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.


    Access

    Download


    Export, share and cite



    Title :

    Rotor, propeller clamp and aircraft


    Contributors:
    HE CHUNWANG (author)

    Publication date :

    2015-12-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft with multi-rotor propeller

    YANG YUN / ZHANG CHI / HUANG CHEN et al. | European Patent Office | 2024

    Free access

    PROPELLER FOR TILT-ROTOR AIRCRAFT

    YAN WENHUI / ZHAO LEI / YAN WENJING et al. | European Patent Office | 2020

    Free access

    Hydraulic propeller tilting rotor aircraft

    DU DINGWEN | European Patent Office | 2015

    Free access

    Propeller for tilt rotor aircraft

    YAN WENHUI / ZHAO LEI / YAN WENJING et al. | European Patent Office | 2020

    Free access

    Four-rotor aircraft with variable propeller wheelbase

    LIU LU / WANG SHENGNAN / FU SEN et al. | European Patent Office | 2023

    Free access