Exterior aircraft light unit and aircraft comprising the same

Patent metadata

Field	Value
Publication number	US-9789975-B2
Application number	US-201514825898-A
Country	US
Kind code	B2
Filing date	Aug 13, 2015
Priority date	Aug 14, 2014
Publication date	Oct 17, 2017
Grant date	Oct 17, 2017

Abstract

An exterior aircraft light unit includes a mounting structure, an LED arranged on the mounting structure, and an optical system, arranged on the mounting structure for creating an output light emission distribution of the exterior aircraft light unit. The optical system has, in a first cross-sectional plane extending through the LED, a first concave reflector and a second concave reflector, each of the first and second concave reflectors having a proximate end positioned adjacent to the mounting structure and a distal end positioned removed from the mounting structure, with the first and second concave reflectors being arranged on opposite sides of the LED in the first cross-sectional plane, and a refractive optical element arranged between the first and second concave reflectors in the first cross-sectional plane. The distal ends of both the first and second concave reflectors that curve towards each other and have back-tapered shapes.

First claim

The invention claimed is:

1. Exterior aircraft light unit, comprising:
a mounting structure,
an LED arranged on the mounting structure, and
an optical system, arranged on the mounting structure for creating an output light emission distribution of the exterior aircraft light unit,
wherein the optical system comprises, in a first cross-sectional plane extending through the LED:
a first concave reflector and a second concave reflector, each of the first and second concave reflectors having a proximate end positioned adjacent to the mounting structure and a distal end positioned separated from the mounting structure, with the first and second concave reflectors being arranged on opposite sides of the LED in the first cross-sectional plane, and
a refractive optical element arranged between the first and second concave reflectors in the first cross-sectional plane,
wherein the distal ends of both the first and second concave reflectors have back-tapered shapes, with the first and second concave reflectors curving towards each other at their distal ends,
wherein the LED, the first concave reflector and the second concave reflector are arranged in such a way that the light emitted by the LED and reflected by the first concave reflector in the first cross-sectional plane crosses the light emitted by the LED and reflected by the second concave reflector in the first cross-sectional plane.

2. Exterior aircraft light unit according to claim 1 , wherein both the first concave reflector and the second concave reflector are elliptical in the first cross-sectional plane.

3. Exterior aircraft light unit according to claim 2 , wherein the LED is positioned in a first focal point of each of the first and second concave reflectors.

4. Exterior aircraft light unit according to claim 2 , wherein a second focal point of the first concave reflector and a second focal point of the second concave reflector are spaced apart.

5. Exterior aircraft light unit according to claim 1 , wherein the LED, the first concave reflector, the second concave reflector and the refractive optical element are arranged in such a way that the light emitted by the LED in operation in the first cross-sectional plane is refracted or reflected by exactly one of the first concave reflector, the second concave reflector and the refractive optical element.

6. Exterior aircraft light unit according to claim 1 , wherein the output light emission distribution has an opening angle of at least 150° in the first cross-sectional plane.

7. Exterior aircraft light unit according to claim 1 , wherein the optical system comprises, in a second cross-sectional plane extending through the LED and being orthogonal to the first cross-sectional plane:
a first planar reflector and a second planar reflector, each of the first and second planar reflectors having a proximate end positioned adjacent to the mounting structure and a distal end positioned separated from the mounting structure, with the first and second planar reflectors being arranged on opposite sides of the LED in the second cross-sectional plane,
wherein the refractive optical element is arranged between the first and second planar reflectors.

8. Exterior aircraft light unit according to claim 7 , wherein the first concave reflector, the second concave reflector, the first planar reflector and the second planar reflector form an integrated reflector structure surrounding the LED and the refractive optical element.

9. Exterior aircraft light unit according to claim 7 , wherein the output light emission distribution has an opening angle of between 40° and 80°, in particular of between 50° and 70°, in the second cross-sectional plane.

10. Exterior aircraft light unit according to claim 1 , wherein the exterior aircraft light unit is an anti-collision light unit, with the first cross-sectional plane being a vertical cross-sectional plane thereof and with the second cross-sectional plane being a horizontal cross-sectional plane thereof.

11. Exterior aircraft light unit according to claim 1 , further comprising at least two additional function light sources, with each of the at least two additional function light sources being arranged adjacent a back side of a respective one of the first and second concave reflectors and emitting at least part of their light towards the back side of the respective one of the first and second concave reflectors, with each of the back sides of the first and second concave reflectors being at least partially reflective and, in particular, being shaped for re-directing the light of the respective additional function light source up to 90°.

12. Exterior aircraft light unit according to claim 11 , further comprising at least two collimating reflectors, with each one of the two collimating reflectors being associated with one of the at least two additional function light sources, wherein each one of the additional function light sources is arranged between the respectively associated one of the first and second concave reflectors and the respectively associated collimating reflector.

13. Exterior aircraft light unit according to any of claim 11 , wherein the exterior aircraft light unit is a combined anti-collision and navigation light unit, with the at least two additional function light sources being in operation used for navigation light functionality of the exterior aircraft light unit.

14. An aircraft comprising at least one exterior aircraft light unit according to claim 1 .

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Jha Anil Kumar
• Von Heimendahl Andre Hessling
• Beermann Franz-Josef
• Schoen Christian
• Lueder Sascha

Classifications

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• F21V7/08

  with elliptical curvature · CPC title

• B64D47/04

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

• B64D7/02

  the armaments being firearms · CPC title

• F21V7/09

  with a combination of different curvatures · CPC title