An aircraft (10) includes a fuselage (17) with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage (17) without changing the structural layout or configuration of the fuselage (17) structural interfaces.


    Access

    Download


    Export, share and cite



    Title :

    КОНСТРУКЦИЯ ФЮЗЕЛЯЖА ДЛЯ РАЗМЕЩЕНИЯ ХВОСТОВОГО ОПЕРЕНИЯ И ПЕРЕДНЕГО ГОРИЗОНТАЛЬНОГО ОПЕРЕНИЯ РАЗЛИЧНЫХ РАЗМЕРОВ И ФОРМ


    Publication date :

    2018-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge