Control system for dimmable windows
Electrically dimmable windows for aircraft are powered by energy harvesting devices on-board the aircraft. The harvested energy is stored and used to control the opacity of the windows based on individual window opacity settings selected either by passengers or a cabin attendant. Each window has an associated control circuit that controls the electrical power applied to the window based on the selected opacity setting. The control circuit includes a low energy usage processor that remains in a sleep mode until a change in the opacity setting is detected. Each control circuit may include a radio transceiver that receives control signals from a transmitter operated by the cabin attendant in order to simultaneously remotely control the opacity settings of multiple windows.
1. A method of controlling electrically dimmable windows on-board an aircraft, comprising the steps of:
(A) harvesting energy on-board the aircraft;
(B) storing the energy harvested in step (A) as electrical power;
(C) using the electrical power stored in step (B) to control the opacity of the windows;
(D) controlling the opacity of the windows from a central control location;
(E) using a processor to control the amount of stored electrical power that is used to control the opacity of the window;
(F) placing the processor in an inactive, sleep mode; and
(G) periodically awaking the processor from the sleep mode to receive signals commanding the processor to change the amount of stored power delivered to the window.
2. The method of claim 1 , wherein converting radiation into electrical power includes converting light into electrical power.
3. The method of claim 1 , wherein step (B) includes storing the electrical power in a battery.
4. The method of claim 1 , wherein step (B) includes storing the electrical power in an electrical capacitor.
5. The method of claim 1 , wherein step (D) is performed using a wireless data link.
6. The method of claim 1 , wherein step (D) includes powering a radio receiver forming part of the wireless data link using electrical power stored in step (B).
7. A method of controlling electrically dimmable windows onboard an aircraft, comprising the steps of:
(A) harvesting energy onboard the aircraft;
(B) storing the harvested energy in a storage device as electrical power;
(C) using the stored electrical power to power a control circuit, onboard the aircraft, coupled with the storage device and a window having electrically controllable opacity;
(D) establishing two-way communication between the control circuit and a central controller onboard the aircraft, the control circuit operable to transmit operational status and location information of the window to the central controller; and
(E) transmitting wireless control signals from the central controller to the control circuit to remotely control a level of opacity of the window.
8. The method of claim 7 , further comprising the step of periodically temporarily powering up the control circuit to check for the wireless control signals transmitted from the central controller.
9. The method of claim 7 , further comprising the step of conditioning electrical power from the energy harvesting device using a power conditioning circuit, before the electrical power is stored in the storage device.
10. The method of claim 7 , further comprising the step of selecting a level of opacity of the window using a window dimming adjustment control of the control circuit.
11. The method of claim 10 , further comprising the step of altering the electrical power applied to the window via a microcontroller associated with the control circuit, the microcontroller being responsive to the operation of the window dimming adjustment control.
12. The method of claim 11 , further comprising the step of selectively placing the microcontroller in one of an awake state and a power-saving sleep state, initiated by the operation of the window dimming adjustment.
13. The method of claim 7 , further comprising the step of selecting the level of opacity of the window via a second dimming control at the window, the second dimming control being coupled with the control circuit.
14. The method of claim 7 , further comprising the step of sensing the level of opacity of the window via the control circuit.
15. The method of claim 7 , further comprising the step of selecting the level of opacity of the window using a photoluminescent window dimming adjustment control associated with the control circuit.
16. A method of controlling electrically dimmable windows onboard an aircraft, comprising the steps of:
(A) harvesting energy onboard the aircraft;
(B) storing the harvested energy as electrical power;
(C) powering a control circuit onboard the aircraft using the stored electrical power, the control circuit being associated with a window having electrically controllable opacity;
(D) establishing two-way wireless communication between the control circuit and a central controller onboard the aircraft; and
(E) controlling a level of opacity of the window by either or both of the central controller and the control circuit.
17. The method of claim 7 , further comprising the steps of:
(F) transmitting operational status and location information of the window from the control circuit to the central controller; and
(G) transmitting opacity control signals from the central controller to the control circuit.
18. The method of claim 1 , wherein step (A) is performed by converting a temperature gradient into electrical power.
19. The method of claim 1 , wherein step (A) is performed by converting motion into electrical power.
20. The method of claim 1 , wherein step (A) is performed by converting radiation into electrical power.