发明名称 |
An aircraft with a foldable wing tip device |
摘要 |
An aircraft comprises a wing 1 and a wing tip device 6. The wing tip device 6 is moveable between a flight configuration for use during flight and a ground configuration for use during ground-based operations. In the ground configuration the wing tip device is folded inwardly from the flight configuration such that the span of the aircraft is reduced. The wing tip device 6 is connected to the wing along a hinge axis 14 by spar beams 10 and 12 of the wing tip device, one of the beams being mounted for pivoting about a fixed axis and the other beam being mounted on a spherical bearing 15 to provide greater freedom of movement. Various actuator arrangements may be provided to pivot the wing tip device. |
申请公布号 |
GB2528231(A) |
申请公布日期 |
2016.01.20 |
申请号 |
GB20140007197 |
申请日期 |
2014.04.24 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
TIM AXFORD;TONY FONG;STUART ALEXANDER |
分类号 |
B64C3/54;B64C3/56;B64C5/08 |
主分类号 |
B64C3/54 |
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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