The present invention relates to a rotary wing aircraft 100 that extends along a roll axis R between a nose region 101 and an aft region 102, comprising: at least one first single-blade rotor 120 and at least one second single-blade rotor 130 which are spaced apart from each other along the roll axis; at least one first electric machine and at least one second electric machine which are at least configured to drive in motor mode the at least one first single-blade rotor 120 and the at least one second single-blade rotor 130 for generating lift in hover condition of the rotary wing aircraft; at least one propulsion device 140 that is at least configured to generate forward thrust in forward flight condition of the rotary wing aircraft; and a fixed-wing arrangement 150 that is at least configured to provide lift in the forward flight condition.


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    Titel :

    A ROTARY WING AIRCRAFT WITH AT LEAST TWO ROTORS AND A PROPULSION UNIT


    Weitere Titelangaben:

    EIN DREHFLÜGELFLUGZEUG MIT WENIGSTENS ZWEI ROTOREN UND EINER ANTRIEBSEINHEIT
    UN AÉRONEF À VOILURE TOURNANTE AVEC AU MOINS DEUX ROTORS ET UNE UNITÉ DE PROPULSION


    Beteiligte:

    Erscheinungsdatum :

    10.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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