Spar buoy platform
An offshore airborne wind turbine system including an aerial vehicle, an electrically conductive tether having a first end secured to the aerial vehicle and a second end secured to a platform, a rotatable drum positioned on the platform, an aerial vehicle perch extending from the platform, wherein the platform is positioned on a top of a spar buoy.
1. An offshore airborne wind turbine system, comprising:
an aerial vehicle;
an electrically conductive tether having a first end secured to the aerial vehicle and a second end secured to a platform;
a rotatable drum positioned on the platform;
an aerial vehicle perch extending from the platform;
wherein the platform is positioned on a top of a spar buoy;
wherein an offset arm downwardly extends at an angle from an upper portion of the spar buoy; and
wherein a mooring line is attached to a downwardly and outwardly extending lower end of the offset arm.
2. The system of claim 1 , wherein a lower arm is attached to a lower end of the offset arm, the lower arm also attached to a lower portion of the spar buoy.
3. The system of claim 2 , wherein the mooring line is attached at an intersection between the offset arm and the lower arm.
4. The system of claim 3 , wherein when the aerial vehicle is in a crosswind flight, the top of the spar buoy tips towards the aerial vehicle.
5. The system of claim 3 , wherein the connection point is positioned at an intersection between the lower end of the offset arm and the lower arm.
6. The system of claim 1 , wherein when the aerial vehicle is being reeled in and the tether is being wound onto the rotatable drum, the aerial vehicle perch is positioned in a path of the tether being wound onto the rotatable drum.
7. The system of claim 6 , wherein the rotatable drum has a horizontal axis of rotation.
8. The system of claim 1 , wherein the platform has a frequency of oscillation that is between 0.5 and 2 times a period of a loop flown by the aerial vehicle.
9. The system of claim 8 , wherein the platform has a frequency of oscillation of 10-20 seconds and the period of the loop flown by the aerial vehicle is 10-20 seconds.
10. The system of claim 1 , wherein the spar buoy has a first orientation when the aerial vehicle is perched on the aerial vehicle perch and a second orientation when the aerial vehicle is in a flying mode.
11. The system of claim 10 , wherein the spar buoy is angled away from vertical towards the aerial vehicle in the second orientation when the aerial vehicle is in the flying mode.
12. The system of claim 10 , wherein a waterline level of the spar buoy in the first orientation is different from a waterline level in a second orientation.
13. The system of claim 10 , wherein a response from the spar buoy changes under flight loads to reduce damping and increase energy stored by the aerial vehicle through a change in a waterline level, a roll or pitch angle, or a change in a tether tension.
14. An offshore airborne wind turbine system, comprising:
an aerial vehicle;
an electrically conductive tether having a first end secured to the aerial vehicle and a second end secured to a platform;
a rotatable drum positioned on the platform;
an aerial vehicle perch extending from the platform;
wherein the platform is positioned on a top of a spar buoy; and
wherein an offset arm downwardly extends at an angle from an upper portion of the spar buoy;
wherein a lower arm is attached to a lower end of the offset arm, the lower arm also attached to a lower portion of the spar buoy;
wherein the offset arm includes a connection point on a lower end of the offset arm for attachment to a mooring line; and
wherein a pulling force of the aerial vehicle causes a tension load to extend axially through the offset arm and the mooring line attached to the lower end of the offset arm.
15. An offshore airborne wind turbine system, comprising:
an aerial vehicle;
an electrically conductive tether having a first end secured to the aerial vehicle and a second end secured to a platform;
a rotatable drum positioned on the platform;
an aerial vehicle perch extending from the platform;
wherein the platform is positioned on a top of a spar buoy;
wherein the spar buoy has a first orientation when the aerial vehicle is perched on the aerial vehicle perch and a second orientation when the aerial vehicle is in a flying mode;
wherein the spar buoy is angled towards the aerial vehicle in the second orientation when the aerial vehicle is in the flying mode; and
wherein the spar buoy is angled in a direction in the first orientation that is opposite of the direction in the second orientation.