Integrated thermal module and back plate structure and related methods
US-9103563-B1 · Aug 11, 2015 · US
US11387771B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11387771-B2 |
| Application number | US-201816002273-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 7, 2018 |
| Priority date | Jun 7, 2018 |
| Publication date | Jul 12, 2022 |
| Grant date | Jul 12, 2022 |
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A solar tracking system is provided and includes a solar array, a plurality of support beams configured to support the solar array, a torque tube coupled to the plurality of support beams, a base configured to rotatably support the torque tube, and an articulation system configured to rotate the torque tube relative to the base. The articulation system includes a first helical tube coupled to the torque tube, a first helical tube support disposed on the base and configured to slidably support the first helical tube, and a gearbox in mechanical communication with the first helical tube. Actuation of the gearbox causes the first helical tube to translate within the first helical tube support and the first helical tube support is configured to rotate the first helical tube as the first helical tube is translated therein to cause a corresponding rotation of the solar array.
Opening claim text (preview).
What is claimed is: 1. A solar tracking system, comprising: a solar array; a plurality of support beams configured to support the solar array; a torque tube coupled to the plurality of support beams; a base configured to rotatably support the torque tube; and an articulation system configured to rotate the torque tube relative to the base, the articulation system comprising: a first helical tube coupled to the torque tube; a first helical tube support disposed on the base and configured to slidably support the first helical tube; and a gearbox in mechanical communication with the first helical tube, wherein actuation of the gearbox causes the first helical tube and the torque tube attached thereto to translate along their longitudinal axes within the first helical tube support, and the first helical tube support is configured to rotate the first helical tube and the torque tube attached thereto as the first helical tube and the torque tube attached thereto are translated along their longitudinal axes therein to cause a corresponding rotation of the solar array. 2. The solar tracking system according to claim 1 , wherein the first helical tube defines a helical portion that follows a helical arc wound about a longitudinal axis defined by the first helical tube. 3. The solar tracking system according to claim 2 , wherein the first helical tube support includes a plurality of rollers rotatably supported thereon, the plurality of rollers configured to abut an outer surface of the helical portion of the first helical tube. 4. The solar tracking system according to claim 3 , wherein the articulation system includes a second helical tube coupled to the torque tube and a second helical tube support disposed on the base and configured to slidably support the second helical tube. 5. The solar tracking system according to claim 4 , wherein the second helical tube defines a helical portion that follows a helical arc wound about a longitudinal axis defined by the second helical tube. 6. The solar tracking system according to claim 5 , wherein the second helical tube support includes a plurality of rollers rotatably supported thereon, the plurality of rollers configured to abut an outer surface of the helical portion of the second helical tube. 7. The solar tracking system according to claim 6 , wherein the articulation system includes a power screw having a threaded outer surface extending between a first end portion and a second, opposite end portion, the power screw rotatably coupled to the gearbox, wherein the first end portion of the power screw is threadably coupled to the first helical tube and the second end portion of the power screw is threadably coupled to the second helical tube. 8. The solar tracking system according to claim 7 , wherein the power screw defines a first threaded outer surface adjacent the first end portion and a second threaded outer surface adjacent the second end portion, wherein the first threaded end portion is threaded in an opposite direction to the second threaded end portion, such that as the power screw is rotated in a first direction, the power screw draws the first and second helical portions toward one another and as the power screw is rotated in a second direction, the power screw pushes the first and second helical portions away from one another. 9. The solar tracking system according to claim 8 , wherein the helical portion of the first and second helical tubes is configured to rotate the first and second helical tubes approximately 100 degrees over a length of approximately 35 inches. 10. The solar tracking system according to claim 6 , wherein the plurality of rollers of the first and second helical tube supports defines an hourglass profile. 11. The solar tracking system according to claim 6 , wherein the plurality of rollers of the first and second helical tube supports defines a cylindrical profile. 12. A solar tracking system, comprising: a solar array; a plurality of support beams configured to support the solar array; a torque tube coupled to the plurality of support beams; a base configured to rotatably support the torque tube; and an articulation system configured to rotate the torque tube relative to the base, the articulation system comprising: a helical tube coupled to the torque tube; and a gearbox disposed on the base and configured to rotatably support the helical tube, the gearbox in mechanical communication with the helical tube, wherein actuation of the gearbox causes the helical tube to translate within the gearbox, and the gearbox is configured to rotate the helical tube and the torque tube attached thereto as the helical tube and the torque tube attached thereto are translated along their longitudinal axes to cause a corresponding rotation of the solar array. 13. The solar tracking system according to claim 12 , wherein the gearbox includes a worm gear rotatably supported therein, the worm gear in mechanical communication with the ring gear and the torque tube. 14. The solar tracking system according to claim 13 , wherein a portion of the torque tube defines a plurality of threads thereon that is configured to engage the worm gear. 15. The solar tracking system according to claim 13 , wherein the gearbox includes a flange assembly having a first flange and a second, opposite flange that is selectively couplable therewith. 16. The solar tracking system according to claim 14 , wherein each of the first and second flanges of the flange assembly defines a respective chamfer thereon that is configured to abut a corresponding tapered surface defined on the housing, wherein the chamfers of the first and second flanges and the respective tapered surfaces cooperate to rotatably support the flange assembly within the housing. 17. The solar tracking system according to claim 12 , wherein the teeth of the ring gear are disposed at an angle relative to a longitudinal axis defined through the through-bore of the housing. 18. The solar tracking system according to claim 17 , wherein the worm gear is disposed at an angle relative to the longitudinal axis defined through the through-bore of the housing. 19. The solar tracking system according to claim 18 , wherein the plurality of teeth of the torque tube is disposed at an angle relative to a longitudinal axis defined through the torque tube. 20. The solar tracking system according to claim 12 , wherein the torque tube is selectively couplable to a drive tube that is disposed within the gearbox, the drive tube defining a plurality of teeth thereon configured to engage the worm gear.
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