Method for disinfecting an aircraft cabin using a lighting assembly and a lighting assembly therefor

US11524783B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11524783-B2
Application numberUS-201816753367-A
CountryUS
Kind codeB2
Filing dateOct 3, 2018
Priority dateOct 6, 2017
Publication dateDec 13, 2022
Grant dateDec 13, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A lighting assembly for an aircraft includes a visible light source generating visible light and an ultraviolet light source generating ultraviolet light. The visible light source is disposed adjacent to the ultraviolet light source. The visible light source illuminates a first illumination area with the visible light when the lighting assembly operates in a first operation mode. The ultraviolet light source illuminates a second illumination area with the ultraviolet light when the lighting assembly operates in a second mode of operation. The first illumination area substantially overlaps the second illumination area.

First claim

Opening claim text (preview).

What is claimed is: 1. A lighting assembly for an aircraft, comprising: a visible light source generating visible light; an ultraviolet light source generating ultraviolet light; and a controller connected to the lighting assembly to control operation of the visible light source and the ultraviolet light source; wherein the visible light source is disposed adjacent to the ultraviolet light source, wherein the visible light source illuminates a first illumination area with the visible light when the lighting assembly operates in a first operation mode, wherein the ultraviolet light source illuminates a second illumination area with the ultraviolet light when the lighting assembly operates in a second mode of operation, wherein the first illumination area substantially overlaps the second illumination area; and wherein the controller is connected to a plurality of window shades and closes the window shades when the ultraviolet light source operates in the second mode of operation. 2. The lighting assembly of claim 1 , wherein the visible light source and the ultraviolet light source are disposed on a single substrate. 3. The lighting assembly of claim 2 , wherein the visible light source comprises a plurality of visible light generators. 4. The lighting assembly of claim 3 , wherein the plurality of visible light generators comprise LEDs. 5. The lighting assembly of claim 3 , wherein the ultraviolet light source comprises a plurality of ultraviolet light generators. 6. The lighting assembly of claim 5 , wherein the plurality of ultraviolet light generators comprise LEDs. 7. The lighting assembly of claim 5 , wherein a first number of the plurality of visible light generators is greater than or equal to a second number of the plurality of ultraviolet light generators. 8. The lighting assembly of claim 1 , further comprising: a first sensor connected to the controller to detect when a door to the aircraft is closed and generate a first input signal for the controller. 9. The lighting assembly of claim 1 , further comprising a second sensor to detect the absence of a person in the aircraft and generate a second input for the controller. 10. The lighting assembly of claim 9 , wherein the second sensor is a motion sensor. 11. The lighting assembly of claim 1 , wherein the controller is operatively connected to a management system and receives a third input from the management system indicating that the aircraft is parked. 12. The lighting assembly of claim 1 , wherein the controller is connected to a plurality of seats and positions the seats in a configuration so that the seats are bathed in the ultraviolet light when the ultraviolet light source operates in the second mode of operation. 13. A method of operating a lighting assembly comprising a visible light source generating visible light, an ultraviolet light source generating ultraviolet light, a controller connected to the lighting assembly to control operation of the visible light source and the ultraviolet light source, a first sensor connected to the controller to detect when a door to an aircraft is closed and generate a first input, and a second sensor to detect the absence of a person in the aircraft and generate a second input, wherein the visible light source is disposed adjacent to the ultraviolet light source, wherein the visible light source illuminates a first illumination area with the visible light when the lighting assembly operates in a first operation mode, and wherein the ultraviolet light source illuminates a second illumination area with the ultraviolet light when the lighting assembly operates in a second mode of operation, wherein the controller is operatively connected to a management system and receives a third input from the management system indicating that the aircraft is parked, and wherein the controller is connected to a plurality of window shades, the method comprising: receiving, by the controller, the first input; receiving, by the controller, the second input; receiving, by the controller, the third input; initiating the second operation mode after receipt of the first input, the second input, and the third input; and closing, by the controller, the window shades when the ultraviolet light source operates in the second mode of operation. 14. The method of claim 13 , wherein the controller is connected to a plurality of seats, the method further comprising: positioning the seats in a configuration so that the seats are bathed in the ultraviolet light when the ultraviolet light source operates in the second mode of operation. 15. The method of claim 13 , wherein the controller is connected to a plurality of seats, the method further comprising: positioning the seats in a configuration so that the seats are bathed in the ultraviolet light when the ultraviolet light source operates in the second mode of operation. 16. The method of claim 13 , further comprising: checking periodically, by the controller, the first input, the second input, and the third input. 17. The method of claim 16 , further comprising: stopping the second operation mode upon failure of receipt of at least one of the first input, the second input, or the third input.

Assignees

Inventors

Classifications

  • Room floors or walls · CPC title

  • Sensor means, e.g. motion, brightness, scent, contaminant sensors · CPC title

  • Lighting means · CPC title

  • Means for controlling sterilisation processes, data processing, presentation and storage means, e.g. sensors, controllers, programs · CPC title

  • A61L2/10Primary

    Ultraviolet [UV] radiation · CPC title

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What does patent US11524783B2 cover?
A lighting assembly for an aircraft includes a visible light source generating visible light and an ultraviolet light source generating ultraviolet light. The visible light source is disposed adjacent to the ultraviolet light source. The visible light source illuminates a first illumination area with the visible light when the lighting assembly operates in a first operation mode. The ultraviole…
Who is the assignee on this patent?
Bombardier Inc
What technology area does this patent fall under?
Primary CPC classification A61L2/10. Mapped technology areas include Human Necessities.
When was this patent published?
Publication date Tue Dec 13 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).