发明名称 |
SYSTEMS AND METHODS FOR CONTROLLING AIRCRAFT FLAPS AND SPOILERS |
摘要 |
Systems and methods for controlling aircraft flaps and spoilers. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned proximate to the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally continuous contour with an upper surface of the wing, a second spoiler position deflected downwardly from the first, and a third spoiler position deflected upwardly from the first. A second actuator can be operatively coupled to the spoiler to move the spoiler among the first, second and third spoiler positions in a manner that is mechanically independent of the motion of the flap. |
申请公布号 |
EP1843943(B1) |
申请公布日期 |
2010.05.12 |
申请号 |
EP20060734316 |
申请日期 |
2006.02.03 |
申请人 |
THE BOEING COMPANY |
发明人 |
BLEEG, ROBERT, J.;HUYNH, NEAL, V.;STANDLEY, JOHN, A.;PEPPER, SCOTT;BOCKSCH, BRIAN, L. |
分类号 |
B64C9/20;B64C9/32 |
主分类号 |
B64C9/20 |
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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