发明名称 |
Method of producing a composite shell element and composite shell element |
摘要 |
The present invention relates to the fabrication of composite shell elements and to the assembly of large scale structures comprising such composite shell elements. The composite shell elements comprise two regions in which the resin is cured to different levels. As a consequence, the flexibility of the first region is greater than the flexibility of the second region. Since the first region defines a bending line, the composite shell element can be deformed along the bending line during assembly of the large scale structure. Thus, tolerances in fabrication of the composite shell elements may be compensated for in a time-efficient manner without the need for applying a shimming process. |
申请公布号 |
EP2730397(A1) |
申请公布日期 |
2014.05.14 |
申请号 |
EP20120191653 |
申请日期 |
2012.11.07 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
GOEHLICH, ROBERT ALEXANDER;VAN HOVE, MATTHIAS |
分类号 |
B29C70/54;B29C35/02;B29C53/02 |
主分类号 |
B29C70/54 |
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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