Patent ID: 9272776
Filing Date: 2016-03-01
CPC Classification: B64C

Claim Text:
1. A device for intermediate fastening between an aircraft fuselage and an aircraft landing gear, the landing gear configured to pivot around at least one main shaft and to be hinged around at least one stay joint to enable the extension or the retraction of the landing gear and comprising a leg having wheels which is linked to the at least one main shaft and a stay coupling the leg to the at least one stay joint, the device comprising: at least one support structure including a first support means configured to receive said at least one main shaft and a second support means configured to receive said at least one stay joint; and a central box structure coupled to the at least one support structure, the central box structure including a front wall, a rear wall and linking walls connecting the front wall and the rear wall; wherein the at least one support structure includes a right support structure and a left support structure linked together by the central box structure, the central box structure configured transverse to the longitudinal axis of the aircraft fuselage when installed on the aircraft.