FR2735565B1 - COMPOSITE MATERIAL HEATER IN PARTICULAR FOR A SATELLITE PANEL AND METHOD FOR MANUFACTURING THE SAME - Google Patents
COMPOSITE MATERIAL HEATER IN PARTICULAR FOR A SATELLITE PANEL AND METHOD FOR MANUFACTURING THE SAMEInfo
- Publication number
- FR2735565B1 FR2735565B1 FR9506962A FR9506962A FR2735565B1 FR 2735565 B1 FR2735565 B1 FR 2735565B1 FR 9506962 A FR9506962 A FR 9506962A FR 9506962 A FR9506962 A FR 9506962A FR 2735565 B1 FR2735565 B1 FR 2735565B1
- Authority
- FR
- France
- Prior art keywords
- composite material
- tube
- manufacturing
- same
- material heater
- 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.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
-
- 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
-
- 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
- F28D15/0233—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 the conduits having a particular shape, e.g. non-circular cross-section, annular
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F2013/005—Thermal joints
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
The heat transmitter includes a thermal joint (3) which forms an interface between an aluminium tube (1) and a girder (7, 9). The joint is made in advance and put around the tube without overlapping. The ends of mandrels (6) are covered with a layer (7) of composite material and pushed against the metal tube. Two plates are then placed on either side of the H-structure and an opposing pressure is applied to ensure polymerisation. The thermal joint is made by spreading out the substance on a sheet to obtain the required dimensions and to polymerise it. The mandrels used are shaped to correspond to the cross-section of the central tube.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9506962A FR2735565B1 (en) | 1995-06-13 | 1995-06-13 | COMPOSITE MATERIAL HEATER IN PARTICULAR FOR A SATELLITE PANEL AND METHOD FOR MANUFACTURING THE SAME |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9506962A FR2735565B1 (en) | 1995-06-13 | 1995-06-13 | COMPOSITE MATERIAL HEATER IN PARTICULAR FOR A SATELLITE PANEL AND METHOD FOR MANUFACTURING THE SAME |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2735565A1 FR2735565A1 (en) | 1996-12-20 |
FR2735565B1 true FR2735565B1 (en) | 1997-08-22 |
Family
ID=9479893
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9506962A Expired - Fee Related FR2735565B1 (en) | 1995-06-13 | 1995-06-13 | COMPOSITE MATERIAL HEATER IN PARTICULAR FOR A SATELLITE PANEL AND METHOD FOR MANUFACTURING THE SAME |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2735565B1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2776763B1 (en) | 1998-03-30 | 2000-07-21 | Atmostat Etudes Et Rech | THERMAL EXCHANGE DEVICE WITH ACTIVE BIPHASIC FLUID AND METHOD FOR MANUFACTURING SUCH A DEVICE |
FR2803908B1 (en) | 2000-01-13 | 2002-08-23 | Atmostat Etudes Et Rech S | METHOD FOR MANUFACTURING THERMAL TRANSFER DEVICES AND DEVICES OBTAINED THEREBY |
US6843308B1 (en) | 2000-12-01 | 2005-01-18 | Atmostat Etudes Et Recherches | Heat exchanger device using a two-phase active fluid, and a method of manufacturing such a device |
FR3089957B1 (en) * | 2018-12-18 | 2020-12-18 | Airbus Defence & Space Sas | Method of fixing dissipative equipment, space vehicle wall and space vehicle |
CN116021838A (en) * | 2022-12-08 | 2023-04-28 | 上海复合材料科技有限公司 | Flexible connection structure of embedded heat pipe and preparation method thereof |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1040560B (en) * | 1973-12-24 | 1979-12-20 | Dornier System Gmbh | DEVICE FOR THE TRANSFORMATION OF ENERGY ABSORBED ENERGY RESPECTIVELY EMITTED |
FR2452078A1 (en) * | 1979-03-22 | 1980-10-17 | Aerospatiale | Radiator for heat rejection cooling - has parallel heat carrying ducts cross connected by others for balancing |
DE3768564D1 (en) * | 1986-06-16 | 1991-04-18 | Lorraine Carbone | THERMAL CONNECTION WITH STRONG TRANSFER COEFFICIENT AND USES FOR COOLING AN ARRANGEMENT SUBJECT TO AN INTENSIVE THERMAL FLOW. |
US4838346A (en) * | 1988-08-29 | 1989-06-13 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Reusable high-temperature heat pipes and heat pipe panels |
US5069274A (en) * | 1989-12-22 | 1991-12-03 | Grumman Aerospace Corporation | Spacecraft radiator system |
-
1995
- 1995-06-13 FR FR9506962A patent/FR2735565B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2735565A1 (en) | 1996-12-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |