Airfield runway lamp controller

Patent metadata

Field	Value
Publication number	US-10638574-B2
Application number	US-201916404414-A
Country	US
Kind code	B2
Filing date	May 6, 2019
Priority date	Feb 20, 2015
Publication date	Apr 28, 2020
Grant date	Apr 28, 2020

Abstract

An airfield runway lamp controller is described herein. One airfield runway lamp controller includes a current sense transformer configured to detect a failure of a light source of an airfield runway lamp, and an alternating current (AC) switch configured to shunt the light source of the airfield runway lamp upon the current sense transformer detecting a failure of the light source.

First claim

What is claimed:

1. An airfield runway lamp controller, comprising:
an alternating current (AC) switch configured to shunt a light source of an airfield runway lamp upon a failure of the light source such that current flows through the AC switch and to a series isolation transformer connected to the airfield runway lamp controller upon the failure of the light source; and
an auxiliary power source configured to provide a gate control voltage to power the AC switch upon the failure of the light source.

2. The controller of claim 1 , wherein the controller includes a current sense transformer configured to detect the failure of the light source.

3. The controller of claim 2 , wherein the current sense transformer is configured to turn the AC switch on upon the failure of the light source.

4. The controller of claim 1 , wherein the controller includes a current sense transformer configured to direct current to the AC switch upon the failure of the light source.

5. The controller of claim 1 , wherein the controller includes gate control logic configured to receive the gate control voltage provided to the AC switch by the auxiliary power source.

6. The controller of claim 1 , wherein the AC switch includes two transistors connected in series.

7. A method for controlling an airfield runway lamp, comprising:
generating, by an auxiliary power source of a controller for an airfield runway lamp, a gate control voltage to cause an alternating current (AC) switch of the controller to turn on in response to a no lamp load condition of a light source of the airfield runway lamp; and
shunting, by the AC switch of the controller, the light source of the airfield runway lamp upon the AC switch turning on such that current flows through the AC switch and to a series isolation transformer connected to the airfield runway lamp controller in response to the no lamp load condition.

8. The method of claim 7 , wherein the method includes generating, by the auxiliary power source, the gate control voltage when no current is flowing to a current sense transformer of the controller.

9. The method of claim 8 , wherein no current flows through the current sense transformer during the no lamp load condition.

10. The method of claim 7 , wherein the method includes sending, by the auxiliary power source, the gate control voltage to gate control logic.

11. The method of claim 10 , wherein the method includes turning on, by the gate control logic, the AC switch in response to the gate control logic receiving the gate control voltage.

12. The method of claim 7 , wherein the AC switch is connected to a current sense transformer such that a current flows through the current sense transformer while the AC switch is turned on.

13. The method of claim 12 , wherein the current flows through the current sense transformer and the AC switch during the no lamp load condition.

14. The method of claim 7 , wherein the method includes detecting, by the controller, a no lamp load condition upon a failure of the light source of the airfield runway lamp.

15. A system for controlling airfield ground runway lighting, comprising:
a number of airfield runway lamps, wherein each of the number of airfield runway lamps includes a light source;
a number of airfield runway lamp controllers, wherein each of the number of airfield runway lamp controllers is configured to shunt the light source of one or more of the number of airfield runway lamps upon a failure of that light source;
wherein each one of the number of airfield runway lamp controllers comprises an alternating current (AC) switch and an auxiliary power source to power the AC switch; and
a number of series isolation transformers, wherein upon a failure of a light source of one of the number of airfield runway lamps, current flows:
through the AC switch of the airfield lamp controller of the airfield runway lamp whose light source has failed; and
to a series isolation transformer of the number of series isolation transformers that is connected to the airfield lamp controller of the airfield runway lamp whose light source has failed.

16. The system of claim 15 , wherein the number of airfield runway lamp controllers corresponds to the number of airfield runway lamps.

17. The system of claim 15 , wherein the number of airfield runway lamp controllers is less than the number of airfield runway lamps.

18. The system of claim 15 , wherein each one of the number of airfield runway lamp controllers are connected to a corresponding current sense transformer.

19. The system of claim 15 , wherein the light source of each of the number of airfield runway lamps is at least one of:
a light emitting diode (LED) light source; and
an incandescent light source.

20. The system of claim 15 , wherein the number of airfield runway lamp controllers corresponds to the number of series isolation transformers.

Assignees

• Honeywell Int Inc

Inventors

• Chawda Nipun Kumar

Classifications

• H05B45/54

  in a series array of LEDs · CPC title

• H05B47/23

  of two or more light sources connected in series · CPC title

• B64F1/18

  Visual or acoustic landing aids · CPC title

• H05B39/00 Primary

  Circuit arrangements or apparatus for operating incandescent light sources (structurally associated with the incandescent lamps H01K1/62) · CPC title

• H05B33/0887

  Electricity · mapped topic