A method, system, and apparatus for a diffractive based coherent aircraft position and anti-collision lighting system may include generating optical source signals in an aircraft lighting system utilizing one or more coherent light sources. The generated optical source signals may be communicated to diffractive optical elements in the aircraft via optical waveguides, and output optical signals may be generated for transmission out of the aircraft via the diffractive optical elements. The lighting system may comprise indicator lights and/or anti-collision lights. The coherent light source may comprise a solid state laser. The diffractive optical elements may be integrated in wingtips and/or a fuselage of the aircraft. The coherent optical sources may be located within a fuselage of the aircraft and/or within wings of the aircraft. The diffractive optical elements may be statically and/or dynamically controlled and may comprise liquid crystals.


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    Title :

    Method, system, and apparatus for a diffractive based coherent aircraft position and anticollision lighting system


    Contributors:

    Publication date :

    2016-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F21W Index-Schema in Verbindung mit den Unterklassen F21K, F21L, F21S und F21V, betreffend den Gebrauch oder Einsatz von Leuchten oder Beleuchtungssystem , INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K,  F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT