Autonomous unit for emergency lighting system for aircraft, eVTOLs, VTOLs and rotorcraft
A light unit executes up to three different functions (cabin area illumination, individual/dedicated/decorative illumination and emergency illumination) and an emergency illuminated sign unit, each one with an internal controller and a rechargeable capacitor. An example non-limiting embodiment also provides a cabin light system and an emergency lighting system, where each illumination unit (light source or illuminated sign) is as described above.
1 . An aircraft lighting system with integrated cabin lighting and emergency lighting functions configured for use on board an aircraft, the aircraft lighting system comprising plural independent illuminators configured to be used in combination and distributed within an aircraft cabin, wherein each of the plural independent illuminators comprises:
at least one aircraft light source;
an ultracapacitor configured to store energy;
a controller configured to selectively connect the ultracapacitor to the at least one aircraft light source and to control activation mode of the at least one aircraft light source; and
an ultracapacitor health monitoring circuit that includes monitoring of component charge and temperature of the ultracapacitor;
wherein failure of any one of said plural independent illuminators does not affect operation of any other ones of the plural independent illuminators.
2 . The aircraft lighting system of claim 1 wherein each illuminator further includes a converter that converts a power supply output to a charging voltage for the ultracapacitor.
3 . The aircraft lighting system of claim 1 wherein the ultracapacitor health monitoring circuit includes a charge monitor operatively coupled to the ultracapacitor, the charge monitor selectively controlling charging of the ultracapacitor based on a voltage of the ultracapacitor.
4 . The aircraft lighting system of claim 1 wherein the aircraft light source comprises at least one light emitting diode or an electric active exit sign.
5 . The aircraft lighting system of claim 1 wherein each illuminator further comprises a converter that converts a voltage output of the ultracapacitor to an operating voltage of the at least one aircraft light source.
6 . The aircraft lighting system of claim 1 wherein the aircraft comprises a rotorcraft, an eVTOL or a VTOL.
7 . The aircraft lighting system of claim 1 wherein the plural independent illuminators are configured to provide individual lighting for corresponding passengers, provide cabin area lighting when all of the plural independent illuminators are commanded on, and provide emergency lighting during emergency conditions where normal aircraft power for cabin illumination is inoperative.
8 . The aircraft lighting system of claim 1 wherein the ultracapacitor health monitoring circuit comprises a temperature sensor that monitors temperature of the ultracapacitor and disables charging of the ultracapacitor when the monitored temperature exceeds a predetermined limit.
9 . The aircraft lighting system of claim 1 wherein no battery external to said illuminators is required to operate said illuminators.
10 . The aircraft lighting system of claim 1 wherein each illuminator is configured to provide the following lighting functions: e cabin area illumination, individual/dedicated illumination, and emergency illumination.
11 . The aircraft lighting system of claim 1 , further comprising:
a cockpit control panel with three states (ON, OFF, ARM) for manually controlling the emergency lighting function; and
an automatic activation controller configured to activate the emergency lighting function upon detection of a loss of primary aircraft power when the system is in an armed state.
12 . The aircraft lighting system of claim 1 , wherein the ultracapacitor health monitoring circuit is configured to assess charging status and temperature of the ultracapacitor, and is further configured to provide a status indication reflecting a health condition of the ultracapacitor based on assessed charging status and temperature of the ultracapacitor.
13 . The aircraft lighting system of claim 1 , wherein the controller is configured to manage charging and discharging of the ultracapacitor to optimize lifespan of the ultracapacitor.