A lift module capable of achieving vertical flight in fixed-wing aircraft and generating low aerodynamic drag during horizontal flight, comprising essentially e: a structural compartment (40) and two lids (41A) and (41B) hinged by means of arms (41A-1) and (41B-1) to the structural compartment (40), which contains within it at least one drive assembly (43) and at least one rotor (42), which is locked when the sustainer module (4) is closed during horizontal flight and which when opened, the rotor is unlocked to generate lift force by its rotation.


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    Title :

    LIFT MODULE FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND AIRCRAFT INCORPORATING SUCH A MODULE


    Additional title:

    AUFTRIEBSMODUL FÜR SENKRECHT STARTENDES UND LANDENDES FLUGZEUG UND FLUGZEUG MIT EINEM SOLCHEN MODUL
    MODULE SUPPORT POUR AÉRONEFS DE DÉCOLLAGE ET D'ATTERRISSAGE VERTICAUX ET AÉRONEF COMPRENANT CE MODULE


    Contributors:

    Publication date :

    2025-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge