Direct air cooling system for airborne electronics

Aeronautics and astronautics – Miscellaneous

Patent

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Details

244117A, 62DIG5, 361383, 361384, B64C 2102

Patent

active

046747044

ABSTRACT:
A direct air cooling system 12 for electronics carried by aircraft. The cooling system provides a submerged air scoop 16 which directs outside air to several electronic modules 14. The air flows through passages 76 in the modules 14 which are adjacent to circuit boards 74, 78 bearing discrete electronic components 88. A foil layer 86 and aluminum fin stock help transfer heat from the electronic components to the directed air. Heated air is then exhausted through exhaust port 24 or 28.

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