Super capacitor based emergency lighting system
An emergency lighting system (ELS) for an aircraft has a capacitor, at least one of an onboard power system and a ground power unit configured to charge the capacitor, and a light emitting diode (LED) selectively powered by the capacitor.
1. An aircraft, comprising:
onboard power supply; and
an emergency lighting system (ELS), comprising:
a capacitor;
a light emitting diode (LED) selectively powered by the capacitor;
a first transistor electrically disposed between the onboard power supply and the capacitor to selectively control charging of the capacitor with power from the onboard power supply; and
a multi-position switch comprising an common node, an On node associated with an On mode of operation of the ELS, an Auto node associated with an Auto mode of operation of the ELS, and an Off node associated with an Off mode of operation of the ELS;
wherein the capacitor maintains a charge while the multi-position switch is in the Off mode of operation.
2. The aircraft of claim 1 , further comprising:
at least one of a sign and a panel disposed relative to the LED so that light emitted from the LED is cast upon at least one of the sign and the panel.
3. The aircraft of claim 1 , further comprising:
a transistor configured to selectively direct electrical energy from the capacitor to the LED.
4. The aircraft of claim 1 , wherein the Off mode of operation prevents the LED from emitting light.
5. The aircraft of claim 1 , wherein the On mode of operation causes the LED to emit light from at least one of the onboard power supply and the capacitor when power is available from at least one of the onboard power supply and the capacitor.
6. The aircraft of claim 1 , wherein the Auto mode of operation causes the LED to emit light when the onboard power supply is not providing power and the capacitor is sufficiently charged to power the LED.