The invention relates to an aircraft wing and an aircraft comprising the aircraft wing. An aircraft wing includes a wing structure that supports a wing cover having an outer aerodynamic surface, and a pop-up spoiler unit that includes an actuation mechanism and a spoiler coupled to the actuation mechanism. The spoiler is movable by an actuation mechanism to deploy through an aperture in the wing cover. The pop-up spoiler unit is mounted to the wing structure so as to be substantially isolated from wing bending deflection. The wing structure has a neutral plane that is substantially neither stretched nor compressed during bending of the wing structure. The pop-up spoiler unit is mounted to the wing structure with only two pin joints, the two pin joints each having a respective pin axis about which the pop-up spoiler unit is substantially free to rotate, and each pin axis lies substantially in a neutral plane.
本发明涉及飞行器机翼及包括该飞行器机翼的飞行器。飞行器机翼包括机翼结构和弹出式扰流板单元,该机翼结构支承具有外部空气动力学表面的机翼覆盖件,该弹出式扰流板单元包括致动机构和联接至致动机构的扰流板。扰流板能够通过致动机构移动以部署通过机翼覆盖件中的孔口。弹出式扰流板单元安装至机翼结构以便基本上与机翼弯曲偏转隔离。机翼结构具有中性平面,该中性平面在机翼结构的弯曲期间基本上既不拉伸也不压缩。弹出式扰流板单元仅以两个销接头安装至机翼结构,两个销接头各自具有相应的销轴线,弹出式扰流板单元绕该销轴线基本上自由旋转,并且每个销轴线基本上位于中性平面中。
Aircraft wing and aircraft comprising same
飞行器机翼及包括该飞行器机翼的飞行器
2024-07-26
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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