Invention Publication
- Patent Title: CURVED STIFFENER FOR A TURBINE ENGINE NACELLE AND METHOD FOR PRODUCING SUCH A STIFFENER
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Application No.: US18552829Application Date: 2022-04-08
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Publication No.: US20240166332A1Publication Date: 2024-05-23
- Inventor: Benjamin PROVOST , Julien LORRILLARD , Bertrand Léon Marie DESJOYEAUX , Pierre PARANT
- Applicant: SAFRAN NACELLES
- Applicant Address: FR Gonfreville-l’Orcher
- Assignee: SAFRAN NACELLES
- Current Assignee: SAFRAN NACELLES
- Current Assignee Address: FR Gonfreville-l’Orcher
- Priority: FR 2103734 2021.04.12
- International Application: PCT/FR2022/050661 2022.04.08
- Date entered country: 2023-09-27
- Main IPC: B64C7/02
- IPC: B64C7/02 ; B29C70/24 ; B29C70/30 ; B64C1/00

Abstract:
Curved stiffener for a turbomachine cowl composed of a resin-impregnated fibrous reinforcement, including a stack of a plurality of layers of fibers stacked along the thickness direction and extending on the entire width of the fibrous reinforcement, each layer of fibers having a plurality of fibers parallel to each other extending along a direction inclined relative to the length direction, the fibers of two consecutive layers of fibers along the thickness direction have directions inclined relative to each other, and the layers of fibers are sewn together by sewing threads extending along the length direction, the fibrous reinforcement includes a layer of reinforcing fibers having a plurality of fibers parallel to each other extending along the length direction, the layer of reinforcing fibers extending at least on the central part, over a width smaller than the width of the fibrous reinforcement.
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