Tethered autonomous air vehicle with wind turbines
View Patent ↗A wind turbine energy conversion device that can take advantage of the higher speed and more persistent winds at higher altitudes is hereinafter disclosed. The wind turbine energy conversion device includes an unmanned aerial vehicle (UAV) connected to one end of a tether (which may include multiple shorter tethers), the other end being connected to a terrestrial anchorage point. The UAV flies at altitudes where wind speeds can reach 40 mph or higher. The UAV comprises a flying wing with one or more trailing wind power turbines and flies airborne maneuvers designed to increase relative wind speed up to about four times the true wind speed.
1. A wind-driven electric power generating apparatus comprising:
an air vehicle comprising:
a flying wing having a direction of travel generally perpendicular to a longitudinal length of the flying wing;
a wind power turbine coupled to a trailing edge of the wing, relative to the direction of travel, wherein the turbine comprises:
a rotor, at least one rotor blade, and an electric power generator; and
a tether comprising an insulated conductor, wherein the tether comprises at least a first end and a second end, and wherein the first end of the tether is coupled to the air vehicle and the second end of the tether is coupled to a terrestrial anchorage point on land or sea.
2. The apparatus of claim 1 , wherein the flying wing includes an elevon control surface.
3. The apparatus of claim 1 , wherein the air vehicle further comprises a wind power turbine coupled to a leading edge of the wing, relative to the direction of travel.
4. The apparatus of claim 1 , wherein the wing comprises a spool motor;
and wherein the tether is a first tether;
and wherein the air vehicle further comprises a second tether with a first end coupled to an attachment point along the first tether and a second end coupled to the spool motor;
and wherein the spool motor is adapted to lengthen or shorten the second tether.
5. The apparatus of claim 1 , wherein the wind power turbine further comprises a rotor pitch control mechanism adapted to adjust pitch of the at least one rotor blade.
6. The apparatus of claim 1 , wherein the wind power turbine further comprises a speed increasing gearbox coupled to the rotor and the electric power generator.
7. The apparatus of claim 1 , wherein the rotor is ducted and includes a nested diffuser.
8. The apparatus of claim 1 , further comprising a lighter-than-air object coupled along the tether between the first and the second end, wherein the lighter-than-air object provides lift to at least a portion of the tether.
9. A method for generating electric power, the method comprising:
coupling an air vehicle to a terrestrial anchorage point using a tether,
wherein the tether comprises an insulated conductor,
and wherein the air vehicle comprises:
a flying wing having a direction of travel generally perpendicular to a longitudinal length of the flying wing;
a wind power turbine coupled to a trailing edge of the wing, relative to the direction of travel, wherein the turbine comprises:
a rotor, at least one rotor blade, and an electric power generator; and
performing in-flight airborne maneuvers that enable the air vehicle to consistently travel at speeds faster than the true wind speed, thereby rotating the wind power turbine and thus the generator.
10. The method of claim 9 , wherein the flying wing includes an elevon control surface.
11. The method of claim 9 , wherein the air vehicle further comprises a wind power turbine coupled to a leading edge of the wing, relative to the direction of travel.
12. The method of claim 9 , wherein the wing comprises a spool motor;
and wherein the tether is a first tether;
and wherein the air vehicle further comprises a second tether with a first end coupled to an attachment point along the first tether and a second end coupled to the spool motor;
and wherein the spool motor is adapted to lengthen or shorten the second tether.
13. The method of claim 9 , wherein the turbine further comprises a rotor pitch control mechanism to adjust pitch of the at least one rotor blade.
14. The method of claim 9 , wherein the wind power turbine further comprises a speed increasing gearbox to couple to the rotor and the electric power generator.
15. The method of claim 9 , wherein the rotor is ducted and includes a nested diffuser.
16. The method of claim 9 , further comprising a lighter-than-air object adapted to couple along the tether in-between the air vehicle and the ground or sea based anchorage point and provide lift to a portion of the tether.
17. The method of claim 9 , wherein performing the in-flight airborne maneuvers comprises traveling in a circular path.
18. The method of claim 9 , wherein performing the in-flight airborne maneuvers comprises traveling in a figure-eight path.
19. The method of claim 9 , wherein the figure-eight path comprises a first generally circular path and a second generally circular path, and traveling in the figure-eight path comprises traversing the first circular path of the figure-eight path a plurality of times then traversing the second circular path of the figure-eight path a plurality of times in an opposite circular direction relative to the first circular path.
20. The method of claim 18 , wherein the figure-eight path is inclined with respect to the ground, and wherein traveling in the figure-eight path comprises reversing direction during the downward portion of the path.