A lead-lag damper for a rotor assembly has a body mounted to either an inboard portion of a blade assembly or a fixed portion of the rotor assembly. A piston carried within the body is configured to allow for relative motion between the body and the piston. The piston defines opposing chambers within the body, the chambers being in fluid communication through a fluid passage. A link connects the piston to the other of the inboard portion of the blade assembly and the fixed portion of the rotor assembly, and the link engages a central portion of the piston. The piston acts on fluid in the chambers during relative motion between the piston and the body and causes fluid flow between the chambers through the fluid passage. Flow through the passage acts to damp lead-lag motion of the blade assembly relative to the fixed portion of the rotor assembly.


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    Titel :

    LEAD-LAG DAMPER FOR ROTOR HUBS


    Weitere Titelangaben:

    AMORTISSEUR DE TRAINEE POUR MOYEUX DE ROTOR


    Beteiligte:
    STAMPS FRANK B (Autor:in) / BRASWELL JAMES L (Autor:in) / HAYNIE DAVID A (Autor:in) / YUCE MITHAT (Autor:in)

    Erscheinungsdatum :

    24.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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