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. A method for docking together two or more aircraft, each aircraft comprising an aerodynamic lifting structure with a first end and a second end, the method comprising the steps of:
moving a first aircraft and a second aircraft such that the second end of a first aerodynamic lifting structure of the first aircraft and the first end of a second aerodynamic lifting structure are within a first predetermined distance of each other;
substantially reducing air vortices located at the second end of the first aerodynamic lifting structure of the first aircraft;
substantially reducing air vortices located at the first end of the second aerodynamic lifting structure of the second aircraft;
moving any aerodynamic lifting structure air vortices existing around tip areas of the aerodynamic lifting structures away from each respective aerodynamic lifting structure tip area; and
hard docking the first aircraft with the second aircraft.
2. The method according to claim 1 , further comprising:
soft docking the first aircraft to the second aircraft.
3. The method according to claim 2 , wherein the step of soft docking the first aircraft to the second aircraft comprises:
extending a soft docking mechanism from the second end of the first aerodynamic lifting structure of the first aircraft;
engaging the first end of the second aerodynamic lifting structure of the second aircraft with the soft docking mechanism; and
retracting the soft docking mechanism into the second end of the first aerodynamic lifting structure of the first aircraft thereby moving the first and second aircraft closer together.
4. The method according to claim 2 , wherein the soft docking mechanism comprises:
a boom assembly.
5. The method according to claim 1 , wherein the step of substantially reducing air vortices comprises:
substantially reducing or eliminating lift at tips of each of the aerodynamic lifting structures.
6. The method according to claim 5 , wherein the step of substantially reducing or eliminating lift at tips of each of the aerodynamic lifting structures comprises:
altering an airflow configuration in the tip area of each of the aerodynamic lifting structures.
7. The method according to claim 6 , wherein the step of altering an airflow configuration in a tip area of each of the aerodynamic lifting structures comprises:
moving an airflow adjustment mechanism to alter the airflow over each of the aerodynamic lifting structures.
8. The method according to claim 7 , wherein the airflow adjustment mechanism comprises a flap, aileron, and/or flaperon.
9. The method according to claim 1 , wherein the step of hard docking the first aircraft with the second aircraft comprises:
moving the first aircraft close enough to the second aircraft such that a first hard docking mechanism located at a second tip of the first aerodynamic lifting structure of the first aircraft can engage and removably attach itself to a second hard docking mechanism located at a first tip of the second aerodynamic lifting structure of the second aircraft; and
engaging the first hard docking mechanism with the second hard docking mechanism.
10. The method according to claim 9 , wherein
the first hard docking mechanism includes a gripper portion, and
the second hard docking mechanism includes a controllable piston portion and a flexible rod, wherein,
the controllable piston portion is configured to extend the flexible rod from the first aerodynamic lifting structure towards the gripper portion, and
the gripper portion is configured to grip the flexible rod, and
the controllable piston portion is further configured to retract the gripped flexible rod, thereby hard docking the first aircraft with the second aircraft.