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
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