LED current regulation circuit for aircraft lighting system

• US 6,600,274 B1
• Filed: 12/14/2001
• Issued: 07/29/2003
• Est. Priority Date: 12/14/2001
• Status: Expired due to Fees

• Current Assignee: Astronics DME LLC (Astronics Corporation)
• Original Assignee: DME Company LLC (Milacron Holdings Corp.)
• Inventors: Hughes, Craig E.
• Primary Examiner(s): Wong, Don
• Assistant Examiner(s): Tran, Chuc
• Application Number:
  US10/017,592
• Time in Patent Office: 592 Days
• Field of Search: 315/291, 315/307, 315/312, 315/185.R, 315/121, 315/122, 315/194, 315/241
• US Class Current: 315/291
• CPC Class Codes: H05B 45/395 Linear regulators
• CPC Class Codes: Y02B 20/30 Semiconductor lamps, e.g. solid state lamps [SSL] light emitting diodes [LED] or organic LED [OLED]

Abstract

An improved LED current regulation circuit for providing continuous electrical current to one or more Light Emitting Diodes (LEDs) in an aircraft illumination system, in particular, an aircraft emergency evacuation system, through a varying voltage source. The circuit comprises a DC voltage source and a current regulation circuit electrically coupled to the one or more light sources, preferably, LEDS. The current regulation circuit comprises a transistor, a collector of which is electrically coupled to the one or more light sources, a zener diode electrically coupled to a base of the transistor, an emitter resistor having a first terminal electrically coupled to an emitter of the transistor and a second terminal electrically coupled to ground, the emitter resistor in parallel connection with the zener diode, wherein the current through each LED is maintained at a constant predetermined level based upon the summation of voltage drops across the zener diode, the transistor and the emitter resistor. In this fashion, each LED will illuminate a desired area on an aircraft despite wide fluctuations in input voltage.

Claims

1. An illumination circuit powered by a DC voltage input in an aircraft lighting system for providing a fixed current through one or more light sources, compensating for varying DC input voltages, said system comprising:

one or more light sources for radiating light signals, each said light source having a corresponding light source current;

a current regulation circuit electrically coupled to said one or more light sources, wherein each said light source current is maintained at a predetermined level based upon a voltage drop across said current regulation circuit;

said current regulation circuit including a transistor, a collector of which is electrically coupled to said one or more said light sources;

diode means electrically coupled across a base-emitter junction of said transistor; and

resistance means having a first terminal electrically coupled to an emitter of said transistor and a second terminal electrically coupled to ground, said resistance means connected in parallel with said diode means, wherein each said light source current is maintained at a predetermined level based upon a summation of voltage drops across said diode means, said transistor and said resistance means.

2. The illumination circuit of claim 1 further comprising biasing means having a first terminal electrically coupled to said voltage input and a second terminal electrically coupled to said diode means and said base of said transistor, said biasing means connected in parallel with said light sources.

3. The aircraft illumination system of claim 1 wherein said transistor is an NPN-type transistor.

4. The aircraft illumination system of claim 1 wherein said transistor is a PNP-type transistor.

5. The aircraft illumination system of claim 1 wherein said one or more light sources are light emitting diodes.

6. An illuminated aircraft emergency evacuation apparatus comprising:

an aircraft evacuation slide to allow aircraft passengers egress from within an aircraft;

one or more light sources for radiating light signals, each having a corresponding light source current, said one or more light sources affixed to said evacuation slide to provide illumination to said aircraft passengers exiting said aircraft; and

a current regulation circuit electrically coupled to said one or more light sources, wherein each said light source current is maintained at a predetermined level based upon a voltage drop across said current regulation circuit;

said current regulation circuit including a transistor, a collector of which is electrically coupled to said one or more said light sources;

diode means electrically coupled across a base-emitter junction of said transistor; and

resistance means having a first terminal electrically coupled to an emitter of said transistor and a second terminal electrically coupled to ground, said resistance means connected in parallel with said diode means, wherein each said light source current is maintained at a predetermined level based upon a summation of voltage drops across said diode means, said transistor and said resistance means.

7. The aircraft illumination system of claim 6 further comprising biasing means having a first terminal electrically coupled to said voltage input and a second terminal electrically coupled to said diode means and said base of said transistor, said biasing means connected in parallel with said light sources.

8. The aircraft illumination system of claim 6 wherein said transistor is an NPN-type transistor.

9. The aircraft illumination system of claim 6 wherein said transistor is a PNP-type transistor.

10. The aircraft illumination system of claim 6 wherein said one or more light sources are light emitting diodes.