A vibration isolation system (208) for an advancing blade concept rotorcraft (200) having a pylon assembly (202) and an airframe (222). The vibration isolation system (208) includes one or more pylon links (210; 212) each having first and second ends with the first end (214; 216) coupled to the pylon assembly (202) and the second end (218; 220) coupled to the airframe (22). Each pylon link (210; 212) includes a vibration isolator (228; 230), such as a Liquid Inertia Vibration Eliminator unit (232), that is interposed between the pylon assembly (202) and the airframe (222). The vibration isolator system (208) is operable to reduce or eliminate transmission of the pylon assembly (202) vibration to the airframe (222).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ADVANCING BLADE CONCEPT ROTORCRAFT WITH A VIBRATION ISOLATION SYSTEM


    Weitere Titelangaben:

    "ADVANCING BLADE CONCEPT ROTORCRAFT" MIT EINEM SCHWINGUNGSISOLATIONSSYSTEM
    "ADVANCING BLADE CONCEPT ROTORCRAFT" AVEC UN SYSTÈME D'ISOLATION DE VIBRATIONS



    Erscheinungsdatum :

    10.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Vibration isolation systems for advancing blade concept rotorcraft

    FOSKEY CHRISTOPHER EDWARD / STAMPS FRANK BRADLEY / SMITH MICHAEL REAUGH | Europäisches Patentamt | 2022

    Freier Zugriff

    Vibration Isolation Systems for Advancing Blade Concept Rotorcraft

    FOSKEY CHRISTOPHER EDWARD / STAMPS FRANK BRADLEY / SMITH MICHAEL REAUGH | Europäisches Patentamt | 2018

    Freier Zugriff

    Vibration Isolation Systems for Advancing Blade Concept Rotorcraft

    FOSKEY CHRISTOPHER EDWARD / STAMPS FRANK BRADLEY / SMITH MICHAEL REAUGH | Europäisches Patentamt | 2020

    Freier Zugriff

    Feasibility Study of a Novel Asymmetric Rotorcraft Configuration: Single-Rotor Advancing Blade Concept

    Cumbreras, P. / Sartorius, S. | British Library Conference Proceedings | 2013


    Rotorcraft vibration isolation systems

    SMITH MICHAEL / STAMPS FRANK BRADLEY / LEE TAEOH et al. | Europäisches Patentamt | 2017

    Freier Zugriff