发明名称 |
HIGH-LIFT SYSTEM ON THE WING OF AN AIRCRAFT, AND METHOD FOR ITS OPERATION |
摘要 |
<p>A high- lift system on the wing of an aircraft and a method for its operation are described. High- lift flaps (2) which are arranged on the wing (1) are extended from a retracted position in order to increase the lift, and a slot (3) through which flow passes from the lower face to the upper face of the wing (1) is opened (advanced slat/flap-gap control). According to the invention, the slot (3) through which flow passes is opened independently of the position of the high-lift flap (2). This makes it possible to selectively achieve a better maximum coefficient of lift (CL) or a better lift-to-drag ratio with less noise being produced.</p> |
申请公布号 |
WO2008058695(A1) |
申请公布日期 |
2008.05.22 |
申请号 |
WO2007EP09785 |
申请日期 |
2007.11.12 |
申请人 |
AIRBUS DEUTSCHLAND GMBH;HOLZHAUSEN, TORSTEN |
发明人 |
HOLZHAUSEN, TORSTEN |
分类号 |
B64C9/22;B64C9/24 |
主分类号 |
B64C9/22 |
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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