LED FLASH LIGHT AND METHOD FOR INDICATING NEAR-END-OF-LIFE STATUS OF SUCH AN LED FLASH LIGHT
First Claim
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 ofdetermining the actual photometric condition of the LED flash light,comparing the actual photometric condition to a given condition in a normal flashing mode, andif 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.
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Accused Products
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.
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Citations
4 Claims
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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, 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 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.
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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: -
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 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).
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Specification