An electric power generation system employs a thermoelectric generator placed between an aircraft inner skin and an aircraft outer skin. The thermoelectric generator is configured to utilize a thermal differential between the inner and outer skin to generate an electric current. An electrical interface is provided for access to the electric current generated by said thermoelectric generator.


    Access

    Download


    Export, share and cite



    Title :

    POWERING AIRCRAFT SENSORS USING THERMAL CAPACITORS


    Additional title:

    STROMVERSORGUNG VON FLUGZEUGSENSOREN MITHILFE THERMISCHER KONDENSATOREN
    CAPTEURS D'ALIMENTATION D'AÉRONEF UTILISANT DES CONDENSATEURS THERMIQUES


    Contributors:

    Publication date :

    2019-06-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H10N / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    POWERING AIRCRAFT SENSORS USING THERMAL CAPACITORS

    HILLER NATHAN D | European Patent Office | 2017

    Free access


    THERMAL ANALYSIS FOR HYDRAULIC POWERING SYSTEM OF A CERTAIN TYPE AIRCRAFT

    Si, Wu / Hualong, Yang / Dingbang, Han et al. | TIBKAT | 2018


    System and method for remotely powering aircraft

    FRANCOIS-XAVIER FILLIAT | European Patent Office | 2022

    Free access