Control systems (20) for a rotorcraft (1) are provided, the rotorcraft (1) including main rotor (5) and auxiliary propulsor assemblies (6). the main rotor assembly (1) including first (50) and second (51) rotors disposed to oppositely rotate relative to an airframe (2) about a same rotational axis (RA), and sensors (30) disposed to generate hub moment, tip clearance and lift offset data of the main rotor assembly (5).


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    Title :

    LIFT OFFSET MANAGEMENT AND CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT


    Additional title:

    LIFT-OFFSET MANAGEMENT UND STEUERUNGSSYSTEME FÜR KOAXIALE HUBSCHRAUBER
    GESTION DE DÉCALAGE DE LEVAGE ET SYSTÈMES DE COMMANDE POUR GIRAVION COAXIAL


    Contributors:
    WULFF OLE (author) / GEIGER DEREK (author)

    Publication date :

    2018-10-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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