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
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