A rotor-lift aircraft has at least two rotors 1, 2 mounted on spaced parallel axes A1, A2. The rotors rotate in use in planes in which the blade envelope subscribed by the tips of the blade(s) of each of the rotors overlaps with the blade envelope subscribed by the tips of the blade(s) of at least one other of the rotors without intermeshing of the blades.


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    Titel :

    ROTOR-LIFT AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    22.06.2017


    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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