发明名称 |
Manufacturing process of a composite turbine blade and the blade obtained thereby |
摘要 |
<p>The procedure consists of creating a three-dimensional preform from woven carbon, glass, silicon aluminium or polymer filaments (20) with visually identifiable tracers (22) that are different to the other filaments to form the blade (12) and its foot (14), and cutting out the preform to leave intact tracers along one reference surface. The preform is then pre-deformed and made compact and rigid before placing it in a mould and injecting a thermo-setting resin bonding agent to impregnate the entire preform and maintain the distance between the filaments. The mould is then heated to produce a moulded article with the shape and dimensions of the blade.</p> |
申请公布号 |
EP1777063(B1) |
申请公布日期 |
2012.07.04 |
申请号 |
EP20060122561 |
申请日期 |
2006.10.19 |
申请人 |
SNECMA |
发明人 |
COUPE, DOMINIQUE;DAMBRINE, BRUNO;LEVEQUE, STEPHANE;MAHIEU, JEAN-NOEL |
分类号 |
B29C70/24;B29B11/16;B29C70/48;B29K307/04;B29L31/08 |
主分类号 |
B29C70/24 |
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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