High strength windable electromechanical tether with low fluid dynamic drag and system using same

US9230714B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9230714-B2
Application numberUS-201414531449-A
CountryUS
Kind codeB2
Filing dateNov 3, 2014
Priority dateJul 19, 2010
Publication dateJan 5, 2016
Grant dateJan 5, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

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A tether, and system using such a tether, adapted to provide mechanical and electrical coupling of an airborne flying platform to the ground. The tether may have a center structural core with electrical conductors on or near the outer diameter of the tether. The tether may utilize exterior configurations adapted to reduce drag.

First claim

Opening claim text (preview).

What is claimed is: 1. A high strength tether adapted for electrical conduction and tensile loading, said tether comprising: a central core, wherein the central core comprises a center layer, and wherein the center layer comprises an axial rod; a low bulk modulus strain relief layer concentrically surrounding the central core; and a plurality of electrical conductors, said plurality of conductors located along the exterior of the low bulk modulus strain relief layer. 2. The high strength tether of claim 1 wherein said plurality of electrical conductors are helically wound along the exterior of the low bulk modulus strain relief layer. 3. The high strength tether of claim 2 wherein said plurality of electrical conductors are separated into a plurality of helically wound groups of one or more conductors defining helical spaces between said helically wound groups of one or more conductors along the exterior surface of said tether. 4. The high strength tether of claim 3 wherein each of said plurality of helically wound groups of one or more conductors are wound around a strength element. 5. The high strength tether of claim 4 wherein said strength element is a composite rod. 6. The high strength tether of claim 1 further comprising an outer sheath layer, said outer sheath layer comprising a plurality of boundary layer tripping features. 7. The high strength tether of claim 1 wherein the center layer axial rod comprises a composite material. 8. The high strength tether of claim 7 wherein the composite material comprises carbon fibers and a constraining matrix element. 9. The high strength tether of claim 7 wherein the center layer is of cylindrical cross-section. 10. A system for power generation with a tethered kite, said system comprising: a ground station; a kite, said kite comprising: a main wing; and a plurality of turbine driven generators; and a tether, said tether attached to said ground station on a first end and to a kite on a second end, said tether comprising: a central core, wherein the central core comprises a center layer, and wherein the center layer comprises an axial rod; a low bulk modulus strain relief layer concentrically surrounding the central core; and a plurality of electrical conductors, said plurality of conductors located along the exterior of the low bulk modulus strain relief layer. 11. The system of claim 10 wherein said plurality of electrical conductors are helically wound along the exterior of the low bulk modulus strain relief layer. 12. The system of claim 11 wherein said plurality of electrical conductors are separated into a plurality of helically wound groups of one or more conductors defining helical spaces between said helically wound groups of one or more conductors along the exterior surface of said tether. 13. The system of claim 12 wherein each of said plurality of helically wound groups of one or more conductors are wound around a strength element. 14. The system of claim 13 wherein said strength element is a composite rod. 15. The system of claim 10 further comprising an outer sheath layer, said outer sheath layer comprising a plurality of boundary layer tripping features. 16. The system of claim 10 wherein the center layer axial rod comprises a composite material. 17. The system of claim 16 wherein the composite material comprises carbon fibers and a constraining matrix element. 18. The system of claim 16 wherein the center layer is of cylindrical cross-section. 19. A high strength tether adapted for electrical conduction and tensile loading, said tether comprising: a central core, wherein the central core comprises a center layer; a low bulk modulus strain relief layer concentrically surrounding the central core; and a plurality of electrical conductors, said plurality of conductors located along the exterior of the low bulk modulus strain relief layer.

Assignees

Inventors

Classifications

  • attached to cables · CPC title

  • Constructional features relating to the conductors · CPC title

  • Cross-Sectional Technologies · mapped topic

  • Arrangements of electric cables or lines between relatively-movable parts · CPC title

  • characterised by their outer shape or surface properties · CPC title

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Frequently asked questions

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What does patent US9230714B2 cover?
A tether, and system using such a tether, adapted to provide mechanical and electrical coupling of an airborne flying platform to the ground. The tether may have a center structural core with electrical conductors on or near the outer diameter of the tether. The tether may utilize exterior configurations adapted to reduce drag.
Who is the assignee on this patent?
Google Inc
What technology area does this patent fall under?
Primary CPC classification D07B1/147. Mapped technology areas include Textiles & Paper.
When was this patent published?
Publication date Tue Jan 05 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).