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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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