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).


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    Title :

    ADVANCING BLADE CONCEPT ROTORCRAFT WITH A VIBRATION ISOLATION SYSTEM


    Additional title:

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



    Publication date :

    2019-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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