Aircraft radome apparatuses and methods are described. In some examples, a radome is to be mounted on an aircraft. In some examples, the radome includes an outer mold line having a closure angle. In some examples, the closure angle is configured to reduce a footprint of the radome. In some examples, the closure angle is also configured to reduce a likelihood of separated airflow from occurring proximate a trailing portion of the radome during a flight of the aircraft. In some examples, the radome is to be mounted on the aircraft at a location that reduces a rate of change of a transverse cross-sectional area of the aircraft.


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    Titel :

    AIRCRAFT RADOME APPARATUSES AND METHODS


    Beteiligte:

    Erscheinungsdatum :

    15.11.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / B64C AEROPLANES , Flugzeuge



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