A compliant tail structure for a rotorcraft having rotating components and a fuselage. The tail structure includes a tail assembly having first and second oppositely disposed tail members. A tail joint connects the tail assembly to an aft portion of the fuselage. The tail joint includes at least four tail mounts configured to establish a nodding axis for the tail assembly. At least two of the tail mounts are resilient tail mounts that are configured to establish a nodding degree of freedom for the tail assembly relative to the fuselage about the nodding axis, thereby detuning dynamic fuselage responses from excitation frequencies generated by the rotating components.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Compliant Tail Structure for Rotorcraft


    Beteiligte:

    Erscheinungsdatum :

    04.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Compliant tail structure for rotorcraft

    DECKER GEORGE RYAN / BAINES ANDREW G / SAUER FRANK DOUGLAS | Europäisches Patentamt | 2022

    Freier Zugriff

    Compliant tail structure for rotorcraft

    DECKER GEORGE RYAN / BAINES ANDREW G / SAUER FRANK DOUGLAS | Europäisches Patentamt | 2023

    Freier Zugriff

    Compliant Tail Structure for Rotorcraft

    DECKER GEORGE RYAN / BAINES ANDREW G / SAUER FRANK DOUGLAS | Europäisches Patentamt | 2022

    Freier Zugriff

    Rotorcraft tail boom, and a rotorcraft

    LEUSINK DEBBIE / ALFANO DAVID | Europäisches Patentamt | 2021

    Freier Zugriff

    TAIL BOOM OF A ROTORCRAFT AND ROTORCRAFT

    Europäisches Patentamt | 2018

    Freier Zugriff