Method for manufacturing a hollow composite material part comprising internal stiffeners
FR3156370A1Pending Publication Date: 2025-06-13SAFRAN AIRCRAFT ENGINES SAS
Patent Information
- Application Number
- FR2023013725
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2023-12-07
- Publication Date
- 2025-06-13
Abstract
The invention relates to a method for manufacturing a composite part (10, 20) comprising steps consisting of: producing a fibrous preform (36) of the composite part; producing mandrels (31-34) from a molded soluble paste; forming a fibrous reinforcement (35) around each mandrel; inserting the assembled mandrels into the preform at a location of a cavity (3) to be formed in the composite part; inserting the preform incorporating the mandrels into a mold; injecting a resin into the mold to obtain the composite part, the resin diffusing into the preform and the fibrous reinforcements; demolding the composite part; forming a channel (38) in the composite part to reach the mandrels; and injecting a solvent into the channel to dissolve the mandrels, and form the cavity in the composite part, the fibrous reinforcements between the mandrels forming stiffeners in the cavity. Figure 4H
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Citation Information
Patent Citations
Method for producing an integral fibre composite part
CA2716984A1
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FR3105291A1
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TW201318890A