Nodes for multiple aerial vehicles connected to a single ground station

Patent metadata

Field	Value
Publication number	US-10145356-B1
Application number	US-201715669008-A
Country	US
Kind code	B1
Filing date	Aug 4, 2017
Priority date	Aug 4, 2017
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

Airborne wind turbine systems with multiple aerial vehicles connected via multiple tethers to a single ground station are disclosed. A node is coupled to the tethers. The node includes a drive system. At a proximate end of the node, each of the tethers is adjacent to neighboring tethers. And at a distal end of the node, each of the tethers is separated from the neighboring tethers. The airborne wind turbine system includes a control system configured to operate the drive system to translate the node along the tethers.

First claim

The invention claimed is:

1. An airborne wind turbine system, comprising:
a ground station;
a plurality of aerial vehicles;
a plurality of tethers, wherein each tether of the plurality of tethers comprises an electrical conductor, wherein a distal end of each tether of the plurality of tethers is coupled to a respective aerial vehicle of the plurality of aerial vehicles, and wherein a proximate end of each tether of the plurality of tethers is coupled to the ground station;
a node coupled to the plurality of tethers, wherein the plurality of tethers pass through the node, wherein, at a proximate end of the node, each tether of the plurality of tethers is adjacent to neighboring tethers of the plurality of tethers, wherein, at a distal end of the node, each tether of the plurality of tethers is separated from the neighboring tethers of the plurality of tethers, wherein the node comprises a drive system, and wherein the drive system comprises:
a first clamp coupled to the node,
a second clamp coupled to the node, and
a linear drive system; and

a control system configured to operate the drive system to translate the node along the plurality of tethers, wherein the control system is further configured to:
operate the first clamp to apply a compressive force to the plurality of tethers,
operate the linear drive system to translate the second clamp,
operate the second clamp to apply a second compressive force to the plurality of tethers, and
operate the linear drive system to translate the node.

2. The airborne wind turbine system of claim 1 , wherein each tether of the plurality of tethers has a length between the distal end of the node and respective aerial vehicle, and wherein the lengths of each tether of the plurality of tethers are substantially the same.

3. The airborne wind turbine system of claim 1 , wherein each tether of the plurality of tethers has a length between the distal end of the node and respective aerial vehicle, and wherein the lengths of each tether of the plurality of tethers is different than the lengths of the other tethers in the plurality of tethers.

4. The airborne wind turbine system of claim 1 further comprising:
a junction between the ground station and the node, wherein the proximate end of each tether of the plurality of tethers is coupled to the junction; and
an auxiliary tether, wherein the auxiliary tether comprises a second electrical conductor, wherein a distal end of the auxiliary tether is coupled to the junction, and wherein a proximate end of the auxiliary tether is coupled to the ground station.

5. The airborne wind turbine system of claim 1 , wherein the node comprises a proximate opening at the proximate end of the node and a distal opening at the distal end of the node, and wherein a diameter of the distal opening is greater than a diameter of the proximate opening.

6. An airborne wind turbine system, comprising:
a ground station;
a plurality of aerial vehicles;
a plurality of tethers, wherein each tether of the plurality of tethers comprises an electrical conductor, wherein a distal end of each tether of the plurality of tethers is coupled to a respective aerial vehicle of the plurality of aerial vehicles, and wherein a proximate end of each tether of the plurality of tethers is coupled to the ground station;
a node coupled to the plurality of tethers, wherein the plurality of tethers pass through the node, wherein, at a proximate end of the node, each tether of the plurality of tethers is adjacent to neighboring tethers of the plurality of tethers, wherein, at a distal end of the node, each tether of the plurality of tethers is separated from the neighboring tethers of the plurality of tethers, wherein the node comprises a drive system, wherein the drive system comprises a plurality of convex surfaces coupled to the node, wherein each tether of the plurality of tethers comprises a plurality of cavities, wherein each convex surface of the plurality of convex surfaces comprises a plurality of protrusions, and wherein, for each tether, a convex surface of the plurality of convex surfaces is configured to mesh with the plurality of cavities; and
a control system configured to operate the drive system to translate the node along the plurality of tethers, wherein the control system is further configured to translate the plurality of convex surfaces along the plurality of tethers.

7. The airborne wind turbine system of claim 6 , wherein each tether of the plurality of tethers has a length between the distal end of the node and respective aerial vehicle, and wherein the lengths of each tether of the plurality of tethers are substantially the same.

8. The airborne wind turbine system of claim 6 , wherein each tether of the plurality of tethers has a length between the distal end of the node and respective aerial vehicle, and wherein the lengths of each tether of the plurality of tethers is different than the lengths of the other tethers in the plurality of tethers.

9. The airborne wind turbine system of claim 6 further comprising:
a junction between the ground station and the node, wherein the proximate end of each tether of the plurality of tethers is coupled to the junction; and
an auxiliary tether, wherein the auxiliary tether comprises a second electrical conductor, wherein a distal end of the auxiliary tether is coupled to the junction, and wherein a proximate end of the auxiliary tether is coupled to the ground station.

10. The airborne wind turbine system of claim 6 , wherein the node comprises a proximate opening at the proximate end of the node and a distal opening at the distal end of the node, and wherein a diameter of the distal opening is greater than a diameter of the proximate opening.

11. An airborne wind turbine system, comprising:
a ground station;
a plurality of aerial vehicles;
a plurality of tethers, wherein each tether of the plurality of tethers comprises an electrical conductor, wherein a distal end of each tether of the plurality of tethers is coupled to a respective aerial vehicle of the plurality of aerial vehicles, and wherein a proximate end of each
tether of the plurality of tethers is coupled to the ground station;
a node coupled to the plurality of tethers, wherein the plurality of tethers pass through the node, wherein, at a proximate end of the node, each tether of the plurality of tethers is adjacent to neighboring tethers of the plurality of tethers, wherein, at a distal end of the node, each tether of the plurality of tethers is separated from the neighboring tethers of the plurality of tethers, and wherein the node comprises a drive system, wherein the drive system comprises a plurality of convex surfaces coupled to the node, wherein each tether of the plurality of tethers comprises a plurality of protrusions, wherein each convex surface of the plurality of convex surfaces comprises a sprocket, and wherein, for each tether, the sprocket is configured to mesh with the plurality of protrusions; and
a control system configured to operate the drive system to translate the node along the plurality of tethers, wherein the control system is further configured to translate the plurality of convex surfaces along the plurality of tethers.

12. The airborne wind turbine system of claim 11 , wherein each tether of the plurality of tethers has a length between the distal end of the node and respective aerial vehicle, and wherein the lengths of each tether of the plurality of tethers are substantially the same.

13. The airborne wind turbine system of claim 11 , wherein each tether of the plurality of tethers has a length between the distal end of the node and respective a

Assignees

• X Dev Llc

Inventors

• Nordstrom Charles
• Su Robbie Philip
• Patten Elias Wolfgang
• Atwater Joel Fraser
• Felker Fort

Classifications

• F05B2240/40

  Use of a multiplicity of similar components · CPC title

• F05B2240/921

  kept aloft due to aerodynamic effects · CPC title

• F03D5/00

  Other wind motors (controlling thereof F03D7/00) · CPC title

• B64F3/02

  with means for supplying electricity to aircraft during flight · CPC title

• F05B2240/917

  attached to cables · CPC title