发明名称 |
Composite compound structural component and method of forming the same |
摘要 |
<p>Composite compound structural component as semi-finished element for subsequent processing to a construction element for application particularly in the aerospace sector. Said semi-finished element comprises at least two separate subpreforms (12, 13, 14) each at least essentially two-dimensional and each assembled of plies of fiber material, particularly of plies of carbon fibers and at least one at least essentially two-dimensional connecting element (6, 15) of preactivated fiber semi-finished products cut to final dimension and connecting the at least two essentially two-dimensional separate subpreforms (12, 13, 14) to a stable semi-finished element. Amethod of producing said composite compound structural component is also disclosed.</p> |
申请公布号 |
EP2886310(A1) |
申请公布日期 |
2015.06.24 |
申请号 |
EP20130400040 |
申请日期 |
2013.12.19 |
申请人 |
AIRBUS HELICOPTERS DEUTSCHLAND GMBH |
发明人 |
OTTO, HANS;SCHMID, EMANUEL;LINDNER, HARALD;OEFNER, WALTER |
分类号 |
B29C70/44;B29B11/16;B29C65/00;B29C70/48 |
主分类号 |
B29C70/44 |
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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