发明名称 |
Fuselage structure for aircraft construction, comprises multiple elements, which are mounted by welded connections in longitudinal direction at each other, where multiple rotating ribs are connection with multiple elements |
摘要 |
<p>The fuselage structure (10), comprises the multiple elements (5a, 5b), which are mounted by welded connections in longitudinal direction at each other. The multiple rotating ribs (8) are connected with the multiple elements and running perpendicular to the longitudinal direction of the elements. The multiple clips (11,21) are arranged between the element (5a) and the ribs in the area of the welding connection such that they do not cover the welding connection (6). The multiple stringers (2) are connected with the ribs over a separate angular element (12).</p> |
申请公布号 |
DE102006026918(A1) |
申请公布日期 |
2007.12.27 |
申请号 |
DE20061026918 |
申请日期 |
2006.06.09 |
申请人 |
AIRBUS DEUTSCHLAND GMBH |
发明人 |
FRANK, CHRISTIAN;PACCHIONE, MARCO;BONDE, AXEL;KULIK, CHRISTIAN;LOHWASSER, DANIELA;WERNER, SVEN;BEHR, ANDREAS |
分类号 |
B64C1/06;B64C1/12;F16B5/00;F16B5/08 |
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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