A semi -levered landing gear (10) is provided that includes a shock strut (12), a truck beam (18) pivotally connected to the shock strut and a semi -levered landing gear mechanism including at least three links (24, 30a, 30b) configured to angularly orient the truck beam and a truck pitch actuation system (40) operatively connected to at least one of the three links. The landing gear mechanism may be configured to cooperate with an extension of a shock strut by positioning the truck pitch actuator in a retracted position, thereby positioning a forward end of the truck beam in a raised position relative to the aft end of the truck beam. The landing gear mechanism may also be configured to cooperate with a retraction of the shock strut into the wheel well by extending the truck pitch actuator to position a forward end (18a) of the truck beam in a lower position relative to the aft end (18b) of the truck beam.


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    Titel :

    SEMI-LEVERED LANDING GEAR AND ASSOCIATED METHOD


    Weitere Titelangaben:

    TRAIN D'ATTERRISSAGE PARTIELLEMENT MANOEUVRE PAR LEVIER ET PROCEDE ASSOCIE


    Beteiligte:
    MELLOR MITCHELL L (Autor:in) / LONG MICHAEL A (Autor:in) / ODELL RICHARD B (Autor:in)

    Erscheinungsdatum :

    2015-09-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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