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

The invention relates to a structural element (101) of an aircraft part, in particular an aircraft engine part, with at least partly a double-curvature shape, comprising a plurality of sets of fibers (11, 12, 13) in textile fabric structure (1), wherein in at least one region (15) of the structural...

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Bibliographische Detailangaben
Hauptverfasser:	TODOROVIC, Predrag, KUBISCH, Thomas
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	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 LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention relates to a structural element (101) of an aircraft part, in particular an aircraft engine part, with at least partly a double-curvature shape, comprising a plurality of sets of fibers (11, 12, 13) in textile fabric structure (1), wherein in at least one region (15) of the structural element (101) the number of fibers in one direction is reduced per area in a flattened out state of the textile fabric structure (1). It also relates to a method for manufacturing a structural element (101). L'invention concerne un élément structural (101) d'une partie d'avion, en particulier d'une partie de moteur d'avion, comportant au moins partiellement une forme à double courbure, comprenant une pluralité d'ensembles de fibres (11, 12, 13) en structure de tissu textile (1), dans au moins une région (15) de l'élément structural (101) le nombre de fibres dans une direction est réduite par superficie dans un état aplati de la structure de tissu textile (1). L'invention concerne également un procédé de fabrication d'un élément structural (101).