Aircraft radome apparatuses and methods are described. In some examples, a radome (102) is to be mounted on an aircraft (100). In some examples, the radome (102) includes an outer mold line (304) having a closure angle (316). In some examples, the closure angle (316) is configured to reduce a footprint of the radome (102). In some examples, the closure angle (316) is also configured to reduce a likelihood of separated airflow from occurring proximate a trailing portion (306) of the radome (102) during a flight of the aircraft (100). In some examples, the radome (102) is to be mounted on the aircraft (100) at a location that reduces a rate of change of a transverse cross-sectional area of the aircraft (100).


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    Title :

    AIRCRAFT RADOME APPARATUSES AND METHODS


    Additional title:

    FLUGZEUGRADOMVORRICHTUNGEN UND -VERFAHREN
    APPAREILS ET PROCÉDÉS DE RADÔME D'AÉRONEF


    Contributors:

    Publication date :

    2021-05-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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