发明名称 |
FLAP PANEL SHUTTLE SYSTEM AND METHOD THEREFOR |
摘要 |
An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally attached to the shuttle at a flap pivot. The flap panel is configured to rotate about the flap pivot. When the shuttle is deployed along a length of the flap track, the shuttle is configured to prevent rotation of the flap panel about the flap pivot, and when the shuttle is withdrawn into a stowed position, the shuttle is configured to allow the flap panel to rotate about the flap pivot. |
申请公布号 |
WO2011156347(A3) |
申请公布日期 |
2012.04.12 |
申请号 |
WO2011US39412 |
申请日期 |
2011.06.07 |
申请人 |
LAM AVIATION, INC.;LAM, LAWRENCE;LAM, MICHAEL |
发明人 |
LAM, LAWRENCE;LAM, MICHAEL |
分类号 |
B64C13/30;B64C9/16 |
主分类号 |
B64C13/30 |
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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