An adaptive landing gear assembly for a rotary wing aircraft, the adaptive landing gear assembly including a controller; a first landing gear support having a first ground contact element; and a second landing gear support having a second ground contact element; the controller independently controlling the first landing gear support and the second landing gear support.


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    Titel :

    ADAPTIVE LANDING GEAR ASSEMBLY FOR ROTARY WING AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2018-05-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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