- 专利标题: BLADE COMPRISING A STRUCTURE MADE OF COMPOSITE MATERIAL AND ASSOCIATED MANUFACTURING METHOD
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申请号: US18278999申请日: 2022-02-24
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公开(公告)号: US20240141917A1公开(公告)日: 2024-05-02
- 发明人: Vincent JOUDON
- 申请人: Safran Aircraft Engines
- 申请人地址: FR Paris
- 专利权人: Safran Aircraft Engines
- 当前专利权人: Safran Aircraft Engines
- 当前专利权人地址: FR Paris
- 优先权: FR 2101966 2021.03.01
- 国际申请: PCT/FR2022/050339 2022.02.24
- 进入国家日期: 2023-08-25
- 主分类号: F04D29/38
- IPC分类号: F04D29/38 ; B29C70/24 ; B29C70/44 ; F04D29/02 ; B29L31/08
摘要:
The present invention relates to a blade comprising: a structure of aerodynamic profile comprising two mutually opposite skins; and a spar comprising a fibrous reinforcement obtained by three-dimensional weaving and densified by the matrix, the spar comprising a blade root portion extending outside the structure of aerodynamic profile and an airfoil portion arranged inside the structure of aerodynamic profile between the two skins. Moreover, within the blade root portion, the fibrous reinforcement of the spar comprises a non-debound region and at least two debound regions extending radially from the non-debound region so as to form at least four separate branches.
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