DEPLOYABLE ULTRAVIOLET SANITATION SYSTEM FOR AN AIRCRAFT

Abstract

A sanitation system includes an overhead passenger service unit panel with a concealed light source providing a single wavelength of Ultraviolet light wherein the light source is deployed and sanitation is performed when the aircraft cabin is free of commercial passengers.

Claims

1. A sanitation system comprising: an overhead passenger service unit panel including a concealed light source providing a single wavelength of Ultraviolet light wherein the light source is deployed and sanitation is performed when the aircraft cabin is free of commercial passengers.

2. The sanitation system of claim 1 wherein the single wavelength of light is in the UV-C band.

3. The sanitation system of claim 1 wherein the UV-C band is in a range of 200 nm to 280 nm.

4. The sanitation system of claim 1 further comprising: a door integrated with the panel, the door accommodating a UV housing.

5. The sanitation system of claim 4 further comprising a drive motor, the drive motor configured to rotate the UV housing through a predetermined sweep.

6. The sanitation system of claim 5 wherein the UV housing includes at least three UV light modules comprising the light source.

7. The sanitation system of claim 6 wherein the at least three UV light modules are arranged in a row and are configured to sweep across a set of two or more seats.

8. The sanitation system of claim 1 further comprising a drip shield positioned around the UV light module.

9. The sanitation system of claim 1 wherein the light source comprises a plurality of UV-C lights emitting light in a range of approximately 200 nm to 280 nm.

10. A sanitation system for an aircraft cabin having a plurality of seats, the sanitation system comprising: an overhead passenger service unit panel; a door integrated with the panel, the door configured to rotate between a stowed position generally flush with the panel and a deployed position; a UV light housing connected with respect to the door; a plurality of UV light modules connected with respect to the UV light housing, the UV light modules emitting UV light in a single wavelength in the UV-C band.

11. The sanitation system of claim 10 wherein the UV-C band is in a range of 200 nm to 280 nm.

12. The sanitation system of claim 10 further comprising a drive motor, the drive motor configured to rotate the UV housing through a predetermined sweep.

13. The sanitation system of claim 10 wherein the UV housing includes at least three UV light modules comprising the light source.

14. The sanitation system of claim 10 wherein the door is configured to open only when each of the plurality of seats is unoccupied.

15. The sanitation system of claim 10 wherein the door is configured to rotate in a direction perpendicular to an alignment of the plurality of seats.

16. The sanitation system of claim 10 wherein the door is configured to rotate across a group of two or more seats.

17. A method of sanitizing an aircraft cabin having a plurality of seats, the method comprising: positioning an overhead passenger service unit panel over two or more seats; integrating a door with the panel to rotate between a stowed position generally flush with the panel and a deployed position; positioning a plurality of UV light modules with respect to the door, the UV light modules emitting UV light in a single wavelength in the UV-C band; configuring the door to deploy when the aircraft cabin is empty; and activating the light modules in a single bandwidth between 200 nm and 280 nm.

18. The method of claim 17 further comprising oscillating the door in a continuous back-and-forth sweep across the two or more seats.

19. The method of claim 17 further comprising pausing rotation of the door for a predetermined time period in a direction of each seat.

20. The method of claim 17 further comprising: activating a lock on the door when the aircraft cabin is occupied.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0009] FIG. 1 illustrates the mechanical system associated with a panel located in the cabin of an aircraft which contains the deployable Ultraviolet panel;

[0010] FIG. 2 shows a view of the Ultraviolet system panel in a deployed state; and

[0011] FIG. 3 shows a view of the Ultraviolet system in a stowed state.

DETAILED DESCRIPTION OF THE INVENTION

[0012] The present invention provides a system and method for sanitizing the surfaces which the passenger interacts with in a commercial aircraft cabin. FIGS. 1-3 show the Ultraviolet Light panel which is typically located above the passenger seats, but can be installed in other locations throughout the aircraft as needed. Applicable areas could include lavatories, galley area, flight attendant seating areas, entryways, crew rest areas and aisleways. The Ultraviolet light panel is preferably concealed while in flight and will only be deployed when persons are clear of the immediate area of the light. Safety features to prevent inadvertent deployment can also be integrated into the system as an added level of safety.

[0013] According to one preferred embodiment of the invention, the Ultraviolet light panel may be positioned above each and every seat on the aircraft and then may be deployed during aircraft turnaround and/or routine maintenance intervals. According to another preferred embodiment of the invention, the Ultraviolet light panel may be positioned over groupings of 2 or 3 or more seats and may be deployed and then manually or automatically rotated to sweep across each seat area in a predefined increment or interval. Whether the Ultraviolet light panel is assigned to a single seat or a series of seats, the focus of the light is preferably adjustable and moveable to ensure coverage over all seat areas.

[0014] As shown in FIGS. 1-3, a sanitation system comprises an overhead passenger service unit panel 20 including a concealed light source providing a single wavelength of Ultraviolet light wherein the light source is deployed and sanitation is performed when the aircraft cabin is free of commercial passengers.

[0015] In particular, according to one embodiment, the panel 20 replaces a spacer panel that is generally found in the ceilings of commercial aircraft. The panel 20 is preferably attachable to aircraft using an outboard rail latch 80 and an inboard rail latch 90 that affix to existing rails within the aircraft cabin structure.

[0016] A door 30 is preferably integrated with the panel 20. The door 30 is desirably flush with the panel 20 while in a stowed condition, that is, while the sanitation system is not deployed. The door 30 preferably accommodates a UV housing 50.

[0017] As shown in FIGS. 1 and 2, the UV housing 50 preferably includes three UV light modules 60 that together comprise the light source used for sanitizing the aircraft cabin. Although three UV light modules 60 are shown, more or fewer UV light modules 60 may be adapted to the sanitation system described based upon factors such as distance from the surfaces to be disinfected, the UV bandwidth desired, the duration of sanitization cycles desired, and other factors. The at least three UV light modules 60 are preferably arranged in a row and are configured to sweep across a set of one, two or three or more seats.

[0018] A drive motor 70 is preferably positioned within the panel 20 and is configured to rotate the UV housing 50 and attached UV light module(s) 60 through a predetermined sweep. The drive motor 70 is preferably powered by a 12 VDC power supply. The drive motor 70 is preferably configured with a controller to rotate in one or more desirable routines, as described in more detail below.

[0019] Preferred UV light modules 60 include a single wavelength of light in the UV-C band. A preferred bandwidth is in a range of 200 nm to 280 nm, most desirably approximately 270 nm.

[0020] The sanitation system and panel 20 as described preferably additionally include a drip shield 40 positioned around the UV light module 60. Condensation may accumulate in the interstitial portions of the aircraft above the cabin infrastructure and such moisture may otherwise create issues for the sanitation system mechanicals and UV light modules 60 if not properly guarded.

[0021] A corresponding method of sanitizing an aircraft cabin having a plurality of seats includes positioning an overhead passenger service unit panel 20 over one or more seats, preferably one panel 20 per seating group; integrating a door 30 with the panel 20 to rotate between a stowed position generally flush with the panel 20 and a deployed position; positioning a plurality of UV light modules 60 with respect to the door 30, the UV light modules 60 emitting UV light in a single wavelength in the UV-C band; configuring the door 30 to deploy when the aircraft cabin is empty; and activating the light modules 60 in a single bandwidth between 200 nm and 280 nm.

[0022] The door 30 may be preferably deployed to oscillate in a continuous back-and-forth sweep across the two or more seats. Alternatively, or in addition, the door 30 may be deployed such that rotation of the door 30 is paused for a predetermined time period generally in alignment with each seat. The duration of efficacy may range between approximately 80 seconds to 30 minutes, depending on factors such as bandwidth, distance to surfaces, surface materials, and inherent cleanliness of surfaces. The door 30 is preferably configured to rotate in a direction perpendicular to an alignment of the plurality of seats.

[0023] To safely deploy and activate the sanitation system, a lock 25 may be activated on the door 30 at all times when the aircraft cabin is occupied. In such a way, the sanitation system and/or the door 30 may be configured to open only when each of the plurality of seats is unoccupied. The system may be additionally integrated with the cabin management system of the aircraft to deploy and/or stow the UV housing 50 during intended and desired increments thereby eliminating passenger exposure to UV light and damage to the system by passengers.

[0024] Preferably the sanitation operation would take place during change over and before or after the cabin cleaning crew has addressed the cabin.

[0025] The invention illustratively disclosed herein suitably may be practiced in the absence of any element, part, step, component, or ingredient which is not specifically disclosed herein.

[0026] While in the foregoing detailed description this invention has been described in relation to certain preferred embodiments thereof, and many details have been set forth for purposes of illustration, it will be apparent to those skilled in the art that the invention is susceptible to additional embodiments and that certain of the details described herein can be varied considerably without departing from the basic principles of the invention.