The present embodiments relate to an aircraft 100 with an aircraft structure that comprises a radome cover opening kinematic 200 and a radome cover shell 112 that is adapted to enclose equipment 115 in a nose region 110 of the aircraft 100 in a closed position. The radome cover opening kinematic 200 may enable movements of the radome cover shell 112 between the closed position and an opened position and vice versa. The radome cover opening kinematic 200 may include a guiding rail 210 that is attached to the radome cover shell 112, and at least three rollers 230 that are attached to the aircraft structure 103, wherein a first and a second roller 230a, 230b are arranged on opposing sides of the guiding rail 210, and wherein the second and a third roller 230b, 230c are arranged on the same side of the guiding rail 210.


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    Title :

    A RADOME COVER SHELL AND OPENING KINEMATIC


    Additional title:

    RADOMABDECKHAUBE UND ÖFFNUNGSKINEMATIK
    COQUE DE RADÔME ET CINÉMATIQUE D'OUVERTURE


    Contributors:
    BOEHME JAN (author) / LE CADET YANN (author) / LAZAK MARTIN (author)

    Publication date :

    2022-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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