WO2009061492A1 - Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior - Google Patents
Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior Download PDFInfo
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- WO2009061492A1 WO2009061492A1 PCT/US2008/012611 US2008012611W WO2009061492A1 WO 2009061492 A1 WO2009061492 A1 WO 2009061492A1 US 2008012611 W US2008012611 W US 2008012611W WO 2009061492 A1 WO2009061492 A1 WO 2009061492A1
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- heat transport
- transport device
- composite material
- carbon
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- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 claims description 6
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/052—Cooling means directly associated or integrated with the PV cell, e.g. integrated Peltier elements for active cooling or heat sinks directly associated with the PV cells
- H01L31/0521—Cooling means directly associated or integrated with the PV cell, e.g. integrated Peltier elements for active cooling or heat sinks directly associated with the PV cells using a gaseous or a liquid coolant, e.g. air flow ventilation, water circulation
-
- 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
- F24S80/10—Materials for heat-exchange conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S90/00—Solar heat systems not otherwise provided for
-
- 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
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/02—Constructions of heat-exchange apparatus characterised by the selection of particular materials of carbon, e.g. graphite
-
- 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
- Y02E10/50—Photovoltaic [PV] energy
Definitions
- the present invention is in the technical field of composite materials.
- the present invention is in the technical field of heat transport, extraction, and cooling.
- the present invention is also related to heat transport, extraction, cooling, storage and management for solar thermal, photovoltaic and other solar electric power generation, as well as all types of cooling and heat management, including but not limited to the electronics industry in general.
- Cooling of photovoltaic cells is one of the main concerns when designing concentrating photovoltaic systems.
- Cells may experience both short-term (efficiency loss) and long-term (irreversible damage) degradation due to excess temperatures.
- Concentrating solar energy maximizes the ability to derive other forms of output therefrom.
- very high heat densities are often produced by sun concentrations of more than 1 ,000 times the nominal concentration of the sun's energy. This concentration is sometimes referred to as "1 ,000X" or "1 ,000 suns.”
- Some or all parts of an arrangement that are exposed to these levels of heat density may be destroyed or are rendered ineffective or inefficient. Consequently, at least some commercially available solar cells specify that they are not intended for use above 1 ,000 suns.
- Design considerations for cooling systems include low and uniform cell temperatures, system reliability, sufficient capacity for dealing with worst case scenarios, and minimal power consumption by the system. For instance, an active cooling system with a thermal resistance of less than 10 ⁇ 4 K m 2 /W is typically necessary for solar cells under high concentrations (>150 suns).
- Conventional nuclear power generation cooling systems typically require large volumes of water. Thus, it is common to locate nuclear power plants in close proximity to large bodies of water, such as lakes. However, severe drought conditions, which may become more prevalent due to climate change, can diminish the availability of enough water to provide adequate cooling. This can result in a disruption of the generation of electrical power. Thus, there is a need to provide a way to enable adequate cooling of nuclear power generation operations with lower volumes of cooling media than is currently utilized.
- the present invention provides materials, arrangements, systems, and methods for improved efficiency in heat transport, extraction, cooling, storage and management.
- the invention can be utilized in a number of potential applications, including but not limited to solar thermal, photovoltaic and other solar electric power generation applications.
- the present invention includes materials, arrangements, systems and methods that may be used in applications with very high heat densities produced by sun concentrations of up to, for example, 10,00OX.
- Heat management for solar electric power generation involves efficient extraction and transportation of heat generated by the solar cell with an incident concentrated solar energy strength of up to, for example, 10,00OX. There are at least two notable aspects of this system: cooling the solar cells and transporting the heat away for other utility applications such as hot water and/or steam.
- Heat management for solar thermal power generation involves efficient extraction and transportation the heat absorbed by the heat collector subsystem with an incident sunlight concentration of up to, for example, 10,00OX.
- this system collection of heat and transporting the heat away for other utility applications such as hot water and/or steam.
- a solar energy receiving device and at least one heat transport device in thermal communication with the solar it energy receiving device, the least one heat transport device formed from a composite material, the composite material comprising a matrix of carbon fibers, the carbon fibers comprising one or more of: mesophase carbon, carbon nanotubes, graphite, graphene and pan carbon.
- the present invention provides a heat transport device comprising: an internal passage; and at least a portion of the internal passage formed from a composite material, the composite material comprising a matrix of carbon fibers, the carbon fibers comprising one or more of: mesophase carbon, carbon nanotubes, graphite, graphene and pan carbon.
- a solar energy receiving device comprising a first surface for receiving solar energy incident thereon, and a second opposing surface, the second surface being electrically conductive; at least one heat transport device in direct contact with at least a portion of the second surface, the at least one heat transport device comprises at least one internal passage and at least one duct; and a heat transport media flowing within the at least one internal passage and at least one duct.
- Figure 1 is a schematic illustration of the molecular structure of carbon fiber.
- Figure 2 is a schematic illustration of thermal gradients present in an anisotropic fiber.
- Figures 3A and 3B are schematic illustrations of plated fibers before and after sintering.
- Figure 4 is schematic illustration of a portion of the fiber matrix, including illustration of heat path and thermal gradient behaviors.
- Figure 5 is a schematic illustration of a basic building block construction including multiple layers of a designer composite.
- Figure 6 is a schematic illustration of a designer composite in the form of an anisotropic XY cross weave, including the matrix material in the Z direction.
- Figure 7 is a schematic illustration of a micro/nano cooling or heat transport channel arrangement.
- Figure 8 is a schematic illustration of certain optional details of the arrangement of Figure 7.
- Figure 9 is a schematic cross-sectional illustration of an arrangement formed according to an additional aspect of the present invention.
- Figure 10 is a schematic illustration of an end view of the arrangement of
- Figure 11 is a schematic illustration of an arrangement including a solar cell and a cooling or heat transport arrangement formed according to one aspect of the present invention.
- Figure 12 is a schematic illustration of an arrangement including a solar cell and a cooling or heat transport arrangement formed according to a further aspect of the present invention.
- heat receiving device or “electromagnetic energy receiving device” means one or more devices arranged for receiving one or more forms of electromagnetic energy, such as solar energy, infrared energy, far infrared energy, microwave energy, sound energy, phonon energy, or radio waves, and possibly converting the electromagnetic energy incident thereon to one or more forms of energy which differ than the form which is incident thereon.
- the converted energy may take the form of electrical current, heat, mechanical energy and/or fluid pressure.
- heat receiving devices include, but are not limited to, photovoltaic solar cells and passive solar devices.
- heat transfer media means a vapor, a single fluid, mixed fluids, or multiphase fluids.
- the heat transfer media may have any suitable pressure, including pressures equal to, less than, or higher than, atmospheric pressure.
- the heat transfer media may include, but is not limited to, one or a combination of: organic fluid, inorganic fluid, biological fluid, water, steam, oil, and particles or structures of organic, inorganic or biological materials. When present in the form of a mixture, the heat transfer media may take the form of a colloidal dispersion or emulsion.
- duct shall mean one or more structures capable of conducting the heat transfer media therethrough.
- the duct includes structures such as channels, canals, tubes, conduits, passageways, tubules and capillaries.
- the term “duct” is not limited to any particular material, cross-sectional geometry or dimension. For purposes of illustration, the duct can be provided with dimensions on the order of 1 nm to a few centimeters.
- designer refers to the ability to control physical and/or thermal properties in the X, Y, Z material indices. Designer materials have made-to-order properties in one or more of the three dimensions.
- the materials of the present invention can be used in any number of different applications.
- the materials of the present invention can be used to provide unexpectedly superior results as heat transport devices such as solar cell package substrate material, micro-channel heat transport devices and fluidic systems, component mounts, connectors, thermal interface materials, heat spreaders, heat sinks, heat pipes, vapor chambers, thermoelectric devices, cooling components in nuclear power generation operations and other cooling components.
- the materials of the present invention can be characterized as designer materials. Generally, conventional composites are made simply by mixing materials of different physical properties, with no special ordering within the composite and can only demonstrate bulk properties.
- the designer materials of the present invention demonstrate different physical properties, thermal conductivity being a very important physical property for cooling and heat transport applications, in different directions and parts of the composite.
- thermal conductivity being a very important physical property for cooling and heat transport applications, in different directions and parts of the composite.
- one or more of the following properties may be tailored: coefficient of thermal expansion (CTE); thermal spreading coefficient Ke; and isothermal morphing of heat flux.
- CTE coefficient of thermal expansion
- Ke thermal spreading coefficient Ke
- isothermal morphing of heat flux isothermal morphing of heat flux.
- Designer materials of the present invention are anisotropic composites and matrices that are thinner, lighter, and stronger, and have eccentric heat spreading. Eccentricity is an important and major property in the designer materials. Heat spreading behavior in the X, Y and Z dimensions can be custom designed based on the application needs. In addition, the thermal conductivity and heat spreading could be custom designed to vary even along X, Y and Z axes.
- the thermal properties in X direction could change as the value of X changes, which is along its length.
- the thermal conductivity and heat spreading could be custom designed to vary even along X, Y and Z axes.
- the thermal properties in X direction could change as the value of X changes, which is along its length. If the heat spreading in an isotropic material could be visualized as a spheroid, the designer techniques enable making the shape an ellipsoid or even any random shape. Another way to visualize the power of the designer paradigm is an onion made up of layers, in which each layer could have different thermal properties, and different even within the layer surface.
- the designer materials of the present invention may comprise an anisotropic carbon-based fiber component and at least one of a high thermal conductivity filler and a high thermal conductivity coating or cladding.
- the anisotropic carbon-based fibers can comprise one or more of: mesophase carbon fiber, carbon nanotube (CNT) based carbon fiber, graphene- based carbon fiber, graphite-based carbon fiber, and polyacrylonitrile (PAN) based carbon fiber.
- the carbon fiber may be derived from pitches, as well known in the art.
- the fibers may be formed from copper, or be clad with copper.
- the fiber component of the composite comprises mesophase carbon fiber.
- Many materials containing polymers can be converted at early stages of carbonization to a structurally ordered anisotropic liquid crystals called mesophase, which can in turn be used to produce an anisotropic high quality carbon fiber.
- the molecular structure 10 of one of the carbon materials used in the composites of the present invention is illustrated in the Figure 1.
- the hexagonal crystalline structure 12 in the XY plane has high covalent bonding 14 responsible for high thermal conductivity in this plane.
- the adjacent planes in the Z direction have weak Van der Walls bonding 16.
- This combination of high thermal conductivity in the XY direction, with significantly less conductivity in the Z direction makes the material anisotropic as indicated by the indication of relevant heat flow 18.
- the thermal conductivity of mesophase-based carbon fibers 20 is anisotropic with very high conductivity in X-direction or along the length of the fiber, while where the thermal conductivity along its Z-direction or thickness or diameter is very poor.
- Thermal conductivity of the mesophase- based carbon fiber along its length ranges from 100 watts per meter-Kelvin (W/mK) to 5,000 watts per meter Kelvin.
- the thermal conductivity in the thickness direction is less than 50 watts per meter-Kelvin.
- the anisotropic carbon-based fibers can be embedded with an isotropic high thermal conductivity filler material.
- Suitable filler materials include CNTs and other high conductivity materials like silver, diamond, aluminum nitride and boron nitride. Boron nitride and aluminum nitride have the special property of high thermal conductivity with no electrical conductivity.
- the amount of filler embedded varies depending on the desired application and performance objectives. For example, filler can be present in amounts of 5% to 50% by volume. By embedding such fillers, the thermal conductivity of the carbon-based can be increased to around 2,000 watts per meter-Kelvin along its length.
- CNT includes Single Wall CNT (SWCNT) and Multi Wall CNT (MWCNT), and combinations thereof.
- SWCNT and MWCNT have different conductivity and structural properties, whereas the choice between the two can depend factors such as the amount of heat to be transferred.
- the carbon-based fibers, whether embedded with filler or not, may also be coated or clad with a high thermal conductivity material 28.
- Suitable coating or cladding materials include aluminum, copper, silver boron nitride, diamond and CNTs.
- the thickness of the coating or cladding may vary depending on the application and performance objectives, and desired final density of the composite. For example, the coating or cladding may range in thickness from 100nm - 5 ⁇ m.
- the coating thickness is approximately 0.5 ⁇ m.
- the anisotropic carbon-based fibers can be spun and aligned to form linear matrix, and then heated to sinter the clad or coated materials to fuse the fibers 28 together. The fibers adhere to each other and pull close together into a compacted or dense matrix. The process boosts the density of the matrix by 5 to 25 times. Other factors being equal, higher density results in better thermal conductivity. Several other factors may also affect the density of the resulting matrix, such as the fiber diameter, density, type and quality of the embedded high conductivity filler material, and the CNT type (single wall or multi-wall). When present, the manner in which the CNTs are grown can also be an important factor that impacts the resulting shape and density of the matrix.
- the coating or cladding 28 deposited on the anisotropic carbon-based fibers 20 can be provided with any suitable thickness t.
- t thickness of the cladding 28 required to fill the void between compressed fibers 20
- r the mean radius of the fiber
- R r + t.
- the void fill area A 0.1616 ⁇ .
- the composite of the present invention may comprise the abovementioned anisotropic carbon-based fiber, high thermal conductivity filler and a foam material.
- Foam composites are made by air blowing and foaming similar to the way all metal foam composites are manufactured.
- the foam composites of the present invention made from anisotropic carbon-based fiber will be lighter than metal foams made solely from aluminum.
- the embedded and/or clad anisotropic carbon-based fibers 20 can be woven in various patterns, thereby forming a woven matrix composite designer material 31.
- Figure 4 is a cross-section illustrating the transverse heat path 32 and thermal gradient 34 through this particular woven matrix composite 31.
- the matrix can be designed to have very high thermal conductivity in the X and Y direction compared to its Z direction. By choosing weaves with a given direction like only X or only Y, the spreading can be controlled or improved only in that chosen direction.
- the matrix is designed to have the thermal conductivity in X, Y and Z directions to be different from each other, the heat spreading will all be different from each other, thus making the heat spreading eccentric.
- the thermal conductivity in metals like copper and aluminum, which are often used in such applications, is the same in all the three directions.
- the designer materials of the present invention allows the thermal spreading properties to be controlled in chosen directions.
- the composite matrix of the present invention can be provided with any suitable size or dimension.
- the composite matrix can have a thickness from 10nm - 1 ,000 ⁇ m, more specifically 10nm-800nm, or 1 ⁇ m-1 ,000 ⁇ m.
- a plurality of layers of composite matrix material can be fused together to build a thicker composite matrix.
- Figure 5 shows multiple layers 42, 44, 46, 48, 50 of composite matrix material which can form the basic building blocks for cooling or heat transfer components.
- Each layer of composite matrix material can be provided with distinct dimensions, weave pattern or orientation, and/or composition to impart the desired properties to the resulting cooling or heat transfer component formed therefrom.
- an eccentric thermal conductivity profile can be achieved by varying the number and type of the composite matrix material layers in building a cooling or heat transport component therefrom.
- each of the layers has a thickness T of 20 ⁇ m to 10O ⁇ m.
- the composite matrix material and cooling or heat transport components formed therefrom can be made by any number of suitable techniques or methods. The following is an illustrative, non-limiting discussion of such techniques and methods.
- the manufacturing process can be continuous starting from the mesophase or the liquid crystal phase of the carbon fiber precursor material, until and including the finished product line of a cooling or heat transport component.
- the different steps of the continuous processes may include one or more of the following, in any particular order.
- One or more high thermal conductivity nano and micro filler materials such as CNTs and diamond, are embedded into carbon fiber at the mesophase and during the drawing of the fiber through fiber-drawing dies and the fiber spinnerets.
- the amount filler materials used depend on the desired increase in thermal conductivity.
- the drawing orifice chosen depends on the amount and type of filler materials as well as the filament diameter that make up the spun carbon fiber. If the orifice is smaller than a micron, the filler material and the carbon fiber filament become few hundred to hundreds of nanometers as the fiber filament drops down due to gravity and joins the other filaments from the other orifices of the drawing tool, thus resulting in thinner spun fiber.
- the next steps may include heating, re-crystallization and cooling through a continuous microwave heating and cooling process. Depending on the desired thermal conductivity, heating up to the mesophase formation temperature is required. This temperature can be on the order of 2000 0 C to 3000 0 C.
- the heat treated fiber can be sent through a pretreatment process for coating or cladding. A variety of metals with high thermal conductivity, such as copper, is coated on the fiber.
- the coating thickness can be approximately 10nm - 5 ⁇ m, and is controlled by the speed at which the fibers pass through the plating cycle.
- the coated or clad fibers may be sintered together, as described above, which allows the fibers to come together or densify.
- the fiber can be spooled into an array of spools.
- the fibers may be sent through a fiber line up and weave processes.
- Figure 6 shows a cross-woven matrix 52. This is a reel to reel process.
- the process may include two steps: in-line weaving and cross weaving.
- the woven fibers can go through a continuous microwave sintering process, where the coated fibers get fused while at the same time forming a woven composite designer matrix material.
- the composite matrix material may be layered and fused together by a continuous roll-to-roll heating process. The type and thickness of the layers are chosen to define the thermal conductivity of the final designer matrix.
- the designer composite matrix layers or films can be spooled into a shippable array of spools for use in the subsequent manufacture of a variety of cooling or heat transport devices or components.
- Some heat transport components may even be manufactured in collocated next steps.
- a full range of cooling or heat transport components and materials can be made at least in part from a composite material of the present invention.
- TIM thermal interface materials
- heat sinks heat pipes
- microchannel heat transport components heat spreaders
- stiffeners stiffeners
- packaging materials PC board laminates
- substrate material microprocessor lid and other specialty packaging materials.
- the composite materials of the present invention can be utilized in the construction of the devices, systems, arrangements and methods disclosed in: U.S. Provisional Application No. 60/996,273 filed November 8, 2007; U.S. Provisional Application No. 61/071 ,410 filed April 28, 2008; U.S. Provisional Application No. 61/071 ,411 filed April 28, 2008; and non-provisional U.S. Patent Application Serial
- a heat transport device is provided.
- a heat transport device of the present invention can be formed, at least in part, from the composite matrix designer material described above.
- An exemplary heat transport device 60 is illustrated in Figure 7. It bears emphasizing that the present invention is not limited to the particular device illustrated in Figure 7.
- the device 60 comprises an internal passage 62 optionally having one or more ducts 64.
- the ducts 64 can have any suitable dimensions, such as a width of 10nm - 5mm.
- the ducts 64 can be designed to have a high aspect ratio, such as at least 10:1 or 50:1 , of height H to width W. At least a portion of the internal passage 62 and/or at least a portion of the one or more ducts 64 is formed from the designer composite matrix material. As illustrated in Figure 8, the ducts 64 can be imprinted with nano grooves 66 and/or spikes 68 to create turbulence and hence efficient heat transfer from the channel surface. Instead, or in addition, CNTs 70 can be coated on the one or more of the inside walls of the ducts 64.
- a heat transfer media 72 may be provided within the internal passage 62 and in communication with the at least one duct 64.
- the heat transfer media 72 can contain CNTs and/or other nano or micro size particles 74 to help create the turbulence and break up laminar flow to enhance the convective heat transport efficiency.
- the CNTs and/or nano or micro particles 74 impinge on the walls of the ducts 64 and collect heat therefrom then bounce back into the heat transfer media 72 and quickly disperse and transfer the heat into the heat transfer media 72, thus acting as heat transfer agents between the ducts 64 and the heat transfer media 72.
- the particles 74 also break up laminar boundary layer flow and create or add to the turbulent flow of the heat transfer media 72.
- the heat transport device 60 may comprise a closed system containing a set volume of heat transfer media 72, that may circulate, if at all, only in a closed loop. Appropriate curvature is designed into the ducts 64 to enhance the fluid flow turbulence.
- the inside walls of the ducts 64 may be provided with CNTs and/or nano/micro fibers 70 are grown vertically from the surface protruding into the heat transfer media. These protrusions transfer the conducted heat into the heat transfer media, swaying back and forth in the flow thereof.
- the heat transport device 60 can be manufactured by any suitable technique.
- nano-imprint lithography NIL
- NIL nano-imprint lithography
- This method also conforms to the International Technology Roadmap for Semiconductors.
- NIL may be the lithography solution at the 32 and 22 nm fabrication nodes.
- a heat transport device of the type described above, is incorporated into an arrangement including one or more solar cells, and is used for cooling the solar cell and/or transporting heat for other uses.
- An exemplary arrangement 80 is illustrated in Figure 9. As illustrated therein, the arrangement 80 includes a solar cell 82.
- the solar cell 82 comprises a first surface 84 and a second surface 86.
- the heat transport device 60 is placed in thermal communication with the solar cell 82, optionally in thermal communication with at least a portion of the second surface 86.
- a heat transport device 61 is in communication with the entire second surface 86 of the solar cell 82.
- the heat transport device 61 may be formed at least in part from the designer composite material as described herein.
- the heat transport device 61 may otherwise have any suitable configuration.
- the heat transport device 61 can be an actively cooled device having a heat transfer media circulated therethrough (e.g. Figure 10).
- the heat transport device 61 can comprise a passive device having a sealed internal chamber 63.
- a heat transfer media may be provided within the chamber 63.
- the heat transport device 61 is provided with one or more of the features described herein in connection with the heat transport device 60.
- the arrangement 80 may include a thermal interface 88, material (TIM) between the solar cell 82 and the heat transport device 60.
- the thermal interface material 88 is thermally conductive, electrically conductive, or both.
- One suitable thermal interface material is a silver-based material.
- the solar cell 82 can be mounted directly on the heat transport device 60 without the use of the package that comes with the solar cell 82. Because the solar cells 82 are typically mounted on a substrate and packaged with materials which have a comparatively low thermal conductivity, mounting the solar cells directly on the cooling assembly enables maximum heat transfer from the solar cell to the heat transport device.
- the present invention can be combined directly with conventional packaged solar cell arrangements that include a standard solar cell soldered onto a 15mil thick ceramic substrate having electrical connectors provided thereon, and still provide advantages and benefits due to the exceptional cooling and heat transport properties.
- the arrangement 80 additionally may comprise optics or other suitable means 90 for producing concentrated solar energy 92 incident upon the solar cell 82.
- An arrangement formed consistent with the principles of the present invention is capable of amplifying the concentration of sunlight up to, for example, 10,000 times the nominal solar intensity level (10,000X). Additional optional features of the arrangement include electrical connections 94 and a printed circuit board 96.
- the heat transport device 60 may additionally include an inlet 98 and outlet 100 for circulation of a heat transfer media therein.
- the arrangement may include an array of solar cells.
- a single heat transport device can be associated with the entire array.
- each individual cell may be provided with a corresponding heat transport device, or any variation is also envisioned wherein there are fewer individual heat transport devices than the number of individual solar cells (i.e., each heat transport device is associated with a plurality of individual solar cells that are smaller in number that the number in the array).
- a heat transport device of the type described above, is incorporated into the cooling system of a nuclear power generation operation.
- An arrangement formed according to the principles of the present invention may include a combination of heat transport devices and other heat transport and/or cooling system components.
- Figure 11 shows an arrangement 110 wherein heat transfer media flows across the solar cell strip 112 through manifolds 114.
- One example of the heat transfer media is water. Heat transfer media enters the manifolds 114, passes through the solar cells 112, picks up the heat and carries the extracted heat away.
- the main heat transfer media inlet 116 is designed to be maintained at a level higher than the manifold 114 and the heat transfer media outlet 118 out of the manifold 114 is designed to be maintained at a level lower than the manifold 114, so that heated media does not enter back into the solar cells 112.
- Flow rate through the manifold 114 is controlled based on the amount of incident sun light on the concentrator and the solar cell strip 112.
- Figure 12 shows an alternative arrangement 120.
- the same general features are present as in the embodiment depicted in Figure 11.
- heat transfer media inlet 122 and the heat transfer media outlet 124 are constructed such that the direction of the flow of fluid is not significantly changed by the arrangement .
- the heat transport arrangements of the present invention may be directly connected to solar cell arrays or strips.
- cooling or heat transport arrangements of the present invention can be combined with conventional solar cell constructions, but where the substrate and/or mounting components of such conventional solar cell arrangements has been removed so as to allow direct connection between the solar cell arrays or strips with the cooling or heat transport arrangements of the present invention, thereby improving the cooling/heat transport performance of the overall arrangement.
- the present invention can be combined directly with conventional solar cell arrangements that include their standard substrate and/or mounting and still provide advantages and benefits due to the exceptional cooling and heat transport properties as described herein.
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2008801243427A CN101918770A (en) | 2007-11-08 | 2008-11-07 | Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior |
EP08847304A EP2217867A1 (en) | 2007-11-08 | 2008-11-07 | Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior |
BRPI0820469A BRPI0820469A2 (en) | 2007-11-08 | 2008-11-07 | methods, arrangements and compositions of composite material having improved thermal conductivity behavior |
IL205628A IL205628A0 (en) | 2007-11-08 | 2010-05-09 | Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior |
Applications Claiming Priority (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US99627307P | 2007-11-08 | 2007-11-08 | |
US60/996,273 | 2007-11-08 | ||
US7141008P | 2008-04-28 | 2008-04-28 | |
US7141108P | 2008-04-28 | 2008-04-28 | |
US7141208P | 2008-04-28 | 2008-04-28 | |
US61/071,411 | 2008-04-28 | ||
US61/071,410 | 2008-04-28 | ||
US61/071,412 | 2008-04-28 | ||
US12/257,235 US20090173334A1 (en) | 2007-11-08 | 2008-10-23 | Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior |
US12/257,235 | 2008-10-23 |
Publications (1)
Publication Number | Publication Date |
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WO2009061492A1 true WO2009061492A1 (en) | 2009-05-14 |
Family
ID=40626092
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/US2008/012611 WO2009061492A1 (en) | 2007-11-08 | 2008-11-07 | Composite material compositions, arrangements and methods having enhanced thermal conductivity behavior |
Country Status (6)
Country | Link |
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US (2) | US20090173334A1 (en) |
EP (1) | EP2217867A1 (en) |
CN (1) | CN101918770A (en) |
BR (1) | BRPI0820469A2 (en) |
IL (1) | IL205628A0 (en) |
WO (1) | WO2009061492A1 (en) |
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Also Published As
Publication number | Publication date |
---|---|
CN101918770A (en) | 2010-12-15 |
IL205628A0 (en) | 2011-08-01 |
US20110271951A1 (en) | 2011-11-10 |
BRPI0820469A2 (en) | 2017-05-23 |
EP2217867A1 (en) | 2010-08-18 |
US20090173334A1 (en) | 2009-07-09 |
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