Disclosed is an aircraft having an aircraft electric motor (114); a motor controller (110); a structure having ribs (108) and spars (106) defining a wingbox (104) of the aircraft; a feeder cable (112) connecting the motor controller and the aircraft electric motor through the wingbox; and a grommet (342) defining an orifice by an inner perimeter sized to receive the feeder cable, the passage (116) housing a thermoelectric cooler (320) having a cooled side (318) thermally conductive with the inner perimeter at a thermal conductivity greater than 100 watts per meter-kelvin at one °C and a heated side (316) thermally conductive with the structure at the thermal conductivity.
AIRCRAFT FEEDER COOLING
ZULEITUNGSKÜHLUNG EINES FLUGZEUGS
REFROIDISSEMENT DE DISPOSITIF D'ALIMENTATION D'AÉRONEF
2023-06-28
Patent
Electronic Resource
English
NTIS | 1988
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