发明名称 Aircraft lighting system
摘要 A flexible lighting fixture includes an elongate channel having a bottom, opposing sides, first and second ends. An elongate electroluminescent lamp, having first and second ends, is disposed in the channel, between the opposing sides, with the first end generally adjacent the first end of the channel and the second end generally adjacent the second end of the channel. The electroluminescent lamp has contacts at the first end thereof, with wire leads connected to contacts on the electroluminescent lamp. A translucent cover is mounted in the channel, over the over the electrohiminescent lamp, and is engaged by the opposing sides of the channel. An encapsulant in the first end of the channel secures the first end of the electroluminescent lamp in the channel, but the remainder of the electroluminescent lamp is unattached to the channel so that when the fixture flexes, the remainder of the electroluminescent lamp can slide relative to the channel. The lighting fixture is preferably incorporated in a lighting system, comprising an inverter adapted to be connected to the DC electrical system of the aircraft to provide AC power; a battery; and a switch for selectively connecting the inverter to the electroluminescent lamp to the DC electrical system of the aircraft or to the battery.
申请公布号 US6179452(B1) 申请公布日期 2001.01.30
申请号 US19980122935 申请日期 1998.07.27
申请人 DUNNING STEPHEN C. 发明人 DUNNING STEPHEN C.
分类号 B60Q3/02;F21S4/00;(IPC1-7):F21V9/16 主分类号 B60Q3/02
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