Invention Grant
- Patent Title: Composite-material casing having an integrated stiffener
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Application No.: US17273528Application Date: 2019-09-03
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Publication No.: US11891910B2Publication Date: 2024-02-06
- Inventor: Clément Bourolleau , Serge Domingues , Vincent Pascal Fiore , Florent Louis André Rognin , Anwer Siraj
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR 57963 2018.09.05
- International Application: PCT/FR2019/052031 2019.09.03
- International Announcement: WO2020/049254A 2020.03.12
- Date entered country: 2021-03-04
- Main IPC: F01D25/24
- IPC: F01D25/24 ; B29C70/22 ; B29C70/32 ; B29C70/86 ; B29L31/00 ; F01D25/28 ; F01D25/26 ; F01D5/14 ; F01D5/28

Abstract:
A method for manufacturing a composite-material casing for a gas turbine, includes producing by three-dimensional weaving a fiber texture in the form of a strip, winding of the fiber texture around several superimposed turns on a mandrel with a profile corresponding to that of the casing to be manufactured in order to obtain a fiber preform of a shape corresponding to that of the casing to be manufactured, and densifying the fiber preform by a matrix. During the winding of the last turn of the fiber texture on the mandrel, at least one stiffening element is interposed between the before-last turn and the last turn of the fiber texture. The stiffening element projects over the outer surface of the before-last turn of the fiber texture. The stiffening element has an axial section of omega-type shape.
Public/Granted literature
- US20210340881A1 COMPOSITE-MATERIAL CASING HAVING AN INTEGRATED STIFFENER Public/Granted day:2021-11-04
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