STRUCTURAL ELEMENT OF AN AIRCRAFT PART AND METHOD FOR MANUFACTURING A STRUCTURAL ELEMENT

A structural element of an aircraft part, in particular an aircraft engine part, with at least partly a double-curvature shape, including a plurality of sets of fibers in textile fabric structure, wherein in at least one region of the structural element the number of fibers in one direction is reduc...

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Bibliographische Detailangaben
Hauptverfasser:	TODOROVIC, Predrag, KUBISCH, Thomas
Format:	Patent
Sprache:	eng
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	A structural element of an aircraft part, in particular an aircraft engine part, with at least partly a double-curvature shape, including a plurality of sets of fibers in textile fabric structure, wherein in at least one region of the structural element the number of fibers in one direction is reduced per area in a flattened out state of the textile fabric structure. It also relates to a method for manufacturing a structural element.