发明名称 |
Transition shim between structure for fastening a wing to a fuselage of an aircraft, and aircraft having such a shim |
摘要 |
A shim adapted for positioning on the upper surface of at least one wing of an aircraft. The shim restores an aerodynamic profile of the wing at the position of a zone of transition between structure fastening the wing to the fuselage of the aircraft and the upper surface of the aircraft. The shim enables a seal to run from the fastening structure to the upper surface of the wing, in eliminating the zones at which the seal may break open. An aircraft provided with such a shim is also disclosed.
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申请公布号 |
US7607614(B2) |
申请公布日期 |
2009.10.27 |
申请号 |
US20050114659 |
申请日期 |
2005.04.26 |
申请人 |
AIRBUS FRANCE |
发明人 |
ROUYRE FRANCOIS |
分类号 |
B64C1/00;B64C7/00;B64D29/06 |
主分类号 |
B64C1/00 |
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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