An embodiment aircraft boom (66, 76) includes a boom member (34, 42), a vertical stabilizer (40, 50), a rear landing gear (114, 116), and a front landing gear (110, 112). The boom member (34, 42) may extend in a first direction and have a front internal structural member (154) disposed therein, where a portion of the front internal structural member (154) is a first attachment point for a first wing. The vertical stabilizer (40, 50) may extend from the boom member (34, 42), where the vertical stabilizer (40, 50) has a rear internal structural member (120) disposed therein and extends from the boom member (34, 42) and through an interior of the vertical stabilizer (40, 50), and where a portion of the rear internal structural member (120) is a second attachment point for a second wing. The rear landing gear (114, 116) may be coupled to the rear internal structural member (120). The front landing gear (110, 112) may be coupled to the front internal structural member (154) of the boom member (34, 42).


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    Title :

    AIRCRAFT WITH MULTIFUNCTIONAL STRUCTURE


    Additional title:

    FLUGZEUG MIT MULTIFUNKTIONSSTRUKTUR
    AÉRONEF À STRUCTURE MULTIFONCTION


    Contributors:
    ANDREJASIC MATEJ (author) / ERZEN DAVID (author) / LAPUH ROK (author) / MOCAN BLAZ (author) / ZNIDAR ANDRES (author) / TOMAZIC TINE (author) / DROFELNIK JERNEJ (author) / CRETNIK GREGOR (author)

    Publication date :

    2025-06-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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