An aircraft radome includes a composite structure including, or according to the circumstances configured to define, at least one housing extending along the radome from a base of the radome. The housing receives an electrically conductive strip in contact with an inner surface of an outer wall, or according to the circumstances flush with the outer wall, of the composite structure. A conductive base is situated in the region of the radome base and connected to a ground of the aircraft. The composite structure of the radome is devoid of any perforations or through-passages in the region of the electrically conductive strip, and a first end of the electrically conductive strip is in contact with the conductive base.


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    Titel :

    AIRCRAFT RADOME INCORPORATING A LIGHTNING PROTECTION SYSTEM, AND AIRCRAFT COMPRISING SUCH A RADOME


    Beteiligte:

    Erscheinungsdatum :

    19.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS



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