A device for intermediate fastening between an aircraft fuselage and an aircraft landing gear is provided. The device includes at least one semi-open support structure comprising a pair of webs, which are substantially parallel to each other. The webs comprise first support means intended to receive the main pivot shaft of the landing gear and second support means intended to receive the stay joint or joints of the landing gear. The device includes two support structures linked together by a central box structure. The central box structure includes a front wall, a rear wall and linking walls linking those two walls.
Device for intermediate fastening between an aircraft fuselage and an aircraft landing gear
2016-03-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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