Described herein is an aircraft that includes a fuselage with a higher portion and a lower portion. The aircraft also includes two fixed wings that are coupled to and extend from opposing sides of the lower portion of the fuselage. Additionally, the aircraft includes a tilt-rotor assembly that is coupled to each of the two fixed wings.


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    Titel :

    TILT-ROTOR VERTICAL-LIFT AIRCRAFT


    Beteiligte:
    HONG ALICIA (Autor:in) / NEWMAN DANIEL I (Autor:in) / HOLTORF CHRISTOPHER R (Autor:in) / CHISHOLM JOHN R (Autor:in) / DYESS STEPHEN (Autor:in)

    Erscheinungsdatum :

    31.12.2015


    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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