发明名称 Stiffener end with staggered slopes and panel with such stiffener end
摘要 <p>The stop has an initial slope (3) inclined from a current height (H) until an intermediate point (A). A flat zone (4) is arranged from the point parallel to an upper side of a base skin (1) of a panel to be stiffened and is extended to a predetermined length (L). A final slope (5) following the zone is terminated in a point (B). The length of the flat zone is three times that of the height (H). An independent claim is also included for a primary panel structure for an aircraft.</p>
申请公布号 EP1566334(A1) 申请公布日期 2005.08.24
申请号 EP20050100898 申请日期 2005.02.09
申请人 AIRBUS FRANCE 发明人 LEON-DUFOUR, JEAN-LUC;SARPY, BRUNO
分类号 B64C1/06;B64C1/12;B64C3/18;B64C3/26;(IPC1-7):B64C1/12 主分类号 B64C1/06
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