PROACTIVE AIR/SURFACE DECONTAMINATION SYSTEM AND DEVICES
20230173128 · 2023-06-08
Assignee
Inventors
Cpc classification
A61L2202/16
HUMAN NECESSITIES
A61L2209/15
HUMAN NECESSITIES
A61L2209/21
HUMAN NECESSITIES
A61L2209/111
HUMAN NECESSITIES
International classification
Abstract
A system for decontaminating/neutralizing breathable air and surfaces in an occupied enclosed space, i.e. building, aircraft, vehicle or greenhouse, includes mounting an atmospheric hydroxyl radical generator along an inside surface of the atmospheric hydroxyl radical generator having respective opposite air inlets and air outlets. The hydroxyl radical generator includes a polygonal housing supporting a plurality of spaced crystal-spliced UV optics, which are tubular, medical grade pure quartz optics to emit/irradiate ultraviolet in the nanometer wavelength/ultraviolet spectrum of between 100 and 400 nanometers for deactivating and neutralizing atmospheric chemicals and pathogens in breathable air and surfaces. The hydroxyl radicals contact the walls of the reaction chamber housing. The hydroxyl radicals become created and excited to react quickly with impurities including VOC, virus, bacteria and fungi, rendering them inactivated and neutral. The breathable air passes through the polygonal housing and is decontaminated and neutralized of impurities before entering the occupied enclosed space.
Claims
1. An aircraft incorporating apparatus for cleaning breathable air in passenger compartments thereof comprising: at least one duct for delivering breathable air into each said passenger compartment; an atmospheric hydroxyl generator comprising a housing having an air inlet at one end and air outlet at an opposite end thereof mounted within each said duct for exposing ambient water vapor to a plurality of spaced crystal-spliced UV lamp optics having hydroxyl activation portions made of medical grade pure quartz material for delivering a stream of hydroxyls into said breathable air for each compartment; each said housing containing said plurality of spaced crystal-spliced UV lamp optics, said UV lamps being tubular, medical grade pure quartz optics designed to emit/irradiate ultraviolet in the nanometer wavelength/ultraviolet spectrum of between 100 and 400 nanometers for deactivating chemicals and pathogens in said breathable air for its respective passenger compartment; whereby hydroxyl radicals, created and excited within said walls, becoming excited sufficiently to react quickly with impurities including VOC, viruses, bacteria and mold, rendering them inactivated; and whereby said breathable air passing through each said housing within its said duct is cleansed of said impurities before entering each said passenger compartment.
2. The aircraft of claim 1 in which a passenger compartment occupied by crew members engaged in the operation of said aircraft is supplied with breathable air by a duct and hydroxyl generator isolated from any other duct and hydroxyl generator on said aircraft for security purposes.
3. The aircraft of claim 2 in which said housing is elongated, polygon-shaped in cross section, and mounted on an inside wall surface of each respective said duct.
4. The aircraft of claim 3 in which each said housing is configured as a clamshell having a top wall, upper side walls, a hinge for opening said housing, and a bottom clamshell portion allowing for opening said housing within said duct for some maintenance, one of said upper side walls being removably attached to said inside wall surface of said duct allowing for removal of each said housing for maintenance and repair.
5. The aircraft of claim 4 in which a master events controller for each said hydroxyl generator is mounted on an outside wall surface of each said duct adjacent a respective said housing for controlling operation of said adjacent hydroxyl generator.
6. The aircraft of claim 5 in which each said housing includes baffles arranged in such a manner that said UV lamp optics are not exposed to eyes of any observers because of dangers of such exposure.
7. The aircraft of claim 6 in which each said duct is part of a separate HVAC system for each said passenger compartment.
8. The aircraft of claim 7 in which each said HVAC system is retro fit using a hole cut into its respective said duct whereby each said respective hydroxyl generator is slid in place.
9. The aircraft of claim 8 in which each said master events controller includes means to indicate failure of any of said UV lamps as detected by a UV light sensor.
10. The aircraft of claim 9 in which said master events controller also includes safety features including means for detecting opening of its respective said housing.
11. The aircraft of claim 1 wherein said retrofitting of said breathable air system comprises the step of adding and coupling said atmospheric hydroxyl generator into one or more aircraft air conduits from a remote site external to the aircraft, which, for safety reasons, provide breathable cabin air through each said conduit, each said conduit being a flexible conduit extending from a source of said fresh air external to the aircraft, to avoid engaging said atmospheric hydroxyl generator at the site of the aircraft tarmac, wherein said atmospheric hydroxyls are added to the breathable cabin air, and wherein said stream of atmospheric hydroxyls are provided from a retrofit box compartment external to the aircraft, directing said atmospheric hydroxyls through said flexible conduit into the cabin of the aircraft.
12. A method for cleaning breathable air in occupied passenger compartments of an aircraft comprising the steps of: retrofitting and inserting an atmospheric hydroxyl generator for exposing ambient water vapor to a plurality of spaced crystal-spliced UV lamp optics having hydroxyl activation portions made of medical grade pure quartz material for delivering a stream of hydroxyls into said breathable air for each compartment, into a duct for delivering said breathable air into each said passenger compartment, each said hydroxyl generator comprising an elongated housing containing said plurality of spaced crystal-spliced UV lamp optics, said UV lamps being tubular, medical grade pure quartz optics designed to emit/irradiate ultraviolet in the nanometer wavelength/ultraviolet spectrum of between 100 and 400 nanometers for deactivating chemicals and pathogens in said breathable air, said housing having an air inlet at one end and an air outlet at an opposite end thereof; mounting each said housing on an inside wall surface of an associated duct whereby at least a portion of air flowing through said associated duct passes through its respective hydroxyl generator; whereby hydroxyl radicals, created and excited within said walls, becoming excited sufficiently to react quickly with impurities including VOC, viruses, bacteria and mold, rendering them inactivated; and whereby said breathable air passing through each said housing within each said duct is cleansed of said impurities before entering an associated passenger compartment.
13. The method of claim 12 in which a passenger compartment occupied by crew members engaged in the operation of said aircraft is supplied with breathable air by a duct and hydroxyl generator isolated from any other duct and hydroxyl generator on said aircraft for security purposes.
14. The method of claim 13 in which each said housing is configured as a clamshell having a top wall, upper side walls, a hinge for opening said housing, and a bottom clamshell portion allowing for opening said housing within said duct for some maintenance, one of said upper side walls being removably attached to said inside wall surface of said duct allowing for removal of said housing for maintenance and repair.
15. The method of claim 14 in which one of said upper side walls is removably attached to said inside wall surface of said duct allowing for removal of said housing for maintenance and repair.
16. The method of claim 15 in which a master events controller for each said hydroxyl generator is mounted on an outside wall surface of each said duct adjacent its respective housing for controlling operation of said hydroxyl generator.
17. The method of claim 16 in which each said housing includes baffles arranged in such a manner that said UV lamp optics are not exposed to eyes of any observers because of dangers of such exposure.
18. The method of claim 17 in which each said duct is part of a HVAC system for each said passenger compartment.
19. The method of claim 18 in which each passenger compartment HVAC system is retro fit using a hole cut into each said duct whereby said hydroxyl generator is slid in place.
20. The method of claim 19 in which each said master events controller includes means to indicate failure of any of said UV lamps as detected by a UV light sensor.
21. The method of claim 20 in which each said master events controller also includes safety features including means for detecting opening of a respective said housing.
22. The method of claim 21 in which atmospheric hydroxyls are produced on site by each said hydroxyl generator.
23. The method of claim 22 in which said atmospheric hydroxyls are introduced for a sufficient period of time for all surfaces, both exposed and hidden, to be cleansed of volatile organic compounds (VOC) and biological contaminants.
24. The method of claim 23 in which said biological contaminants are selected from the group consisting of viruses, bacteria, protozoa, and fungi.
25. The method of claim 22 in which said site comprises a passenger cabin interior of a passenger aircraft before all passengers have departed and before and while new passengers enter.
26. The method of claim 12 in which said atmospheric hydroxyls are introduced for a sufficient period of time for all surfaces, both exposed and hidden, to be decontaminated/neutralized of volatile organic compounds (VOC) and biological contaminants.
27. The method as in claim 12 wherein said retrofitting of said breathable air system comprises the step of adding and coupling said atmospheric hydroxyl generator into one or more aircraft air conduits from a remote site external to the aircraft, which, for safety reasons, provide breathable cabin air through each said conduit, each said conduit being a flexible conduit extending from a source of said fresh air external to the aircraft, to avoid engaging said atmospheric hydroxyl generator at the site of the aircraft tarmac, wherein said atmospheric hydroxyls are added to the breathable cabin air, and wherein said stream of atmospheric hydroxyls are provided from a retrofit box compartment external to the aircraft, directing said atmospheric hydroxyls through said flexible conduit into the cabin of the aircraft.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0037] The present invention can best be understood in connection with the following drawings, which are not deemed to be limiting in scope.
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DETAILED DESCRIPTION OF THE DRAWINGS
[0049]
[0050] In contrast to the medical grade quartz tubular optics, it is noted that total glass tubes cannot be used when generating UV. The glass would simply be vaporized. Some companies use a fusion of glass and quartz crystal, which is not optimal as the glass portion creates a frequency that actually attracts contaminants. This problematic action neutralizes the desired UV action. Such a fusion lamp of glass and quartz crystal is cheaper to produce, however the poor performance of the lamp would be the end result.
[0051] Other similar Medical Grade quartz tubed UV optics can be used. The optic 12 and 13 are preferably symmetrically positioned in the housing of the hydroxyl generator 1, as shown in
[0052] Furthermore, once these radicals are emitted, they can penetrate any crevices in any area, such as between seats of mass transit vehicles, between the surfaces of desks; anywhere where ultraviolet light by itself would not be capable of eradicating the undesirable VOCs, fungi, virus, bacteria, etc. The polygon-shaped housing is strategically located within an air duct wall, which can be in a building which has sub walls extending to various rooms in the building, or it can be into the central area of a mass transit railroad or other mass transit vehicles, or it may be provided in the three air systems of an aircraft cabin, including the flight deck and the areas of the main cabin where passengers are seated.
[0053] As shown in the end view of
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[0055]
[0056]
[0057] In the diagrammatic flow chart of
[0058] While
[0059] In another embodiment, as shown in
[0060] The greenhouse has a top roof area 300a, side walls 300b and 300c, and a base ground level 300d. The greenhouse 300 is adjacent to a utility room 350, which has utility controls 320 for controlling the electronics and mechanics of the system, as well as a hydroponic fluid source 390, which provides the hydroponic fluid through a pipe conduit 360. The pipe 360 has the lower parts of the roots and the media soaking in the fluid, with an upper portion of the roots and media being exposed to air of the plants 370, which have roots 370a held in place by media 370B. The hydroponic fluid 370e is provided through the hydroponic fluid pipe 360. The polygonal-shaped hydroxyl generators 310 are produced in an enclosed air duct, which is preferably a fan 351, and produces an airflow into an air duct 330, which emanates horizontally from the fan 351, or other air source, then makes an upward 90-degree turn, through an air duct portion 330a, which then turns at 90 degrees horizontally at an upper portion of the utility room 350 through a horizontal portion 330b, within which is located the hydroxyl generator, just before a further downward air duct portion 330c emanates downward to the level of trough 334 inside the greenhouse, so that the air from the downward portion 330c of the air duct is then sent horizontally through a flexible sock sleeve 340, having multiple upper apertures 341 to permit the radical hydroxyl flows below and then around the hydroponic fluid pipe, and then contacting the air and plant roots 370a of the plants 370, within the media, such as the coconut fiber 370b. Optionally, an overhead mister hose 365 may be provided in case the plants are not hydroponically bred. In any case, the hydroxyls, whether they are blown or pumped through the root system and media in the greenhouse trough in the hydroponic growing system in the greenhouse, the hydroxyl radicals are exposed to the portions of the roots 370a and growing media 370b, so that they can be misted exposed therein while being irrigated and/or fertigated, either hydroponically, or alternatively within conventional soil media. In this version, the greenhouse 300 is connected to the utility room 350. The hydroxyl generators are installed in a strategic position at the top of the air duct 330b, before the hydroxylated air is sent downward through portion 330c of undulating air duct 330 spanning from utility laboratory room 350 and greenhouse 300 and then the air filled with hydroxyls is sent to the flexible sock sleeve 340, having upper apertures 341 for release of the hydroxyls to intermingle with the plant roots 370a of the hydroponically grown plants 370 located above the parallel troughs 334 of greenhouse 300.
[0061]
[0062] In an alternate embodiment in a non-hydroponic system, as shown in
[0063] The hydroxyl generators shown in
[0064] In addition, in the greenhouse embodiment, the hydroxyl generators are provided so that the hydroxyl radicals will flow adjacent to and through the media of the plants being farmed therein.
[0065] In the foregoing description, certain terms and visual depictions are used to illustrate the preferred embodiment. However, no unnecessary limitations are to be construed by the terms used or illustrations depicted, beyond what is shown in the prior art, since the terms and illustrations are exemplary only, and are not meant to limit the scope of the present invention.
[0066] It is further known that other modifications may be made to the present invention, without departing the scope of the invention, as noted in the appended Claims