The invention is related to a compound helicopter 1 with a fuselage 2 and at least one main rotor 3 that is at least adapted for generating lift in operation, the at least one main rotor being arranged in an upper region 5 of the fuselage, wherein at least one propeller 10 is provided that is at least adapted for generating forward and/or backward thrust in operation. The at least one propeller is mounted to a fixed wing arrangement 11, 12 that is laterally attached to the fuselage, the fixed wing arrangement comprising at least one upper wing 11 and at least one lower wing 12. An upper stub wing arrangement 14 is provided in the upper region of the fuselage, the at least one upper wing of the fixed wing arrangement being mounted to the upper stub wing arrangement.


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    Titel :

    A COMPOUND HELICOPTER WITH A FIXED WING ARRANGEMENT


    Weitere Titelangaben:

    FLUGSCHRAUBER MIT EINEM STARREN FLÜGELANORDNUNG
    HÉLICOPTÈRE COMPOSÉ DOTÉ D'UN AGENCEMENT À VOILURE FIXE


    Beteiligte:
    BLACHA MARTIN (Autor:in)

    Erscheinungsdatum :

    24.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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