The invention provides a wing assembly for an aircraft and the aircraft. In particular, the wing assembly includes a wing structure for supporting a wingtip device, the wing structure including a first spanwise portion having an outer surface profile with a depth tapering outward in a spanwise direction and a second spanwise portion disposed outward of the first spanwise portion in the spanwise direction, the first spanwise portion having an outer surface profile with a depth tapering outward in the spanwise direction, and the second spanwise portion having an outer surface profile with a depth tapering outward in the spanwise direction. The second span-wise portion has an outer surface profile substantially consistent in depth along the span-wise direction; a wing tip device located at an outboard end portion of the wing structure; and a coupling device configured to support the wingtip device for movement between a flight configuration used during flight, in which the wingtip device protrudes from the wing structure for increasing the wingspan of the aircraft, and a ground configuration used during ground-based maneuver, in which the wingtip device extends from the wing structure for increasing the wingspan of the aircraft, in which the wingtip device extends from the wing structure for increasing the wingspan of the aircraft. The wingtip device is positioned away from the flight configuration for reducing the span of the aircraft.
本发明提供了一种用于飞行器的机翼组件和飞行器。特别地,该机翼组件包括:机翼结构件,其用于支承翼梢装置,该机翼结构件包括第一翼展部分和第二翼展部分,第一翼展部分具有沿翼展方向向外深度逐渐减小的外表面轮廓,第二翼展部分沿翼展方向设置在第一翼展部分的外侧,第二翼展部分具有沿着翼展方向深度基本上一致的外表面轮廓;翼梢装置,其位于机翼结构件的外侧端部部分处;以及联结装置,其造成支承翼梢装置,翼梢装置用于在飞行期间使用的飞行构型与基于地面操纵期间使用的地面构型之间移动,在飞行构型中,翼梢装置从机翼结构件伸出以用于增加飞行器的翼展,在地面构型中,翼梢装置远离飞行构型定位以用于减小飞行器的翼展。
Wing assembly for aircraft and aircraft
用于飞行器的机翼组件和飞行器
2023-11-28
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |