A hydraulic piston actuator (24), which may be used for an aircraft nacelle assembly (20), includes a housing (30), a piston (32), an end gland (42), and a bearing ring (44). The housing (30) is concentrically disposed along an axis (A). The piston (32) is adapted to axially reciprocate within the housing (30). The end gland (42) is disposed radially between the housing (30) and the piston (32). The bearing ring (44) is disposed radially between the end gland (42) and the piston (32).


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    Title :

    AIRCRAFT NACELLE ASSEMBLY


    Additional title:

    ANORDNUNG FÜR EINE FLUGZEUGGONDEL
    ASSEMBLAGE POUR UNE NACELLE D'AVION



    Publication date :

    2023-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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