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
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