The invention relates to an air inlet for a nacelle of an aircraft, comprising: a lip having a front edge configured to divide an air flow into an inner air flow and an outer air flow, the inner air flow entering the air inlet; an outer panel; the middle panel is inserted between the lip edge and the outer panel and is provided with a first edge connected to the lip edge at least through a first connecting part and a second edge connected to the outer panel at least through a second connecting part, the first connecting part connecting the first edge of the middle panel with the lip edge comprises at least one butt welding seam, and the second connecting part comprises at least one butt welding seam. And the outer surface of the middle panel is positioned in an extension part of the outer surface of the lip and the middle panel. The invention also relates to an aircraft comprising such an air inlet and a method for assembling an air inlet. With such air inlets, aircraft drag and fuel consumption may be reduced.
本发明涉及飞行器的短舱的空气入口,包括:唇缘,具有前边缘,前边缘被配置成将空气流分成内部和外部空气流,内部空气流进入空气入口;外部面板;中间面板,插置在唇缘与外部面板之间,具有至少通过第一连接部连接到唇缘的第一边缘和至少通过第二连接部连接到外部面板的第二边缘,将中间面板的第一边缘与唇缘相连接的第一连接部包括至少一个对接焊缝,其外面位于唇缘和中间面板的外面的延伸部中。本发明还涉及包括这种空气入口的飞行器和用于组装空气入口的方法。利用这种空气入口,飞行器的阻力和燃料消耗可以减少。
Air inlet for nacelle of aircraft, aircraft comprising air inlet and method for assembling such air inlet
飞行器的短舱的空气入口、包括空气入口的飞行器及用于组装这种空气入口的组装方法
2024-08-02
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |