Variable cross section tether
The exemplary embodiments herein provide a tether for use with an airborne device, where the tether contains an elongate member having a first end for attaching to a ground attachment point and an opposing second end for attaching to the airborne device where the elongate member has a cross-sectional area which varies across the member. In some embodiments, the tether contains one or more electrically conductive elements, an optional strength element, insulation separating any adjacent electrically conductive elements, and a jacket which surrounds and protects each of the tether components.
1. A tether for use with an airborne device, the tether comprising:
an elongate member having
a first end for attaching to a ground attachment point,
an opposing second end for attaching to the airborne device, and
an electrically conductive element that runs from the first end of the elongate member to the second end of the elongate member;
wherein the electrically conductive element has a cross-sectional area which varies across the elongate member.
2. The tether of claim 1 wherein:
the cross-sectional area of the electrically conductive element varies in discreet variation points.
3. The tether of claim 1 wherein:
the cross-sectional area of the electrically conductive element varies continuously across the member.
4. The tether of claim 1 wherein:
the cross-sectional area of the electrically conductive element varies near the mid-point of the tether.
5. The tether of claim 1 wherein:
the cross-sectional area of the electrically conductive element varies at least 2 times.
6. The tether of claim 1 further comprising:
a strength member running alongside the electrically conductive element and a jacket which surrounds the electrically conductive element, insulation, and strength member.
7. The tether of claim 1 wherein:
the cross-sectional area of a portion of the electrically conductive element that is near the ground connection point has a larger cross-sectional area than the remainder of the electrically conductive element.
8. The tether of claim 1 further comprising:
the cross-sectional area of a portion of the electrically conductive element that is near the attachment with the airborne device has a larger cross-sectional area than the remainder of the electrically conductive element.
9. The tether of claim 1 wherein:
the elongate member further comprises
a layer of insulation surrounding the electrically conductive element;
a second electrically conductive element which is alongside the first electrically conductive element and separated by the layer of insulation,
a strength member alongside the first and second electrically conductive elements, and
a jacket which surrounds the electrically conductive element, second electrically conductive element, insulation, and strength member.
10. An airborne wind energy system comprising:
an airborne device;
a tether comprised of an elongate member having a first end connected to the airborne device for and an opposing second end for; and
a ground station connected to the second end of the tether;
where the elongate member is comprised of an electrically conductive element having at least two sections with different cross-sectional areas.
11. The tether of claim 10 wherein:
the cross-sectional area of a section of the electrically conductive element found near the ground station has a larger cross-sectional area than the remainder of the electrically conductive element found along the elongate member.
12. The airborne wind energy system of claim 10 wherein:
one section of the electrically conductive element has a cross-sectional area that varies continuously.
13. The airborne wind energy system of claim 10 wherein:
one section of the electronically conductive element is near the attachment point with the ground station and has a smaller cross-sectional area than the remainder of the electronically conductive element.
14. The airborne wind energy system of claim 10 wherein:
one section of the electronically conductive element is near the attachment point with the airborne device and has a larger cross-sectional area than the remainder of the electronically conductive element.
15. A tether for use with an airborne device, the tether comprising:
an elongate member comprised of:
an electrically conductive member,
an insulation layer which surrounds the electrically conductive member,
a strength member; and
an outer jacket which surrounds the electrically conductive member, the insulation layer, and the strength member,
where the cross-sectional area of the electrically conductive member is different at two or more positions along the elongate member.
16. The tether of claim 15 further comprising:
a second electrically conductive member inside the outer jacket.
17. The tether of claim 15 wherein:
the electrically conductive member, the insulation layer, the strength member, and the outer jacket are each co-axial with one another.
18. The tether of claim 15 wherein:
the cross-sectional area of the electrically conductive member at a first position along the elongate member is approximately double the cross-sectional area of the electrically conductive member at a second position along the elongate member.
19. The tether of claim 18 wherein:
the tether has a first cross-sectional area of the electrically conductive member near an end of the elongate member while a central portion of the tether has a second cross-sectional area of the electrically conductive member,
where the second cross-sectional area is smaller than the first cross-sectional area.
20. The tether of claim 19 wherein:
the portion of the tether having the first cross-sectional area attaches to a ground connection.