metal atoms dispersed in a matrix of a dielectric material.
- the simultaneous co-deposition of the metal and dielectric material may be carried out by known vapor evaporating techniques under vacuum and results in a semiconductive coating forming a solid solution of atoms of the metal dispersed in a matrix of the dielectric material.
- the semiconductive coating may comprise by weight from about 5% to about 95% of the metal and from about 5% to about 95% of the dielectric material.
- the amounts of the metal and dielectric material are varied relative to each other during the co-deposition.
- the concentration of each can be varied to meet diverse requirements widthwise of the semiconductive coating.
- the amount of metal gradually decreases during the co-deposition and the amount of dielectric material gradually increases to form concentration gradients of the metal and dielectric material in the coating. This results in the greatest concentration of metal being adjacent the substrate and the greatest concentration of dielectric material being adjacent the outer surface of the semiconductive coating remote from the substrate.
- Figure 1 is a fragmentary, highly magnified, cross-section of a solar energy collector of the present invention
- Figure 2 is a diagrammatic representation of the collector of Figure 1 and illustrates the reverse concentration gradients of the metal and dielectric material in the semiconductive coating
- Figure 3 is a side elevational view, partly in section, of a tubular solar energy collector having a solar absorptive coating of the present invention.
- Figure 4 is a graph of comparative spectral reflectance curves of three solar absorptive coatings , including two of the present invention and one of the prior art, and shows the decreased reflectance obtained by the present semiconductive coatings in the visible solar spectrum.
- the present invention relates to a solar selective or absorptive semiconductor coating for a solar energy collector in which the coating has an improved absorptivity while avoiding the introduction of any deleterious property.
- Semiconductor coatings of the present invention may have an absorptivity of at least 0.85 to as high as 0.96. The higher value is intended to be exemplary only and not limiting of the present invention.
- the semiconductive coating is formed by the co deposition of a metal and a dielectric material onto a metal or metallized substrate.
- the codeposition takes place in proportions rendering the coating semiconductive and forming a solid solution of atoms of the metal dispersed in a matrix of the dielectric material.
- an outer portion of the semiconductive coating that is, a portion remote from the substrate, contains more of the dielectric material than the metal; while an inner portion of the semiconductive coating adjacent the substrate contains more of the metal than the dielectric material.
- the semiconductive coating contains the metal and dielectric material in reverse gradients. More particularly, the concentration of the metal in the semiconductive coating gradually increases in a direction from an outer surface thereof toward the substrate; and the concentration of the dielectric material in the semiconductive coating gradually increases in a direction from the substrate toward the outer surface of the semi conductive coating.
- the present semiconductive coating comprises a material which, in the preferred form of the invention, has a graded energy gap extending from a relatively high electron volt value adjacent the outer surface of the coating to a relatively low electron volt value adjacent the substrate on which the semiconductive coating lies.
- energy gap refers to the energy difference between the electron bands which concentrically surround the nucleus of an atom.
- Metals have relatively low or small energy gaps since their highest energy bands are only partially filled. Electrons are loosely held by these bands and are easily transported. Dielectric materials have relatively high energy gaps since their highest energy bands are completely filled. Accordingly, as one approaches a relatively high energy gap, the electrons of the outer bands become less free to move about and therefore materials comprising such atoms become more and more like an insulator.
- a semiconductive coating has an energy gap from about 0.5 eV to about 1.24 eV.
- Metals useful in the present invention are those having a relatively low emissivity and include aluminum, silver, copper, gold, chromium, nickel, molybdenum, tungsten, stainless steel, alloys thereof, and the like. Aluminum, copper, silver, and chromium are preferred for the metal.
- Preferred dielectric materials include magnesium fluoride, aluminia, calcium fluoride, magnesia, and silica. While specific examples of metals and dielectric materials are given, the number of combinations is limited only by the periodic table, the vapor pressures of the materials, and deposition techniques available.
- the metal and dielectric materials are jointly applied to a substrate by standard, known, vacuum evaporation techniques, such as electric resistance heating, election beam, sputtering, and the like, followed by condensation on a substrate to produce a synthesized, semiconductive coating.
- standard, known, vacuum evaporation techniques such as electric resistance heating, election beam, sputtering, and the like
- condensation on a substrate to produce a synthesized, semiconductive coating.
- small reservoirs of each material may be heated in vacuum by electric resistant circuits to evaporate the material and deposit it on an adjacent substrate.
- the co-deposition of the two materials can vary in any ratio and/or time-space program desired, although it is preferred to deposit them in reverse gradients, as previously described, so that the resulting semiconductive coating has properties approaching those of a metal at its lower surface adjacent the substrate and properties approaching those of an insulator at an upper surface remote from the substrate.
- the resulting semiconductive coating has a relatively high absorptivity in the solar spectrum and a relatively low emissivity at normal operating temperatures of a solar collector.
- Deposition of the metal and dielectric material can occur either randomly or in a precise constant or varying ratio.
- the metal is diluted with the dielectric material so that the resulting coating is a solid solution of metal atoms commingled or dispersed in a matrix of the dielectric material.
- the resulting semiconductive coating has the optical properties of a semiconductor, that is, relatively high solar absorptance and relatively high infrared transmittance. But in addition, the present semiconductive coating therefore possesses the reflective properties of a dielectric.
- the semiconductive coating may comprise from about 5% to about 95% of the metal and from 5% to about 95% of the dielectric material by weight.
- the substrate can be composed entirely of one of the indicated metals.
- the substrate can comprise a non-metallic substrate that is conventionally covered or metallized by one of such metals.
- Other non-metallic substrates that may be used include porcelain, refractory materials, organic polymeric materials, and the like.
- Figure 1 illustrates a collector system that can contain the present solar selective semiconductive coating.
- Figure 1 semi-schematically shows a panel that is part of a flat plate.
- a non-metallic substrate 10 which can be glass, plastic, ceramic, and the like has a metallized film 11. If the substrate is composed entirely of metal, it effectively replaces strata 10 and 11.
- ' dielectric material in accordance with the present invention is generally represented at 12 and overlies the metallized substrate.
- the relative thicknesses of the layers of coatings have no significance in any of the figures and are for purposes of illustration only.
- Figure 2 diagramatically illustrates reverse concentration gradients of the metal and dielectric material which are present in a preferred embodiment of the invention.
- the non-metallic substrate 10 As a model, there are shown in Figure 2 the non-metallic substrate 10, its metallized film 11, and semiconductor coating 12.
- the content of coating 12 is graphically indicated by the crossing lines 13 and 14 in which line 13 represents the content of the metal and line 14 represents the content of a dielectric material.
- This embodiment includes a collector generally represented at 15 comprising concentric, transparent glass tubes.
- An outer or cover tube 16 is circumferentially transparent, open at the right hand end, as viewed in Figure 3, and closed at the opposite end when tipping off the tubulation as at 17.
- the open end of cover tube 16 is sealed to an inner glass absorber tube 18 by a glass-to-glass hermetic seal at 19. The sealed space between the tubes
- Absorber tube 18 is preferably made of glass and has a less outside diameter and slightly greater length than the inside diameter and length, respectively, of cover tube 16. Tube 18 is closed at end 18a and opened at opposite end 18b. Prior to assembly, the exterior peripheral glass surface of absorber tube 18 is coated with the energy absorbing, solar selective layer of the present invention which is illustrated in Figure 2 by the shaded area 20.
- a central feeder tube 21 of smaller diameter than tube 18 may be inserted into open end 18b of the absorber tube to extend longitudinally of concentric tubes 16 and 18 to a point near the closed end 18a of absorber tube 18. End 18a nests within a coiled spring 22 which resiliently retains that end of tube 18 in place.
- the operation of the present semiconductive coating is the same as for other corresponding semiconductive coatings in known solar energy collectors.
- the semiconductive coating absorbs energy directly from solar radiation.
- the semconductive coating also has higher absorptivity and lower reflectance than prior semiconductor coatings and therefore helps retain the absorbed energy and reduce radiation losses as well.
- a glass substrate was used measuring 50.8mm by 50.8mm by 3.17mm and comprising a borosilicate glass.
- Each substrate has been previously metallized with aluminum in a standard manner to a film thickness of about 1,000 angstroms.
- Each substrate in its turn was placed in a bell jar along with a tungsten boat in the case of Examples 1, 2 and 4.
- the boat containing the metal is in powder or pellet form and was adapted for heating by electric resistance circuitry.
- a coil filament of tungsten metal was used and chromium evaporated from it by resistance heating.
- a hearth carrying a supply of magnesium fluoride was included within the bell jar for each run.
- the bell jar was evacuated to 2 x 10 -5 Torr and evaporation of the metal then begun.
- co-deposition with magnesium fluoride was begun by subjecting the magnesium fluoride on the hearth to an electron beam gun (EB) .
- EB electron beam gun
- the deposition of the metal was slowly phased out, and the deposition of the magnesium fluoride was maintained at least at a constant value and optionally could be slowly increased after which its deposition was also terminated.
- the total elapsed time of the deposition for each example was about three minutes.
- the total coating thickness of the resulting semiconductive coating including both the metal and the magnesium fluoride was about 2,000 angstroms. Table C summarizes the results of these examples in which Example 2 provided an absorptivity of 0.961.
- Figure 4 compares the reflectance spectra of the semiconductive coatings of Examples 2 and 3 with a prior semiconductive coating comprising black chrome, CrOx, over an aluminized substrate.
- Figure 4 includes reflectance spectra from a wavelength of about 350 nanometers to about 2500 nanometers. Of this range a wavelength of about 350 nanometers to about 700 nanometers represents the visible.
- a substrate of borosilicate glass measuring
- 50.8mm by 50.8mm by 3.17mm was coated by the vacuum deposition of aluminum, using a filament evaporation technique known in the art, until a metallized film having a thickness of about 1500 angstroms was developed.
- a charge of 0.3 gram of aluminum was placed in an alumina coated tantalum boat, and a charge of 0.3 gram of magnesium fluoride was placed in a tungsten boat.
- the metallized substrate and two boats were then placed inside a bell jar with the two boats electrically connected in parallel.
- the aluminum and magnesium fluoride were then simultaneously co-evaporated and co-deposited onto the aluminum metallized substrate under the following conditions:
- the electrical power was raised slowly to the maximum indicated in about 90 seconds and held there for an additional 30 seconds.
- the thickness of the resulting synthesized semiconductive coating was about 2,000 angstroms.
- the absorptivity of this coating calculated from its reflectance curve using
- the resulting semiconductive coating had a thickness of about 1200 angstroms and an absorptivity of 0.839.
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU71745/81A AU7174581A (en) | 1980-07-28 | 1980-07-28 | Solar energy collector having semiconductive coating formed from metal and dielectric |
PCT/US1980/000987 WO1982000510A1 (en) | 1980-07-28 | 1980-07-28 | Solar energy collector having semiconductive coating formed from metal and dielectric |
EP81901346A EP0056373A1 (en) | 1980-07-28 | 1980-07-28 | Solar energy collector having semiconductive coating formed from metal and dielectric |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US1980/000987 WO1982000510A1 (en) | 1980-07-28 | 1980-07-28 | Solar energy collector having semiconductive coating formed from metal and dielectric |
WOUS80/00987800728 | 1980-07-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1982000510A1 true WO1982000510A1 (en) | 1982-02-18 |
Family
ID=22154459
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1980/000987 WO1982000510A1 (en) | 1980-07-28 | 1980-07-28 | Solar energy collector having semiconductive coating formed from metal and dielectric |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0056373A1 (en) |
AU (1) | AU7174581A (en) |
WO (1) | WO1982000510A1 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0092452A1 (en) * | 1982-03-31 | 1983-10-26 | Commissariat A L'energie Atomique | Coating for photothermal conversion |
EP0107412A1 (en) * | 1982-10-08 | 1984-05-02 | The University Of Sydney | Solar selective surface coating |
US4735457A (en) * | 1986-12-24 | 1988-04-05 | Bonerb Vincent C | Freight vehicle with a convertible cargo space |
US20110138811A1 (en) * | 2009-12-14 | 2011-06-16 | Cheng-Yi Lu | Solar receiver and solar power system having coated conduit |
CN103954059A (en) * | 2014-06-11 | 2014-07-30 | 江苏奥蓝工程玻璃有限公司 | Solar selective absorption composite coating layer and preparation method thereof |
CN104755854A (en) * | 2012-10-26 | 2015-07-01 | 株式会社丰田自动织机 | Heat conversion member and heat conversion laminate |
EP2913605A4 (en) * | 2012-10-26 | 2016-06-22 | Toyota Jidoshokki Kk | Heat conversion member and heat conversion laminate |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3272986A (en) * | 1963-09-27 | 1966-09-13 | Honeywell Inc | Solar heat absorbers comprising alternate layers of metal and dielectric material |
US3920413A (en) * | 1974-04-05 | 1975-11-18 | Nasa | Panel for selectively absorbing solar thermal energy and the method of producing said panel |
US4037014A (en) * | 1975-10-21 | 1977-07-19 | Rca Corporation | Semiconductor absorber for photothermal converter |
US4082907A (en) * | 1975-09-22 | 1978-04-04 | Reynolds Metals Company | Thin molybdenum coatings on aluminum for solar energy absorption |
US4098956A (en) * | 1976-08-11 | 1978-07-04 | The United States Of America As Represented By The Secretary Of The Interior | Spectrally selective solar absorbers |
US4122239A (en) * | 1976-01-19 | 1978-10-24 | Centre National D'etudes Spatiales | Solar absorbers with layers of nickel/chromium alloy and dielectric material |
US4148294A (en) * | 1976-04-15 | 1979-04-10 | Dornier System Gmbh | Solar collector panel and method of making |
US4177325A (en) * | 1977-08-31 | 1979-12-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aluminium or copper substrate panel for selective absorption of solar energy |
-
1980
- 1980-07-28 AU AU71745/81A patent/AU7174581A/en not_active Abandoned
- 1980-07-28 EP EP81901346A patent/EP0056373A1/en not_active Ceased
- 1980-07-28 WO PCT/US1980/000987 patent/WO1982000510A1/en not_active Application Discontinuation
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3272986A (en) * | 1963-09-27 | 1966-09-13 | Honeywell Inc | Solar heat absorbers comprising alternate layers of metal and dielectric material |
US3920413A (en) * | 1974-04-05 | 1975-11-18 | Nasa | Panel for selectively absorbing solar thermal energy and the method of producing said panel |
US4082907A (en) * | 1975-09-22 | 1978-04-04 | Reynolds Metals Company | Thin molybdenum coatings on aluminum for solar energy absorption |
US4037014A (en) * | 1975-10-21 | 1977-07-19 | Rca Corporation | Semiconductor absorber for photothermal converter |
US4122239A (en) * | 1976-01-19 | 1978-10-24 | Centre National D'etudes Spatiales | Solar absorbers with layers of nickel/chromium alloy and dielectric material |
US4148294A (en) * | 1976-04-15 | 1979-04-10 | Dornier System Gmbh | Solar collector panel and method of making |
US4098956A (en) * | 1976-08-11 | 1978-07-04 | The United States Of America As Represented By The Secretary Of The Interior | Spectrally selective solar absorbers |
US4177325A (en) * | 1977-08-31 | 1979-12-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aluminium or copper substrate panel for selective absorption of solar energy |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0092452A1 (en) * | 1982-03-31 | 1983-10-26 | Commissariat A L'energie Atomique | Coating for photothermal conversion |
US4504553A (en) * | 1982-03-31 | 1985-03-12 | Commissariat A L'energie Atomique | Covering for photothermal conversion |
EP0107412A1 (en) * | 1982-10-08 | 1984-05-02 | The University Of Sydney | Solar selective surface coating |
US4735457A (en) * | 1986-12-24 | 1988-04-05 | Bonerb Vincent C | Freight vehicle with a convertible cargo space |
US20110138811A1 (en) * | 2009-12-14 | 2011-06-16 | Cheng-Yi Lu | Solar receiver and solar power system having coated conduit |
EP2513573A2 (en) * | 2009-12-14 | 2012-10-24 | Pratt & Whitney Rocketdyne Inc. | Solar receiver and solar power system having coated conduit |
US8783246B2 (en) * | 2009-12-14 | 2014-07-22 | Aerojet Rocketdyne Of De, Inc. | Solar receiver and solar power system having coated conduit |
CN104755854A (en) * | 2012-10-26 | 2015-07-01 | 株式会社丰田自动织机 | Heat conversion member and heat conversion laminate |
EP2913605A4 (en) * | 2012-10-26 | 2016-06-22 | Toyota Jidoshokki Kk | Heat conversion member and heat conversion laminate |
EP2913604A4 (en) * | 2012-10-26 | 2016-06-22 | Toyota Jidoshokki Kk | Heat conversion member and heat conversion laminate |
CN103954059A (en) * | 2014-06-11 | 2014-07-30 | 江苏奥蓝工程玻璃有限公司 | Solar selective absorption composite coating layer and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
AU7174581A (en) | 1982-03-02 |
EP0056373A1 (en) | 1982-07-28 |
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