发明名称 Multi-platform LED-based aircraft rear position light
摘要 An aircraft rear position light device ( 1 ) has a modular configuration. The device utilizes solid-state light sources. In an exemplary embodiment, the light sources are side-emitting light-emitting diodes (LEDs) ( 40 ), which are attached to a heat sink ( 30 ). A reflector ( 200 ) is positioned next to each of the LEDs. The device further includes an outer lens ( 10 ) with an integrated cut-off shield ( 110 ) and optical treatments ( 120 ). The configuration of LEDs and reflectors, in conjunction with the cut-off shield and optical treatments, allows the emitted light to satisfy predetermined minimum and maximum angular intensity requirements. An electronics module ( 50 ) is also attached to the heat sink to connect the LEDs to a power source in the aircraft. Electronic updates may be made by replacing the electronics module.
申请公布号 US2005201112(A1) 申请公布日期 2005.09.15
申请号 US20040920524 申请日期 2004.08.18
申请人 MACHI NICOLO F.;SINGER JEFFREY M.;MCKENZIE MARK A. 发明人 MACHI NICOLO F.;SINGER JEFFREY M.;MCKENZIE MARK A.
分类号 B64D47/02;B64D47/06;(IPC1-7):B64D47/02 主分类号 B64D47/02
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