Exterior aircraft light unit and method of disabling a light output of an exterior aircraft light unit

Patent metadata

Field	Value
Publication number	US-10299343-B2
Application number	US-201715705517-A
Country	US
Kind code	B2
Filing date	Sep 15, 2017
Priority date	Sep 16, 2016
Publication date	May 21, 2019
Grant date	May 21, 2019

Abstract

An exterior aircraft light unit includes a power input coupleable to an aircraft on-board power supply; at least one LED coupled to the power input for receiving power from the aircraft on-board power supply and configured to emit a light output; an optical sensor arranged for sensing an intensity detection portion of the light output and configured to output a detection signal indicative of an intensity level of the light output; an end of life detector, coupled to the optical sensor for receiving the detection signal and configured to determine an end of life condition; and a fuse circuit coupled to the end of life detector; wherein the fuse circuit is configured to irreversibly disable an LED circuit board upon the end of life detector communicating the end of life condition to the fuse circuit.

First claim

The invention claimed is:

1. An exterior aircraft light unit, comprising:
a power input coupleable to an aircraft on-board power supply,
at least one LED coupled to the power input for receiving power from the aircraft on-board power supply and configured to emit a light output,
an optical sensor arranged for sensing an intensity detection portion of the light output and configured to output a detection signal indicative of an intensity level of the light output,
an end of life detector, coupled to the optical sensor for receiving the detection signal and configured to determine an end of life condition, and
a fuse circuit coupled to the end of life detector,
wherein the at least one LED, the optical sensor and the fuse circuit are arranged on an LED circuit board and wherein the fuse circuit is configured to irreversibly disable power reception at the LED circuit board upon the end of life detector communicating the end of life condition to the fuse circuit.

2. The exterior aircraft light unit according to claim 1 , wherein the fuse circuit comprises a one time settable latch.

3. The exterior aircraft light unit according to claim 1 , wherein the end of life detector is configured to determine the end of life condition if the detection signal indicates that the intensity level of the light output is below a set threshold value.

4. The exterior aircraft light unit according to claim 3 , wherein the end of life detector comprises a timer circuit and wherein the end of life detector is configured to determine the end of life condition if the detection signal indicates that the intensity level of the light output is below the set threshold value for a set time interval.

5. The exterior aircraft light unit according to claim 3 , further comprising a temperature sensing circuit configured to sense an operating temperature of the at least one LED, wherein the temperature sensing circuit is coupled to the end of life detector and wherein the end of life detector is configured to determine the end of life condition only if the operating temperature of the at least one LED, sensed by the temperature sensing circuit, is below a normal operation threshold value.

6. The exterior aircraft light unit according to claim 5 , wherein the temperature sensing circuit is arranged on the LED circuit board.

7. The exterior aircraft light unit according to claim 1 , wherein the optical sensor is arranged on the LED circuit board.

8. The exterior aircraft light unit according to claim 1 , further comprising a time of use recorder configured to record an aggregate operation time of the at least one LED, wherein the time of use recorder is coupled to the end of life detector and is configured to communicate the aggregate operation time to the end of life detector, with the time of use recorder in particular being arranged on the LED circuit board.

9. An LED circuit board for use in an exterior aircraft light unit, LED circuit board comprising:
at least one LED configured to emit a light output, and
an optical sensor arranged for sensing an intensity detection portion of the light output and configured to output a detection signal indicative of an intensity level of the light output; and
a fuse circuit configured to irreversibly disable power reception at the LED circuit board upon receiving an end of life condition signal indicating an end of life condition of the at least one LED;
wherein the LED circuit board is coupleable to a power input for receiving power from an aircraft on-board power supply.

10. The exterior aircraft light unit according to claim 1 in combination with a an aircraft that includes an on-board power supply coupled to the unit and wherein the one exterior aircraft light unit is arranged in an outer portion of the aircraft for lighting an outside environment of the aircraft.

11. A method of disabling a light output of an exterior aircraft light unit upon detection of an end of life condition, with the exterior aircraft light unit having at least one LED arranged on an LED circuit board, the method comprising:
operating the at least one LED for emitting the light output;
sensing an intensity level of the light output using an optical sensor which is arranged on the LED circuit board;
determining the end of life condition on the basis of the intensity level of the light output; and
irreversibly disabling power reception at the LED circuit board upon determining the end of life condition.

12. A method according to claim 11 , wherein determining the end of life condition comprises determining the end of life condition if the intensity level of the light output is below a set threshold value for a set time interval.

13. A method according to claim 11 , wherein the step of determining the end of life condition comprises:
sensing an operating temperature of the at least one LED; and
determining the end of life condition only if the operating temperature of the at least one LED is below a normal operation threshold value.

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Klein Frank
• Hessling-Von Heimendahl Andre
• Trinschek Robert

Classifications

• F21V5/08

  producing an asymmetric light distribution · CPC title

• H05B45/58 Primary

  involving end of life detection of LEDs · CPC title

• F21W2107/30

  for aircraft · CPC title

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• B64D47/02 Primary

  Arrangements or adaptations of signal or lighting devices · CPC title