Super capacitor based emergency lighting system

1. An emergency lighting system (ELS) for an aircraft, comprising:

a capacitor;

at least one of an onboard power system and a ground power unit configured to selectively charge the capacitor;

a light emitting diode (LED) selectively powered by the capacitor;

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; and

a switch configured to prevent illumination of the light emitting diode without discharging the capacitor;

wherein the capacitor is only discharged through the light emitting diode.

2. The ELS of claim 1 , wherein the capacitor comprises a supercapacitor.

3. The ELS of claim 1 , further comprising:

a transistor configured to selectively direct electrical energy from at least one of the onboard power system and the ground power unit to the capacitor.

4. The ELS of claim 1 , further comprising:

a transistor configured to selectively direct electrical energy from the capacitor to the LED.

5. The ELS of claim 1 , wherein the

multi-position switch is configured to selectively connect and disconnect the LED from at least one of the capacitor, the onboard power system, and a ground power unit.

6. The ELS 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 onto at least one of the sign and the panel.

7. The ELS of claim 6 , further comprising:

an edge light diffuser optically disposed between the LED and at least one of the sign and the panel.

8. A method of providing lighting for an aircraft, comprising:

providing power from at least one of an onboard power supply and a ground power unit;

charging a capacitor using power provided from at least one of the onboard power supply and the ground power unit;

discontinuing providing power from the at least one of the onboard power supply and the ground power unit;

selectively powering a light emitting diode (LED) using the capacitor;

selectively preventing illumination of the light emitting diode without discharging the capacitor; and

emitting light from the LED;

wherein the capacitor is only discharged through the light emitting diode.

9. The method of claim 8 , wherein the light emitted from the LED is cast onto at least one of a sign and a panel.

10. The method of claim 9 , further comprising:

reflecting the light emitted from the LED from at least one of the sign and the panel.

11. The method of claim 8 , wherein during the providing the power from at least one of the onboard power supply and the ground power unit, the LED is powered by power from at least one of the onboard power supply and the ground power unit.

12. The method of claim 8 , wherein the powering the LED using the capacitor is initiated as a function of the discontinuing providing power from the at least one of the onboard power supply and the ground power unit.

13. The method of claim 8 , wherein the LED is selectively prevented from operation during the charging the capacitor.

14. The method of claim 8 , wherein the LED is selectively prevented from operation after the discontinuing providing power from the at least one of the onboard power supply and the ground power unit.

15. The method of claim 8 , further comprising:

selecting a multi-position switch comprising an common node, an On node associated with an On mode of operation of the LED, an Auto node associated with an Auto mode of operation of the LED, and an Off node associated with an Off mode of operation of the LED.