Exterior aircraft light unit and aircraft comprising the exterior aircraft light unit

Patent metadata

Field	Value
Publication number	US-9718560-B2
Application number	US-201414458483-A
Country	US
Kind code	B2
Filing date	Aug 13, 2014
Priority date	Aug 13, 2013
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

An exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength is disclosed. The exterior aircraft light unit has an integrated optical structure, which in turn has a first light source configured to emit the light of the first wavelength, a second light source configured to emit the light of the second wavelength, the second light source being positioned adjacent to the first light source, and an optical element for shaping a light emission distribution of the integrated optical structure. The optical element is arranged with respect to the first light source and the second light source in such a way that it affects both the light of the first wavelength and the light of the second wavelength.

First claim

The invention claimed is:

1. An aircraft comprising:
an exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength,
wherein the exterior aircraft light unit is mounted to an exterior of the aircraft, and
wherein the exterior aircraft light unit comprises:
an integrated optical structure, comprising:
a first light source configured to emit the light of the first wavelength and having a first principal light emission direction,
a second light source configured to emit the light of the second wavelength and having a second principal light emission direction, the second light source being positioned adjacent to the first light source,
an optical element for shaping a light emission distribution of the integrated optical structure, wherein the optical element is arranged with respect to the first light source and the second light source in such a way that it affects both the light of the first wavelength and the light of the second wavelength, and
a mounting arm supporting the first light source and the second light source,
wherein the optical element is a substantially parabolic reflector, with the first and second light sources being directed towards the substantially parabolic reflector and the first and second principal light emission directions being substantially reversed by the substantially parabolic reflector and with one of the first principal light emission direction and the second principal light emission direction running through the vertex of the parabolic reflector.

2. The aircraft according to claim 1 , wherein the first wavelength is in the visible range and the second wavelength is in the infrared range.

3. The aircraft according to claim 1 , wherein the first light source is an LED and wherein the second light source is a solid state infrared emitter.

4. The aircraft according to claim 1 , wherein the first principal light emission direction is parallel to the second principal light emission direction.

5. The aircraft according to claim 1 , wherein the exterior aircraft light unit comprises a plurality of integrated optical structures, with each integrated optical structure comprising:
a respective first light source configured to emit light of the first wavelength,
a respective second light source configured to emit light of the second wavelength, the respective second light source being positioned adjacent to the respective first light source, and
a respective optical element for shaping a light emission distribution of the respective integrated optical structure, wherein the respective optical element is arranged with respect to the respective first light source and the respective second light source in such a way that it affects both the light of the first wavelength and the light of the second wavelength.

6. The aircraft according to claim 5 , wherein the plurality of integrated optical structures have corresponding light emission directions.

7. The aircraft according to claim 1 , wherein the exterior aircraft light unit is adapted to be a fixed position or movable search, taxi and/or landing light.

8. An aircraft comprising:
an exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength,
wherein the exterior aircraft light unit is mounted to an exterior of the aircraft, and
wherein the exterior aircraft light unit comprises:
an integrated optical structure, comprising:
a first light source configured to emit the light of the first wavelength and having a first principal light emission direction,
a second light source configured to emit the light of the second wavelength and having a second principal light emission direction, the second light source being positioned adjacent to the first light source, and
an optical element for shaping a light emission distribution of the integrated optical structure, wherein the optical element is arranged with respect to the first light source and the second light source in such a way that it affects both the light of the first wavelength and the light of the second wavelength,
wherein the optical element is a collimating lens, spaced from the first and second light sources, and wherein the first and second principal light emission directions are perpendicular to the plane of extension of the lens, with one of the first and second principal light emission directions running through the center of the lens.

9. The aircraft according to claim 8 , wherein the first wavelength is in the visible range and the second wavelength is in the infrared range.

10. The aircraft according to claim 8 , wherein the first light source is an LED and wherein the second light source is a solid state infrared emitter.

11. The aircraft according to claim 8 , wherein the first principal light emission direction is parallel to the second principal light emission direction.

12. The aircraft according to claim 8 , wherein the exterior aircraft light unit comprises a plurality of integrated optical structures, with each integrated optical structure comprising:
a respective first light source configured to emit light of the first wavelength,
a respective second light source configured to emit light of the second wavelength, the respective second light source being positioned adjacent to the respective first light source, and
a respective optical element for shaping a light emission distribution of the respective integrated optical structure, wherein the respective optical element is arranged with respect to the respective first light source and the respective second light source in such a way that it affects both the light of the first wavelength and the light of the second wavelength.

13. The aircraft according to claim 8 , wherein the exterior aircraft light unit is adapted to be a fixed position or movable search, taxi and/or landing light.

14. An aircraft comprising:
an exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength,
wherein the exterior aircraft light unit is mounted to an exterior of the aircraft, and
wherein the exterior aircraft light unit comprises:
an integrated optical structure, comprising:
a first light source configured to emit the light of the first wavelength and having a first principal light emission direction,
a second light source configured to emit the light of the second wavelength and having a second principal light emission direction, the second light source being positioned adjacent to the first light source, and
a plurality of optical elements for shaping a light emission distribution of the integrated optical structure, wherein each of the plurality of optical elements is arranged with respect to the first light source and the second light source in such a way that it affects both the light of the first wavelength and the light of the second wavelength,
wherein the plurality of optical elements comprises a collimating lens, spaced from the first and second light sources, and a reflector, with the reflector being arranged around the lens, with the collimating lens and the reflector affecting different portions of the light of the first wavelength and the light of the second wavelength, with the collimating lens being arranged to transform a portion of light from the first and second light sources that contains the first and second principal light emission directions.

15. The aircraft according to claim 14 , wherein the first wavelength is in the visible range and the second wavele

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Lapujade Philippe G
• Hessling Von Heimendahl Andre
• Schoen Christian
• Jha Anil Kumar

Classifications

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• F21W2107/30

  for aircraft · CPC title

• B64D47/02

  Arrangements or adaptations of signal or lighting devices · CPC title

• F21S41/336

  with discontinuity at the junction between adjacent areas · CPC title

• F21S41/19

  Attachment of light sources or lamp holders (achieving variable light distribution by movable light sources F21S41/657) · CPC title