Portable cockpit illumination device

A portable cockpit illumination device for the purpose of supplementing existing cockpit illumination from an overhead type lamp assembly provides for an even illumination of all cockpit panel instruments. A portable design allows installation or removal from the cockpit in seconds without using any tools. Two modes of operation insure cockpit illumination under any flight conditions. An accessory power receptacle internal to an aircraft cockpit provides power during normal operation, and a self contained battery source provides cockpit illumination during emergency situations when no external power source is available. During normal operation, a charging circuit insures optimal battery performance. A plurality of light emitting diodes (LED's) wired in a series-parallel array receives power from a DC to DC buck converter, whereby an input source voltage is reduced to a lower output voltage. A rheostat controlled feedback voltage loop provides for load current and illumination control.

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What is claimed is:

1. A portable nighttime and emergency instrument panel illumination apparatus comprising: an external power source means and a housing for containing: a plurality of lightemitting diodes, an internal battery, a battery recharging circuit, a direct current converter circuit, and a mounting means; said external power source means includes an external receptacle and a wire pair electrically connected inside said housing tosaid light emitting diodes, said battery charging, and said converter circuits, mounting means comprises both elements of a hook and loop fastener and is permanently attached to said housing accommodating for quick installation and removal from saidcockpit,

electrical connection means of: (A) said external power source to said converter and said light emitting diodes for illumination of said instrument panel during said nighttime or low ambient light conditions, (B) said internal battery to saidconverter and said light emitting diodes for illumination of said instrument panel during failure or malfunction of said external power source, (C) said external power source and said battery recharging circuit for maintaining charge of said internalbattery.

2. The apparatus in claim 1 wherein the luminance from said light emitting diodes is rheostat adjustable.

3. The apparatus in claim 1 wherein the voltage range of said external power source is from 10 to 30 volts direct current.

4. The apparatus in claim 1 wherein said cockpit further has a visor and said housing is attached to said visors wherein the illuminated beam path is absent of shadows and is adjusted by changing said visor angle.