IP Library › Granted Patent US 10,236,822
Granted Patent B2
US 10,236,822 · App. 14/656,259 · Granted Mar 19, 2019

Method and apparatus for calibrating a micro-concentrator solar array

Inventors: Scott Benjamin Singer (Sherman Oaks, CA); Dimitri D. Krut (Encino, CA); Nasser H. Karam (LaCanada, CA)
Assignee: The Boeing Company
H02S20/32H01L31/0543H01L31/0547H02S40/22H02S50/00Y02E10/52
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Quick Facts
Patent No.
US 10,236,822
App. No.
14/656,259
Filed
Mar 12, 2015
Granted
Mar 19, 2019
Kind
B2
Art Unit
1721
USPC
136/246
Abstract

A method and apparatus for calibrating a reflector in a solar array. A switch device is switched from a first state to a second state. A calibration voltage is applied to each of a set of actuation devices associated with the reflector in response to the switch device switching to the second state when the calibration circuit is electrically connected to the set of actuation devices.

Claims (34)

1. An apparatus comprising:

a plurality of actuation devices connected to a corresponding plurality of reflectors in a solar array, the plurality of actuation devices configured to change corresponding angles of the corresponding plurality of reflectors relative to a single focusing lens that focuses light from the plurality of reflectors onto a single solar cell, the single solar cell behind the single focusing lens relative to the plurality of reflectors; and

a calibration circuit comprising:

a power source independent of the single solar cell;

a plurality of capacitors connected to the power source;

a plurality of resistors connected to the plurality of capacitors and to the power source, and configured to control a charging rate and discharging rate of the plurality of capacitors;

a switch device operable to switch between a first state and a second state, wherein switching the switch device from the first state to the second state causes the calibration circuit to apply a calibration voltage from the power source to each of the plurality of actuation devices when the calibration circuit is electrically connected to the plurality of actuation devices, and wherein switching the switch device from the second state to the first state causes the calibration circuit to disconnect the calibration voltage from each of the plurality of actuation devices;

a selector having a tracking state and a calibrating state, wherein the selector electrically connects the calibration circuit to the plurality of actuation devices when the selector is in the calibrating state, and wherein selector electrically disconnects the calibration circuit from the plurality of actuation devices when the selector is in the tracking state; and

a voltage manager electrically connected to the single solar cell and to the plurality of actuation devices, the voltage manager configured to send at least a portion of electrical output from the single solar cell to the plurality of actuation devices when the selector is in the tracking state, but to electrically disconnect the single solar cell from the plurality of actuation devices when the selector is in the calibration state.

2. The apparatus of claim 1 , wherein the calibration circuit maintains the calibration voltage applied to each actuation device of plurality set of actuation devices after the switch device switches from the second state to the first state.

3. The apparatus of claim 1 , wherein

each of the plurality of capacitors charges while the switch device is in the second state and discharges after the switch device switches from the second state to the first state.

4. The apparatus of claim 3 , wherein the power source charges the set of capacitors.

5. The apparatus of claim 4 , wherein the power source is a rechargeable power source.

6. The apparatus of claim 5 , wherein the rechargeable power source is selected from one of a rechargeable battery, a capacitor bank, and an inductor bank.

7. The apparatus of claim 1 , wherein the selector is moved from the tracking state to the calibrating state when an electrical output of the solar array drops below a minimum output value.

8. The apparatus of claim 1 , wherein the plurality of reflectors are micro-electromechanical systems based reflectors.

9. The apparatus of claim 1 , wherein applying the calibration voltage to each of the plurality of actuation devices positions the reflector in a calibrated position.

10. The apparatus of claim 9 further comprising:

a substrate, wherein the plurality of reflectors are coupled to the substrate and wherein the calibrated position for the plurality of reflectors is rotationally offset with respect to at least one axis relative to a plane of the substrate.

11. A method for calibrating a solar array using a calibration circuit including a power source independent of the solar array, a plurality of capacitors connected to the power source, a plurality of resistors connected to the plurality of capacitors and to the power source and configured to control a charging rate and discharging rate of the plurality of capacitors, wherein the solar array includes a plurality of actuators connected to corresponding ones of a plurality of reflectors, the plurality of actuators configured to change angles of the plurality of reflectors with respect to a single solar cell in the solar array, and wherein the calibration circuit further includes a switch device electrically connected to the power source and to the plurality of reflectors, the method comprising:

applying a calibration voltage from the power source to each of the plurality of actuation devices in response to the switch device switching to the second state when the calibration circuit is electrically connected to the plurality of actuation devices;

removing the calibration voltage from the power source to each of the plurality of actuation devices in response to the switch device switching to the first state when the calibration circuit is electrically connected to the plurality of actuation devices;

connecting, using a selector, the calibration circuit to the plurality of actuation devices when the selector is in a calibrating state;

disconnecting, using the selector, the calibration circuit from the plurality of actuation devices when the selector is in a tracking state; and

sending, using a voltage manager, at least a portion of electrical output from the single solar cell to the plurality of actuation devices when the selector is in the tracking state, but electrically disconnecting the single solar cell from the plurality of actuation devices when the selector is in the calibration state.

12. The method of claim 11 further comprising:

maintaining the calibration voltage applied to each actuation device after the switch device switches from the second state to the first state.

13. The method of claim 12 further comprising:

switching the switch device from the second state to the first state in response to an event occurring, wherein the event is selected from one of a lapse of a preselected period of time and receiving an electrical signal.

14. The method of claim 11 , further comprising:

maintaining the calibration voltage at each actuation device using the plurality of capacitors and the plurality of resistors in the calibration circuit after the switch device switches from the second state to the first state.

15. The method of claim 11 further comprising:

moving the selector from the tracking state to the calibrating state to electrically connect the calibration circuit to the plurality of actuation devices, wherein when the calibration circuit is not connected to the calibration circuit the plurality of actuators are powered by electrical energy taken from the solar cell instead of from the power source.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 12, 2015
From: SINGER, SCOTT BENJAMIN; KRUT, DIMITRI D.; KARAM, NASSER H.
To: THE BOEING COMPANY
Reel/Frame 035152/0847 →
Continuity (3)
Continuation In Part 14532356 · Nov 4, 2014
Continuation In Part 14186703 · Feb 21, 2014
Related Publication 20150256124A1 · Sep 10, 2015