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

机译:用于基于衍射的相干飞机位置和防撞照明系统的方法,系统和装置

摘要

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.
机译:用于基于衍射的相干飞行器位置和防撞照明系统的方法,系统和装置可包括在利用一个或多个相干光源的飞行器照明系统中生成光源信号。所产生的光源信号可以经由光波导被传送到飞机中的衍射光学元件,并且可以产生输出光信号以经由衍射光学元件传输出飞机。照明系统可以包括指示灯和/或防撞灯。相干光源可以包括固态激光器。衍射光学元件可以被集成在飞机的翼尖和/或机身中。相干光源可以位于飞机的机身内和/或飞机的机翼内。衍射光学元件可以是静态和/或动态控制的,并且可以包括液晶。

著录项

  • 公开/公告号US9469415B1

    专利类型

  • 公开/公告日2016-10-18

    原文格式PDF

  • 申请/专利权人 ERIC JOSEPH HARVEY;

    申请/专利号US201213442398

  • 发明设计人 ERIC JOSEPH HARVEY;

    申请日2012-04-09

  • 分类号B64D47/00;B64D47/06;B64D47/04;F21W101/06;F21Y101/02;

  • 国家 US

  • 入库时间 2022-08-21 14:34:52

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