发明名称 |
ENGINE MOUNTING STRUCTURE INTERPOSED BETWEEN AN AIRCRAFT WING SYSTEM AND SAID ENGINE |
摘要 |
The device has a rigid structure (8) and a front aerodynamic structure (24) that is mounted on the structure (8) via a mounting unit. The mounting unit comprises two connecting rods (32) placed in a symmetric manner with respect to a vertical median plane of the device, parallel to a longitudinal direction (X) of the device. A lower end of each rod is connected to an upper spar of the structure (8) and an upper end of each rod is connected in an articulated manner to a lower spar of the structure (24). The rods are designed such that their lengths are adjustable. |
申请公布号 |
EP1928738(A1) |
申请公布日期 |
2008.06.11 |
申请号 |
EP20060806820 |
申请日期 |
2006.09.26 |
申请人 |
AIRBUS FRANCE SAS |
发明人 |
COMBES, STEPHANE;LAFONT, LAURENT |
分类号 |
B64D27/18;B64D29/02 |
主分类号 |
B64D27/18 |
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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