FR3028515B1 - Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite - Google Patents

Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite Download PDF

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Publication number
FR3028515B1
FR3028515B1 FR1402561A FR1402561A FR3028515B1 FR 3028515 B1 FR3028515 B1 FR 3028515B1 FR 1402561 A FR1402561 A FR 1402561A FR 1402561 A FR1402561 A FR 1402561A FR 3028515 B1 FR3028515 B1 FR 3028515B1
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Prior art keywords
composite structure
satellite
thermal conductivity
electrical conductivity
plate sheets
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Application number
FR1402561A
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FR3028515A1 (fr
Inventor
Martine Lutz
Dima TANZILLI
Nicolas BURGER
Abdelghani LAACHACHI
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Thales SA
Luxembourg Institute of Science and Technology LIST
Original Assignee
Thales SA
Centre De Rech Public Henri Tudor
Centre de Recherche Public Henri Tudor
Luxembourg Institute of Science and Technology LIST
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Application filed by Thales SA, Centre De Rech Public Henri Tudor, Centre de Recherche Public Henri Tudor, Luxembourg Institute of Science and Technology LIST filed Critical Thales SA
Priority to FR1402561A priority Critical patent/FR3028515B1/fr
Priority to PCT/EP2015/076556 priority patent/WO2016075290A2/fr
Priority to US15/526,725 priority patent/US20170321020A1/en
Priority to EP15797926.1A priority patent/EP3218428A2/fr
Publication of FR3028515A1 publication Critical patent/FR3028515A1/fr
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    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
    • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
    • B64G1/503—Radiator panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
    • B64G1/506—Heat pipes
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/005—Reinforced macromolecular compounds with nanosized materials, e.g. nanoparticles, nanofibres, nanotubes, nanowires, nanorods or nanolayered materials
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
    • C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
    • 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
    • F28D15/02—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 in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/0275—Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
    • 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
    • F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081—Heat exchange elements made from metals or metal alloys
    • F28F21/084—Heat exchange elements made from metals or metal alloys from aluminium or aluminium alloys
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00—Details of semiconductor or other solid state devices
    • H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/36—Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
    • H01L23/373—Cooling facilitated by selection of materials for the device or materials for thermal expansion adaptation, e.g. carbon
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00—Details of semiconductor or other solid state devices
    • H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/36—Selection of materials, or shaping, to facilitate cooling or heating, e.g. heatsinks
    • H01L23/373—Cooling facilitated by selection of materials for the device or materials for thermal expansion adaptation, e.g. carbon
    • H01L23/3737—Organic materials with or without a thermoconductive filler
    • 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
    • H01L31/042—PV modules or arrays of single PV cells
    • H01L31/048—Encapsulation of modules
    • 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
    • H01L31/042—PV modules or arrays of single PV cells
    • H01L31/048—Encapsulation of modules
    • H01L31/049—Protective back sheets
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/40—Thermal components
    • H02S40/42—Cooling means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1007—Communications satellites
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B82—NANOTECHNOLOGY
    • B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
    • B82Y30/00—Nanotechnology for materials or surface science, e.g. nanocomposites
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2300/00—Characterised by the use of unspecified polymers
    • 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
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L2924/00—Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
    • H01L2924/0001—Technical content checked by a classifier
    • H01L2924/0002—Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
    • 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

Abstract

L'invention a pour objet une structure composite comprenant une résine organique et des fibres de carbone, caractérisée en ce qu'elle comprend en outre des nanofeuillets de structure plane de graphène noyés dans ladite résine. Cette structure combinant de bonnes propriétés en termes de tenue mécanique, de conductivité thermique et de conductivité électrique peut avantageusement être utilisée pour des dispositifs de dissipation thermique, comme substrat de générateur solaire ou bien encore comme boîtier de composants électroniques, embarqués dans des satellites.
FR1402561A 2014-11-14 2014-11-14 Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite Active FR3028515B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1402561A FR3028515B1 (fr) 2014-11-14 2014-11-14 Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite
PCT/EP2015/076556 WO2016075290A2 (fr) 2014-11-14 2015-11-13 Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite
US15/526,725 US20170321020A1 (en) 2014-11-14 2015-11-13 Composite structure comprising a resin loaded with flat graphene sheets having enhanced thermal and electrical conductivity, in particular for a satellite
EP15797926.1A EP3218428A2 (fr) 2014-11-14 2015-11-13 Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1402561A FR3028515B1 (fr) 2014-11-14 2014-11-14 Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite
FR1402561 2014-11-14

Publications (2)

Publication Number Publication Date
FR3028515A1 FR3028515A1 (fr) 2016-05-20
FR3028515B1 true FR3028515B1 (fr) 2018-01-12

Family

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FR1402561A Active FR3028515B1 (fr) 2014-11-14 2014-11-14 Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite

Country Status (4)

Country Link
US (1) US20170321020A1 (fr)
EP (1) EP3218428A2 (fr)
FR (1) FR3028515B1 (fr)
WO (1) WO2016075290A2 (fr)

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US20170191498A1 (en) * 2015-12-30 2017-07-06 General Electric Company Graphene ultra-conductive casing wrap
DE102017202751A1 (de) 2017-02-21 2018-08-23 Airbus Defence and Space GmbH Raumfahrtsystem
CN107189354B (zh) * 2017-07-07 2019-08-16 齐鲁工业大学 一种石墨烯纳米片增强碳纤维复合材料的制备方法
CN109703788B (zh) * 2018-12-13 2021-04-13 航天东方红卫星有限公司 一种基于石墨烯和铜条适用于微纳卫星的等温化热控装置
CN110673418A (zh) * 2019-10-11 2020-01-10 深圳航天东方红海特卫星有限公司 一种石墨烯智能热控薄膜
CN111465260B (zh) * 2020-03-19 2022-03-04 北京空间机电研究所 一种用于减轻质量的航天器用大面积辐射散热装置
CN112873895B (zh) * 2020-12-03 2023-10-24 武汉格罗夫氢能汽车有限公司 一种燃料电池氢能汽车用碳纤维复合材料预制体制作方法
CN114537716B (zh) * 2022-01-25 2023-10-27 上海卫星工程研究所 点阵式热源温度一致性控制方法及系统

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AT503907A1 (de) * 2006-07-04 2008-01-15 Hans-Peter Dr Bierbaumer Solarmodul
US20080020193A1 (en) * 2006-07-24 2008-01-24 Jang Bor Z Hybrid fiber tows containning both nano-fillers and continuous fibers, hybrid composites, and their production processes
US8324515B2 (en) * 2007-10-16 2012-12-04 Honeywell International Inc. Housings for electronic components
FR2960218B1 (fr) * 2010-05-21 2012-08-03 Thales Sa Dispositif de dissipation thermique pour equipement spatial, notamment pour satellite
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US8232129B2 (en) * 2010-12-16 2012-07-31 The Boeing Company Bonding solar cells directly to polyimide
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Also Published As

Publication number Publication date
FR3028515A1 (fr) 2016-05-20
US20170321020A1 (en) 2017-11-09
WO2016075290A3 (fr) 2017-03-30
EP3218428A2 (fr) 2017-09-20
WO2016075290A2 (fr) 2016-05-19

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