A system for shrinking landing gear includes a shock strut (202) having a cylinder (204) and a piston (206) to be received by the cylinder (204). The system further includes a collar (210) coupled to a brace linkage (208) and the piston (206), a torque arm (212) configured to resist rotation between the collar (210) and the piston (206), and a shrink linkage (240) coupled between the torque arm (212) and the cylinder (204). The collar (210) rotates relative to the cylinder (204) in response to retraction of the landing gear. Rotation of the collar (210) rotates the piston (206) and the torque arm (212) relative to the cylinder (204). The rotation of the collar (210) relative to the cylinder (204) forces, via the shrink linkage (240), the piston (206) towards the aircraft attachment within the cylinder (204).


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    Titel :

    SHOCK STRUT SHRINKING SYSTEM


    Weitere Titelangaben:

    FEDERBEINSCHRUMPFSYSTEM
    SYSTÈME DE RÉTRACTATION D'AMORTISSEUR DE CHOC


    Beteiligte:
    DITZLER ADAM J (Autor:in)

    Erscheinungsdatum :

    2021-02-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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