Interior aircraft lighting assembly, aircraft passenger service unit with an interior aircraft lighting assembly, and method of operating an interior aircraft lighting assembly

Patent metadata

Field	Value
Publication number	US-12420927-B2
Application number	US-202418980381-A
Country	US
Kind code	B2
Filing date	Dec 13, 2024
Priority date	Mar 30, 2023
Publication date	Sep 23, 2025
Grant date	Sep 23, 2025

Abstract

An interior aircraft lighting assembly comprises: at least one infrared lighting device for emitting infrared light; at least one further lighting device for emitting visible light; a lighting assembly controller for controlling an operation of the at least one infrared lighting device and of the at least one further lighting device; a supplementary infrared lighting device controller; and a power supply network, which is configured for supplying electric power from the lighting assembly controller to the at least one further lighting device. The supplementary infrared lighting device controller is tapped into the power supply network. The lighting assembly controller is configured to provide an electric trigger pulse on the power supply network for activating the at least one infrared lighting device.

First claim

The invention claimed is:

1. An interior aircraft lighting assembly, comprising:
at least one infrared lighting device for emitting infrared light;
at least one passenger reading light for emitting visible light;
a lighting assembly controller for controlling an operation of the at least one infrared lighting device and of the at least one passenger reading light;
a supplementary infrared lighting device controller; and
a power supply network, which is configured for supplying electric power from the lighting assembly controller to the at least one passenger reading light;
wherein the supplementary infrared lighting device controller is tapped into the power supply network;
wherein the power supply network comprises a permanent power supply line, a permanent ground line, and at least one switchable ground line;
wherein the supplementary infrared lighting device controller is electrically coupled between the permanent power supply line and the permanent ground line; and
wherein each of the at least one passenger reading light is electrically coupled between the permanent power supply line and a respective switchable ground line, which is switchable by the lighting assembly controller for selectively activating and deactivating the respective reading light.

2. The interior aircraft lighting assembly according to claim 1 , wherein the power supply network comprises a separate switchable ground line for each of the at least one passenger reading light.

3. The interior aircraft lighting assembly according to claim 1 , wherein the lighting assembly controller is configured to provide an electric trigger pulse on the power supply network for activating the at least one infrared lighting device.

4. The interior aircraft lighting assembly according to claim 3 , wherein the lighting assembly controller is configured to provide the electric trigger pulse on the permanent power supply line.

5. The interior aircraft lighting assembly according to claim 3 , wherein the supplementary infrared lighting device controller is coupled to the at least one infrared lighting device and is configured to enable power flow to the at least one infrared lighting device in response to detecting the electric trigger pulse, provided by the lighting assembly controller on the power supply network.

6. An aircraft passenger service unit, comprising at least one interior aircraft lighting assembly according to claim 1 .

7. The aircraft passenger service unit of claim 6 , wherein the aircraft passenger service unit further comprises at least one of a loudspeaker, a gasper and a passenger oxygen supply mask.

8. An aircraft, comprising an interior aircraft lighting assembly according to claim 1 .

9. An interior aircraft lighting assembly, comprising:
at least one infrared lighting device for emitting infrared light;
at least one visual sign lighting device for emitting visible light;
a lighting assembly controller for controlling an operation of the at least one infrared lighting device and of the at least one visual sign lighting device;
a supplementary infrared lighting device controller; and
a power supply network, which is configured for supplying electric power from the lighting assembly controller to the at least one visual sign lighting device;
wherein the supplementary infrared lighting device controller is tapped into the power supply network;
wherein the power supply network comprises at least one switchable power supply line and a permanent ground line;
wherein each of the at least one visual sign lighting device is electrically coupled between a respective switchable power supply line and the permanent ground line, with the respective switchable power supply line being switchable by the lighting assembly controller for selectively activating and deactivating the respective visual sign lighting device; and
wherein the supplementary infrared lighting device controller is electrically coupled between one or more of the at least one switchable power supply line and the permanent ground line.

10. The interior aircraft lighting assembly according to claim 9 , wherein the power supply network comprises a separate switchable power supply line for each visual sign lighting device.

11. The interior aircraft lighting assembly according to claim 9 , wherein the lighting assembly controller is configured to provide an electric trigger pulse on the power supply network for activating the at least one infrared lighting device.

12. The interior aircraft lighting assembly according to claim 11 , wherein the lighting assembly controller is configured to provide the electric trigger pulse on one or more of the at least one switchable power supply line, coupled to the supplementary infrared lighting device controller.

13. The interior aircraft lighting assembly according to claim 11 , wherein the supplementary infrared lighting device controller is coupled to the at least one infrared lighting device and is configured to enable power flow to the at least one infrared lighting device in response to detecting the electric trigger pulse, provided by the lighting assembly controller on the power supply network.

14. The interior aircraft lighting assembly according to claim 9 , wherein the supplementary infrared lighting device controller is electrically coupled between the permanent ground line and a particular switchable power supply line that is associated with a particular visual signal lighting device that is normally on.

15. The interior aircraft lighting assembly according to claim 14 , wherein the particular visual signal lighting device is a non-smoking signal light.

16. An aircraft passenger service unit, comprising at least one interior aircraft lighting assembly according to claim 9 .

17. The aircraft passenger service unit of claim 16 , wherein the aircraft passenger service unit further comprises at least one of a loudspeaker, a gasper and a passenger oxygen supply mask.

18. An aircraft, comprising an interior aircraft lighting assembly according to claim 9 .

Assignees

• Goodrich Lighting Systems Gmbh & Co Kg

Inventors

• Schön Christian
• Hessling-Von Heimendahl Andre

Classifications

• F21V23/02

  the elements being transformers, impedances {or power supply units, e.g. a transformer with a rectifier} · CPC title

• F21V23/003

  the elements being electronics drivers or controllers for operating the light source, e.g. for a LED array · CPC title

• B64D2011/0053

  Cabin passenger reading lights · CPC title

• F21Y2113/30

  of visible and non-visible spectrum · CPC title

• F21W2106/00

  Interior vehicle lighting devices · CPC title