Aircraft with vertical takeoff and landing capability and casing bodies The invention relates to an aircraft (1) with vertical takeoff and landing capability, comprising a fuselage (2) with a longitudinal axis (L) and with multiple casing bodies (30) arranged on the fuselage (2), wherein at least one of the casing bodies (30) is mounted so as to be rotatable about a transverse axis (Q) arranged at an angle with respect to the longitudinal axis (L), and wherein the aircraft (1) comprises at least one propulsion device (10) with a rotatable turbomachine (20) and one of the casing bodies (30), wherein the rotatable turbomachine (20) has an axis of rotation (R) which is rotatable by means of the transverse axis (Q), and the casing body (30) has a substantially cylindrical section (31) extending along the axis of rotation (R), wherein the cylindrical section (31) coaxially surrounds the turbomachine (20). It is provided that the casing body (30) is designed to generate lift, in particular during horizontal flight of the aircraft (1), whereby the casing body is thus in the form of an annular wing.


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    Titel :

    VERTIKAL START- UND LANDFÄHIGES FLUGOBJEKT


    Weitere Titelangaben:

    VERTICAL TAKEOFF AND LANDING OBJECT
    OBJET À DÉCOLLAGE ET ATTERRISSAGE VERTICAL


    Beteiligte:
    SAUER SEBASTIAN (Autor:in) / KURZ CARLO (Autor:in) / ZLATKOV BRANISLAV (Autor:in) / FRICKE MARTIN (Autor:in) / TAPPE OLIVER (Autor:in) / SANCHA GARCIA LUIS ANTONIO (Autor:in) / LÜDERS RALF (Autor:in)

    Erscheinungsdatum :

    01.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Deutsch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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