A synchronized, aircraft light system includes a first light emitting diode (LED) light source disposed on the aircraft and a second LED light source disposed on the aircraft. The first LED light source and the second LED light source are operatively coupled to a direct current (DC) power source by a DC power bus. A power line communication (PLC) modem is operatively coupled to the DC power bus. The PLC modem is operable to impart a synchronization signal on the DC power bus, such that the first LED light source and the second LED light source are caused to illuminate via power supplied from the DC power source via the DC power bus, in a predetermined, synchronous manner with respect to each other.
Aircraft beacon light synchronization
2018-10-02
Patent
Electronic Resource
English
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