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.

    La présente invention concerne un ensemble train d'atterrissage adaptatif pour un aéronef à voilure tournante, l'ensemble train d'atterrissage adaptatif comprenant un dispositif de commande ; un premier support de train d'atterrissage présentant un premier élément de contact au sol ; et un second support de train d'atterrissage présentant un second élément de contact au sol ; le dispositif de commande commandant indépendamment le premier support de train d'atterrissage et le second support de train d'atterrissage.


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    Title :

    ADAPTIVE LANDING GEAR ASSEMBLY FOR ROTARY WING AIRCRAFT


    Additional title:

    ENSEMBLE TRAIN D'ATTERRISSAGE ADAPTATIF POUR AÉRONEF À VOILURE TOURNANTE


    Contributors:

    Publication date :

    2016-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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