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.


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    Title :

    AIRCRAFT FEEDER COOLING


    Additional title:

    ZULEITUNGSKÜHLUNG EINES FLUGZEUGS
    REFROIDISSEMENT DE DISPOSITIF D'ALIMENTATION D'AÉRONEF


    Contributors:

    Publication date :

    2023-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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