An aircraft structure and a method of manufacturing the aircraft structure. Systems and methods for an aerodynamic device with a lap splice that includes an edge panel is described herein. In edge panel can include a tapered section. A portion of a skin of the aerodynamic device can be disposed below the tapered section. One or both of the edge panel or the skin can be composite. The tapered section of the edge panel can be formed by decreasing the ply thickness of the edge panel.
本公开涉及飞机结构和制造飞机结构的方法。一种用于空气动力学设备的系统和方法,该空气动力学设备具有包括边缘面板的互搭接头。在边缘中,面板可包括锥形段。空气动力学设备的蒙皮的一部分可设置在锥形段的下方。边缘面板或蒙皮中的一者或两者可以是复合的。可以通过减小边缘面板的板层厚度形成边缘面板的锥形段。
Aircraft structure and method of manufacturing aircraft structure
飞机结构和制造飞机结构的方法
2020-12-11
Patent
Electronic Resource
Chinese
AIR-CONDITIONING DUCT STRUCTURE OF AIRCRAFT, AIRCRAFT, AND METHOD OF MANUFACTURING AIRCRAFT
European Patent Office | 2020
|European Patent Office | 2016
|European Patent Office | 2018
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