发明名称 |
REAR SECTION OF AN AIRCRAFT INCLUDING AN ENGINE MOUNTING STRUCTURE SWINGABLY MOUNTED ON THE FUSELAGE |
摘要 |
<p>A rear part of an aircraft including two connecting rods positioned symmetrically on either side of a median vertical plane, wherein each connecting rod has an end mounted on a support structure of the engines and another end mounted on the fuselage, wherein this part is configured to allow, by rotation of the connecting rods around their axes of rotation, an oscillating movement of limited amplitude of the assembly formed by the support structure and the engines, relative to the fuselage, through the first and second fuselage openings.</p> |
申请公布号 |
EP2414228(B1) |
申请公布日期 |
2015.03.11 |
申请号 |
EP20100715989 |
申请日期 |
2010.03.29 |
申请人 |
AIRBUS OPERATIONS |
发明人 |
LAFONT, LAURENT;SAUCRAY, JEAN MICHEL;QUIROZ-HERNANDEZ, ESTEBAN;ANTYPAS, JÉRÔME;BONNET, MATHIEU;JOURNADE, FRÉDÉRIC |
分类号 |
B64D27/20;B64D27/14;B64D29/04 |
主分类号 |
B64D27/20 |
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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