A landing gear assembly is also provided. The landing gear assembly may include a thin-skin support member defining a cavity and a cylindrical cavity. A cylinder may extend from the cylindrical cavity with an axle extending from the cylinder. A torsion link may be coupled to the axle and a torsion interface of the thin-skin support member.
AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE
2017-12-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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