发明名称 BRAIDED COMPOSITE SPAR
摘要 A winglet comprising a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. The winglet is manufactured by co-curing the upper skin to the upper main spar cap and the upper front spar cap; and co-curing the lower skin to the lower main spar cap and the lower front spar cap.
申请公布号 EP2986503(A1) 申请公布日期 2016.02.24
申请号 EP20140718720 申请日期 2014.04.17
申请人 AIRBUS OPERATIONS LIMITED 发明人 FONG, TONY;AXFORD, TIMOTHY
分类号 B64C23/06;B29C70/22;B64C3/18 主分类号 B64C23/06
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