Heat exchange device for artificial satellite, wall and assembly of walls comprising such a heat exchange device

• US 10,677,533 B2
• Filed: 11/16/2016
• Issued: 06/09/2020
• Est. Priority Date: 11/16/2015
• Status: Active Grant

• Current Assignee: Airbus Defence and Space GmbH
• Original Assignee: Airbus Defence and Space GmbH
• Inventors: Flemin, Christian, Coquard, Typhaine, Walker, Andrew
• Primary Examiner(s): Raymond, Keith M
• Assistant Examiner(s): Jones, Gordon A
• Application Number:
  US15/772,444
• Publication Number:
  US 20180320983A1
• Time in Patent Office: 1,301 Days
• CPC Class Codes: B64G 1/503 Radiator panels
• CPC Class Codes: B64G 1/506 Heat pipes
• CPC Class Codes: F28D 15/0233 the conduits having a particular shape, e.g. non-circular cross-section, annular F28D15/0241, F28D15/0266 take precedence
• CPC Class Codes: F28D 15/0275 Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
• CPC Class Codes: F28D 15/04 with tubes having a capillary structure
• CPC Class Codes: F28D 2021/0021 for aircrafts or cosmonautics air-treatment for aircraft B64D13/00, temperature control of cosmonautic vehicles B64G1/50
• CPC Class Codes: F28F 13/00 Arrangements for modifying heat-transfer, e.g. increasing, decreasing F28F1/00 - F28F11/00 take precedence
• CPC Class Codes: F28F 7/02 Blocks traversed by passages for heat-exchange media F28D7/0008 takes precedence

Abstract

Disclosed is a heat exchange device for effecting a heat exchange between a heat transfer fluid of a first network of capillary heat pipes and a heat transfer fluid of a second network of capillary heat pipes. The heat exchange device includes a solid block provided with a first channel and a second channel which are independent of one another, the first channel having at least one opening intended to be connected to a capillary heat pipe of the first network, the second channel having at least one opening intended to be connected to a capillary heat pipe of the second network, the first channel having a portion which lies near a portion of the second channel such that the heat transfer fluid of the first network is able to exchange heat with the heat transfer fluid of the second network via the heat exchanging portions.

Claims

1. A wall configured to be mounted in an artificial satellite, the wall comprising:

a support panel; and

at least one heat exchange device supported by the support panel, the at least one heat exchange device comprising;

first capillary heat pipes containing a first heat transfer fluid, the first capillary heat pipes forming a first network,

second capillary heat pipes containing a second heat transfer fluid, the second capillary heat pipes forming a second network, and

a solid block provided with a first channel and a second channel independent of the first channel, each of the first channel and the second channel having a capillary internal structure, the capillary internal structure being formed directly on the first channel and the second channel of the solid block,

the first channel having

at least one first opening connected to one of the first capillary heat pipes of the first network, and

at least one first side channel having a longitudinal length extending perpendicularly in a direction through the solid block toward the second channel, and

the second channel having

at least one second opening connected to one of the second capillary heat pipes of the second network, and

at least one second side channel having a longitudinal length extending perpendicularly in a direction through the solid block toward the first channel,

the at least one first side channel of the first channel lying near the at least one second side channel of the second channel such that the first heat transfer fluid is able to exchange heat with the second heat transfer fluid via said at least one first side channel and the at least one second side channel,

wherein the solid block is void of space, except for the first and second channels.

2. The wall according to claim 1, wherein the at least one first side channel has a closed terminal end, the at least one second side channel has a closed terminal end, said at least one first side channel extending parallel and adjacent to said at least one second side channel.

3. The wall according to claim 1, wherein the first channel comprises an additional first opening connected to another one of the first capillary heat pipes of the first network and the second channel comprises an additional second opening connected to another one of the second capillary heat pipes of the second network.

4. The wall according to claim 3, wherein said at least one first opening is located on a first face of said solid block, and said additional first opening is located on a second face of said solid block, said first face being perpendicular to said second face.

5. The wall according to claim 3, wherein said at least one first opening is located on a first face of said solid block, and said additional first opening is located on a second face of said solid block, said first face being parallel to said second face.

6. The wall according to claim 1, wherein the at least one first side channel is located at a distance of between 1 millimeter and 3 millimeters from the at least one second side channel.

7. The wall according to claim 1, wherein said solid block comprises a bearing face configured to be fixed to a panel of the artificial satellite, and the first channel and second channel are arranged in one and the same plane, said plane being parallel to said bearing face.

8. The wall according to claim 1, wherein said solid block comprises a bearing face configured to be fixed to a panel of the artificial satellite, and the first channel and second channel are arranged in two separate planes, said planes being parallel to said bearing face.

9. The wall according to claim 1, wherein said solid block comprises a bearing face configured to be fixed to a panel of the artificial satellite, the first channel and second channel respectively comprising the at least one first side channel and the at least one second side channel as a first cavity and a second cavity which each extend in a plane parallel to said bearing face.

15. The wall according to claim 1, wherein the solid block is made in one piece.

10. A wall configured for mounting in an artificial satellite, said wall comprising:

a support panel;

at least one heat exchange device supported by said support panel, the at least one heat exchange device comprising

first capillary heat pipes containing a first heat transfer fluid, the first capillary heat pipes forming a first network,

second capillary heat pipes containing a second heat transfer fluid, the second capillary heat pipes forming a second network, and

a solid block provided with a first channel and a second channel independent of the first channel, each of the first channel and the second channel having a capillary internal structure, the capillary internal structure being formed directly on the first channel and the second channel of the solid block,

the first channel having

at least one first opening connected to one of the first capillary heat pipes of the first network, and

a first side channel having a longitudinal length extending perpendicularly in a direction through the solid block toward the second channel, and

the second channel having

at least one second opening connected to one of the second capillary heat pipes of the second network, and

a second side channel having a longitudinal length extending perpendicularly in a direction through the solid block toward the first channel,

the first side channel of the first channel lying near the second side channel of the second channel such that the first heat transfer fluid is able to exchange heat with the second heat transfer fluid via the first side channel and the second side channel,

wherein the solid block is void of space, except for the first and second channels, and

the first channel having two openings to the exterior including the at least one first opening, the second channel having two openings to the exterior including the at least one second opening, the first channel of the at least one heat exchange device being connected to the first capillary heat pipes, the second channel of the at least one heat exchange device being connected to the second capillary heat pipes.

11. The wall according to claim 10, further comprising at least one electronic device fixed to said support panel, in direct or indirect thermal contact with said at least one heat exchange device.

12. The wall according to claim 10, further comprising angles,

wherein the first capillary heat pipes are fixed to said angles to form a comb-shaped configuration.

13. The wall according to claim 10, further comprising angles,

wherein the first capillary heat pipes are fixed to said angles to form an S-shaped configuration.

14. The wall according to claim 10, further comprising angles,

wherein the first capillary heat pipes are fixed to said angles to form a matrix-shaped configuration.