Mechanical-thermal structure suitable for a space environment

Patent metadata

Field	Value
Publication number	US-9841241-B2
Application number	US-201314033211-A
Country	US
Kind code	B2
Filing date	Sep 20, 2013
Priority date	Sep 21, 2012
Publication date	Dec 12, 2017
Grant date	Dec 12, 2017

Abstract

A monolithic mechanical-thermal structure which is suitable for a space environment is provided, in which the structure contains at least one hole. The walls of the hole are lined with filaments. The monolithic mechanical-thermal structure may be made of metal. And a process for manufacturing the structure is also provided.

First claim

The invention claimed is:

1. A system to transfer heat suitable for a space environment, the system comprising:
a monolithic metal mechanical-thermal structure, comprising: at least one hole, said hole comprising walls lined with filaments, the structure and the filaments constituting a single part made of the same material, a filament of the filaments having a first end fixed to the wall and a second end left free, a length of the filament being between 0.2 and 5 mm and a diameter of the filament being between 0.3 and 0.8 mm; and
a pipe inserted in the hole, the filaments being greater in length than a distance separating an outside of the pipe from an inside of the hole, the filaments bending in response to the pipe being inserted into the hole and the filaments contacting the pipe, wherein heat is transmitted from the monolithic metal mechanical-thermal structure via the filaments to the pipe.

2. The system according to claim 1 , in which the filaments are greater in length than a distance separating an outside of the pipe from an inside of the hole, such that the filaments bend when the pipe is introduced.

3. The system according to claim 2 , in which the pipe is a liquid ammonia heat pipe.

4. The system according to claim 1 , in which the pipe is a liquid ammonia heat pipe.

5. The system according to claim 1 , in which the walls comprise between 30 and 100 filaments per square centimeter.

6. The system according to claim 1 , in which a percentage of the wall surface covered with filaments is between 10 and 50%.

7. The system according to claim 1 , in which the mechanical-thermal structure comprises aluminum.

8. The system according to claim 1 , in which the walls are covered with grease, allowing better thermal conduction.

9. A process for producing the system according to claim 1 , further comprising a first stage of manufacturing the mechanical-thermal structure by an additive manufacturing method, a second stage of manufacturing the pipe and a third stage of inserting a heat pipe inside the hole in the mechanical-thermal structure.

10. The process according to claim 9 , in which the pipe is manufactured by an extrusion method.

11. The process according to claim 10 , further comprising a stage of coating the walls of the hole in the mechanical-thermal structure with grease.

12. The process according to claim 9 , further comprising a stage of coating the walls of the hole in the mechanical-thermal structure with grease.

Assignees

• Thales Sa

Inventors

• Chaix Alain
• Legrand Silvain
• Masse Christian

Classifications

• B64G1/503

  Radiator panels · CPC title

• B23P15/26

  heat exchangers {or the like (making heat exchangers by methods covered by other subclasses B21D53/02)} · CPC title

• F28F23/00

  Features relating to the use of intermediate heat-exchange materials, e.g. selection of compositions (heat-transfer, heat-exchange or heat-storage materials C09K5/00) · CPC title

• F28D15/02 Primary

  in which the medium condenses and evaporates, e.g. heat pipes {(heat pipes used in solar heat collectors F24S10/95; in radiators F28D1/0226; in nuclear reactors G21C15/257)} · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title