发明名称 |
PROCEDE DE REALISATION D'UN RENFORT METALLIQUE D'AUBE DE TURBOMACHINE |
摘要 |
<p>A method for making a metal reinforcement for the leading edge or trailing edge of the blade of a turbine engine that includes making a metal insert defining the base of the metal reinforcement; positioning the metal insert at the end of a blank of a shaping tool, the blank repeating the shape of the turbine-engine blade; shaping a planar metal sheet on the metal insert and the blank of the shaping tool using a superplastic hot-shaping method.</p> |
申请公布号 |
FR2956602(B1) |
申请公布日期 |
2012.05.25 |
申请号 |
FR20100051364 |
申请日期 |
2010.02.25 |
申请人 |
SNECMA |
发明人 |
KLEIN GILLES CHARLES, CASIMIR;LEVEQUE STEPHANE ANDRE;MAGNAUDEIX DOMINIQUE;MAROLLE PHILIPPE |
分类号 |
B23P15/04;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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