Invention Grant
- Patent Title: Method for local reinforcement of a composite fiber reinforced panel and panel obtained using said method
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Application No.: US14130057Application Date: 2012-07-02
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Publication No.: US09889603B2Publication Date: 2018-02-13
- Inventor: Michael Hugon , Alexandre Pelard , Dominique Soubelet
- Applicant: Michael Hugon , Alexandre Pelard , Dominique Soubelet
- Applicant Address: FR Saint Julien de Chedon
- Assignee: Daher Aerospace
- Current Assignee: Daher Aerospace
- Current Assignee Address: FR Saint Julien de Chedon
- Agency: Im IP Law
- Agent C. Andrew Im
- Priority: FR1155981 20110701
- International Application: PCT/EP2012/062861 WO 20120702
- International Announcement: WO2013/004671 WO 20130110
- Main IPC: B29C65/00
- IPC: B29C65/00 ; B29C65/02 ; B29C70/34 ; B29D99/00 ; B32B5/26 ; B32B37/10 ; B32B38/00 ; B64C1/12 ; B29L31/30

Abstract:
A laminated composite structural panel with fiber reinforcement comprising a skin with a thickness e1 and a localized reinforcement or patch. The skin is made up of a stack of fibrous plies in a matrix made of a thermoplastic polymer. The localized reinforcement or patch is joined to the surface of the skin and rises to a thickness of e2 in a direction that is locally normal to the skin, which is made up of a stack of fibrous plies in a matrix made of thermoplastic polymer. The surface of the plies that make up the patch is decreasing from the ply of the patch in contact with the skin so that the edges of the patch have a slope p greater than 0.5. The patch and the skin is joined by a weld.
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