One example of a rotor assembly comprises: a rotor hub operable to rotate based on rotation of a mast; a first rotor blade pivotally attached to the rotor hub; a bracing member pivotally attached to the rotor hub at a first end and pivotally attached to the first rotor blade at a second end; and a linkage mechanism coupling the first rotor blade to a second rotor blade. The bracing member is operable to transfer a coning movement of the first rotor blade to a movement of the linkage mechanism and a corresponding coning movement of the second rotor blade.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ROTOR HUB WITH ENFORCED COLLECTIVE CONING


    Beteiligte:

    Erscheinungsdatum :

    2019-10-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotor hub with enforced collective coning

    CHOI JOUYOUNG JASON / STAMPS FRANK B | Europäisches Patentamt | 2020

    Freier Zugriff


    The role of rotor coning in helicopter proneness to collective bounce

    Muscarello, Vincenzo / Quaranta, Giuseppe / Masarati, Pierangelo | Elsevier | 2014


    Updating and Optimization of a Coning Rotor Concept

    Crawford, Curran / Platts, Jim | AIAA | 2006