초록

This invention provides a fuselage of an aircraft or space vehicle with a fuselage section having an outer skin, wherein at least the outer skin of the fuselage section consists of a glass-fiber reinforced aluminum laminate to form a safety zone for passengers in the event of a fire.

대표청구항 ▼

1. 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

1. 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; andconnecting 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. 2. The aircraft or space vehicle according to claim 1, wherein the fuselage section forming the safety zone extends at least throughout a cabin region of the fuselage. 3. The aircraft or space vehicle according to claim 1, wherein the connecting elements are designed as at least one of rivets, screws and bolts. 4. The aircraft or space vehicle according to claim 1, wherein the fuselage or at least a section of the fuselage is provided on an inside with at least one of a thermal and acoustic insulation. 5. The aircraft or space vehicle according to claim 1, wherein all or some of thrust vanes of at least the fuselage section forming the safety zone consist of glass-fibre reinforced aluminium laminate. 6. The aircraft or space vehicle according to claim 1, wherein the aircraft or space vehicle is a passenger or commercial aircraft. 7. The aircraft or space vehicle according to claim 1, wherein the fuselage section forming the safety zone is in a wing region. 8. The aircraft or space vehicle according to claim 1, wherein the connecting elements are titanium bolts. 9. The aircraft or space vehicle according to claim 1, wherein the fuselage section forming a safety zone is provided at least in one of a front cabin region of the fuselage, a rear cabin region of the fuselage, and a central cabin region. 10. The aircraft or space vehicle according to claim 9, wherein the fuselage section forming the safety zone is provided in a cabin region behind a cockpit. 11. The aircraft or space vehicle according to claim 9, wherein the fuselage section forming the safety zone is provided in a cabin region in front of a rear pressure bulkhead.