Invention Grant
- Patent Title: Blade comprising a composite material structure and associated manufacturing method
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Application No.: US17793877Application Date: 2021-01-19
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Publication No.: US12134460B2Publication Date: 2024-11-05
- Inventor: Vincent Joudon , Vivien Mickaël Courtier , Clément Pierre Postec
- Applicant: Safran Aircraft Engines
- Applicant Address: FR Paris
- Assignee: Safran Aircraft Engines
- Current Assignee: Safran Aircraft Engines
- Current Assignee Address: FR Paris
- Agency: BIRCH, STEWART, KOLASCH & BIRCH, LLP
- Priority: FR2000527 20200120
- International Application: PCT/FR2021/050090 WO 20210119
- International Announcement: WO2021/148750 WO 20210729
- Main IPC: B64C11/26
- IPC: B64C11/26 ; B29C70/24 ; B29C70/34 ; B29L31/08 ; F01D5/28

Abstract:
The present invention relates to a blade (7) comprising: —a composite material structure (17), —a blade root fastening portion (9) further comprising a shoulder (10) extending into the recess from the wall —a base (18) arranged in the recess and comprising a support member configured to abut against the shoulder (10) of the blade root fastening portion (9) and a passage (39) formed in the support member, the sections (23) of the blade root portion (22) of the composite material structure extending through the passage (39), and —a blocking part (19) arranged in the recess between the two sections (23) of the blade root portion (22) such that each section of the blade root portion (23) is pressed against the support member by the blocking part (19).
Public/Granted literature
- US20230044779A1 BLADE COMPRISING A COMPOSITE MATERIAL STRUCTURE AND ASSOCIATED MANUFACTURING METHOD Public/Granted day:2023-02-09
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