In some embodiments, an aircraft may include a retractable or extendable landing gear. The landing gear may include a wheel connected to an axle, a strut configured to resist longitudinal compression, and a linear actuator that is partially disposed within an opening of the strut.


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    Titel :

    Aircraft landing gear


    Beteiligte:
    FENNY CARLOS A (Autor:in) / ROSS BRENT C (Autor:in) / KELL KEVIN (Autor:in) / BAINES ANDREW (Autor:in)

    Erscheinungsdatum :

    2017-05-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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