Patent ID: 8899523

Claim:
An aircraft or space vehicle comprising a fuselage, wherein the fuselage comprises: a fuselage section forming a safety zone for passengers in the event of a fire, having: an outer skin that includes skin panels having sheet ends, wherein the skin panels consist completely of high static strength glass-fibre reinforced aluminium laminate; stringers and ribs in the safety zone, the stringers provided in a longitudinal direction of the aircraft or space vehicle for longitudinal stiffening and the ribs provided in a transverse direction of the aircraft or space vehicle for transverse stiffening, all of the stringers and the ribs consisting of high static strength glass-fibre reinforced aluminum laminate, wherein the stringers are fastened to the skin panels and the ribs are fastened to the skin panels by clips consisting of high static strength glass-fibre reinforced laminate; and connecting elements in the safety zone connecting the sheet ends of the skin panels with each other and connecting the stringers and the ribs to the skin panels, the connecting elements in the safety zone formed from at least one of titanium and a titanium alloy.