Systems and methods to improve controllability of an aerial vehicle responsive to degraded operational conditions are described. For example, one or more propeller blades of an aerial vehicle may be modifiable between two or more configurations. The configurations may include a low torque configuration suitable for normal operational conditions, and a high torque configuration suitable for degraded operational conditions. Various aspects or portions of a propeller blade may be modified to increase torque generated by the propeller blade due to drag or air resistance. The additional generated torque may then be used as a source of additional torque to improve controllability of the aerial vehicle responsive to degraded operational conditions.


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    Title :

    AERIAL VEHICLE PROPELLERS HAVING VARIABLE FORCE-TORQUE RATIOS


    Additional title:

    LUFTFAHRZEUG-PROPELLER MIT VARIABLEN KRAFT-DREHMOMENT-VERHÄLTNISSEN
    HÉLICES DE VÉHICULE AÉRIEN AYANT DES RAPPORTS FORCE-COUPLE VARIABLES


    Contributors:

    Publication date :

    2024-07-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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