发明名称 |
ACTUATION SYSTEM FOR LEADING EDGE HIGH-LIFT DEVICE |
摘要 |
<p>An actuation system configured to deploy a high-lift device on a leading edge of an aircraft wing. The system comprises: a link pivotally connected to the wing at a first pivot point and to the high-lift device at a second pivot point; a first actuation mechanism configured to rotate the high-lift device about the first pivot point; and a second actuation mechanism configured to rotate the high-lift device about the second pivot point. The second actuation mechanism is operable independently of the first actuation mechanism, and can be operated in order to generate a sealing force between the high-lift device and the leading edge of the aircraft wing.</p> |
申请公布号 |
EP2214959(A1) |
申请公布日期 |
2010.08.11 |
申请号 |
EP20080806803 |
申请日期 |
2008.10.27 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
CATHELAIN, FRANCOIS;KAY, EDMUND |
分类号 |
B64C9/24 |
主分类号 |
B64C9/24 |
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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