发明授权
- 专利标题: Blade for a turbine engine, associated turbine engine distributor and turbine engine
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申请号: US17594071申请日: 2020-03-16
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公开(公告)号: US11795828B2公开(公告)日: 2023-10-24
- 发明人: Matthieu Simon , Jean-Luc Bacha , Paul Danre , Léandre Ostino
- 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
- 代理机构: Bookoff McAndrews, PLLC
- 优先权: FR 03586 2019.04.03
- 国际申请: PCT/FR2020/050559 2020.03.16
- 国际公布: WO2020/201653A 2020.10.08
- 进入国家日期: 2021-10-01
- 主分类号: F01D5/18
- IPC分类号: F01D5/18 ; F01D9/06
摘要:
A blade for a turbomachine intended to be disposed about an axis while extending radially between a radially outer end and a radially inner end, the blade having at least one cooling cavity opening out to the radially outer end of the blade and to the radially inner end of the blade, the blade having at least a first tubular liner and at least a second tubular liner each engaged in the cavity, the radially outer end of the first liner opening out to the radially outer end of the blade, and the radially inner end of the second liner opening out to the radially inner end of the blade.
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