A rotor assembly for a rotary wing aircraft includes a plurality of rotor blades operably connected to a rotor shaft. Two or more active adaptive devices are located at one or more rotor blades of the plurality of rotor blades. The one or more active adaptive devices are operably connected to an aircraft flight control system such that, when activated, the one or more active adaptive devices change one or more operational characteristics of the rotor assembly. A method of operating a rotor assembly of a rotary wing aircraft includes rotating a plurality of rotor blades about a rotor shaft. Two or more active adaptive devices located at one or more rotor blades of the plurality of rotor blades are activated and change one or more operational characteristics of the rotor assembly.


    Access

    Download


    Export, share and cite



    Title :

    Mission adaptive rotor blade


    Contributors:

    Publication date :

    2016-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Mission-adaptive rotor blade

    GROEN DAVID L | European Patent Office | 2017

    Free access

    Mission-adaptive rotor blade with circulation control

    VAN DER WESTHUIZEN JACOB JOHANNES | European Patent Office | 2017

    Free access

    MISSION-ADAPTIVE ROTOR BLADE WITH CIRCULATION CONTROL

    VAN DER WESTHUIZEN JACOB JOHANNES | European Patent Office | 2016

    Free access

    Adaptive rotor blade

    SCOTT MARK W | European Patent Office | 2019

    Free access

    Adaptive rotor blade for vibration reduction

    Büter, A. / Ehlert, U.C. / Matthias, M. et al. | Tema Archive | 2000