Lift offset management and control systems are provided for a rotorcraft including main rotor and auxiliary propulsor assemblies, the main rotor assembly including first and second rotors disposed to oppositely rotate relative to an airframe about a same rotational axis, and sensors disposed to generate hub moment, tip clearance and lift offset data of the main rotor assembly.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Lift offset management and control systems for coaxial rotorcraft


    Beteiligte:
    WULFF OLE (Autor:in) / GEIGER DEREK (Autor:in)

    Erscheinungsdatum :

    2017-09-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    LIFT OFFSET MANAGEMENT AND CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT

    WULFF OLE / GEIGER DEREK | Europäisches Patentamt | 2018

    Freier Zugriff

    LIFT OFFSET MANAGEMENT AND CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT

    WULFF OLE / GEIGER DEREK | Europäisches Patentamt | 2016

    Freier Zugriff

    Modeling and control of lift offset coaxial and tiltrotor rotorcraft

    Berger, Tom / Juhasz, Ondrej / Lopez, Mark J. S. et al. | Online Contents | 2019


    Modeling and control of lift offset coaxial and tiltrotor rotorcraft

    Berger, Tom / Juhasz, Ondrej / Lopez, Mark J. S. et al. | Springer Verlag | 2020


    Rotorcraft Comprehensive Analysis Calculations of a Coaxial Rotor with Lift Offset

    Ho, Jimmy / Yeo, Hyeonsoo | British Library Conference Proceedings | 2018