A rotary wing aircraft comprising a fuselage tail boom, a tail cone and an interface frame, the interface frame in turn having a connecting structure directly attached to the tail cone by means of a tail cone mechanical connection and a connecting sleeve fitting axially the fuselage tail boom, the connecting sleeve and the fuselage tail boom being directly attached by means of a one boom mechanical connection; the interface frame thereby joining the fuselage tail boom and the tail cone.


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    Title :

    ROTARY WING AIRCRAFT WITH AN INTERFACE FRAME JOINING THE FUSELAGE TAIL BOOM AND THE TAIL CONE


    Contributors:

    Publication date :

    2017-11-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotary wing aircraft with an interface frame joining the fuselage tail boom and the tail cone

    PROBST STEFAN / WALCH PHILIPP / NOTHEN MARC et al. | European Patent Office | 2020

    Free access


    ROTARY WING AIRCRAFT WITH AN INTERFACE FRAME JOINING THE FUSELAGE TAIL BOOM AND THE TAIL CONE

    PROBST STEFAN / WALCH PHILIPP / NOTHEN MARC et al. | European Patent Office | 2017

    Free access

    ROTARY AIRCRAFT WITH AN INTERFACE FRAME JOINING THE FUSELAGE TAIL BOOM AND THE TAIL CONE

    PROBST STEFAN / WALCH PHILIPP / NOTHEN MARC et al. | European Patent Office | 2020

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