发明名称 Method and apparatus with relief drum for producing a core for a composite structural panel
摘要 A winglet 3 has an inner end 5 and an outer 7. The winglet 3 has a varying radius of curvature (R) which: (i) decreases along the winglet over a first distance d1; (ii) remains constant over a second distance d2; and (iii) increases along the winglet 3 over a third distance d3. The sum of the first and third distances (d1+d3) is greater than the second distance (d2). The radius of curvature may vary according to the equation R=k1/dn. The parameter n may be equal to 1, such that the curvature follows an Euler spiral.
申请公布号 GB201400878(D0) 申请公布日期 2014.03.05
申请号 GB20140000878 申请日期 2014.01.20
申请人 AIRBUS OPERATIONS LIMITED 发明人
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