Patent ID: 8100362

Claim:
An aircraft having a hollow fuselage, at least in a front part thereof, wherein said aircraft includes: a cockpit partially inserted into an orifice positioned in an upper part of said fuselage and connected to said fuselage by connection means; said cockpit comprising: a front section of said aircraft, wherein said cockpit includes a pressure bulkhead sealing the front section and a pressurization system for pressurizing said front section and in that said pressure bulkhead is substantially plane and includes attaching devices for receiving devices for fixing said front section to said fuselage; wherein said fuselage comprising at least two transverse beams positioned at a front and at a back of said front section, respectively, said connection means comprise means for fixing said front section to said transverse beams and at least four slanted stiffening link rods laterally connected in pairs, at one of the ends thereof, to the front and to the back of said front section and at the other end thereof, to said transverse beams by a ball and socket joint.