A windshield (10) of an aircraft (1) of the present invention includes a conductive member (21, 22, 23, 26, 27, 28) that is configured to generate heat when a current is supplied. The conductive member (21, 22, 23, 26, 27, 28) is oriented in a lateral direction (DH) that is a horizontal direction included in an in-plane direction of the windshield (10).


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    Titel :

    WINDSHIELD OF AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2016-08-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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