The invention is related to a vibration dampening structure 7 for dampening vibrations occurring during operation of a rotary wing aircraft 1, comprising: a floating body 8; and a floating body support structure 9 that supports the floating body 8. The floating body support structure 9 comprises a mounting device 10 that is rigidly mountable to the rotary wing aircraft 1; and a pneumatic shock absorber system 29 that couples the floating body 8 to the mounting device 10. The pneumatic shock absorber system 29 dampens the vibrations occurring during operation of the rotary wing aircraft 1 for stabilizing the floating body 8 relative to the mounting device 10.


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    Title :

    A VIBRATION DAMPENING STRUCTURE FOR A ROTARY WING AIRCRAFT


    Additional title:

    VIBRATIONSDÄMPFUNGSSTRUKTUR FÜR EIN DREHFLÜGELFLUGZEUG
    STRUCTURE D'AMORTISSEMENT DE VIBRATIONS POUR UN AÉRONEF À VOILURE TOURNANTE


    Contributors:

    Publication date :

    2021-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B62D MOTOR VEHICLES , Motorfahrzeuge / F16F SPRINGS , Federn




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