Wing tip docking system for aircraft
View Patent ↗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.
1. An aircraft, comprising:
(a) an aerodynamic lifting structure;
(b) a soft docking system configured to soft dock said aircraft with a second aircraft; and
(c) a hard docking system configured to hard dock said aircraft with the second aircraft; wherein the hard docking system comprises:
(i) a first hard docking mechanism located at a first end of the aerodynamic lifting structure; and
(ii) a second hard docking mechanism located at a second end of the aerodynamic lifting structure, wherein the first hard docking mechanism of said aircraft is configured to engage and removably attach to the second hard docking mechanism of the second aircraft, following soft docking and when said aircraft and the second aircraft are located at or less than a first predetermined distance;
(d) a first airflow adjustment mechanism located at a first end of the aerodynamic lifting structure; and
(e) a second airflow adjustment mechanism located at a second end of the aerodynamic lifting structure;
wherein the first airflow adjustment mechanism of said aircraft is adjusted to substantially reduce air vortices at the first end of the aerodynamic lifting structure, and a second airflow adjustment mechanism of the second aircraft is adjusted to substantially reduce vortices at the second end of the aerodynamic lifting structure prior to soft docking of said aircraft to the second aircraft;
wherein aerodynamic lifting structure air vortices existing around tip areas of the aerodynamic lifting structures are moved away from each respective aerodynamic lifting structure tip area.