Aircraft vertical stabilizer illumination light unit and method of operating an aircraft vertical stabilizer illumination light unit

Patent metadata

Field	Value
Publication number	US-10336468-B2
Application number	US-201615183828-A
Country	US
Kind code	B2
Filing date	Jun 16, 2016
Priority date	Jun 19, 2015
Publication date	Jul 2, 2019
Grant date	Jul 2, 2019

Abstract

An aircraft vertical stabilizer illumination light unit, configured for being arranged in a rotatable horizontal stabilizer of an aircraft and for being oriented towards a vertical stabilizer of the aircraft for illuminating the vertical stabilizer, includes an LED group, having a plurality of LEDs, and an optical system, having at least one optical element, the optical system being associated with the LED group for shaping an output light intensity distribution from the light emitted by the LED group.

First claim

The invention claimed is:

1. An aircraft vertical stabilizer illumination light unit, comprising:
an LED group, comprising a plurality of LEDs, and
an optical system, comprising at least one optical element, the optical system being associated with the LED group for shaping an output light intensity distribution from the light emitted by the LED group;
wherein the unit is configured for being arranged in a rotatable horizontal stabilizer of an aircraft and for being oriented towards a vertical stabilizer of the aircraft for illuminating the vertical stabilizer;
wherein the LED group and the optical system are stationary within the aircraft vertical stabilizer illumination light unit, with each LED of the LED group having a set position with respect to the optical system;
wherein at least some of the plurality of LEDs are independently controllable; and
wherein the aircraft vertical stabilizer illumination light unit is configured to be operated in a plurality of operating modes, with a respective subset of the plurality of LEDs being switched on in each of the plurality of operating modes and with a different output light intensity distribution being emitted by the aircraft vertical stabilizer illumination light unit in each of the plurality of operating modes, with a selection of the operating mode being carried out in response to a rotation angle of the rotatable horizontal stabilizer.

2. The aircraft vertical stabilizer illumination light unit according to claim 1 , wherein the aircraft vertical stabilizer illumination light unit is configured to carry out the selection of the operating mode in such a way that substantially the entire vertical stabilizer of the aircraft is illuminated for a given rotation angle of the rotatable horizontal stabilizer within a predefined rotation angle range.

3. The aircraft vertical stabilizer illumination light unit according to claim 2 , wherein the predefined rotation angle range covers an angular range of at least 10°.

4. The aircraft vertical stabilizer illumination light unit according to claim 1 , wherein, for each of the plurality of operating modes, the respective subset of the plurality of LEDs emits light illuminating a respective illumination sector of a vertical plane through the vertical stabilizer, with the respective illumination sector being less than 120% in area, as compared to the vertical stabilizer.

5. The aircraft vertical stabilizer illumination light unit according to claim 4 , wherein the respective illumination sector substantially corresponds in area to the vertical stabilizer.

6. The aircraft vertical stabilizer illumination light unit claim 1 , wherein the plurality of operating modes comprises a reference operating mode for illuminating the vertical stabilizer with a reference output light intensity distribution, when the rotatable horizontal stabilizer is in a reference position, and a plurality of adjusted operating modes, having respective adjusted output light intensity distributions, wherein each of the adjusted output light intensity distributions compensates for a particular rotation of the aircraft vertical stabilizer illumination light unit.

7. The aircraft vertical stabilizer illumination light unit according to claim 1 , wherein each of the plurality of operating modes has a vertical light output opening angle, based on a height extension of the vertical stabilizer, and a horizontal light output opening angle, based on a length extension of the vertical stabilizer, with a combined horizontal light output opening angle of all of the plurality of operating modes being 5° to 20° larger than the horizontal light output opening angle of each one of the plurality of operating modes.

8. The aircraft vertical stabilizer illumination light unit according to claim 1 , wherein, for each of the plurality of operating modes, a vertical light opening angle is between 70° and 90°.

9. The aircraft vertical stabilizer illumination light unit according to claim 1 , having exactly one optical system, with all of the plurality of LEDs being associated with the exactly one optical system and with light output by the plurality of LEDs being affected differently by the exactly one optical system due to their different positioning with respect thereto.

10. The aircraft vertical stabilizer illumination light unit according to any of claim 8 , wherein the LED group comprises at least two LED sub-groups and wherein the optical system comprises at least two optical sub-systems, with each LED sub-group forming an optical set with a respective optical sub-system and with each optical set being optically independent from the other optical sets.

11. The aircraft vertical stabilizer illumination light unit according to claim 1 ,
wherein the aircraft vertical stabilizer illumination light unit comprises a rotation angle sensor configured to sense the rotation angle of the horizontal stabilizer.

12. An aircraft having in a tail portion of the aircraft a vertical stabilizer, a left rotatable horizontal stabilizer and a right rotatable horizontal stabilizer,
wherein each of the left rotatable horizontal stabilizer and the right rotatable horizontal stabilizer comprises an aircraft vertical stabilizer illumination light unit according to claim 1 , oriented towards the vertical stabilizer for illumination thereof.

13. A method of operating an aircraft vertical stabilizer illumination light unit, installed in a rotatable horizontal stabilizer of an aircraft for illuminating a vertical stabilizer of the aircraft, the method comprising the steps of:
operating the aircraft vertical stabilizer illumination light unit in a reference operating mode, having a reference output light intensity distribution for illuminating substantially the entire vertical stabilizer, when the rotatable horizontal stabilizer is in a reference position, and
operating the aircraft vertical stabilizer illumination light unit in one of a plurality of adjusted operating modes, each having an adjusted output light intensity distribution, as a response to the rotatable horizontal stabilizer being rotated from the reference position by a particular rotation angle,
wherein each of the plurality of adjusted output light intensity distributions compensates for a respective particular rotation angle of the aircraft vertical stabilizer illumination light unit, such that substantially the entire vertical stabilizer is illuminated in each of the plurality of adjusted operating modes.

14. The method according to claim 13 , wherein the aircraft vertical stabilizer illumination light unit comprises an LED group having a plurality of LEDs and wherein the method comprises the step of switching on, for each of the reference operating mode and the plurality of adjusted operating modes, a respective subset of the plurality of LEDs for illuminating the vertical stabilizer.

15. The method according to claim 14 , wherein, for each of the reference operating mode and the plurality of adjusted operating modes, the respective selected subset of the plurality of LEDs emits light illuminating a respective illumination sector of a vertical plane through the vertical stabilizer, with the respective illumination sector being less than 120% in area, as compared to the vertical stabilizer.

16. The aircraft vertical stabilizer illumination light unit according to claim 2 , wherein the predefined rotation angle range covers an angular range of between 10° and 20°.

17. The aircraft vertical stabilizer illumination light unit according to claim 1 , wherein each of the plurality of operating modes has a verti

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Lueder Sascha

Classifications

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• B64C5/16

  about spanwise axes · CPC title

• B64D47/06 Primary

  for indicating aircraft presence · CPC title

• B64C5/02

  Tailplanes · CPC title

• B64D45/0005

  Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear · CPC title