An aircraft (100) has a fuselage (102), an engine (112) disposed within the fuselage (102), a rotatable wing (104) disposed above the fuselage (102) and selectively rotatable about a wing rotation axis, and a plurality of interconnect driveshafts (128) disposed within the rotatable wing (104), and at least one drive system component that is connected between the engine (112) and the interconnect driveshaft (128) is disposed along the wing rotation axis.


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    Title :

    AIRCRAFT WITH A FUSELAGE-MOUNTED ENGINE AND WING STOW


    Additional title:

    FLUGZEUG MIT TRIEBWERK IM RUMPF UND FLÜGELVERSTAUUNG
    AERONEF AVEC UN MOTEUR MONTÉ DANS LE FUSELAGE ET UNE AILE ESCAMOTABLE


    Contributors:

    Publication date :

    2018-10-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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