SUPER CAPACITOR BASED EMERGENCY LIGHTING SYSTEM

An emergency lighting system for an aircraft, comprising a capacitor, at least one of an onboard power system and a ground power unit configured to charge the capacitor, a light emitting diode, a switch configured to selectively connect and disconnect the light emitting diode from at least one of th...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Oltheten, Erik John
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:An emergency lighting system for an aircraft, comprising a capacitor, at least one of an onboard power system and a ground power unit configured to charge the capacitor, a light emitting diode, a switch configured to selectively connect and disconnect the light emitting diode from at least one of the capacitor, the onboard power system and the ground power unit, and at least one of a sign and a panel disposed relative to the light emitting diode so that light emitted from the light emitting diode is cast onto at least one of the sign and the panel when the switch is set to connect the light emitting diode to at least one of the capacitor, the onboard power system and the ground power unit, wherein the light emitted by the light emitting diode is incident on a front-facing surface of at least one of the sign and the panel.