PHOTOVOLTAIC RECEIVER FOR BEAMED POWER

• US 20080017239A1
• Filed: 07/21/2006
• Published: 01/24/2008
• Est. Priority Date: 07/21/2006
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Tillotson, Brian J.
• Granted Patent: US 8,735,712 B2
• Time in Patent Office: Days
• US Class Current: 136/246
• CPC Class Codes: H01L 31/0232 Optical elements or arrangements associated with the device H01L31/0236 takes precedence; for photovoltaic cells H01L31/054; for photovoltaic modules H02S40/20
• CPC Class Codes: H01L 31/0543 comprising light concentrating means of the refractive type, e.g. lenses
• CPC Class Codes: H01L 31/0547 comprising light concentrating means of the reflecting type, e.g. parabolic mirrors, concentrators using total internal reflection
• CPC Class Codes: H02J 5/00 Circuit arrangements for transfer of electric power between ac networks and dc networks H02J3/36 takes precedence
• CPC Class Codes: Y02E 10/52 PV systems with concentrators

Abstract

A system and method directed to using a PV array and laser beamed-power for aircraft and satellites is provided. More specifically, a system and method directed to a PV receiver that reduces power losses caused by variations in irradiance is provided. The use of a sloped array with a grooved cover glass coated with reflective coating allows the system and method to receive the laser beamed power at an angle and reduce any losses while producing a maximum power output. In addition, the use of capacitors in parallel with the PV cells in the array reduces resistive losses caused by short-term optical fluctuations and assists in maximizing power output for the array.

Claims

1. A photovoltaic (PV) array comprising:

a plurality of photovoltaic (PV) cells, each PV cell of the plurality of PV cells being configured to receive at least one optical power beam and convert power from the at least one optical power beam to electrical power; and

wherein the PV array has a surface geometry arrangement to equalize irradiance of the PV cells received from the at least one optical power beam across the PV array.

2. The PV array of claim 1, wherein the surface geometry arrangement is a curved conical arrangement.

3. The PV array of claim 1, wherein the surface geometry arrangement is a sawtooth configuration having a plurality of cusps and a plurality of slopes.

4. The PV array of claim 3, wherein the plurality of slopes increase progressively in angle from an edge of the PV array to a center of the PV array.

5. The PV array of claim 1, wherein the PV array is configured symmetrically about an axis of the PV array and forms a circular periphery.

6. The PV array of claim 3, wherein the PV array has a rectangular side profile.

7. The PV array of claim 1, wherein the PV array having a first axis and a second axis, the PV array being rotatable about the first axis and fixed with respect to the second axis, such that the angle of incidence of the at least one optical power beam when rotatably adjusted with respect to the at least one optical power beam provides a substantially uniform irradiance along a vertical portion of the PV array.

8. The PV array of claim 7, wherein the PV array is configured in an elliptical shape.

9. The PV array of claim 1, wherein the PV array is formed by at least one string of electrically interconnected PV cells attached to a side of the PV array.

10. The PV array of claim 9 wherein the plurality of PV cells in the at least one string being electrically connected in series.

11. The PV array of claim 9 wherein each PV cell of the plurality of PV cells further includes a capacitor electrically connected in parallel therewith.

12. The PV array of claim 6 comprising a plurality of strings of PV cells, the plurality of strings in the PV array being electrically connected in parallel.

13. The PV array of claim 1 wherein the PV array further comprising a transparent, smooth window disposed over at least one surface of the PV array for reducing air turbulence when applied to an aircraft in flight.

14. The PV array of claim 1, wherein at least one PV cell of the plurality of PV cells having a coverglass covering the PV cell, and wherein the coverglass configured in a sawtooth profile having a plurality of ridges and a plurality of grooves.

15. The PV array of claim 14 wherein each groove of the plurality of grooves has a transparent first surface substantially perpendicular to the optical power beam.

16. The PV array of claim 15 wherein each groove of the plurality of grooves has a second surface, the second surface having a reflective coating and being substantially parallel to the optical power beam, wherein at least a portion of a beam impinging on the PV cell through the first surface is reflected at the reflective coating and directed back towards the PV cell to reduce reflective losses in the PV cell.

17. The PV array of claim 14 wherein the PV array is configured substantially circular or elliptical.

18. The PV array of claim 14 wherein the PV array having a first axis and a second axis, the PV array being rotatable about the first axis and fixed with respect to the second axis, such that the angle of incidence of the at least one optical power beam when rotatably adjusted with respect to the at least one optical power beam provides a substantially uniform irradiance along a vertical portion of the PV array.

19. A method of converting laser beam power to electrical energy with a photovoltaic (PV) array, the PV array comprised of a plurality of PV cells, the method comprising:

providing the PV array on an airborne vehicle, the PV array having a surface geometry arranged to equalize irradiance of the plurality of PV cells received from the laser power beam across the PV array;

directing the laser beam toward the PV array;

receiving the laser beam on the PV array;

converting the laser beam into electrical power; and

powering the airborne vehicle with the converted electrical power.

20. The method of claim 19, wherein the PV array is formed by at least one string of PV cells electrically interconnected in series attached to a side of the PV array.

21. The method of claim 19, wherein each PV cell of the plurality of PV cells further includes a capacitor electrically connected in parallel therewith.

22. The method of claim 19, wherein the step of receiving the laser beam on the PV array further comprises rotating the PV array along a first axis with respect to a second axis, such that the angle of incidence of the laser beam when rotatably adjusted with respect to the laser beam provides a substantially uniform irradiance along a vertical portion of the PV array.