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).
Routings for articulated landing gear
Leitwege für ein Gelenkfahrwerk
Acheminements pour train d'atterrissage articulé
10.04.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Rotorcraft Slope Landings with Articulated Landing Gear
AIAA | 2013
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