White position taillight for aircraft
First Claim
Patent Images
1. An aircraft position light comprising:
- a support comprising adjacent, substantially planar surfaces defining a reentrant angle, said support defining an interior angle between said planar surfaces, measured within said support, greater than 180°
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a plurality of LEDs mounted to each said planar surface; and
a circuit for energizing said LEDs,wherein said LEDs produce light when energized in a pattern subtending an obtuse angle centered on a line bisecting said reentrant angle.
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Abstract
An aircraft position light employs selected colored LEDs to produce a white appearing warning light with a reduced light component in the amplification spectrum of night vision imaging equipment. A combination of amber and cyan LEDs are selected to produce approximately three amber flux units for every cyan flux unit resulting in a white composite light. Both of the selected LEDs have dominant wavelengths of less than 600 nm.
43 Citations
18 Claims
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1. An aircraft position light comprising:
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a support comprising adjacent, substantially planar surfaces defining a reentrant angle, said support defining an interior angle between said planar surfaces, measured within said support, greater than 180°
;a plurality of LEDs mounted to each said planar surface; and a circuit for energizing said LEDs, wherein said LEDs produce light when energized in a pattern subtending an obtuse angle centered on a line bisecting said reentrant angle. - View Dependent Claims (2, 3, 4, 5)
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6. An aircraft position light comprising:
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two substantially planar elongate PC boards; a linear array of LEDs mounted to each said PC board, each said LED having an optical axis, the optical axes of each said linear array collectively defining a direction of light transmission for each linear array; and a circuit for simultaneously energizing said LEDs, wherein said LEDs produce light when energized, said PC boards supported so that said linear arrays are substantially parallel and the direction of light transmission of said linear arrays intersect at an angle of approximately 90°
. - View Dependent Claims (7, 8, 9, 10, 11)
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12. An aircraft position light comprising:
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a support defining two substantially planar surfaces adjacent to each other along one edge, said surfaces defining an included angle of less than 180°
;a substantially planar, thermally conductive PC board mounted in thermally conductive relationship to each said planar surface, a plurality of LEDs mounted to each said PC board, each said LED having an optical axis, the optical axes of said plurality of LEDs collectively defining a direction of light transmission for each said plurality of LEDs; wherein the direction of light transmission of one said plurality of LEDs intersect the direction of light transmission of the other said plurality of LEDs. - View Dependent Claims (13, 14, 15, 16, 17, 18)
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Specification