An aircraft that includes a canard having a leading edge and a trailing edge, a forward swept and fixed wing having a trailing edge, and a plurality of tilt rotor submodules. The plurality of tilt rotor submodules includes a first tilt rotor submodule where the leading edge of the canard contacts the first tilt rotor submodule at position that is within a range of 40% to 60%, inclusive, of the length of the first tilt rotor submodule where 0% corresponds to a forward tip of the first tilt rotor submodule and 100% corresponds to an aft tip of the first tilt rotor submodule. The trailing edge of the canard contacts the first tilt rotor submodule at position that is within a range of 55% to 80%, inclusive, of the length of the first tilt rotor submodule. The plurality of tilt rotor submodules also includes a second tilt rotor submodule that is coupled to the trailing edge of the forward swept and fixed wing.


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    Titel :

    FIXED WING AIRCRAFT WITH TRAILING ROTORS AND T-TAIL


    Weitere Titelangaben:

    STARRFLÜGLER MIT HINTEREN ROTOREN UND T-LEITWERK
    AÉRONEF À AILE FIXE AVEC ROTORS DE FUITE ET QUEUE EN T


    Beteiligte:
    SINHA PRANAY (Autor:in) / VANDER LIND DAMON (Autor:in)

    Erscheinungsdatum :

    2023-08-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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