发明名称 |
METHOD FOR PRODUCING A METAL REINFORCEMENT |
摘要 |
A metal reinforcing piece for mounting on a leading edge or trailing edge of a composite blade for a turbine engine is made by shaping two metal sheets, positioning them on either side of a core, assembling the two sheets together around the core under a vacuum, shaping them on the core by hot isostatic compression, and cutting them to separate the reinforcing piece and release the core. A predetermined roughness is given to at least a portion of the surface of the core and is transferred to a corresponding portion of an inside surface of the reinforcing piece by the hot isostatic compression. |
申请公布号 |
EP2668001(B1) |
申请公布日期 |
2016.08.17 |
申请号 |
EP20120704861 |
申请日期 |
2012.01.10 |
申请人 |
SNECMA |
发明人 |
KLEIN, GILLES, CHARLES, CASIMIR;FRANCHET, JEAN-MICHEL, PATRICK, MAURICE;LECONTE, GILBERT, MICHEL, MARIN;MAGNAUDEIX, DOMINIQUE |
分类号 |
B23P15/04;B21D53/78;B23K20/02;B23K20/18;F01D5/14;F04D29/38 |
主分类号 |
B23P15/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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