The present invention provides a windshield (10) of an aircraft, including a plurality of conductive members (21, 22, 23) that are disposed along an in-plane direction of the windshield (10), and are wire-connected together, wherein the plurality of conductive members (21, 22, 23) are heaters that generate heat when supplied with an alternating current, and the conductive members (21, 22, 23) are wire-connected such that induced currents induced in the respective conductive members (21, 22, 23) by a magnetic field in association with a lightning current are circulated between the conductive members (21, 22, 23).


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    Title :

    WINDSHIELD OF AIRCRAFT


    Additional title:

    WINDSCHUTZSCHEIBE EINES FLUGZEUGS
    PARE-BRISE D'AÉRONEF


    Contributors:

    Publication date :

    2018-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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