US2015241144A1PendingUtilityA1

Thermal regulation system for at least one electronic module embedded onboard an aircraft

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Assignee: THALES SAPriority: Feb 21, 2014Filed: Feb 18, 2015Published: Aug 27, 2015
Est. expiryFeb 21, 2034(~7.6 yrs left)· nominal 20-yr term from priority
Inventors:Claude SarnoPhilippe OconteRomain Hodot
H05K 7/20681F28D 1/02F28F 9/007H05K 7/20645
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Claims

Abstract

Heat regulation system ( 1 ) for at least one equipment item ( 2 ) embedded onboard an aircraft, includes a thermal regulation circuit ( 5 ) connected to the equipment item(s) ( 2 ). The thermal regulation circuit ( 5 ) includes a modular thermal regulation device ( 6 ) adapted to receive a modifiable number of thermal regulation modules ( 8 ).

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . Thermal regulation system for at least one equipment item embedded onboard an aircraft, comprising:
 a thermal regulation circuit external to said equipment item(s) and connected to said equipment item(s), said thermal regulation circuit comprising a modular thermal regulation device adapted to receive a modifiable number of thermal regulation modules of different kinds, the modular thermal regulation device comprising a frame adapted to receive a modifiable number of thermal regulation modules; and   said thermal regulation circuit comprising at least one thermal connector connected to an embedded electronic module.   
     
     
         2 . System according to  claim 1 , in which the equipment item(s) comprise at least one electronic module. 
     
     
         3 . System according to  claim 2 , in which said thermal regulation circuit comprises a two-phase heat transfer fluid. 
     
     
         4 . System according to  claim 3 , in which at least one thermal regulation module comprises at least one condenser. 
     
     
         5 . System according to  claim 2 , in which said thermal regulation circuit comprises a heat transfer fluid. 
     
     
         6 . System according to  claim 5 , in which at least one thermal regulation module comprises at least one pump. 
     
     
         7 . System according to  claim 5 , in which at least one thermal regulation module comprises at least one compressor. 
     
     
         8 . System according to  claim 2 , in which said thermal regulation circuit comprises air as heat transfer fluid. 
     
     
         9 . System according to  claim 8 , in which at least one thermal regulation module comprises at least one fan. 
     
     
         10 . System according to  claim 1 , comprising at least one frame adapted to receive a modifiable number of embedded electronic modules. 
     
     
         11 . System according to  claim 1 , in which said thermal regulation circuit comprises a two-phase heat transfer fluid. 
     
     
         12 . System according to  claim 11 , in which at least one thermal regulation module comprises at least one condenser. 
     
     
         13 . System according to  claim 1 , in which said thermal regulation circuit comprises a heat transfer fluid. 
     
     
         14 . System according to  claim 13 , in which at least one thermal regulation module comprises at least one pump. 
     
     
         15 . System according to  claim 13 , in which at least one thermal regulation module comprises at least one compressor. 
     
     
         16 . System according to  claim 1 , in which said thermal regulation circuit comprises air as heat transfer fluid. 
     
     
         17 . System according to  claim 16 , in which at least one thermal regulation module comprises at least one fan. 
     
     
         18 . Aircraft comprising the thermal regulation system according to  claim 1 . 
     
     
         19 . Aircraft according to  claim 18 , in which said thermal regulation circuit comprises a heat transfer fluid. 
     
     
         20 . Aircraft according to  claim 18 , in which said thermal regulation circuit comprises air as heat transfer fluid.

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