A rotor or propeller may have rotor blades and a passive pitch angle adjustment apparatus. The passive pitch angle adjustment apparatus may include levers, rods, and central rod. Levers may be connected to rotor blades and rotate them around a respective pitch axis. Rods may be connected to levers and mechanically link levers with each other via central point that is located outside rotor plane. Central rod may connect central point with base point that is located in a longitudinal direction of rotor axis. The passive pitch angle adjustment apparatus may enable a cyclic pitch adjustment of the rotor blades and block a collective pitch adjustment of the rotor blades.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PASSIVE PITCH ANGLE ADJUSTMENT APPARATUS


    Beteiligte:
    SCHMIEDEL PATRIK (Autor:in) / LEITNER HARALD (Autor:in) / KRAUS JULIAN (Autor:in) / DANNEMANN LUDWIG (Autor:in) / KIESEWETTER UWE (Autor:in)

    Erscheinungsdatum :

    2019-08-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Passive pitch angle adjustment apparatus

    SCHMIEDEL PATRIK / LEITNER HARALD / KRAUS JULIAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    A PASSIVE PITCH ANGLE ADJUSTMENT APPARATUS

    SCHMIEDEL PATRIK / LEITNER HARALD / KRAUS JULIAN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    CYCLIC PITCH ANGLE ADJUSTMENT APPARATUS

    CZECH IAN-LUCA | Europäisches Patentamt | 2022

    Freier Zugriff

    Cyclic pitch angle adjustment apparatus

    CZECH IAN-LUCA | Europäisches Patentamt | 2024

    Freier Zugriff

    Periodic pitch angle adjustment apparatus

    CECH JAN-LUC | Europäisches Patentamt | 2022

    Freier Zugriff