An aerodynamic friction energy deicing system (100) can include a heat energy device (101) configured to be operatively connected to an aircraft structure (103) and to convert heat energy due to aerodynamic friction on the aircraft structure into another form or to store heat energy due to aerodynamic friction on the aircraft structure. The converted or stored energy can be used for any suitable purpose, e.g., for use in ice prevention and/or deicing and/or powering one or more aircraft systems.


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    Title :

    FRICTION ENERGY SAVERS


    Additional title:

    REIBUNGSENERGIEEINSPARER
    ÉCONOMISEURS D'ÉNERGIE DE FRICTION


    Contributors:

    Publication date :

    2020-12-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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