发明名称 BRAIDED COMPOSITE SPAR
摘要 A braided composite spar (10) or preform for a braided composite spar, comprising a plurality of tubular plies of braided fibres, wherein the spar (10) or preform has a centre line which extends lengthwise from a root (10a) to a tip (10b), and at least part of the centre line follows a curved path which does not lie in a single plane. The spar (10) or preform can be used to provide a tubular main spar for a winglet (5). The winglet (5) also has a front spar (11) with a front spar web (16), an upper front spar cap (17), and a lower front spar cap (18). An upper skin (19) of the winglet (5) is joined to the braided spar (10) and the upper front spar cap (17). A lower skin (20) of the winglet (5) is joined to the braided spar (10) and the lower front spar cap (18).
申请公布号 CA2909533(A1) 申请公布日期 2014.10.23
申请号 CA20142909533 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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