IMPACT RESISTANT FUSELAGE

An impact resistant fuselage of an aircraft, the fuselage extending along a central longitudinal direction, wherein transversal sections of the fuselage are comprised in a vertical plane perpendicular to the central longitudinal direction. The impact resistant fuselage comprises at least a ballistic...

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Bibliographische Detailangaben
Hauptverfasser:	INIESTA LOZANO, Fernando, MARTINO GONZÁLEZ, Esteban, MENARD, Edouard
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARMOUR ARMOURED OR ARMED VEHICLES ARMOURED TURRETS AVIATION BLASTING COSMONAUTICS HEATING HELICOPTERS LIGHTING MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An impact resistant fuselage of an aircraft, the fuselage extending along a central longitudinal direction, wherein transversal sections of the fuselage are comprised in a vertical plane perpendicular to the central longitudinal direction. The impact resistant fuselage comprises at least a ballistic material membrane extended along the longitudinal direction for absorbing high energy impacts. The membrane according to a transversal section, comprising at least one section between two tensional elements, wherein the material membrane is located inside the fuselage of the aircraft, the at least one section of the membrane is mechanically linked to the inside of the fuselage by the tensional elements, and the two tensional elements stress the membrane.