An aircraft wing element comprises two temperature sensors that are situated on each side of an electrothermal mat, between a structure portion and a shield of said wing element. A shield temperature can be measured more accurately, and a thermal energy flow that is transferred to the shield can be evaluated.


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    Titel :

    AIRCRAFT WING ELEMENT


    Beteiligte:
    LE GARREC STÉPHANE (Autor:in) / PORTIER PHILIPPE (Autor:in) / BURON MARTIAL (Autor:in) / DELEHELLE ADAO (Autor:in)

    Erscheinungsdatum :

    2016-06-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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