A rotary-wing aircraft with a fuselage that comprises a load carrying shell structure and a load carrying stiffening member structure
AssigneeAirbus Helicopters Deutschland GmbH
InventorAxel FINK
Life of this patent
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Abstract
A rotary-wing aircraft with a fuselage that comprises a load carrying shell structure and a load carrying stiffening member structure, wherein the load carrying shell structure delimits an aircraft inner volume, and wherein the load carrying stiffening member structure is arranged outside of the aircraft inner volume on an outer surface of the load carrying shell structure.
Claims14
A rotary-wing aircraft with a fuselage that comprises a load carrying shell structure and a load carrying stiffening member structure, wherein the load carrying shell structure delimits an aircraft inner volume, and wherein the load carrying stiffening member structure is arranged outside of the aircraft inner volume on an outer surface of the load carrying shell structure wherein the load carrying stiffening member structure is covered by outer cover panels which are free of load carrying duties and which define an outer perimeter of the fuselage.
Dependencies are inferred from the claim text.