Invention Grant
- Patent Title: Turbomachine rotary fan blade, fan, and turbomachine provided therewith
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Application No.: US17776103Application Date: 2020-11-18
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Publication No.: US11885239B2Publication Date: 2024-01-30
- Inventor: Guillaume Pascal Jean-Charles Gondre , Thomas Alain De Gaillard , Pierre Jean Faivre D'Arcier
- 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: FR 12933 2019.11.20
- International Application: PCT/FR2020/052110 2020.11.18
- International Announcement: WO2021/099736A 2021.05.27
- Date entered country: 2022-05-11
- Main IPC: F01D5/28
- IPC: F01D5/28 ; F01D5/14

Abstract:
The invention relates to a turbomachine rotary-fan blade having a predetermined breaking zone, which extends from the upstream edge along a given length and from the blade-tip edge over a given height. According to the invention, the body is made of a composite material comprising a fibre reinforcement obtained by three-dimensional weaving of warp and weft strands, and a resin matrix in which the fibre reinforcement is embedded, and has, in or in the vicinity of the zone, a discontinuity of at least some of the strands, configured such that the zone partially detaches when there is tangential friction in the thickness direction against the blade-tip edge, the height being less than 3% of the aerodynamic stream height of the blade.
Public/Granted literature
- US20220381148A1 TURBOMACHINE ROTARY FAN BLADE, FAN, AND TURBOMACHINE PROVIDED THEREWITH Public/Granted day:2022-12-01
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