Kite configuration and flight strategy for flight in high wind speeds
View Patent ↗An airborne tethered flight system including a base unit, a tether having a first end attached to the base unit and a second end attached to a kite, wherein the kite comprises a main wing, a tail wing, and a tail boom attached to said main wing on a first end, said tail boom coupled to said tail wing on a second end, a plurality of vertical pylons attached to the main wing, said pylons comprising vertical airfoils adapted to provide lift, turbine driven generators mounted on the vertical airfoils attached to the main wing, and an additional vertical airfoil extending between the tail boom and tail wing.
1. An airborne tethered flight system adapted for flight in high winds, said system comprising:
a base unit;
a tether having a first end attached to the base unit and a second end attached to a kite; wherein said kite comprises:
a main wing;
a tail wing, and
a tail boom attached to said main wing on a first end, said tail boom coupled to said tail wing on a second end;
a plurality of vertical pylons attached to the main wing, said pylons comprising vertical airfoils adapted to provide lift;
turbine driven generators mounted on the vertical airfoils attached to the main wing; and
an additional vertical airfoil extending between the tail boom and tail wing.
2. The airborne tethered flight system of claim 1 wherein said vertical airfoils comprise asymmetric airfoils, wherein said asymmetric airfoils are adapted to provide lift in a direction that is the same.
3. The airborne tethered flight system of claim 1 wherein said tether comprises an external profile having helical grooves.
4. The airborne tethered flight system of claim 1 wherein said main wing comprises:
a multi-element airfoil, said multi-element airfoil comprising:
a main airfoil; and
a plurality of trailing elements, said trailing elements coupled to said main wing, said trailing elements adapted to rotate relative to said main airfoil, said trailing elements adapted to alter a coefficient of lift of said multi-element airfoil.
5. The airborne tethered flight system of claim 1 , wherein one or more of the vertical airfoils includes a rudder to control an angle of attack of the vertical airfoils.
6. The airborne tethered flight system of claim 5 , wherein a rudder is attached to the additional vertical airfoil.
7. The airborne tethered flight system of claim 1 further comprising a control system, said control system comprising flight control instructions for moderating structural loads on said flight system during cyclical flight in high winds by controlling control surfaces on said kite, said flight control instructions comprising:
instructions for commanding the kite to fly in a substantially circular flight path;
instructions for reducing the lift of said kite; and instructions for increasing the drag of said kite.
8. The airborne tethered flight system of claim 7 wherein said instructions for reducing the lift of said kite comprise instruction for adjusting the angle of said trailing elements of said multi-element airfoil.
9. The airborne tethered flight system of claim 7 wherein said instructions for increasing the drag of said kite comprise ruddering said kite, thereby increasing the drag of said vertical airfoils.
10. The airborne tethered flight system of claim 1 , wherein the additional vertical airfoil also extends beneath the tail boom.
11. A method for controlling a tethered airborne flying system, said method comprising the steps of:
providing an assessment of a structural load on the flying system while the flying system is in flight, wherein said flying system comprises:
a base unit;
a tether having a first end attached to the base unit and a second end attached to a kite; said kite comprising:
a main wing;
a tail wing, and
a tail boom attached to said main wing on a first end, said tail boom coupled to said tail wing on a second end;
a plurality of vertical pylons attached to the main wing, said pylons comprising vertical airfoils adapted to provide lift;
turbine driven generators mounted on the vertical airfoils attached to the main wing; and an additional vertical airfoil extending between the tail boom and tail wing; and
moderating the structural load on the flying system in response to the assessment of the structural load on the flying system by operating a rudder positioned on one or more of the vertical airfoils.
12. The method of claim 11 wherein said step of providing an assessment of the structural load on the flying system comprises the step of monitoring a tension of the tether.
13. The method of claim 11 wherein said step of moderating the structural load on the flying system comprises the step of:
reducing a coefficient of lift of the main wing.
14. The method of claim 11 wherein said step of moderating the structural load on the flying system comprises the step of:
increasing the drag of the flying system.
15. The method of claim 14 wherein said step of increasing the drag of the flying system comprises the step of turning the kite using rudder control adapted to increase an angle of attack of the vertical airfoils.
16. The method of claim 13 wherein the step of reducing the coefficient of lift of the main wing comprises the step of deflecting trailing elements on the main wing upwards.
17. The method of claim 11 , wherein the additional vertical airfoil also extends beneath the tail boom.
18. The method of claim 11 , wherein the rudder is positioned on the additional vertical airfoil.
19. The method of claim 11 , wherein said tether comprises an external profile having helical grooves.