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.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT FEEDER COOLING


    Contributors:

    Publication date :

    2021-08-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS



    AIRCRAFT FEEDER COOLING

    BELLIS ANDREW DAVID | European Patent Office | 2023

    Free access

    FASTENER FEEDER FOR AIRCRAFT

    European Patent Office | 2020

    Free access

    FASTENER FEEDER FOR AIRCRAFT

    LEE YOUNG ROK | European Patent Office | 2020

    Free access

    MPC-75 Feeder Civil Aircraft

    K. Ming | NTIS | 1988


    Aircraft feeder cable system with thermoelectric cooler

    BELLIS ANDREW DAVID | European Patent Office | 2022

    Free access