Articulation joints for terrain following solar tracker

Patent metadata

Field	Value
Publication number	US-11874030-B2
Application number	US-202218080314-A
Country	US
Kind code	B2
Filing date	Dec 13, 2022
Priority date	Oct 21, 2021
Publication date	Jan 16, 2024
Grant date	Jan 16, 2024

Abstract

A coupling system for use with a solar tracker includes a support flange, a swivel flange rotatably supported on the support flange, an articulation joint interposed between each of the support flange and the swivel flange and rotatably supported by each of the support flange and the swivel flange, wherein opposed first and second end portions of the articulation joint are configured to be operably coupled to a respective first and second torque tube, and at least one locking fastener selectively coupled to a portion of the support flange and a portion of the swivel flange, the at least one locking fastener configured to selectively inhibit rotation of the swivel flange relative to the support flange.

First claim

What is claimed is:

1. A coupling system for use with a solar tracker, comprising:
a pair of cradles, each cradle of the pair of cradles operably coupled to a respective portion of an articulation joint interposed between the pair of cradles, wherein a first cradle of the pair of cradles is rotatable relative to a second cradle of the pair of cradles about a transverse axis, the transverse axis offset from a center portion defined between the pair of cradles in a longitudinal direction,
wherein each of the pair of cradles is configured to receive a portion of a respective torque tube therein.

2. The coupling system according to claim 1 , further comprising a support flange rotatably supporting a first portion of the articulation joint and a swivel flange rotatably supporting a second portion of the articulation joint, the second portion of the articulation joint operably coupled to the first portion of the articulation joint.

3. The coupling system according to claim 2 , wherein the swivel flange is rotatably supported on the support flange such that the swivel flange is selectively permitted to rotate relative to the support flange about a first axis.

4. The coupling system according to claim 3 , wherein the articulation joint is rotatably supported by the support flange and the swivel flange about a second axis that is generally transverse to the first axis.

5. The coupling system according to claim 2 , further comprising at least one locking fastener, the at least one locking fastener selectively coupled to a portion of each of the support flange and the swivel flange, the at least one locking fastener configured to selectively inhibit rotation of the swivel flange relative to the support flange.

6. The coupling system according to claim 5 , wherein the at least one locking fastener is configured to permit rotation of the pair of cradles relative to one another when placed in a first, unlocked position and inhibit rotation of the pair of cradles relative to one another when placed in a second, locked position.

7. The coupling system according to claim 5 , wherein the at least one locking fastener is operably coupled to a slot having an arcuate profile.

8. The coupling system according to claim 2 , further comprising a pair of stow stops disposed on the support flange, the pair of stow stops configured to selectively abut a respective portion of a cradle of the pair of cradles to inhibit over rotation of the pair of cradles in a first direction and in a second direction.

9. A solar tracker, comprising:
at least one pier;
a pair of torque tubes, wherein the at least one pier is interposed between the pair of torque tubes; and
a coupling system, the coupling system including:
a pair of cradles, each cradle of the pair of cradles operably coupled to a respective portion of an articulation joint interposed between the pair of cradles, wherein a first cradle of the pair of cradles is rotatable relative to a second cradle of the pair of cradles about a transverse axis, the transverse axis offset from a center portion defined between the pair of cradles in a longitudinal direction,
wherein each of the pair of cradles is configured to receive a portion of a respective torque tube therein.

10. The solar tracker according to claim 9 , wherein the coupling system further comprises a support flange rotatably supporting a first portion of the articulation joint and a swivel flange rotatably supporting a second portion of the articulation joint, the second portion of the articulation joint operably coupled to the first portion of the articulation joint.

11. The solar tracker according to claim 10 , wherein the swivel flange is rotatably supported on the support flange such that the swivel flange is selectively permitted to rotate relative to the support flange about a first axis.

12. The solar tracker according to claim 11 , wherein the articulation joint is rotatably supported by the support flange and the swivel flange about a second axis that is generally transverse to the first axis.

13. The solar tracker according to claim 10 , further comprising at least one locking fastener, the at least one locking fastener selectively coupled to a portion of each of the support flange and the swivel flange, the at least one locking fastener configured to selectively inhibit rotation of the swivel flange relative to the support flange.

14. The solar tracker according to claim 13 , wherein the at least one locking fastener is configured to permit rotation of the pair of cradles relative to one another when placed in a first, unlocked position and inhibit rotation of the pair of cradles relative to one another when placed in a second, locked position.

15. The solar tracker according to claim 13 , wherein the at least one locking fastener is operably coupled to a slot having an arcuate profile.

16. The solar tracker according to claim 10 , further comprising a pair of stow stops disposed on the support flange, the pair of stow stops configured to selectively abut a respective portion of a cradle of the pair of cradles to inhibit over rotation of the pair of cradles in a first direction and in a second direction.

17. A coupling system for use with a solar tracker, comprising:
a support flange;
a swivel flange rotatably supported on the support flange at a location that is offset from a center portion of the support flange;
an articulation joint, the articulation joint interposed between each of the support flange and the swivel flange and rotatably supported by each of the support flange and the swivel flange, wherein opposed first and second end portions of the articulation joint are configured to be operably coupled to a respective first and second torque tube.

18. The coupling system according to claim 17 , wherein the swivel flange is rotatably supported on the support flange such that the swivel flange is selectively permitted to rotate relative to the support flange about a first axis.

19. The solar tracker according to claim 18 , wherein the articulation joint is rotatably supported by the support flange and the swivel flange about a second axis that is generally transverse to the first axis.

20. The solar tracker according to claim 17 , further comprising a pair of stow stops disposed on the support flange, the pair of stow stops configured to selectively abut a respective portion of a cradle of the pair of cradles to inhibit over rotation of the pair of cradles in a first direction and in a second direction.

Assignees

• Nextracker Llc

Inventors

• Delgado-Nanez Ricardo
• Tsim Kin

Classifications

• F24S2025/019

  Means for accommodating irregularities on mounting surface; Tolerance compensation means · CPC title

• F24S30/455 Primary

  Horizontal primary axis · CPC title

• F24S30/458

  with inclined primary axis · CPC title

• F24S2030/16

  Hinged elements; Pin connections · CPC title

• F24S2030/19

  Movement dampening means; Braking means · CPC title