发明名称 |
AIRCRAFT ENGINE ATTACHMENT PYLON COMPRISING TWO FRONT WING SYSTEM ATTACHMENTS WITH ORTHOGONAL SHEARING PINS |
摘要 |
The present invention relates to an aircraft assembly (200) comprising a wing (2) and an engine attachment pylon (4) fixed to the wing by means of attachment means comprising a first and a second front wing system cleat (109, 109) connecting a rigid structure (108) of the attachment pylon and a front longeron (201) of the wing. The first front wing system cleat (109) comprises a first shearing pin (202) oriented in the transversal direction (Y) to ensure take-up of forces exerted in the longitudinal (X) and vertical (Z) directions of the pylon, and the second front wing system cleat (109) comprises a second shearing pin (208) oriented in the longitudinal direction (X) to ensure take-up of forces exerted in the transversal (Y) and vertical (Z) directions of the pylon.
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申请公布号 |
US2012080554(A1) |
申请公布日期 |
2012.04.05 |
申请号 |
US201113239464 |
申请日期 |
2011.09.22 |
申请人 |
LAFONT LAURENT;JOURNADE FREDERIC;RENAUD ERIC;AIRBUS OPERATIONS (S.A.S.) |
发明人 |
LAFONT LAURENT;JOURNADE FREDERIC;RENAUD ERIC |
分类号 |
B64D27/26;B64D27/02 |
主分类号 |
B64D27/26 |
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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