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Autonomous emergency light unit for an aircraft and emergency lighting system comprising such light unit

机译:用于飞机的自主应急灯单元以及包括这种照明单元的应急照明系统

摘要

An autonomous emergency light unit (2) for an aircraft has a power input (4) for receiving power from an external power supply, a capacitor (8), at least one LED (10a, 10b, 10n) and a light unit control logic (12) for operating the emergency light unit (2) in a plurality of operating states as a response to external control information. The plurality of operating states includes a discharge and illumination state when no power input is sensed at the power input, a charge and illumination state when power is still sensed at the power input, an armed and charged state, a sensed crash state and a shutdown state. The control unit activates a respective state by controlling switches in the light unit.
机译:飞机的自主应急照明单元(2)具有用于从外部电源接收功率的电源输入(4),电容器(8),至少一个LED(10a,10b,10n)和照明单元控制逻辑(12)用于响应于外部控制信息在多个操作状态下操作应急灯单元(2)。多个操作状态包括当在电源输入处未感测到电源输入时的放电和点亮状态,在电源输入处仍感测到电源时的充电和点亮状态,待命和充电状态,感测的碰撞状态和关闭状态州。控制单元通过控制照明单元中的开关来激活相应的状态。

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