Exterior aircraft light unit and method of operating an exterior aircraft light unit

• US 9,758,259 B2
• Filed: 07/23/2014
• Issued: 09/12/2017
• Est. Priority Date: 07/30/2013
• Status: Active Grant

• Current Assignee: Goodrich Lighting Systems GmbH (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Goodrich Lighting Systems GmbH (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Schoen, Christian
• Primary Examiner(s): Ton, Anabel
• Application Number:
  US14/338,364
• Publication Number:
  US 20150036366A1
• Time in Patent Office: 1,147 Days
• Field of Search: 362470
• CPC Class Codes: B64D 47/02 Arrangements or adaptations of signal or lighting devices

Abstract

An exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength, with corresponding emission characteristics is disclosed. The exterior aircraft light unit has at least one first light source configured to emit the light of the first wavelength, at least one second light source configured to emit the light of the second wavelength, and a wavelength selective optical element, which wavelength selective optical element is reflective for the light of the first wavelength and transparent for the light of the second wavelength.

Claims

1. An exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength, with corresponding emission characteristics, the exterior aircraft light unit comprising:

at least one first light source configured to emit the light of the first wavelength,

at least one second light source configured to emit the light of the second wavelength, and

a wavelength selective optical element, which wavelength selective optical element is reflective for the light of the first wavelength and transparent for the light of the second wavelength,

wherein the at least one first light source, the at least one second light source and the wavelength selective optical element are arranged in such a way that both the light of the first wavelength and the light of the second wavelength hit the wavelength selective optical element, with the light of the first wavelength being reflected by the wavelength selective optical element and the light of the second wavelength being passed through by the wavelength selective optical element, and with the light of the at least one first light source, upon being reflected by the wavelength selective optical element, and the light of the at least one second light source, upon being passed through by the wavelength selective optical element, having corresponding directional characteristics,

wherein the at least one first light source and the at least one second light source are positioned on the same side of the wavelength selective optical element, and

wherein the exterior aircraft light unit further comprises at least one additional optical element, disposed on a side of the wavelength selective optical element where the at least one first light source and the at least one second light source are not positioned, wherein the wavelength selective optical element is shaped to give the light of the first wavelength the corresponding directional characteristics and wherein the at least one additional optical element is shaped to give the light of the second wavelength the corresponding directional characteristics.

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

3. The Exterior aircraft light unit according to claim 1, wherein the light of the first wavelength and the light of the second wavelength, when emitted from the exterior aircraft light unit, is a substantially collimated beam.

4. The Exterior aircraft light unit according to claim 1, wherein the wavelength selective optical element has one of a parabolic shape and a spherical shape and wherein the at least one additional optical element has one of a parabolic shape and a spherical shape.

5. The Exterior aircraft light unit according to claim 1, adapted to be one of a fixed position light and a movable search and/or landing light.

6. The Exterior aircraft light unit according to claim 1, wherein each of the at least one first light source and the at least one second light source is an LED.

7. The Aircraft, such as an air plane or a helicopter, comprising at least one exterior aircraft light unit according to claim 1.

8. The Method of operating an exterior aircraft light unit to claim 1, comprising the steps of:

controlling the at least one first light source to emit light of the first wavelength, resulting in the exterior aircraft light unit emitting light of the first wavelength with first emission characteristics, and

controlling the at least one second light source to emit light of the second wavelength, resulting in the exterior aircraft light unit emitting light of the second wavelength with second emission characteristics, corresponding to the first emission characteristics.

9. An exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength, with corresponding emission characteristics, the exterior aircraft light unit comprising:

at least one first light source configured to emit the light of the first wavelength,

at least one second light source configured to emit the light of the second wavelength, and

a wavelength selective optical element, which wavelength selective optical element is reflective for the light of the first wavelength and transparent for the light of the second wavelength,

wherein the at least one first light source, the at least one second light source and the wavelength selective optical element are arranged in such a way that both the light of the first wavelength and the light of the second wavelength hit the wavelength selective optical element, with the light of the first wavelength being reflected by the wavelength selective optical element and the light of the second wavelength being passed through by the wavelength selective optical element, and with the light of the at least one first light source, upon being reflected by the wavelength selective optical element, and the light of the at least one second light source, upon being passed through by the wavelength selective optical element, having corresponding directional characteristics,

wherein the at least one first light source and the at least one second light source are positioned on opposite sides of the wavelength selective optical element,

wherein the wavelength selective optical element is plane, oriented substantially orthogonal to a connection line between the at least one first light source and the at least one second light source, and

wherein the exterior aircraft light unit further comprises at least one additional optical element, disposed on a side of the wavelength selective optical element where the at least one first light source is positioned, the at least one additional optical element being one of a parabolic reflector and a spherical reflector and being configured to equally affect the light of the first wavelength as well as of the light of the second wavelength.

10. The Exterior aircraft light unit according to claim 9, wherein the first wavelength is in the visible light range and wherein the second wavelength is in the infrared range.

11. The Exterior aircraft light unit according to claim 9, wherein the light of the first wavelength and the light of the second wavelength, when emitted from the exterior aircraft light unit, is a substantially collimated beam.

12. The Exterior aircraft light unit according to claim 9, adapted to be one of a fixed position light and a movable search and/or landing light.

13. The Exterior aircraft light unit according to claim 9, wherein each of the at least one first light source and the at least one second light source is an LED.

14. The Aircraft, such as an air plane or a helicopter, comprising at least one exterior aircraft light unit according to claim 9.

15. The Method of operating an exterior aircraft light unit to claim 9, comprising the steps of:

controlling the at least one first light source to emit light of the first wavelength, resulting in the exterior aircraft light unit emitting light of the first wavelength with first emission characteristics, and

controlling the at least one second light source to emit light of the second wavelength, resulting in the exterior aircraft light unit emitting light of the second wavelength with second emission characteristics, corresponding to the first emission characteristics.

16. An exterior aircraft light unit for emitting light of a first wavelength and light of a second wavelength, different from the first wavelength, with corresponding emission characteristics, the exterior aircraft light unit comprising:

at least one first light source configured to emit the light of the first wavelength,

at least one second light source configured to emit the light of the second wavelength, and

a wavelength selective optical element, which wavelength selective optical element is reflective for the light of the first wavelength and transparent for the light of the second wavelength,

wherein the at least one first light source, the at least one second light source and the wavelength selective optical element are arranged in such a way that both the light of the first wavelength and the light of the second wavelength hit the wavelength selective optical element, with the light of the first wavelength being reflected by the wavelength selective optical element and the light of the second wavelength being passed through by the wavelength selective optical element, and with the light of the at least one first light source, upon being reflected by the wavelength selective optical element, and the light of the at least one second light source, upon being passed through by the wavelength selective optical element, having corresponding directional characteristics,

wherein the at least one first light source and the at least one second light source are positioned on opposite sides of the wavelength selective optical element, and

wherein the exterior aircraft light unit further comprises at least one additional optical element, disposed on a side of the wavelength selective optical element where the at least one second light source is positioned, wherein the wavelength selective optical element is shaped to give the light of the first wavelength the corresponding directional characteristics and wherein the at least one additional optical element is shaped to give the light of the second wavelength the corresponding directional characteristics, and

wherein the wavelength selective optical element has one of a parabolic shape and a spherical shape and wherein the at least one additional optical element is a reflective optical element and has one of a parabolic shape and a spherical shape.

17. The Exterior aircraft light unit according to claim 16, wherein the at least one second light source is a plurality of n second light sources and wherein the at least one additional optical element is a plurality of n additional optical elements, with n□

2, with each of the plurality of n additional optical elements being provided for shaping the light of a respective second light source.

18. The Exterior aircraft light unit according to claim 16, wherein the first wavelength is in the visible light range and wherein the second wavelength is in the infrared range.

19. The Exterior aircraft light unit according to claim 16, wherein the light of the first wavelength and the light of the second wavelength, when emitted from the exterior aircraft light unit, is a substantially collimated beam.

20. The Exterior aircraft light unit according to claim 16, adapted to be one of a fixed position light and a movable search and/or landing light.

21. The Exterior aircraft light unit according to claim 16, wherein each of the at least one first light source and the at least one second light source is an LED.

22. The Aircraft, such as an air plane or a helicopter, comprising at least one exterior aircraft light unit according to claim 16.

23. The Method of operating an exterior aircraft light unit to claim 16, comprising the steps of:

controlling the at least one first light source to emit light of the first wavelength, resulting in the exterior aircraft light unit emitting light of the first wavelength with first emission characteristics, and

controlling the at least one second light source to emit light of the second wavelength, resulting in the exterior aircraft light unit emitting light of the second wavelength with second emission characteristics, corresponding to the first emission characteristics.