The invention provides a rotor, a propeller clamp and an aircraft, and provides the rotor and the aircraft. The rotor provided by the invention comprises a propeller hub and at least two propeller blades, the propeller blades are mounted on the propeller hub and together rotate under driving of a first motor. The propeller hub is provided with sliding channels arranged along the radial direction of the propeller hub, a mounting end of each propeller blade is provided with a sliding rod penetrating through the sliding channel, and elastic bias devices provide the bias pressure for the propeller blades to make the propeller blades close to the axis of the propeller hub. The rotor has an adjustable rotor diameter, the response speed of the rotor on power adjustment is accelerated, and the power adjustable range is increased.


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    Titel :

    Rotor, propeller clamp and aircraft


    Beteiligte:
    HE CHUNWANG (Autor:in)

    Erscheinungsdatum :

    09.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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