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WING TIP DOCKING SYSTEM FOR AIRCRAFT

机译:飞机翼尖对接系统

摘要

A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.
机译:公开了一种用于对接各种类型的飞机的系统和方法。提供了一种用于对接两个或更多个飞机的空气动力学升降结构对接机构,其包括空气动力学升降结构。气动升降结构包括第一和第二气流调节机构。空气动力学提升结构还包括第一硬对接机构和第二硬对接机构,并且还包括软对接机构。第一气流调节机构和第二气流调节机构构造成基本去除围绕每个空气动力学提升结构末端区域的任何空气动力学提升结构旋涡。软对接机构构造成将第一空气动力学提升结构与第二空​​气动力学提升结构软对接。第一硬对接机构构造成与第二硬对接机构硬对接,从而将第一空气动力学提升结构与第二空​​气动力学提升结构临时附接。

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