A rotor assembly for a rotary wing aircraft includes a rotor hub having a central axis, the rotor hub rotatable about the central axis. A plurality of flexible structural members extend radially outwardly from the rotor hub, each flexible structural member substantially U-shaped and having a first arm extending from the hub, a second arm extending from the hub, and an end portion connecting the first arm to the second arm at a radially outboard end of the flexible structural member. A clamp member is positioned between the first arm and the second arm of each structural member and secured thereto to tie deflection of the first arm to deflection of the second arm. A rotor blade is secured to each flexible structural member of the plurality of flexible structural members via the clamp member.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FLEX BEAM CLAMP FOR ROTOR ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    18.05.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    FLEX BEAM CLAMP FOR ROTOR ASSEMBLY

    NUSSENBLATT ERIC LUCIEN / HUNTER DAVID H / THOMAS JUSTIN | Europäisches Patentamt | 2015

    Freier Zugriff

    Flex beam clamp for rotor assembly

    NUSSENBLATT ERIC LUCIEN / HUNTER DAVID H / THOMAS JUSTIN | Europäisches Patentamt | 2020

    Freier Zugriff

    Flex beam for rotor assembly

    NUSSENBLATT ERIC LUCIEN / HUNTER DAVID H | Europäisches Patentamt | 2020

    Freier Zugriff

    FLEX BEAM FOR ROTOR ASSEMBLY

    NUSSENBLATT ERIC LUCIEN / HUNTER DAVID H | Europäisches Patentamt | 2020

    Freier Zugriff

    FLEX BEAM FOR ROTOR ASSEMBLY

    NUSSENBLATT ERIC LUCIEN / HUNTER DAVID H | Europäisches Patentamt | 2016

    Freier Zugriff