发明名称 |
DEVICE FOR ATTACHING AN AIRCRAFT ENGINE COMPRISING A THRUST FORCE TAKE-UP DEVICE WITH A COMPACT DESIGN |
摘要 |
An aircraft engine attachment device including a rigid structure and a mechanism attaching the engine on the rigid structure, the attachment mechanism including a rear engine attachment and a device for taking-up thrust forces generated by the engine. The rear engine attachment is attached to the rigid structure by two lateral fittings attached to the rigid structure. The force take-up device includes two connecting rods mechanically connected to a spreader beam by a mechanical connection, a connection fitting attached to the rear engine attachment and mechanically connected to the rigid structure by a thrust pin, the lateral fittings including a stop mechanism to limit pivoting of the spreader beam if a connecting rod breaks and ensuring transmission of thrust forces to the rigid structure.
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申请公布号 |
US2011114786(A1) |
申请公布日期 |
2011.05.19 |
申请号 |
US20080674555 |
申请日期 |
2008.08.22 |
申请人 |
AIRBUS OPERATIONS (INC. AS A SOC. PAR ACT. SIMPL.) |
发明人 |
GUILLET EMMANUEL;MARTINOU JEAN-MARC;GARDES PASCAL |
分类号 |
B64D27/02;B64D27/26 |
主分类号 |
B64D27/02 |
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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