Aircraft fuselage, ballistic shield for use on an inner surface of an aircraft fuselage, ballistic shield assembly and aircraft having a fuselage
AssigneeAirbus Operations GmbH
InventorsPeer Konitzer, Manuel Schweers
Life of this patent
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Abstract
An aircraft fuselage, in particular of an open fan propeller aircraft, includes a primary structure having frame members extending in a circumferential direction of the fuselage and stringers extending in a longitudinal direction of the fuselage and a ballistic shield covering an inner surface of a longitudinal section of the fuselage. The ballistic shield is inserted between adjacent frame members of the primary structure and extends in a longitudinal direction and a circumferential direction of the fuselage section. A ballistic shield for use on an inner surface of an aircraft fuselage, a ballistic shield assembly and aircraft are disclosed.
Claims15
An aircraft fuselage of an open fan propeller aircraft, comprising a primary structure having frame members extending in a circumferential direction of the fuselage and stringers extending in a longitudinal direction of the fuselage and a ballistic shield covering an inner surface of a longitudinal section of the fuselage, wherein the ballistic shield is inserted between adjacent frame members of the primary structure and extends in a longitudinal direction and a circumferential direction of the fuselage section.
Dependencies are inferred from the claim text.