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SOLID STATE POWER CONTROLLER FOR AEROSPACE LED SYSTEMS

机译:航空航天LED系统的固态功率控制器

摘要

A light emitting diode (LED) control system may include a LED control system for an aircraft. The LED control system may include an LED power controller, and a solid state power controller (SSPC) that includes a processor in communication with the LED power controller, where the LED power controller and the solid state power controller are integrated onto a single power module. The LED control system is configured to receive DC power from a power source, determine, via the processor, current flow through a series MOSFET element connecting to at least one LED, to control operational voltage across the at least one LED, and adjust, via the processor, a gate voltage of the series MOSFET element with the LED power controller.
机译:发光二极管(LED)控制系统可以包括用于飞机的LED控制系统。 LED控制系统可以包括LED功率控制器和固态功率控制器(SSPC),该固态功率控制器包括与LED功率控制器通信的处理器,其中,LED功率控制器和固态功率控制器被集成到单个功率模块上。 。 LED控制系统被配置为从电源接收DC功率,经由处理器确定流过连接到至少一个LED的串联MOSFET元件的电流,以控制至少一个LED上的工作电压,并通过处理器,串联MOSFET元件与LED功率控制器的栅极电压。

著录项

  • 公开/公告号US2017202068A1

    专利类型

  • 公开/公告日2017-07-13

    原文格式PDF

  • 申请/专利权人 HAMILTON SUNDSTRAND CORPORATION;

    申请/专利号US201614991538

  • 发明设计人 JOHN A. DICKEY;JOSH C. SWENSON;

    申请日2016-01-08

  • 分类号H05B33/08;B64D47/02;

  • 国家 US

  • 入库时间 2022-08-21 13:52:25

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