Device for intermediate fastening between an aircraft fuselage and an aircraft landing gear

An assembly, comprising;

• an aircraft landing gear adapted 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;
• and
• a device for intermediate fastening between an aircraft fuselage and the landing gear, comprising:
• at least one support structure including a first support means intended to receive said at least one main shaft and a second support means intended to receive said at least one stay joint, the at least one support structure being hollow;
• 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.

An aircraft, comprising:

• a fuselage;
• a landing gear adapted 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;
• and
• a device for intermediate fastening between the fuselage and the landing gear, comprising:
• two support structures, each support structure including a first support means intended to receive said at least one main shaft and a second support means intended to receive said at least one stay joint;
• and
• a central box structure coupled to the two support structures, the central box structure including a front wall, a rear wall and linking walls connecting the front wall and the rear wall.