An energy harvester (18), in particular an aircraft (10), comprises a first portion (20), a second portion (22) and an energy storing unit (24). The first portion (20) includes a charge collecting device (26) having an electrical permittivity different to the one of air. The charge collecting device (26) is configured to be exposed to an air flow (A). The second portion (22) is configured to be exposed to air wherein the second portion (22) includes a conductive material. The energy storing unit (24) is electrically connected between the first portion (20) and the second portion (22).


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    Title :

    Energy harvester, aircraft component comprising the energy harvester and an aircraft comprising the energy harvester or the aircraft component


    Additional title:

    Energiesammler, Flugzeugkomponente mit dem Energiesammler und Flugzeug mit dem Energiesammler oder der Flugzeugkomponente
    Collecteur d'énergie, composant d'aéronef comprenant un tel collecteur et aéronef comprenant ledit collecteur ou le composant d'aéronef


    Contributors:

    Publication date :

    2015-06-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02N Elektrische Maschinen, soweit nicht anderweitig vorgesehen , ELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR



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