PL2388195T3 - Przyrząd do rozproszenia termicznego przeznaczony do sprzętu kosmicznego, w szczególności do satelity - Google Patents
Przyrząd do rozproszenia termicznego przeznaczony do sprzętu kosmicznego, w szczególności do satelityInfo
- Publication number
- PL2388195T3 PL2388195T3 PL11166968T PL11166968T PL2388195T3 PL 2388195 T3 PL2388195 T3 PL 2388195T3 PL 11166968 T PL11166968 T PL 11166968T PL 11166968 T PL11166968 T PL 11166968T PL 2388195 T3 PL2388195 T3 PL 2388195T3
- Authority
- PL
- Poland
- Prior art keywords
- satellite
- dissipation device
- thermal dissipation
- space equipment
- equipment
- Prior art date
Links
Classifications
-
- 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
-
- 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
-
- 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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/14—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally
- F28F1/22—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally the means having portions engaging further tubular elements
-
- 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
-
- 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
- F28F21/06—Constructions of heat-exchange apparatus characterised by the selection of particular materials of plastics material
- F28F21/067—Details
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Remote Sensing (AREA)
- Environmental & Geological Engineering (AREA)
- Environmental Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Biodiversity & Conservation Biology (AREA)
- Aviation & Aerospace Engineering (AREA)
- Nanotechnology (AREA)
- Health & Medical Sciences (AREA)
- Composite Materials (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Sustainable Development (AREA)
- Geometry (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1002159A FR2960218B1 (fr) | 2010-05-21 | 2010-05-21 | Dispositif de dissipation thermique pour equipement spatial, notamment pour satellite |
EP11166968.5A EP2388195B1 (fr) | 2010-05-21 | 2011-05-20 | Dispositif de dissipation thermique pour équipement spatial, notamment pour satellite |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2388195T3 true PL2388195T3 (pl) | 2020-02-28 |
Family
ID=43086056
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL11166968T PL2388195T3 (pl) | 2010-05-21 | 2011-05-20 | Przyrząd do rozproszenia termicznego przeznaczony do sprzętu kosmicznego, w szczególności do satelity |
Country Status (5)
Country | Link |
---|---|
US (1) | US20120125571A1 (pl) |
EP (1) | EP2388195B1 (pl) |
JP (1) | JP2011246112A (pl) |
FR (1) | FR2960218B1 (pl) |
PL (1) | PL2388195T3 (pl) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2660155B1 (en) * | 2012-04-30 | 2015-12-09 | Airbus Defence and Space Limited | Apparatus and method for mounting heat pipes to panels |
FR2995877B1 (fr) * | 2012-09-21 | 2014-10-24 | Thales Sa | Structure meca-thermique adaptee pour un environnement spatial |
FR3028515B1 (fr) * | 2014-11-14 | 2018-01-12 | Thales | Structure composite comportant une resine chargee avec des feuillets plans de graphene a conductivite thermique et conductivite electrique renforcees, notamment pour satellite |
US9878808B2 (en) | 2015-01-08 | 2018-01-30 | The Boeing Company | Spacecraft and spacecraft radiator panels with composite face-sheets |
US10392135B2 (en) | 2015-03-30 | 2019-08-27 | Worldvu Satellites Limited | Satellite radiator panels with combined stiffener/heat pipe |
KR101641616B1 (ko) * | 2015-05-28 | 2016-07-29 | 주식회사 솔루엠 | 방열 기능이 향상된 충전기 및 그 제조 방법 |
US9920178B2 (en) | 2015-12-11 | 2018-03-20 | Northrop Grumman Systems Corporation | Compressible, thermally-conductive, removable nanocomposite gasket |
JP6736332B2 (ja) * | 2016-04-04 | 2020-08-05 | 株式会社Ihiエアロスペース | 人工衛星の機器搭載装置 |
US10018426B2 (en) | 2016-05-12 | 2018-07-10 | The Boeing Company | Composite heat pipes and sandwich panels, radiator panels, and spacecraft with composite heat pipes |
US10138340B2 (en) * | 2016-10-11 | 2018-11-27 | Palo Alto Research Center Incorporated | Low volatility, high efficiency gas barrier coating for cryo-compressed hydrogen tanks |
US10780998B1 (en) * | 2017-03-22 | 2020-09-22 | Space Systems/Loral, Llc | Spacecraft design with multiple thermal zones |
CN111470069B (zh) * | 2020-04-08 | 2021-11-16 | 上海卫星工程研究所 | 适用于卫星承力筒的下端框结构 |
KR102286175B1 (ko) | 2021-04-16 | 2021-08-04 | 김병환 | 인공위성을 위한 히트파이프 |
WO2023161722A1 (en) * | 2022-02-25 | 2023-08-31 | Network Access Associates Limited | Space vehicle heat dissipation systems |
WO2023161717A1 (en) * | 2022-02-25 | 2023-08-31 | Network Access Associates Limited | Space vehicle thermal management system and method for manufacture thereof |
WO2024004355A1 (ja) * | 2022-06-30 | 2024-01-04 | パナソニックホールディングス株式会社 | 熱制御構造体および熱制御構造体を備えた人工衛星 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4806704A (en) * | 1987-06-08 | 1989-02-21 | General Electric Company | Metal matrix composite and structure using metal matrix composites for electronic applications |
JPH11148787A (ja) * | 1997-11-17 | 1999-06-02 | Mitsubishi Electric Corp | ヒートパイプ入りサンドイッチパネル |
US6230790B1 (en) * | 1999-05-10 | 2001-05-15 | Lockheed Martin Corporation | Thermal control system for spacecraft |
US20020102384A1 (en) * | 2001-01-29 | 2002-08-01 | Peck Scott O. | Embedded heat pipe sandwich panel constructed using dissimilar materials |
US7105235B2 (en) * | 2002-05-17 | 2006-09-12 | Her Majesty The Queen In Right Of Canada As Represented By The Minister Of Natural Resources | Isotropic zero CTE reinforced composite materials |
US20040035558A1 (en) * | 2002-06-14 | 2004-02-26 | Todd John J. | Heat dissipation tower for circuit devices |
JP3735651B2 (ja) * | 2002-10-08 | 2006-01-18 | 独立行政法人 宇宙航空研究開発機構 | カーボンナノファイバー分散樹脂繊維強化複合材料 |
US6810944B2 (en) * | 2003-01-30 | 2004-11-02 | Northrop Grumman Corporation | Soldering of saddles to low expansion alloy heat pipes |
CN1841713A (zh) * | 2005-03-31 | 2006-10-04 | 清华大学 | 热界面材料及其制作方法 |
US8534348B2 (en) * | 2005-09-01 | 2013-09-17 | Molex Incorporated | Heat pipe and method for manufacturing same |
US7583506B1 (en) * | 2005-10-14 | 2009-09-01 | The Boeing Company | Multi operational system apparatus and method |
FR2905933B1 (fr) * | 2006-09-15 | 2008-12-26 | Astrium Sas Soc Par Actions Si | Dispositif de gestion des flux thermiques dans un engin spatial et engin spatial equipe d'un tel dispositif |
US8388795B2 (en) * | 2007-05-17 | 2013-03-05 | The Boeing Company | Nanotube-enhanced interlayers for composite structures |
KR101524545B1 (ko) * | 2008-02-28 | 2015-06-01 | 페어차일드코리아반도체 주식회사 | 전력 소자 패키지 및 그 제조 방법 |
JP5117911B2 (ja) * | 2008-04-03 | 2013-01-16 | 新日鉄住金マテリアルズ株式会社 | セラミックスおよび炭素繊維強化プラスチックを含む構造体 |
-
2010
- 2010-05-21 FR FR1002159A patent/FR2960218B1/fr not_active Expired - Fee Related
-
2011
- 2011-05-20 EP EP11166968.5A patent/EP2388195B1/fr active Active
- 2011-05-20 PL PL11166968T patent/PL2388195T3/pl unknown
- 2011-05-20 JP JP2011114173A patent/JP2011246112A/ja active Pending
- 2011-05-20 US US13/112,657 patent/US20120125571A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP2388195A1 (fr) | 2011-11-23 |
FR2960218A1 (fr) | 2011-11-25 |
EP2388195B1 (fr) | 2019-09-11 |
FR2960218B1 (fr) | 2012-08-03 |
US20120125571A1 (en) | 2012-05-24 |
JP2011246112A (ja) | 2011-12-08 |
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