In various embodiments, a landing gear arrangement may comprise a first composite layer (240) having an outer surface, a metallic load transfer member (250) comprising an inner surface having a constant diameter, the metallic load transfer member perimetrically surrounding at least a portion of the first composite layer, wherein the constant diameter and a diameter of the outer surface is substantially equal, and a second composite layer (260) partially perimetrically surrounding at least a portion of the metallic load transfer member.
MANUFACTURING METHOD OF POLYMER COMPOSITE/METAL LOAD TRANSFER JOINT FOR LANDING GEAR
VERFAHREN ZUR HERSTELLUNG EINES LASTÜBERTRAGUNGSGELENKS AUS POLYMERVERBUNDWERKSTOFF/METALL FÜR FLUGZEUGFAHRWERK
PROCÉDÉ DE FABRICATION D'UN JOINT DE TRANSFERT COMPOSITE POLYMÈRE/MÉTAL POUR TRAIN D'ATTERRISSAGE
2020-03-04
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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