An articulated landing gear (100) may include electrical lines and/or hydraulic lines (170) located within the articulated landing gear (100). The articulated landing gear (100) may have a hollow structural post (110) and a hollow trailing arm (120) coupled by a pivot joint (140). The electrical lines and/or hydraulic lines (170) may be routed through an interior of the hollow structural post (110) and through an interior of the hollow trailing arm (120). A bulkhead (210A-210F) within the hollow structural post (110) or the hollow trailing arms (120) may include guide holes (330). The electrical lines and/or hydraulic lines (170) may be supported by the bulkhead (210A-210F) by passing through the guide holes (330). The electrical lines and/or hydraulic lines (170) may be flexible around the pivot joint (140).


    Access

    Download


    Export, share and cite



    Title :

    Routings for articulated landing gear


    Additional title:

    Leitwege für ein Gelenkfahrwerk
    Acheminements pour train d'atterrissage articulé


    Contributors:

    Publication date :

    2019-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Routings for articulated landing gear

    REBER KOREY M / MILSOM DEREK C | European Patent Office | 2016

    Free access

    SEMI-LEVERED ARTICULATED LANDING GEAR SYSTEM

    WILSON PHILLIP K | European Patent Office | 2016

    Free access

    Rotorcraft Slope Landings with Articulated Landing Gear

    Manivannan, Vasudevan / Langley, Jared P. / Costello, Mark et al. | AIAA | 2013


    Dynamics of Articulated Landing Gear in Tail-Down Landing Condition

    Kadam, Mahesh / Sathish, S. / Bujurke, Aditya et al. | Springer Verlag | 2018