FR2452078A1 - Radiator for heat rejection cooling - has parallel heat carrying ducts cross connected by others for balancing - Google Patents
Radiator for heat rejection cooling - has parallel heat carrying ducts cross connected by others for balancingInfo
- Publication number
- FR2452078A1 FR2452078A1 FR7907315A FR7907315A FR2452078A1 FR 2452078 A1 FR2452078 A1 FR 2452078A1 FR 7907315 A FR7907315 A FR 7907315A FR 7907315 A FR7907315 A FR 7907315A FR 2452078 A1 FR2452078 A1 FR 2452078A1
- Authority
- FR
- France
- Prior art keywords
- heat
- balancing
- radiator
- cross connected
- connectors
- 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
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
- F28D15/04—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 tubes having a capillary structure
-
- 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)
- Sustainable Development (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Biodiversity & Conservation Biology (AREA)
- Health & Medical Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Environmental Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Duct Arrangements (AREA)
Abstract
The radiator disposes of heat from a heat source (4,5). It has, fixed to a support, heat ducts (6,7) joined thermally by heat connectors. The connectors are fixed to one support face to be in contact with the heat source. The connectors are auxiliary ducts (8), in contact with the others. The main heat ductwork does the heat transfer and the auxiliary is for balancing only between parts of the main ductwork. There can be several main ductworks and a single auxiliary one joining them at right angles.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7907315A FR2452078A1 (en) | 1979-03-22 | 1979-03-22 | Radiator for heat rejection cooling - has parallel heat carrying ducts cross connected by others for balancing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7907315A FR2452078A1 (en) | 1979-03-22 | 1979-03-22 | Radiator for heat rejection cooling - has parallel heat carrying ducts cross connected by others for balancing |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2452078A1 true FR2452078A1 (en) | 1980-10-17 |
FR2452078B3 FR2452078B3 (en) | 1981-11-27 |
Family
ID=9223466
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7907315A Granted FR2452078A1 (en) | 1979-03-22 | 1979-03-22 | Radiator for heat rejection cooling - has parallel heat carrying ducts cross connected by others for balancing |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2452078A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5372183A (en) * | 1991-08-22 | 1994-12-13 | Strickberger; Harold P. | Thermal control arrangements for a geosynchronous spacecraft |
US5506032A (en) * | 1994-04-08 | 1996-04-09 | Martin Marietta Corporation | Structural panel having integral heat pipe network |
FR2735565A1 (en) * | 1995-06-13 | 1996-12-20 | Aerospatiale | Heat transmitter for satellite panel in composite material |
US6481670B1 (en) * | 2000-10-20 | 2002-11-19 | Bigelow Aerospace Division, Llc | Apparatus for spacecraft thermal management |
CN114993084A (en) * | 2022-05-31 | 2022-09-02 | 浙江陆博储能技术有限公司 | Array type waste heat recovery unit, device and heat exchange system |
-
1979
- 1979-03-22 FR FR7907315A patent/FR2452078A1/en active Granted
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5372183A (en) * | 1991-08-22 | 1994-12-13 | Strickberger; Harold P. | Thermal control arrangements for a geosynchronous spacecraft |
US5506032A (en) * | 1994-04-08 | 1996-04-09 | Martin Marietta Corporation | Structural panel having integral heat pipe network |
FR2735565A1 (en) * | 1995-06-13 | 1996-12-20 | Aerospatiale | Heat transmitter for satellite panel in composite material |
US6481670B1 (en) * | 2000-10-20 | 2002-11-19 | Bigelow Aerospace Division, Llc | Apparatus for spacecraft thermal management |
CN114993084A (en) * | 2022-05-31 | 2022-09-02 | 浙江陆博储能技术有限公司 | Array type waste heat recovery unit, device and heat exchange system |
Also Published As
Publication number | Publication date |
---|---|
FR2452078B3 (en) | 1981-11-27 |
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