Multifunctional aircraft landing light with static function switching

Patent metadata

Field	Value
Publication number	US-10899470-B2
Application number	US-201716343685-A
Country	US
Kind code	B2
Filing date	Oct 17, 2017
Priority date	Oct 19, 2016
Publication date	Jan 26, 2021
Grant date	Jan 26, 2021

Abstract

An aircraft landing light with static function switching for producing at least two beams having different characteristics, in particular different orientations and/or openings, comprises an array of light-emitting diode lighting modules ( 6 ) each comprising at least two sets of at least one light source (S 1 , S 2 ), operable selectively and statically to provide at least one of the lighting functions. Each lighting module ( 6 ) comprises a common converging lens (L) for the light sources, the converging lens comprising a light input optical surface (Li) and a light output optical surface (L 2 ), said light sources being positioned in relation to the light input optical surface.

First claim

The invention claimed is:

1. An aircraft landing light with static function switching, intended to produce at least two beams having different characteristics, comprising: an array of LED lighting modules each comprising at least two sets of at least one selectively and statically activatable light source in order to generate at least one of the lighting functions, each LED lighting module comprising a convergent lens that is common to two light sources of the respective LED lighting module, the convergent lens possessing an entrance dioptric interface the profile of which is planar or spherical on the whole and an exit dioptric interface the profile of which is elliptical or aspherical, said two light sources being positioned with respect to the light entrance dioptric interface, wherein a focal plane of the convergent lens is located at a distance from the entrance dioptric interface smaller than 10 mm.

2. The light as claimed in claim 1 , wherein the two light sources are off-axis with respect to an axis of the lens so as to generate either beams of different orientation or beams of different aperture, or beams of different orientation and aperture, the two light sources being off-axis with respect to the axis of the lens so that the beams mutually diverge by 5 to 30°.

3. The light as claimed in claim 1 , wherein the entrance dioptric interface has a shape that is planar on the whole and comprises a disk-shaped central dioptric area, an annular exterior dioptric area and a frustoconical toroidal median area placed between the central and exterior areas.

4. The light as claimed in claim 1 , wherein the two light sources are defocused with respect to the lens by being brought closer to the entrance dioptric interface.

5. The light as claimed in claim 1 , wherein the lens is catadioptric and comprises a dioptric central zone in which the two light sources are placed and a conical or parabolic exterior annular zone that reflects light by total reflection.

6. The light as claimed in claim 1 , wherein the two light sources are mounted on a printed circuit board and wherein the lens comprises feet for fastening and positioning the lens on the board.

7. The light as claimed in claim 6 , comprising an optical device comprising a set of grouped convergent lenses each associated with the at least two sets of at least one light source.

Assignees

• Zodiac Aero Electric

Inventors

• Millet Philippe
• Doule Claude
• Tsao Christian

Classifications

• B64D47/04 Primary

  the lighting devices being primarily intended to illuminate the way ahead · CPC title

• F21S41/663

  by switching light sources (by switching incandescent light sources F21S41/162) · CPC title

• F21S41/265

  Composite lenses; Lenses with a patch-like shape · CPC title

• F21S41/153

  arranged in a matrix · CPC title

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title