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1. 发明申请

US20090127376A1 WING TIP DOCKING SYSTEM FOR AIRCRAFT 有权
标题翻译：飞机起落架系统
公开(公告)号：US20090127376A1
公开(公告)日：2009-05-21
申请号：US12210711
申请日：2008-09-15
申请人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
发明人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
IPC分类号： B64C37/02
CPC分类号： B64C37/02 , B64C23/076 , B64C39/024 , B64D2211/00 , Y02T50/164 , Y02T50/55
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.
摘要翻译：公开了用于对接各种类型的飞机的系统和方法。提供了用于对接两个或更多个飞行器的空气动力提升结构对接机构，其包括空气动力提升结构。空气动力提升结构包括第一和第二气流调节机构。空气动力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。第一和第二气流调节机构构造成基本上去除围绕每个空气动力提升结构尖端区域的任何空气动力学提升结构涡流。柔性对接机构被配置为使第一空气动力提升结构与第二空气动力提升结构软对接。第一硬对接机构构造成与第二硬对接机构硬地对接，从而将第一空气动力提升结构临时附接到第二空气动力提升结构。

2. 发明授权

US08172172B2 Wing tip docking system for aircraft 有权
标题翻译：翼尖飞机对接系统
公开(公告)号：US08172172B2
公开(公告)日：2012-05-08
申请号：US13299924
申请日：2011-11-18
申请人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
发明人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
IPC分类号： B64C37/02 , B64C23/06
CPC分类号： B64C37/02 , B64C23/076 , B64C39/024 , B64D2211/00 , Y02T50/164 , Y02T50/55
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.
摘要翻译：公开了用于对接各种类型的飞机的系统和方法。提供了用于对接两个或更多个飞行器的空气动力提升结构对接机构，其包括空气动力提升结构。空气动力提升结构包括第一和第二气流调节机构。空气动力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。第一和第二气流调节机构构造成基本上去除围绕每个空气动力提升结构尖端区域的任何空气动力学提升结构涡流。柔性对接机构被配置为使第一空气动力提升结构与第二空气动力提升结构软对接。第一硬对接机构构造成与第二硬对接机构硬地对接，从而将第一空气动力提升结构临时附接到第二空气动力提升结构。

3. 发明授权

US08226025B2 Wing tip docking system for aircraft 有权
公开(公告)号：US08226025B2
公开(公告)日：2012-07-24
申请号：US13299883
申请日：2011-11-18
申请人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
发明人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
IPC分类号： B64C37/02 , B64C23/06 , B64D5/00
CPC分类号： B64C37/02 , B64C23/076 , B64C39/024 , B64D2211/00 , Y02T50/164 , Y02T50/55
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.

4. 发明授权

US08061646B2 Wing tip docking system for aircraft 有权
标题翻译：翼尖飞机对接系统
公开(公告)号：US08061646B2
公开(公告)日：2011-11-22
申请号：US12210711
申请日：2008-09-15
申请人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
发明人： Martin L. Gomez , Robert Parks , Adam J. Woodworth
IPC分类号： B64C37/02 , B64C23/06 , B64D5/00
CPC分类号： B64C37/02 , B64C23/076 , B64C39/024 , B64D2211/00 , Y02T50/164 , Y02T50/55
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.
摘要翻译：公开了用于对接各种类型的飞机的系统和方法。提供了用于对接两个或更多个飞行器的空气动力提升结构对接机构，其包括空气动力提升结构。空气动力提升结构包括第一和第二气流调节机构。空气动力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。第一和第二气流调节机构构造成基本上去除围绕每个空气动力提升结构尖端区域的任何空气动力学提升结构涡流。柔性对接机构被配置为使第一空气动力提升结构与第二空气动力提升结构软对接。第一硬对接机构构造成与第二硬对接机构硬地对接，从而将第一空气动力提升结构临时附接到第二空气动力提升结构。

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