LED flash light and method for indicating near-end-of-life status of such an LED flash light

Patent metadata

Field	Value
Publication number	US-9258871-B2
Application number	US-201313890356-A
Country	US
Kind code	B2
Filing date	May 9, 2013
Priority date	May 10, 2012
Publication date	Feb 9, 2016
Grant date	Feb 9, 2016

Abstract

The invention comprises a method for indicating that an LED flash light for an aircraft such as an anti-collision or beacon or strobe LED light has reached a near-end-of-life status, wherein the LED flash light under normal operational condition within a given time interval generates a predetermined number of normal flashes with the number being one or more than one, e.g. two. The method comprises the steps of determining the actual photometric condition of the LED flash light, and comparing the actual photometric condition to a given condition in a normal flashing mode. If the actual condition deviates from the given condition by more than a predetermined amount, the LED flash light is operated in order to generate within the given time interval one additional near-end-of-life-indicating flash.

First claim

The invention claimed is:

1. Method for indicating that an LED flash light for an aircraft such as an anti-collision or beacon or strobe LED light has reached a near-end-of-life status, wherein the LED flash light under a normal operational condition within a given time interval generates a predetermined number of normal flashes, with the number being one or more than one, e.g. two, wherein the method comprises the steps of
determining the actual photometric condition of the LED flash light by integrating a light intensity of the LED flash light for a single normal flash,
comparing the actual photometric condition to a given condition in a normal flashing mode, and
if the actual condition deviates from the given condition by less than a predetermined amount, adapting a flash duration of the predetermined number of normal flashes such that an integrated light intensity of a single normal flash reaches a pre-set threshold intensity value,
if the actual condition deviates from the given condition by more than a predetermined amount, operating the LED flash light for generating within the given time interval at least one additional near-end-of-life-indicating flash ( 3 ) during the given time interval;
wherein the given time interval is at most 200 ms and a pause between the predetermined number of normal flashes and the at least one additional near-end-of-life-indicating flash is at least 20 ms.

2. Method according to claim 1 , wherein the flash light is operated so as to generate a single flash ( 1 ) per predetermined time interval and wherein the flash light, if its actual photometric condition deviates from the given condition by more than the predetermined amount, is operated so as to generate for each time interval at least a second or additional flash ( 3 ).

3. Method according to claim 1 , wherein the second or additional flash ( 3 ) is generated after a delay ( 2 ) of 20 ms to 50 ms or 30 ms to 50 ms or 40 ms to 50 ms after the first or last normal flash ( 1 ).

4. LED flash light for an aircraft, such as an anti-collision or beacon or strobe aircraft light, wherein the LED flash light under a normal operational condition within a given time interval generates a predetermined number of normal flashes, with the number being one or more than one, e.g. two, the LED flash light comprising
at least one LED light source ( 10 ) and
a control unit ( 12 ) for controlling the LED light source ( 10 ) in a normal flashing mode,
wherein the control unit ( 12 ) performs the followings steps:
determining the actual photometric condition of the LED flash light by integrating a light intensity of the LED flash light for a single normal flash,
comparing the actual photometric condition to a given condition in the normal flashing mode, and
if the actual condition deviates from the given condition by less than a predetermined amount, adapting a flash duration of the predetermined number of normal flashes such that an integrated light intensity of a single normal flash reaches a pre-set threshold intensity value,
if the actual condition deviates from the given condition by more than a predetermined amount, operating the LED flash light for generating within the given time interval at least one additional near-end-of-life-indicating flash ( 3 );
wherein the given time interval is at most 200 ms and a pause between the predetermined number of normal flashes and the at least one additional near-end-of-life-indicating flash is at least 20 ms.

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Mueller Bernhard

Classifications

• H05B47/20

  Responsive to malfunctions or to light source life; for protection · CPC title

• H05B45/58

  involving end of life detection of LEDs · CPC title

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• H05B45/10

  Controlling the intensity of the light · CPC title

• B64D47/02 Primary

  Arrangements or adaptations of signal or lighting devices · CPC title