A rotor (8a) comprises at least two rotor blades (10), and each rotor blade (10) of the at least two rotor blades (10) rotates around a rotor axis (Y) and performs pitching around a pitch axis (X). The rotor axis (Y) and the pitch axis (X) intersect in a rotor center (P0). The rotor (8a) is characterized in that each rotor blade (10) comprises at least one permanent magnet (25) having a first spherical magnet surface (19). Each rotor blade (10) further comprises a pitch control apparatus (20) for controlling the pitching of the at least two rotor blades (10). The pitch control apparatus (20) comprises electrically controlled magnets (24) having a second spherical magnet surface (15).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    A ROTOR WITH PITCH CONTROL APPARATUS


    Weitere Titelangaben:

    ROTOR MIT BLATTVERSTELLUNGSVORRICHTUNG
    ROTOR À APPAREIL DE COMMANDE DE PAS


    Beteiligte:
    RIES TOBIAS (Autor:in)

    Erscheinungsdatum :

    2022-12-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ROTOR WITH PITCH CONTROL APPARATUS

    RIES TOBIAS | Europäisches Patentamt | 2021

    Freier Zugriff

    Rotor with pitch control apparatus

    RIES TOBIAS | Europäisches Patentamt | 2022

    Freier Zugriff

    A ROTOR WITH PITCH CONTROL APPARATUS

    RIES TOBIAS | Europäisches Patentamt | 2021

    Freier Zugriff

    Rotor blade pitch trajectory control

    BERGER THOMAS KARL / MILANES DAVID WADE / ROBERTSON JAMES STEWART | Europäisches Patentamt | 2023

    Freier Zugriff

    Rotor Blade Pitch Trajectory Control

    BERGER THOMAS KARL / MILANES DAVID WADE / ROBERTSON JAMES STEWART | Europäisches Patentamt | 2023

    Freier Zugriff