System and method for flexible solar tracker and testing
Disclosed herein is a technique of configuring flexible photovoltaic tracker systems with high damping and low angle stow positions. Under dynamic environmental loads implementing a high amount of damping (e.g., greater than 25% of critical damping, greater than 50% of critical damping) or a very high amount of damping (e.g., 100% or greater of critical damping, infinite damping) enables the flexible tracker system to prevent problematic aeroelastic behaviors while positioned in a low stow angle. The disclosed technique is further applied to a prototyping process during wind tunnel testing.
1. A flexible solar tracker system comprising:
a set of dampers having total system damping ratio against row rotation greater than 25% of critical damping when measured under peak design wind loading, wherein total system damping of the flexible solar tracker system is predetermined; and
a set of actuators configured to position the flexible solar tracker system in a low angle stow position.
2. The system of claim 1 , wherein the low angle stow position is less than 20 degrees from horizontal plane.
3. The system of claim 1 , wherein the total system damping is predetermined based on any of:
a pluck test;
a predictive model; or
previous wind tests.
4. The system of claim 1 , wherein the total system damping ratio is critically damped.
5. The system of claim 1 , wherein total system damping ratio is overdamped.
6. The system of claim 1 , further including:
a set of panels that are positioned by the set of actuators.
7. The system of claim 6 , wherein the set of panels are non-functional, substitute panels.
8. A method of prototyping a solar tracker in a wind testing region comprising:
determining total system damping of a flexible solar tracker system when measured under peak design wind loading;
configuring the flexible solar tracker system in a testing space, the flexible solar tracker system having total system damping ratio against row rotation greater than 25% of critical damping when measured under peak design wind loading and the flexible solar tracker system arranged via a point of fixity in a low angle stow position; and
in response to said configuring, executing a dynamic loading wind test on the flexible solar tracker system.
9. The method of claim 8 , further comprising:
in response to said executing, selecting the total system damping ratio against row rotation based on results of the dynamic loading wind test.
10. The method of claim 8 , further comprising:
in response to said executing, modifying structural components of the flexible solar tracker system based on results of the dynamic loading wind test.
11. The method of claim 8 , wherein the low angle stow position is less than 20 degrees from horizontal plane.
12. The method of claim 8 , wherein said determining total system damping is based on any of:
a pluck test;
a predictive model; or
previous wind tests.
13. The method of claim 8 , wherein the total system damping ratio is critically damped.
14. The method of claim 8 , wherein total system damping ratio is overdamped.
15. The method of claim 8 , wherein measurements of loading into a damper assembly with an aeroelastic wind test or similar analysis shows the damper assembly to prevent damage resulting from environmental wind loading.
16. The method of claim 8 , wherein the flexible solar tracker system includes substitute panels.
17. A method of prototyping a solar tracker in a wind testing region comprising:
arranging a flexible solar tracker system in a testing region, the flexible solar tracker system having total system damping ratio against row rotation at or greater than critical damping when measured under peak design wind loading and the flexible solar tracker system arranged via a point of fixity in a low angle stow position;
in response to said arranging, executing a dynamic loading wind test on the flexible solar tracker system; and
in response to said executing, selecting the total system damping ratio against row rotation based on results of the dynamic loading wind test.
18. The method of claim 17 , further comprising:
determining a total system damping of the flexible solar tracker system when measured under peak design wind loading.
19. The method of claim 17 , further comprising:
in response to said executing, modifying structural components of the flexible solar tracker system based on results of the dynamic loading wind test.
20. The method of claim 17 , wherein measurements of loading into a damper assembly with an aeroelastic wind test or similar analysis shows the damper assembly to prevent damage resulting from an environmental wind loading.
21. The method of claim 17 , wherein the flexible solar tracker system includes substitute panels.
22. The method of claim 17 , wherein the low angle stow position is less than 20 degrees from horizontal plane.