A rotor comprising a hub and a plurality of lift assemblies. Each lift assembly is connected to two adjacent lift assemblies respectively by a first damper and a second damper. The first damper is hinged to a lift assembly about a first axis, and the second damper is hinged to said lift assembly about a second axis. A first plane contains a lead-lag axis of the lift assembly and orthogonally to the pitch axis of the lift assembly. The first axis is situated in a volume lying between the first plane and an axis of rotation of the rotor, the second axis being positioned outside said volume.


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    Title :

    ROTOR ET AERONEF POURVU D'UN TEL ROTOR


    Additional title:

    A ROTOR AND AN AIRCRAFT PROVIDED WITH SUCH A ROTOR
    ROTOR UND MIT EINEM SOLCHEN ROTOR AUSGESTATTETES LUFTFAHRZEUG


    Contributors:

    Publication date :

    2018-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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