发明名称 |
Mechanism for streamwise fowler deployment of the wing trailing or leading edge |
摘要 |
The invention is a mechanism for the streamwise deployment of an aircraft trailing or leading edge flap. The mechanism connects the spar and flap. There are a pair of swivel links which pivotally connect the spar to the flap. There are also a pair of slaving mechanisms which rotationally connect the spar to the flap by spherical bearings. A linear flap actuator initiates the combined pivotal and rotational action from the spar which translates into a single downward and rearward motion of the flap.
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申请公布号 |
US5836550(A) |
申请公布日期 |
1998.11.17 |
申请号 |
US19960757145 |
申请日期 |
1996.11.27 |
申请人 |
BOEING COMPANY |
发明人 |
PAEZ, CARLOS A. |
分类号 |
B64C9/22;(IPC1-7):B64C9/04;B64C9/28;B64C13/28 |
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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