The invention relates to an aircraft, an aircraft wing and a manufacturing method thereof. An aircraft wing includes a fixed structure and a linear hydraulic slat actuator attached to the fixed structure. A linear hydraulic slat actuator is oriented in a spanwise direction along an aircraft wing. The aircraft wing also includes an actuator output link and a slat attached to the actuator output link. The aircraft wing also includes a crank coupled to the linear hydraulic slat actuator and the actuator output link. In response to spanwise movement of the linear hydraulic slat actuator, the crank is configured to move the actuator output link in different directions that enable movement of the slat between a retracted position and an extended position.
本公开涉及飞机、飞机机翼及其制造方法。飞机机翼包括固定结构和附接至固定结构的线性液压缝翼致动器。线性液压缝翼致动器沿飞机机翼沿翼展方向定向。飞机机翼还包括致动器输出连杆和附接到致动器输出连杆的缝翼。飞机机翼还包括曲柄,该曲柄耦接到线性液压缝翼致动器和致动器输出连杆。响应于线性液压缝翼致动器的翼展方向的运动,曲柄被配置为沿能够使缝翼在收缩位置和伸展位置之间移动的不同方向移动致动器输出连杆。
Aircraft, aircraft wing and manufacturing method thereof
飞机、飞机机翼及其制造方法
2025-03-07
Patent
Electronic Resource
Chinese
European Patent Office | 2016
|Aircraft wing rib, aircraft wing and application of aircraft wing rib and aircraft wing
European Patent Office | 2024
|Tandem wing tilting rotor aircraft and aircraft manufacturing method
European Patent Office | 2020
|