SIMULATOR SYSTEM AND METHOD FOR MEASURING ACCEPTANCE ANGLE CHARACTERISTICS OF A SOLAR CONCENTRATOR
A simulator system for simulating operation of a solar module comprises a frame for holding the solar module in a testing position, a light source positioned adjacent to the solar module for directing light from the light source to the solar module, and a movable assembly for simulating movement of a solar tracker system, wherein the movable assembly moves in two axes to change an incident angle of the light with respect to the testing position of the solar module.
1 . A system for simulating operation of a solar module, the system comprising:
a frame for holding the solar module in a testing position;
a light source positioned adjacent to the solar module for directing light from the light source to the solar module; and
a movable assembly for simulating movement of a solar tracker system, wherein the movable assembly moves in two axes to change an incident angle of the light with respect to the testing position of the solar module.
2 . The system of claim 1 , further comprising a collimating optic positioned adjacent to the solar module, wherein divergent light from the light source is transformed into collimated light that is directed to the solar module.
3 . The system of claim 1 , wherein the movable assembly moves the frame.
4 . The system of claim 1 , wherein the movable assembly moves the light source.
5 . The system of claim 1 , wherein the movable assembly is capable of rotating in a vertical axis and a horizontal axis.
6 . The system of claim 1 , wherein the movable assembly is an X-Y robot device.
7 . The system of claim 1 , wherein the movable assembly is capable of moving the light source from a first position to a second position and the system further comprising a circuit for measuring a first characteristic of a solar module with the assembly in the first position and a second characteristic with the assembly in the second position.
8 . The system of claim 7 , wherein the first characteristic is an acceptance angle.
9 . The system of claim 1 further comprising a circuit for measuring a characteristic of the solar module, and wherein the characteristic is power produced by reflected light on the solar module.
10 . The system of claim 1 , wherein the movable assembly comprises a movable inner frame and a movable outer frame.
11 . The system of claim 10 , wherein the movable inner frame comprises a clamping assembly for mounting the solar module.
12 . The system of claim 1 , wherein the movable assembly is capable of moving the solar module from a first position to a second position, and the system further comprising a circuit for measuring a first characteristic of the solar module with the movable assembly in the first position and a second characteristic of the solar module with the movable assembly in the second position.
13 . The system of claim 12 , wherein the first characteristic is an acceptance angle.
14 . A method for simulating operation of a solar module, the method comprising the steps of:
providing a frame for holding the solar module in a testing position;
positioning a light source adjacent to the frame for directing light from the light source to the solar module; and
providing a movable assembly to simulate movement of a solar tracker system, wherein the assembly moves in two axes to change an incident angle of the light with respect to the testing position of the solar module.
15 . The method of claim 14 further comprising the step of positioning a reflector across from the solar module, wherein light is directed from the light source to the reflector for reflecting light to the solar module.
16 . The method of claim 14 further comprising the step of moving the frame.
17 . The method of claim 14 further comprising the step of moving the light source.
18 . The method of claim 14 further comprising the step of moving the movable assembly for translating the light source from a first position to a second position and providing a circuit for measuring a first characteristic of the solar module with the movable assembly in the first position and a second characteristic of the solar module with the movable assembly in the second position.
19 . The method of claim 18 , wherein the first characteristic is an acceptance angle.
20 . The method of claim 18 , wherein the second characteristic is an acceptance angle.