Disclosed is an aircraft having an aircraft electric motor; a motor controller; a structure having ribs and spars defining a wingbox of the aircraft; a feeder cable connecting the motor controller and the aircraft electric motor through the wingbox; and a grommet defining an orifice by an inner perimeter sized to receive the feeder cable, the passage housing a thermoelectric cooler having a cooled side thermally conductive with the inner perimeter at a thermal conductivity greater than 100 watts per meter-kelvin at one ° C. and a heated side thermally conductive with the structure at the thermal conductivity.
AIRCRAFT FEEDER COOLING
12.08.2021
Patent
Elektronische Ressource
Englisch
NTIS | 1988
|Aircraft feeder cable system with thermoelectric cooler
Europäisches Patentamt | 2022
|