An energy harvester for an aircraft comprises a first portion, a second portion and an energy storing unit. The first portion includes a charge collecting device having an electrical permittivity different to the one of air. The charge collecting device is configured to be exposed to an air flow. The second portion is configured to be exposed to air and includes a conductive material. The energy storing unit is electrically connected between the first portion and the second portion.


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    Title :

    ENERGY HARVESTER, AIRCRAFT COMPONENT COMPRISING THE ENERGY HARVESTER AND AN AIRCRAFT COMPRISING THE ENERGY HARVESTER OR THE AIRCRAFT COMPONENT


    Contributors:

    Publication date :

    2015-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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