发明名称 FIBRE COMPOSITE COMPONENT, WINGLET AND AIRCRAFT WITH A FIBRE COMPOSITE COMPONENT
摘要 A fiber composite component made of a fiber composite material comprises at least one first surface section, at least one second surface section and at least one transition region. The first surface section and the second surface section are arranged at an angle to each other and incorporate the transition region. The transition region comprises at least one first curvature section and at least one second curvature section whose mean curvatures differ from each other, which curvature sections connect to each other in a tangentially continuous manner. The first surface section connects to the transition region, and the transition region connects to the second surface section in each case in a tangentially continuous manner. In one example, the radius of curvature of the first curvature section is smaller than that of the second curvature section.
申请公布号 EP2699475(B1) 申请公布日期 2016.11.16
申请号 EP20120716362 申请日期 2012.04.18
申请人 AIRBUS OPERATIONS GMBH 发明人 KREMER, TOBIAS
分类号 B64C1/06;B64C1/14;B64C3/18 主分类号 B64C1/06
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