A series of aircraft (1, 1') that can be converted, each aircraft having a core (100) with an airframe (2) defining a first axis (Y) and six rotors (20a, 20b, 21a, 21b, 22a, 22b) which are rotatable about respective six axes (B, C, D, E, F, G) and operable independently of each other so as to generate respectively six thrust value (Tl, T2, T3, T4, T5, T6) independent of each other; the core (100) comprising first and second portions (11, 17) of respective half-wings (3) and aerodynamic surfaces (9) connected to the airframe, the aircraft having in addition four wing and aerodynamic surface modules, whereas each module (110, 120, 130, 140) comprises third and fourth portions (12, 18) of respective half-wings (3) and aerodynamic surfaces (9), said modules being different for each aircraft of the series.


    Access

    Download


    Export, share and cite



    Title :

    SERIES OF CONVERTIBLE AIRCRAFTS CAPABLE OF HOVERING AND METHOD FOR CONFIGURING A CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING


    Additional title:

    EINE REIHE VON UMWANDELBAREN LUFTFAHRZEUGEN MIT FÄHIGKEIT ZUM SCHWEBEN UND VERFAHREN ZUR KONFIGURIERUNG EINES UMWANDELBAREN LUFTFAHRZEUGS MIT FÄHIGKEIT ZUM FLIEGEN
    SÉRIE D'AÉRONEFS CONVERTIBLES CAPABLE D'EFFECTUER UN VOL STATIONNAIRE ET PROCÉDÉ DE CONFIGURATION D'UN AÉRONEF CONVERTIBLE CAPABLE D'EFFECTUER UN VOL STATIONNAIRE


    Contributors:

    Publication date :

    2023-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U