An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail.


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    Title :

    RADOME COVER SHELL AND OPENING KINEMATIC


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

    Publication date :

    2022-04-28


    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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    BOEHME JAN / LE CADET YANN / LAZAK MARTIN | European Patent Office | 2022

    Free access