DE10340092A1 - Sandwich Struktur mit Kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren - Google Patents
Sandwich Struktur mit Kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren Download PDFInfo
- Publication number
- DE10340092A1 DE10340092A1 DE10340092A DE10340092A DE10340092A1 DE 10340092 A1 DE10340092 A1 DE 10340092A1 DE 10340092 A DE10340092 A DE 10340092A DE 10340092 A DE10340092 A DE 10340092A DE 10340092 A1 DE10340092 A1 DE 10340092A1
- Authority
- DE
- Germany
- Prior art keywords
- sandwich structure
- metallic
- radiator
- heat pipe
- loop heat
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title abstract 2
- 229910052782 aluminium Inorganic materials 0.000 title abstract 2
- 239000000835 fiber Substances 0.000 abstract 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 1
- 229910000831 Steel Inorganic materials 0.000 abstract 1
- 229910052799 carbon Inorganic materials 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 239000006262 metallic foam Substances 0.000 abstract 1
- 239000011148 porous material Substances 0.000 abstract 1
- 239000010959 steel Substances 0.000 abstract 1
Classifications
-
- 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
- F28D15/0266—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 with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers
-
- 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
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Sustainable Development (AREA)
- Health & Medical Sciences (AREA)
- Biodiversity & Conservation Biology (AREA)
- Environmental & Geological Engineering (AREA)
- Environmental Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Laminated Bodies (AREA)
Abstract
Eine Sandwich Struktur besteht aus kohlenfaserverstärkten Deckschichten und einem Kern aus metallischem oder nichtmetallischem Wabenmaterial oder aus offen-/geschlossenporigen metallischen oder nichtmetallischen Schaummaterialien. Gegen die Innenfläche der Deckschichten sind Kondensierrohre eines Loop-Wärmerohrs angebracht, die entweder aus einem extruierten Aluminiumprofil oder aus einer Kombination zwischen Aluminiumprofil und Stahlrohr bestehen. Die Profile haben integrierte Flansche zur Vergrößerung der Kontaktfläche zur Deckschicht. Anzahl der thermisch leitenden Faserlagen als auch der Winkel der Faserrichtung relativ zu den Kondensierrohren sind so gewählt, dass sowohl das thermische als auch das mechanische Verhalten der Struktur optimiert ist. Zum Ausgleich der thermo-mechanischen Spannungen, hervorgerufen durch die ungleichen thermischen Ausdehnungskoeffizienten, sind flanschfreie Abschnitte der Kondensierrohre gebogen und nicht mit den Deckschichten verbunden. Andere Rohre sind am Rande der Struktur, jedoch außerhalb des Sandwichkerns, verlegt.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10340092A DE10340092B4 (de) | 2003-08-30 | 2003-08-30 | Sandwich Struktur mit kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10340092A DE10340092B4 (de) | 2003-08-30 | 2003-08-30 | Sandwich Struktur mit kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren |
Publications (2)
Publication Number | Publication Date |
---|---|
DE10340092A1 true DE10340092A1 (de) | 2005-05-04 |
DE10340092B4 DE10340092B4 (de) | 2005-09-01 |
Family
ID=34398664
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10340092A Expired - Fee Related DE10340092B4 (de) | 2003-08-30 | 2003-08-30 | Sandwich Struktur mit kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE10340092B4 (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005039783B3 (de) * | 2005-08-22 | 2007-03-22 | Orbitale Hochtechnologie Bremen-System Ag | Kohlenstofffaser-Sandwichstruktur mit integrierten metallischen Rohren |
CN102673803A (zh) * | 2011-03-17 | 2012-09-19 | 塔莱斯公司 | 带有集成热交换器的人造卫星用结构板 |
CN102941926A (zh) * | 2012-11-06 | 2013-02-27 | 北京空间飞行器总体设计部 | 一种空间碎片防护型热辐射器 |
CN103482083A (zh) * | 2013-08-21 | 2014-01-01 | 上海利正卫星应用技术有限公司 | 一种轻量化低热阻辐射器 |
JP2016124535A (ja) * | 2015-01-08 | 2016-07-11 | ザ・ボーイング・カンパニーThe Boeing Company | 宇宙機、及び複合材フェースシートを有する、宇宙機用ラジエータパネル |
CN106347714A (zh) * | 2016-08-31 | 2017-01-25 | 北京空间飞行器总体设计部 | 一种具备在轨弹抛功能的舱外辐射器防护罩系统 |
CN112284172A (zh) * | 2020-10-29 | 2021-01-29 | 上海卫星装备研究所 | 空间辐射散热器 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0438938A2 (de) * | 1989-12-22 | 1991-07-31 | Grumman Aerospace Corporation | Abstrahlersystem für ein Raumfahrzeug |
US5506032A (en) * | 1994-04-08 | 1996-04-09 | Martin Marietta Corporation | Structural panel having integral heat pipe network |
JP2000129857A (ja) * | 1998-10-26 | 2000-05-09 | Mitsubishi Electric Corp | 炭素繊維表皮ヒートパイプパネル |
JP2000130971A (ja) * | 1998-10-28 | 2000-05-12 | Mitsubishi Electric Corp | 炭素繊維表皮ヒートパイプパネル |
JP2001153576A (ja) * | 1999-11-22 | 2001-06-08 | Mitsubishi Electric Corp | 炭素繊維表皮ヒートパイプパネルおよびヒートパイプ |
US20020102384A1 (en) * | 2001-01-29 | 2002-08-01 | Peck Scott O. | Embedded heat pipe sandwich panel constructed using dissimilar materials |
US6478258B1 (en) * | 2000-11-21 | 2002-11-12 | Space Systems/Loral, Inc. | Spacecraft multiple loop heat pipe thermal system for internal equipment panel applications |
-
2003
- 2003-08-30 DE DE10340092A patent/DE10340092B4/de not_active Expired - Fee Related
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0438938A2 (de) * | 1989-12-22 | 1991-07-31 | Grumman Aerospace Corporation | Abstrahlersystem für ein Raumfahrzeug |
US5506032A (en) * | 1994-04-08 | 1996-04-09 | Martin Marietta Corporation | Structural panel having integral heat pipe network |
JP2000129857A (ja) * | 1998-10-26 | 2000-05-09 | Mitsubishi Electric Corp | 炭素繊維表皮ヒートパイプパネル |
JP2000130971A (ja) * | 1998-10-28 | 2000-05-12 | Mitsubishi Electric Corp | 炭素繊維表皮ヒートパイプパネル |
JP2001153576A (ja) * | 1999-11-22 | 2001-06-08 | Mitsubishi Electric Corp | 炭素繊維表皮ヒートパイプパネルおよびヒートパイプ |
US6478258B1 (en) * | 2000-11-21 | 2002-11-12 | Space Systems/Loral, Inc. | Spacecraft multiple loop heat pipe thermal system for internal equipment panel applications |
US20020102384A1 (en) * | 2001-01-29 | 2002-08-01 | Peck Scott O. | Embedded heat pipe sandwich panel constructed using dissimilar materials |
Non-Patent Citations (1)
Title |
---|
Deployable Radiators - A Multi-Discipline Appro- ach, 28th ICES, July 13-16, 1998, SAE 981691 * |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005039783B3 (de) * | 2005-08-22 | 2007-03-22 | Orbitale Hochtechnologie Bremen-System Ag | Kohlenstofffaser-Sandwichstruktur mit integrierten metallischen Rohren |
EP2500275A3 (de) * | 2011-03-17 | 2014-03-12 | Thales | Strukturplatte eines Satelliten mit integrierten Wärmetauschern |
CN102673803A (zh) * | 2011-03-17 | 2012-09-19 | 塔莱斯公司 | 带有集成热交换器的人造卫星用结构板 |
FR2972714A1 (fr) * | 2011-03-17 | 2012-09-21 | Thales Sa | Panneau structural de satellite avec echangeurs thermiques integres |
CN102941926B (zh) * | 2012-11-06 | 2015-07-08 | 北京空间飞行器总体设计部 | 一种空间碎片防护型热辐射器 |
CN102941926A (zh) * | 2012-11-06 | 2013-02-27 | 北京空间飞行器总体设计部 | 一种空间碎片防护型热辐射器 |
CN103482083A (zh) * | 2013-08-21 | 2014-01-01 | 上海利正卫星应用技术有限公司 | 一种轻量化低热阻辐射器 |
JP2016124535A (ja) * | 2015-01-08 | 2016-07-11 | ザ・ボーイング・カンパニーThe Boeing Company | 宇宙機、及び複合材フェースシートを有する、宇宙機用ラジエータパネル |
EP3042854A1 (de) * | 2015-01-08 | 2016-07-13 | The Boeing Company | Raumfahrzeug und raumfahrzeugradiatorpaneele mit deckschicht aus verbundwerkstoff |
CN105775172A (zh) * | 2015-01-08 | 2016-07-20 | 波音公司 | 飞行器的散热器组、飞行器及装配散热器组的方法 |
US9878808B2 (en) | 2015-01-08 | 2018-01-30 | The Boeing Company | Spacecraft and spacecraft radiator panels with composite face-sheets |
CN105775172B (zh) * | 2015-01-08 | 2018-03-27 | 波音公司 | 飞行器的散热器组、飞行器及装配散热器组的方法 |
EP3620395A1 (de) * | 2015-01-08 | 2020-03-11 | The Boeing Company | Raumfahrzeug und raumfahrzeugradiatorpaneele mit deckblatt aus verbundwerkstoff |
CN106347714A (zh) * | 2016-08-31 | 2017-01-25 | 北京空间飞行器总体设计部 | 一种具备在轨弹抛功能的舱外辐射器防护罩系统 |
CN112284172A (zh) * | 2020-10-29 | 2021-01-29 | 上海卫星装备研究所 | 空间辐射散热器 |
Also Published As
Publication number | Publication date |
---|---|
DE10340092B4 (de) | 2005-09-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OP8 | Request for examination as to paragraph 44 patent law | ||
8364 | No opposition during term of opposition | ||
R073 | Re-establishment requested | ||
R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |
Effective date: 20130301 |
|
R074 | Re-establishment allowed | ||
R074 | Re-establishment allowed |
Effective date: 20131123 Effective date: 20131120 |
|
R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |
Effective date: 20140301 |