发明名称 |
Flap System For An Aircraft, Method For Adjusting The Lift Of An Aircraft And Aircraft Comprising A Main Wing And At Least One Flap System |
摘要 |
A flap system for an aircraft includes a flow body, a trailing flap and a movement means. The flow body includes an upper surface and a lower surface, the lower surface having a recess. The movement means is attachable to the flow body and the trailing flap. The trailing flap includes a shape that corresponds to the recess in the lower surface. The movement means is adapted for conducting at least a chordwise movement of the trailing flap such that it is movable out of and into the recess of the flow body in absence of a gap between the leading edge of the trailing flap and the flow body. Thereby, a clear increase in a lift coefficient may be achieved, while at the same time maintaining a low complexity and a high reliability of the flap system. |
申请公布号 |
US2014166819(A1) |
申请公布日期 |
2014.06.19 |
申请号 |
US201314134102 |
申请日期 |
2013.12.19 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
Saliveros Efstratios;Friedel Hendrik |
分类号 |
B64C9/18 |
主分类号 |
B64C9/18 |
代理机构 |
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代理人 |
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主权项 |
1. A flap system for an aircraft, the flap system comprising:
a flow body; a trailing flap; and a movement means; wherein the flow body comprises an upper surface and a lower surface, the lower surface having a recess, wherein the movement means is attachable to the flow body and the trailing flap; wherein the trailing flap comprises a shape corresponding to the recess in the lower surface; and wherein the movement means is adapted for conducting at least a chordwise movement of the trailing flap such that the trailing flap is movable out of and into the recess of the flow body in absence of a gap between the leading edge of the trailing flap and the flow body.
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地址 |
Hamburg DE |