Aircraft disinfection system and device

Abstract

To provide systems and devices for sterilizing aircraft surfaces during a flight at frequent time intervals to stop transmission of pathogenic microorganisms in an aircraft.SOLUTION: An aircraft sterilization system includes a frame, and a tray that is operatively coupled to at least first two corners of the frame and rotatable about a pivot axis. The tray is configured to be in one of a locked state and an unlocked state based on rotation about the pivot axis. In the unlocked state, the tray is at an angle greater than zero with respect to the frame; and, in the locked state, the tray is at an angle equal to zero with respect to the frame. The aircraft sterilization system further includes a set of ultraviolet (UV) light emitting diodes (LEDs) attached onto an exposed surface of the frame, where the set of UV LEDs is configured to sterilize the tray when the tray is in the locked state.SELECTED DRAWING: Figure 1

Description

Technical Field

[0001] The present invention generally relates to disinfection systems, and more specifically to disinfection systems and devices for aircraft.

Background Art

[0002] In the era of the pandemic, it is of utmost importance to monitor the surface contamination by pathogenic microorganisms (such as viruses or bacteria). Disinfection of frequently contacted surfaces such as the surfaces inside an aircraft is as necessary as disinfecting body parts in order to suppress the pandemic without interrupting international trade and travel. Since pathogenic microorganisms can maintain their activity on the surface for several days, rapid spread of infection becomes possible. Pathogenic microorganisms include, for example, coronavirus, Ebola virus, Nipah virus, Salmonella typhi, Mycobacterium tuberculosis, etc. Local outbreaks of epidemics such as COVID-19 may spread domestically or internationally with a higher probability through air travel. In such outbreaks, air travel is severely restricted, causing social and economic damage to each country.

[0003] Ultraviolet (UV) light waves with a wavelength range of 100 nanometers (nm) to 280 nm are inherently bactericidal. The bactericidal wavelength range of UV corresponds to short-wavelength UV, also known as UV-C. Since inexpensive and energy-efficient UV-C light-emitting diodes (LEDs) have been developed, UV-C has been used for the sterilization of surfaces, water, or air.

[0004] In the state-of-the-art technology at present, there are technologies for using UV-C light to disinfect surfaces. However, the existing technologies do not provide an overall disinfection system and are limited to some surfaces and enclosures inside the aircraft, such as galleys, air ducts, aircraft cabins, lavatories, etc. Furthermore, with this technology, it is necessary to keep passengers or crew away for surface disinfection using UV light. Surfaces such as trays, handles of overhead storage bins, and handles of lavatories are frequently contacted by multiple passengers and crew during flights.

[0005] Therefore, in order to suppress the spread of pathogenic microorganisms inside the aircraft, there is a need for a system and device for disinfecting the surfaces of the aircraft at frequent time intervals during flight.

Summary of the Invention

[0006] In one embodiment of the present invention, a disinfection system for an aircraft is disclosed. In one example, the disinfection system for an aircraft includes a safety belt. The safety belt includes a first portion attached to the first fabric portion of the safety belt and a second portion attached to the second fabric portion of the safety belt. The first portion is for receiving the second portion and fastening the safety belt. The disinfection system for an aircraft further includes a first storage casing for completely enclosing the first portion. The first storage casing includes a first inner wall for enclosing the outer surface of the first portion. The first storage casing is attached to the first inner wall and further includes a first set of ultraviolet (UV) light-emitting diodes (LEDs) for disinfecting the outer surface of the first portion. The first storage casing further includes a tongue for cooperating with the first portion of the safety belt. The first storage casing is attached to the surface of the tongue and further includes a second set of UV LEDs for disinfecting the inner surface of the first portion. The disinfection system for an aircraft further includes a second storage casing for enclosing the second portion. The second storage casing includes a second inner wall for enclosing the second portion. The second storage casing is attached to the second inner wall and further includes a third set of UV LEDs for disinfecting the second portion.

[0007] In other embodiments of the present invention, a disinfection system for an aircraft is disclosed. In one example, the aircraft disinfection system includes a frame. The aircraft disinfection system further includes a tray operatively coupled to at least a first two corner portions of the frame and rotatable about a pivot axis. The tray is configured to be in either a locked state or an unlocked state based on rotation about the pivot axis. The tray forms an angle greater than zero with respect to the frame in the unlocked state and an angle equal to zero with respect to the frame in the locked state. The aircraft disinfection system includes a set of UV LEDs attached to the exposed surface of the frame. The set of UV LEDs is configured to disinfect the tray when the tray is in the locked state.

[0008] In still other embodiments of the present invention, a disinfection system for an aircraft is disclosed. The aircraft disinfection system includes an armrest that includes a pocket and an upper lid. The pocket is for storing a tray, and the upper lid covers the pocket. The aircraft disinfection system further includes a storage mechanism enclosed in the pocket. A first end of the storage mechanism is removably attached to the tray, and a second end of the storage mechanism is fixed within the pocket. The storage mechanism is configured to pull the tray out of the pocket in an open state. In the open state, the tray is at least partially located outside the pocket. The storage mechanism is further configured to retract the tray into the pocket in a closed state. In the closed state, the tray is completely located inside the pocket. The aircraft disinfection system further includes a first set of UV LEDs attached to each inner wall of the pocket. The first set of UV LEDs is configured to disinfect each surface of the tray when the tray is in the closed state.

[0009] In still other embodiments of the present invention, a disinfection device for an aircraft is disclosed. The disinfection device for an aircraft includes a curved enclosure operatively coupled to a first surface of a containment area. In a first position, the curved enclosure at least partially encloses a handle attached to the first surface. The handle allows access to the containment area. The curved enclosure further includes an inner surface facing the first surface in the first position of the curved enclosure. The curved enclosure further includes an outer surface opposite the first surface in the first position. The disinfection device for an aircraft further includes a set of UV LEDs attached to the inner surface. The set of UV LEDs is configured to disinfect the handle. The disinfection device for an aircraft further includes at least one switch disposed on at least one of the first surface and the second surface of the containment area. Each of the at least one switch is turned on in a closed state of the containment area and turned off in an open state of the containment area. The disinfection device for an aircraft further includes at least one locking mechanism. The at least one locking mechanism is configured to engage the first surface in a closed state. The at least one locking mechanism is further configured to be disengaged from the first surface in an open state. The disinfection device for an aircraft further includes a controller communicatively connected to each set of UV LEDs, the at least one switch, and the at least one locking mechanism. The controller is configured to activate the set of UV LEDs when each of the at least one switch is turned on and the locking mechanism is in a closed state and engaged with the first surface.

[0010] It should be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the claimed invention.

Brief Description of the Drawings

[0011] The accompanying drawings, which are incorporated in and constitute a part of this disclosure, illustrate exemplary embodiments and, together with the description, serve to explain the disclosed principles.

Figure 1

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Best Mode for Carrying Out the Invention

[0012] Hereinafter, exemplary embodiments of the present invention will be described with reference to the accompanying drawings. For convenience, the same reference numbers are used throughout the drawings to refer to the same or similar components. This specification describes examples and features of the disclosed principles, but appropriate modifications, adaptations, and other applications are possible without departing from the spirit and scope of the disclosed embodiments. The following detailed description is intended to be considered as illustrative only, and the true scope and spirit of the present invention are defined based on the description in the appended claims. Additional exemplary embodiments are as described below.

[0013] FIG. 1 is an explanatory diagram illustrating an aircraft cabin 100 that can adopt various embodiments. The aircraft cabin 100 can include a plurality of passenger seats (e.g., passenger seat 102a, passenger seat 102b, passenger seat 104a, and passenger seat 104b), a plurality of overhead storage bins (e.g., overhead storage bin 106), and a lavatory 110. Each of the plurality of passenger seats can include a safety belt (e.g., safety belt 112). In one embodiment, passenger seat 102a can include an armrest 114a, and passenger seat 102b can include an armrest 114b. Each of armrest 114a and armrest 114b can include a pocket (e.g., pocket 116), a tray (e.g., tray 118), and an upper lid (e.g., upper lid 120). When the tray is enclosed within the pocket, the pocket can be configured to store the tray, and the upper lid can be configured to cover the pocket. Further, the tray can be in an open state or a closed state. The tray is at least partially located outside the pocket in the open state and completely located inside the pocket in the closed state. In passenger seat 102a, tray 118 is in the open state, and in passenger seat 102b, the tray is in the closed state and covered by upper lid 120. This is as will be described in more detail later in relation to FIG. 5.

[0014] The passenger seat 104a can include a back. A frame (e.g., frame 122) can be attached to the back. Further, a tray (e.g., tray 124a or tray 124b) can be operatively coupled to at least first two corner portions of the frame, such that the tray is rotatable about a pivot axis (not shown in FIG. 1). The tray can be in an unlocked state, in which the tray forms an angle greater than zero with respect to the frame. Alternatively, the tray can be in a locked state, in which the tray forms an angle equal to zero with respect to the frame. That is, the tray is in full contact with the frame. Further, a latch (not shown in FIG. 1) can be provided to cooperate or engage with the tray. For this purpose, the tray can include a recess, cavity or protrusion in which the latch can engage in the locked state. In the unlocked state, the latch can disengage from the tray. Tray 124a is in the unlocked state and tray 124b is in the locked state. This will be described in more detail later in connection with FIG. 4.

[0015] The passenger seats each include a safety belt, e.g., a seat belt 112 The safety belt can include a first portion attached to the first fabric portion thereof and a second portion attached to the second fabric portion of the safety belt. The first portion can be configured, for example, as a female portion of a buckle used to secure the seat belt. Also, the second portion can be configured, for example, as a male portion of the buckle. That is, the first portion is configured to receive the second portion for securing the safety belt. This will be described in more detail later in connection with FIGS. 2 and 3. Also, the plurality of overhead storage bins can each include a handle (e.g., handle 126a or handle 126b). Also, the dressing room 110 can include a handle 128.

[0016] Needless to say, contact of body parts (such as fingers, hands, arms, elbows, etc.) with various aircraft surfaces during flight is assumed. As an example, aircraft surfaces include, but are not limited to, safety belt 112, tray 118, trays 124a and 124b, handles 126a and 126b, and handle 128. Also, body parts can be a source of contamination. Infectious diseases can be transmitted if at least one of the aircraft surfaces is contaminated. As an example, infectious diseases include, but are not limited to, coronavirus disease (COVID-19), Ebola virus disease, H1N1 infection, Nipah virus infection, Salmonella infection, tuberculosis, etc. Therefore, each surface of the aircraft may need to be regularly disinfected even during flight.

[0017] For this purpose, multiple sets of ultraviolet (UV) light-emitting diodes (LEDs) can be installed in various locations of the aircraft cabin 100. The multiple sets of UV LEDs can be configured to disinfect each surface of the aircraft. Needless to say, light in the UV wavelength range is bactericidal. By exposing to UV light for a predetermined threshold time, each surface of the aircraft can be disinfected. However, since ultraviolet rays are carcinogenic, it may be necessary to avoid exposure to the human body. Therefore, it is desirable to perform disinfection of each surface of the aircraft by UV light when there are no passengers or crew on board the aircraft or in a state of being isolated from exposure to the human body during the flight of the aircraft. This will be described in detail later in relation to FIGS. 2 to 10.

[0018] FIG. 2 is a series of explanatory diagrams illustrating an aircraft disinfection system 200 according to an embodiment for disinfecting a first portion 202 of a safety belt. The safety belt can be the safety belt 112 in the aircraft cabin 100. The series of explanatory diagrams of the aircraft disinfection system 200 are a perspective view 204a, a perspective view 204b, a top view 204c, a side view 204d, and a front view 204e. The aircraft disinfection system 200 can include a first portion 202 of the safety belt (e.g., the female part of the buckle) attached to a first fabric portion 206 of the safety belt (e.g., safety belt 112). The safety belt can include a second portion (not shown in FIG. 2, e.g., the male part of the buckle) attached to a second fabric portion of the safety belt (not shown in FIG. 2). The first portion 202 is configured to receive the second portion to fix the safety belt. The second portion and the second fabric portion of the safety belt are as described in detail later in relation to FIG. 3. The perspective view 204a shows the first portion 202 and the first fabric portion 206 of the safety belt. The aircraft disinfection system 200 can further include a first storage casing 208. The first storage casing 208 is configured to completely enclose the first portion 202 for disinfecting it.

[0019] The first storage casing 208 can include a first inner wall 210, a first set of UV LEDs 212, and a tong 214. The first inner wall 210 can be configured to surround the first outer surface. Further, the first set of UV LEDs 212 can be attached to the first inner wall 210. The first set of UV LEDs 212 can be configured to disinfect the outer surface of the first portion 202. In some embodiments, the first set of UV LEDs 212 can include at least one UV-C LED. Further, the tong 214 can be configured to cooperate with the first portion 202 of the safety belt 112. The perspective view 204b shows the cooperation relationship between the tong 214 and the first portion 202. In the perspective view 204b, when the insertion of the first portion 202 into the first storage casing 208 is completed, the tong 214By lifting the flap 202a, it is possible to disinfect the inner wall of the flap 202a in the first part 202 (not shown in FIG. 2) and the area of the first part 202 that was not covered by the flap 202a before lifting. The tongs 214 can be fixed within the first storage casing 208 and can be at least partially disposed inside the first part 202. In another embodiment, the tongs 214 can be completely disposed inside the first part 202.

[0020] The tongs 214 can have a second set of UV LEDs 216 attached to each of its surfaces. The second set of UV LEDs 216 is shown in the front view 204e. The second set of UV LEDs 216 can be configured to disinfect the inner surface of the first part 202. In one embodiment, the second set of UV LEDs 216 can disinfect the inner wall (not shown in FIG. 2). In some embodiments, the second set of UV LEDs 216 can include at least one UV-C LED. The top view 204c shows the first part 202 surrounded by the first storage casing 208. The side view 204d shows the cooperation between the tongs 214 and the first part 202. Also, the front view 204e shows the first part 202 surrounded by the first storage casing 208.

[0021] In some embodiments, the first storage casing 208 includes a first slit 218 (shown in side view 204d) for receiving the first fabric portion 206. The first slit 218 can include a first pair of rollers (not shown in FIG. 2) for cooperating with the first fabric portion 206. That is, after passing through the first slit 218, the first fabric portion 206 is fixed or attached to the first portion 202. The first pair of rollers confines the first portion 202 by sliding the first storage casing 208 over the first fabric portion 206. As described above, the first fabric portion 206 passes through the first storage casing 208 via the first slit 218. In one embodiment, the first storage casing 208 can include a first electric mechanism (not shown in FIG. 2) coupled to the first pair of rollers. The first electric mechanism can be configured to slide the first storage casing 208 over the first fabric portion 206 by operating the first pair of rollers. The first electric mechanism can be constituted by, for example, an electric motor.

[0022] The aircraft disinfection system 200 can further include a first set of sensors (not shown in FIG. 2) within the first storage casing 208. The first set of sensors can be configured to determine the complete confinement of the first portion 202. As an example, the first set of sensors can include, but is not limited to, proximity sensors, cameras, ultrasonic sensors, etc. Further, the aircraft disinfection system 200 can include a controller (not shown in FIG. 2) communicatively connected to each of the first set of UV LEDs 212, the second set of UV LEDs 216, the first set of sensors, and the first electrification mechanism.

[0023] The controller can be configured to respond to a disinfection execution signal, give an instruction to the first electric mechanism to slide on the first cloth portion 206, thereby enclosing 208 that wraps the first storage casing. The disinfection execution signal can be generated, for example, when the crew and passengers disembark from the aircraft and no one is on board the aircraft. Alternatively, the disinfection execution signal can be generated when the second portion of the safety belt is not inserted into the first portion 202. That is, the disinfection execution signal can be generated when the male part of the safety belt buckle is removed from the female part of the safety belt buckle.

[0024] Furthermore, the controller can be configured to activate each of the first set of UV LEDs 212 and the second set of UV LEDs 216 in response to a first set of sensors that confirm the complete enclosure of the first portion 202 by the first storage case. After a predetermined period has elapsed since the activation of the first set of UV LEDs 212 and the second set of UV LEDs 216, the controller can be configured to give an instruction to the first electric mechanism to slide on the first cloth portion 206, thereby exposing the first storage casing 208. In some embodiments, the controller can be configured to deactivate the first set of UV LEDs 212 and the second set of UV LEDs 216 in response to confirmation of partial enclosure of the first set of sensors. In other words, if someone tries to pull out the first portion 202 currently enclosed in the first storage casing 208, the controller can deactivate the first set of UV LEDs 212 and the second set of UV LEDs 216. The controller can be configured to deactivate the first set of UV LEDs 212 and the second set of UV LEDs 216 respectively when any movement is detected by the first set of sensors. As will be apparent to those skilled in the art, the aircraft disinfection system 200 is not limited to aircraft and can be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 200 can also be applied to public facilities such as movie theaters and malls.

[0025] FIG. 3 is a series of explanatory diagrams illustrating an aircraft disinfection system 300 according to an embodiment for disinfecting a second portion 302 of a safety belt. The safety belt can be the safety belt 112 of the aircraft cabin 100. The series of explanatory diagrams showing the aircraft disinfection system 300 are a perspective view 304a, a top view 304b, a front view 304c, and a side view 304d. The perspective view 304a shows the second portion 302 attached to the second fabric portion 306 of the safety belt. Further, the aircraft disinfection system 300 can include a second storage casing 308 for surrounding the second portion 302. The second storage casing 308 can include a second inner wall 310 and a third set of UV LEDs 312. The inner wall 310 can be configured to surround the second portion 302. The third set of UV LEDs 312 can be attached to the second inner wall 310. The third set of UV LEDs 312 is configured to disinfect the second portion 302. In some embodiments, the third set of UV LEDs 312 can include at least one UV-C LED.

[0026] In some embodiments, the second storage casing 308 includes a second slit 314 (shown in the side view 304d) configured to receive the second fabric portion 306. That is, the second fabric portion 306 passes through the second slit and is attached to the second portion. Further, the second slit 314 can include a second pair of rollers (not shown in FIG. 3) for cooperating with the second fabric portion 306. That is, the second pair of rollers enables the second storage casing 308 to slide on the second fabric portion 306 to enclose the second second portion 302. The second fabric portion 306 passes through the second storage casing 308 via the second slit 314. In one embodiment, the second storage casing 308 can include an electric mechanism (not shown in FIG. 3) coupled to the second pair of rollers. The second electric mechanism can be configured to slide the second storage casing 308 on the second fabric portion 306 by operating the second pair of rollers. The second electric mechanism can be composed of, for example, an electric motor.

[0027] The aircraft disinfection system 300 can further include a second set of sensors (not shown in FIG. 3) within the second storage casing 308. The second set of sensors can be configured to determine complete containment of the second portion by the second storage casing 308. As an example, the second set of sensors can include, but is not limited to, proximity sensors, cameras, ultrasonic sensors, etc. The aircraft disinfection system 300 can include a controller (not shown in FIG. 3) communicatively connected to each of the third set of UV LEDs 312, the second set of sensors, and the second electric mechanism. The controller can be configured to give an instruction to the second electric mechanism to slide on the second cloth portion 306 in response to the disinfection execution signal described in detail in FIG. 2, thereby containing the second storage casing 308.

[0028] Furthermore, the controller can be configured to activate a third set of UV LEDs 312 in response to a second set of sensors that determine a complete containment of the second portion 302 by the second housing 308. The controller can be configured to give an instruction to the second motor mechanism after a predetermined period has elapsed to slide on the second fabric component 306, thereby exposing the second housing 308. In some embodiments, the controller can be configured to deactivate the third set of UV LEDs 312 in response to a second set of sensors that determine a partial containment of the second portion 302 by the second housing 308. That is, if someone attempts to pull out the second portion 302 currently contained by the second housing 308, the controller can deactivate the third set of UV LEDs 312. Also, the controller can be configured to deactivate the third set of UV LEDs 312 when the second set of sensors detect any movement. As will be apparent to those skilled in the art, the aircraft disinfection system 300 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks, or any vehicle. The aircraft disinfection system 300 can also be applied to public use facilities, such as movie theaters and malls.

[0029] FIG. 4 is a series of explanatory diagrams illustrating an aircraft disinfection system 400 according to an embodiment for disinfecting a tray 402. This series of explanatory diagrams includes a perspective view 404a, a top view 404b, a front view 404c, a top view 404d, a front view 404e, a side view 404f in the closed state, and a side view 404g in the open state. The aircraft disinfection system 400 can include a frame 406 and a tray 402. In one embodiment, the frame 406 can be attached to the back of a passenger seat (e.g., passenger seat 104a) in the aircraft cabin 100. In other embodiments, the frame can be attached to the cabin wall of the aircraft.

[0030] The tray 402 can be operably coupled to at least the first two corner portions (e.g., corner portions 406a and 406b) of the frame 406 and can be rotatable about a pivot axis 408 (intersecting the corners 406a and 406b). The tray 402 can be configured to be in a locked state and / or an unlocked state based on rotation about the pivot axis 408. The tray 402 forms an angle greater than zero with respect to the frame 406 in the unlocked state and an angle equal to zero with respect to the frame 406 in the locked state. The tray 402 is shown in the unlocked state in each of the top view 404d, the front view 404e, and the side view 404f. The tray 402 is shown in the unlocked state in each of the perspective view 404a, the top view 404b, the front view 404c, and the side view 404g.

[0031] The aircraft disinfection system 400 can further include a set of UV LEDs 410 attached to the exposed surface of the frame 402. The tray 402 can face the exposed surface of the frame 402 in the locked state. The set of UV LEDs 410 can be configured to disinfect the tray 402 when the tray 402 is in the locked state. In some embodiments, the set of UV LEDs 410 can include at least one UV-C LED. The frame 406 can include at least one switch (e.g., switch 412a and switch 412b) disposed on the outer periphery of the frame 406. The tray 402 can be configured to enclose each of the at least one switch in the locked state. The frame 406 can also include a latch 414 for cooperating with the tray 402. The latch 414 can engage with the tray 402 in the locked state and can be released from the tray 402 in the unlocked state. For this purpose, the tray 402 can include a recess, a cavity, or a protrusion for engaging the latch 414 in the locked state.

[0032] Frame 406 can include a controller communicatively connected to at least one switch and latch 414. The controller can be configured to activate a set of UV LEDs 410 when a set of predetermined conditions are met. The set of conditions can include that the trays 402 are each in a locked state, that at least one switch is turned on, and that the latch 414 engages the tray 402. In some embodiments, frame 406 can include at least one sensor for generating an inactivate signal based on a predetermined criterion. As an example, the predetermined criterion can be a transition of the tray 402 from a locked state to an unlocked state. As another example, the predetermined criterion can be the detection of some movement or a human body part. The controller can be communicatively connected to the at least one sensor. Thus, the controller can be configured to deactivate the set of UV LEDs 410 in response to an inactivate signal generated by the at least one sensor. The at least one sensor can be disposed on the outer periphery of the frame 406 and can be enclosed by the tray 402 in the locked state. As will be apparent to those skilled in the art, the aircraft disinfection system 400 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 400 can also be applied to public use facilities, such as movie theaters and malls.

[0033] FIG. 5 is a series of explanatory diagrams illustrating an aircraft disinfection system 500 according to another embodiment for disinfecting a tray 502. These series of explanatory diagrams are a perspective view 504a, a perspective view 504b, a front view 504c, and a side view 504d. The aircraft disinfection system 500 can include an armrest 506 of a passenger seat. As an example, the passenger seat is the passenger seat 102a in the aircraft cabin 100. The armrest 506 can include a pocket 508 and an upper lid 510. The pocket 508 can be configured to store a tray. When the tray 502 is stored in the pocket 508, the upper pocket 508 is covered by the lid 510. Further, the aircraft disinfection system 500 can include a storage mechanism 506a that is enclosed within the pocket. The storage mechanism 506a has its first end (not shown in FIG. 5) removably attached to the tray 502 and its second end (not shown in FIG. 5) fixed within the pocket 508. The storage mechanism 506a can be configured to pull the tray 502 out of the pocket 508 in an open state. The tray 502 can be positioned at least partially outside the pocket 508 in an open state. Further, the storage mechanism 506a can be configured to store the tray 502 within the pocket 508 in a closed state. The tray 502 can be positioned completely inside the pocket 508 in a closed state. The tray 502 is shown in an open state in the perspective view 504a and in a closed state in the perspective view 504b.

[0034] Furthermore, the aircraft disinfection system 500 can include a first set of UV LEDs 512 attached to each inner wall of the pocket 508. The first set of UV LEDs 512 can be configured to disinfect each surface of the tray 502 when the tray 502 is in the closed state. In some embodiments, the first set of UV LEDs 512 can include at least one UV-C LED. In one embodiment, the first end (not shown in FIG. 5) of the upper lid 510 is hinged to the armrest 506 to enable the upper lid 510 to rotate around a pivot axis, and the second end (not shown in FIG. 5) of the upper lid 510 can be configured to cooperate with the armrest 506 to enable the closed and open states. Furthermore, the aircraft disinfection system 500 can include at least one switch (not shown in FIG. 5) disposed on the armrest 506. Each of the at least one switch is configured to be enclosed and turned on by the upper lid 510 in the closed state. Furthermore, each of the at least one switch is configured to be exposed and turned off by the upper lid 510 in the open state.

[0035] The aircraft disinfection system 500 can further include a locking mechanism (not shown in FIG. 5). The locking mechanism can be configured to cooperate with the second end of the upper lid 510 to enable the closed and open states. The locking mechanism can be configured to engage with the upper lid 510 in the closed state and disengage from the upper lid 510 in the open state. Furthermore, the aircraft disinfection system 500 can include a controller (not shown in FIG. 5) communicatively connected to each of the at least one switch and the locking mechanism. When each of the at least one switch is actuated and the locking mechanism engages with the upper lid 510 in the closed state, the controller can be configured to activate the first set of UV LEDs 512.

[0036] In one embodiment, the aircraft disinfection system 500 can include at least one sensor for generating an inoperative signal in response to a predetermined criterion. As an example, the predetermined criterion can be the transition of the tray 502 from a locked state to an unlocked state. As another example, the predetermined criterion can be the detection of any movement or a body part. The controller can be communicatively connected to the at least one sensor. The controller can be configured to deactivate the first set of UV LEDs 512 in response to the inoperative signal generated by the at least one sensor. As will be apparent to those skilled in the art, the aircraft disinfection system 500 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 500 can also be applied to public use facilities, such as movie theaters, malls, etc.

[0037] FIG. 6 is a series of explanatory diagrams illustrating an aircraft disinfection system 600 according to an embodiment for disinfecting a foldable tray 602. These series of explanatory diagrams are a perspective view 604a, a perspective view 604b, a front view 604c, and a side view 604d. The aircraft disinfection system 600 can include an armrest 606 of a passenger seat. The passenger seat is the passenger seat 102a of the aircraft cabin 100. The armrest 606 can include a pocket 608 and an upper lid 610. The pocket 608 can be configured to store the foldable tray 602. The upper lid 610 can be configured to cover the pocket 608. The storage tray 602 can include a plurality of parts (for example, part 612a and part 612b) hinged to each other. Further, at least one of the plurality of parts can be stored around the associated pivot axis 614 on the remaining plurality of parts. Further, the aircraft disinfection system 600 can include a storage mechanism 606a enclosed in the pocket 608. The first end (not shown in FIG. 6) of the storage mechanism 606a can be removably attached to the storage tray 602, and the second end (not shown in FIG. 6) of the storage mechanism 606a can be fixed within the pocket 608. The storage mechanism 606a can be configured to pull out the storage tray 602 from the pocket 608 in an open state. The storage tray 602 can be positioned at least partially outside the pocket 608 in an open state. Further, the storage mechanism 606a can be configured to retract the storage tray 602 into the pocket 608 in a closed state. The storage tray 602 can be positioned completely inside the pocket 608 in a closed state. The storage tray 602 is shown in an open state in the perspective view 604a and in a closed state in the perspective view 604b.

[0038] The aircraft disinfection system 600 can further include a first set of UV LEDs 616 attached to each inner wall of the pocket 608. The first set of UV LEDs 616 can be configured to disinfect each surface of the storage tray 602 when the storage tray 602 is in the closed state. In some embodiments, the first set of UV LEDs 616 can include at least one UV-C LED. In one embodiment, a first end (not shown in FIG. 6) of the upper lid 610 is hinged to the armrest 606 and can be rotated about a pivot axis, and a second end (not shown in FIG. 6) of the upper lid 610 can be configured to cooperate with the armrest 606 to enable a closed state and an open state. Further, the aircraft disinfection system 600 can include at least one switch (not shown in FIG. 6) disposed on the armrest 606. Each of the at least one switch can be enclosed by the closed upper lid 610 and can be configured to be turned on. Further, each of the at least one switch can be exposed by the upper lid 610 in the open state and can be configured to be turned off.

[0039] Furthermore, the pocket 608 can include at least one tong (e.g., tong 618) disposed between its inner walls. A second set of UV LEDs (not shown in FIG. 6) can be mounted facing the at least one tong. The second set of UV LEDs can be configured to disinfect at least one of a plurality of portions in the storage tray 602. As an example, the portion 612a can be pivoted around the pivot axis 614 on the portion 612b so that when the storage tray 602 is in the closed state, the storage tray 602 can be fully positioned inside the pocket 608. Further, the portion 612a can be configured to be stored such that the angle formed between each edge portion thereof and each edge portion of the portion 612b is zero. The tong 618 can be positioned between the portion 612a and the portion 612b in the closed state. The second set of UV LEDs can be mounted on each surface of the tong 618 and can be configured to disinfect each surface of the portion 612a and the portion 612b of the storage tray 602.

[0040] The aircraft disinfection system 600 can include a locking mechanism (not shown in FIG. 6). The locking mechanism can be configured to cooperate with the second end of the upper lid 610 to enable a closed state and an open state. The locking mechanism can be configured to engage with the upper lid 610 in the closed state and disengage from the upper lid 610 in the open state. Further, the aircraft disinfection system 600 can include at least one switch and a controller communicatively connected to each of the locking mechanisms. The controller can be configured to activate the first set of UV LEDs 616 and the second set of UV LEDs when each of the at least one switch is turned on and the locking mechanism engages with the upper lid 610 in the closed state. In one embodiment, the aircraft disinfection system 600 can include at least one sensor for generating an inoperative signal in response to a predetermined criterion. As an example, the predetermined criterion is the transition of the foldable tray 602 from the locked state to the unlocked state. As another example, the predetermined criterion is the detection of any movement or body part. The controller can be communicatively connected to at least one sensor. The controller can be configured to deactivate the first set of UV LEDs 616 and the second set of UV LEDs in response to an inoperative signal generated by at least one sensor. As will be apparent to those skilled in the art, the aircraft disinfection system 600 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 600 can also be applied to public use facilities, such as movie theaters and malls.

[0041] FIG. 7 is a series of explanatory diagrams illustrating an aircraft disinfection device 700 according to an embodiment for disinfecting a handle 702 of an overhead storage bin 704. The overhead storage bin 704 can be made similar to the overhead storage bin 108 in the aircraft cabin 100. A series of explanatory diagrams of the aircraft disinfection system 700 include a perspective view 706a, a front view 706b, a front view 706c of the handle 702, a bottom view 706d of the handle 702, and a side view 706e. The aircraft disinfection device 700 can include a curved enclosure 708 operatively coupled to a first surface 710 of an enclosed area (in this case, the overhead storage bin 704). The curved enclosure 708 at least partially encloses the handle 702 attached to the first surface 710 in a first position. The first position is shown in each of the perspective view 706a, front view 706b, front view 706c, bottom view 706d, and side view 706e of the handle 702. The handle 702 allows access to the enclosed area. The curved enclosure 708 can include an inner surface 712 facing the first surface 710 in its first position. Further, the curved enclosure 708 can include an outer surface 714 opposite to the first surface 710 in the first position.

[0042] The aircraft disinfection device 700 can also include a set of UV LEDs 716 attached to the inner surface 712. The set of UV LEDs 716 can be configured to disinfect the handle 702. In some embodiments, the set of UV LEDs 716 can include at least one UV-C LED. Furthermore, the aircraft disinfection device 700 can include at least one switch disposed on at least one of the first surface 710 and the second surface (not shown in FIG. 7) of the containment area. Each of the at least one switch is turned on in the closed state of the containment area and turned off in the open state of the containment area. Furthermore, the aircraft disinfection device 700 can include at least one locking mechanism (not shown in FIG. 7). The at least one locking mechanism can be configured to engage with the first surface 710 in the closed state and be disengaged from the first surface 710 in the open state. Furthermore, the aircraft disinfection device 700 can include a controller communicatively connected to each of the sets of UV LEDs 716, at least one switch, and at least one locking mechanism. The controller can be configured to activate the sets of UV LEDs 716 when each of the at least one switch is turned on and the locking mechanism is in the closed state and engaged with the first surface 710.

[0043] The aircraft disinfection device 700 can be attached to the inner surface 712 of the curved enclosure 708 and can further include at least one sensor (not shown in FIG. 7) for generating a non-operation signal based on a predetermined criterion. As an example, the predetermined criterion can include detection of a user's body part. The controller can be communicatively connected to the at least one sensor. The controller can be configured to deactivate the sets of UV LEDs 716 based on the non-operation signal generated by the at least one sensor. In one embodiment, the sets of UV LEDs 716 can be attached to the first surface 710 and can be configured to disinfect the inner surface 712 of the curved enclosure 708. In other embodiments, the curved enclosure 708 can be configured to disinfect the handle 702 of the overhead storage bin 704. As will be apparent to those skilled in the art, the aircraft disinfection system 700 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 700 can also be applied to public use facilities, such as movie theaters and malls.

[0044] FIG. 8 is a series of explanatory diagrams illustrating an aircraft disinfection device 800 according to another embodiment for disinfecting a handle 802 of an overhead storage bin 804. The overhead storage bin 804 can have a configuration similar to the overhead storage bin 108 in the aircraft cabin 100. The series of explanatory diagrams showing the aircraft disinfection system 800 are a perspective view 806a, a side view 806b, and a side view 806c. The aircraft disinfection device 800 can include a curved enclosure 808 operatively coupled to a first surface 810 of the containment area (in this case, the overhead storage bin 804). The curved enclosure 808, in a first position, at least partially encloses the handle 802 attached to the first surface 810, which allows access to the containment area. In this exemplary embodiment, the curved enclosure 908 remains only in the first position. Its first position is shown in side view 806b. Further, the curved enclosure 808 can include an inner surface 812 facing the first surface 810 in its first position. The curved enclosure 808 can also include an outer surface 814 opposite to the first surface 810 in the first position.

[0045] The aircraft disinfection device 800 can include a set of UV LEDs 816 attached to the inner surface 812. The set of UV LEDs 816 can be configured to disinfect the handle 802. In some embodiments, the UV LEDs 816 can include at least one UV-C LED. The aircraft disinfection device 800 can also include at least one switch (not shown in FIG. 8) disposed on at least one of the first surface 810 and the second surface of the containment area. Each of the at least one switch is turned on in the closed state of the containment area and turned off in the open state of the containment area. The closed state is shown in side view 806b, and the open state is shown in side view 806c.

[0046] The aircraft disinfection device 800 can also include at least one locking mechanism (not shown in FIG. 8). The at least one locking mechanism can be configured to engage with the first surface 810 in a closed state and to be disengaged from the first surface 810 in an open state. The aircraft disinfection device 800 can include a controller communicatively connected to each of the sets of UV LEDs 816, at least one switch, and at least one locking mechanism. The controller can be configured to activate the set of UV LEDs 816 when each of the at least one switch is turned on and the locking mechanism is in the closed state and engaged with the first surface 810.

[0047] The aircraft disinfection device 800 can include a rotation mechanism 818 operatively coupled to the curved enclosure to move the curved enclosure 808 from the first position to at least one of the second position and at least one intermediate position. The rotation mechanism 818 is shown in each of side views 806b and 806c. The curved enclosure 808 fully exposes the handle 802 in the second position and partially exposes the handle 802 in each of the at least one intermediate position. In one embodiment, the first surface 810 of the containment region can include a slit 820 for enabling the curved enclosure 808 to move through the first surface 810 between the first position, the second position, and the at least one intermediate position. This slit 820 is shown in each of side views 806b and 806c. The controller can be communicatively connected to the rotation mechanism. The controller can be configured to give an instruction to the rotation mechanism 818 to move the curved enclosure 808 to the first position when each of the at least one switch is turned on and the locking mechanism is in the closed state and engaged with the first surface 810. Further, the controller can be configured to give an instruction to the rotation mechanism 818 to move the curved enclosure 808 to one of the second position and the at least one intermediate position when at least one of the at least one switch is turned off and the locking mechanism is disengaged from the first surface 810.

[0048] The aircraft disinfection device 800 can further include at least one sensor attached to the inner surface 812 of the curved enclosure 808 and can be configured to generate a non-operation signal based on a predetermined criterion. As an example, the predetermined criterion can include the detection of a user's body part. The controller can be communicatively connected to the at least one sensor. Further, the controller can be configured to deactivate the set of UV LEDs 816 based on the non-operation signal generated by the at least one sensor. As will be apparent to those skilled in the art, the aircraft disinfection system 800 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks, or any vehicle. The aircraft disinfection system 800 can also be applied to public use facilities, such as movie theaters and malls.

[0049] FIG. 9 is a series of explanatory diagrams illustrating a disinfection device 900 according to an embodiment for disinfecting a handle 902. The handle 902 can be attached to a door 904, and the door 904 can be used to open and close a closed area such as a lavatory (e.g., the lavatory 110 in the aircraft cabin 100), an exit, an emergency exit, a cockpit, a galley, etc. The series of explanatory diagrams showing the aircraft disinfection system 900 are a perspective view 906a, a front view 906b, a side view 906c, and a bottom view 906d. The aircraft disinfection device 900 can include a curved enclosure 908 operatively coupled to a first surface 910 of the containment area. The first surface 910 is shown in each of the perspective view 906a, the side view 906c, and the bottom view 906d. In the first position, the curved enclosure 908 at least partially encloses the handle 902 attached to the first surface 910. In this exemplary embodiment, the curved enclosure 908 remains only in the first position. The handle 902 allows access to the containment area. Further, the curved enclosure 908 can include an inner surface 912 facing the first surface 910 in its first position and an outer surface 914 opposite the first surface 910 in the first position.

[0050] The aircraft disinfection device 900 can further include a set of UV LEDs 916 attached to the inner surface 912. The set of UV LEDs 916 can be configured to disinfect the handle 902. The set of UV LEDs 916 can include at least one UV-C LED. The set of UV LEDs 916 is shown in the bottom view 906d. Further, the aircraft disinfection device 900 can include at least one switch (not shown in FIG. 9) disposed on at least one of the first surface 910 and the second surface of the containment area. Each of the at least one switch is turned on in the closed state of the containment area and turned off in the open state of the containment area. As an example, when the containment area is a toilet, the switch can be arranged such that it is turned on when the door of the washroom is closed and turned off when the door is opened.

[0051] The aircraft disinfection device 900 can further include at least one locking mechanism (not shown in FIG. 9). The at least one locking mechanism can be configured to engage with the first surface 910 in the closed state and be disengaged from the first surface 910 in the open state. As an example, when the containment area is a washroom, the locking mechanism can be constituted by a slide latch that can be slid in one horizontal direction to close the door and slid in the opposite horizontal direction to open the door. The aircraft disinfection device 900 can include a controller communicatively connected to each of the set of UV LEDs 916, at least one switch, and at least one locking mechanism. The controller can be configured to activate the set of UV LEDs 916 when each of the at least one switch is turned on and the locking mechanism engages with the first surface 910 in the closed state.

[0052] The aircraft disinfection device 900 may further include at least one sensor attached to the inner surface 912 of the curved enclosure 908 and be configured to generate a non-operating signal based on a predetermined criterion. As an example, the predetermined criterion may include detection of a user's body part. The controller can be communicatively connected to the at least one sensor. The controller can further be configured to deactivate the set of UV LEDs 916 based on the non-operating signal generated by the at least one sensor. As will be apparent to those skilled in the art, the aircraft disinfection system 900 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 900 can also be applied to public facilities such as movie theaters and malls.

[0053] FIG. 10 is a series of explanatory diagrams illustrating an aircraft disinfection device 1000 according to an embodiment for disinfecting a handle 1002. The handle 1002 can be attached to a door 1004. The door can be configured to open and close an enclosed area such as a lavatory (e.g., lavatory 110 in aircraft cabin 100), an exit, an emergency exit, a cockpit, a galley, etc. The series of explanatory diagrams showing the aircraft disinfection system 1000 are a perspective view 1006a, a side view 1006b, and a side view 1006c. The aircraft disinfection device 1000 can include a curved enclosure 1008 operatively coupled to a first surface 1010 of the enclosed area. The curved enclosure 808 can be configured to at least partially enclose the handle 1002 attached to the first surface 1010 in a first position, thereby allowing access to the enclosed area. The first position is shown in side view 1006b. The curved enclosure 1008 can include an inner surface 1012 facing the first surface 1010 at the first position of the curved enclosure 1008 and an outer surface 1014 facing away from the first surface 1010 at the first position.

[0054] The aircraft disinfection device 1000 can include a set of UV LEDs 1016 attached to the inner surface 1012. The set of UV LEDs 1016 can be configured to disinfect the handle 1002. The set of UV LEDs 1016 can include at least one UV-C LED. The inner surface 1012 and the set of UV LEDs 1016 are shown in each of side view 1006b and side view 1006c. The aircraft disinfection device 1000 can include at least one switch disposed on at least one of the first surface 1010 and the second surface of the containment area. Each of the at least one switch is turned on in the closed state of the containment area and turned off in the open state of the containment area. As an example, when the containment area is a lavatory, the switch can be arranged such that it is turned on when the lavatory door is closed and turned off when the door is opened. The closed state is shown in side view 1006b and the open state is shown in side view 1006c. The aircraft disinfection device 1000 can include at least one locking mechanism. The at least one locking mechanism can be configured to engage with the first surface 1010 in the closed state and be disengaged from the first surface 1010 in the open state. As an example, when the containment area is a washroom, the locking mechanism can be constituted by a slide latch that can be slid in one horizontal direction to close the door and slid in the opposite horizontal direction to open the door. Further, the aircraft disinfection device 1000 can include a controller (not shown in FIG. 10) that is communicatively connected to each of the set of UV LEDs 1016, at least one switch, and at least one locking mechanism. The controller can be configured to activate the set of UV LEDs 1016 when each of the at least one switch is turned on and the locking mechanism is in the closed state and engaged with the first surface 1010.

[0055] The aircraft disinfection device 1000 can further include a rotation mechanism 1018 operatively coupled to the curved enclosure 1008 for moving the curved enclosure housing 1008 from the first position to at least one of the second position and at least one intermediate position. The rotation mechanism 1018 is shown in each of side view 1006b and side view 1006c. The curved enclosure 1008 fully exposes the handle 1002 in the second position and partially exposes the handle 1002 in each of the at least one intermediate position. In one embodiment, the first surface 1010 of the containment region can include a slit 1020 that enables the curved enclosure 1008 to move through the first surface 1010 between the first position, the second position, and the at least one intermediate position. The slit 1020 is shown in each of side view 1006b and side view 1006c. The curved enclosure 1008 can be configured to be moved via the rotation mechanism 1018.

[0056] The controller can be communicatively connected to the rotation mechanism 1018 and can be configured to give an instruction to the rotation mechanism 1018 to move the curved enclosure 1008 to the first position when each of the at least one switch is turned on and the lock mechanism engages the first surface 1010 in the closed state. In contrast, the controller can be configured to give an instruction to the rotation mechanism 1010 to move the curved enclosure 1008 to one of the second position and the at least one intermediate position when at least one of the at least one switch is turned off and the lock mechanism is disengaged from the first surface 1010.

[0057] The aircraft disinfection device 1000 can include at least one sensor attached to the inner surface 1012 of the curved enclosure 1008, and can be configured to generate an inoperative signal based on a predetermined criterion. As an example, the predetermined criterion can include the detection of a user's body part. The controller can be communicatively connected to the at least one sensor. The controller can further be configured to deactivate the set of UV LEDs 1016 based on the inoperative signal generated by the at least one sensor. As will be apparent to those skilled in the art, the aircraft disinfection system 1000 is not limited to aircraft and can also be applied to trains, buses, passenger cars, trucks or any vehicle. The aircraft disinfection system 1000 can also be applied to public use facilities, such as movie theaters and malls.

[0058] As can be further understood by those skilled in the art, current disinfection systems lack a mechanism to effectively disinfect the surfaces of an aircraft on which passengers and crew are boarding. The technologies described above are for disinfecting the surfaces of an aircraft. In particular, the technologies described above are for disinfecting the surfaces of an aircraft via multiple sets of UV LEDs. According to the technologies described above, surfaces such as trays, door handles in the lavatory, or handles on overhead storage bins can be disinfected while passengers and crew are boarding. The technologies described above provide an effective means to prevent exposure of ultraviolet rays to the body parts of users. Surfaces such as the locking part of a seatbelt can be disinfected before and after a flight when passengers and crew are not boarding. The technologies described above provide an enclosure composed of a storage casing for storing the locking part of a seatbelt, a frame and pockets for storing trays, or a curved enclosure for covering a handle. Each set of UV LEDs is mounted inside such an enclosure. Further, the technologies described above use sensors to detect the presence of the body parts of users inside the enclosure. The sensors activate the UV LEDs in a closed or locked state of the surface to prevent exposure of UV light radiation to the body parts of users. The technologies described above can be applied to air ducts of the air conditioning system inside an aircraft, the inside of the lavatory, the inside of the aircraft cabin, handheld devices (e.g., in-flight entertainment controllers), etc.

[0059] This specification describes a disinfection system and apparatus for aircraft. The illustrated steps are set for explaining the illustrated exemplary embodiments, and according to the ongoing technological development, it is also assumed that the way a specific function is executed may be changed. These examples are not limiting and are presented in this specification for the purpose of explanation. Furthermore, the boundaries of functional components are defined for convenience in this specification for the sake of convenience. Alternative boundaries can be defined as long as the specified functions and their relationships are properly executed. Alternatives including equivalents, extensions, variations, departures, etc. of the matters described in this specification will be apparent to those skilled in the relevant technical field based on the teachings contained in this specification. Such alternatives are included within the scope and spirit of the disclosed embodiments.

[0060] Furthermore, in embodiments compatible with the present disclosure, one or more computer-readable storage media can be utilized. A computer-readable storage medium refers to any form of physical memory capable of storing information or data readable by a processor. Thus, a computer-readable storage medium can store instructions for execution by one or more processors, and the instructions include instructions for causing the processor to execute steps or stages consistent with the embodiments described in this specification. The term "computer-readable medium" should be understood to include tangible substances and exclude carrier waves and transient signals, that is, non-transient ones. Examples include random access memory (RAM), read-only memory (ROM), volatile memory, non-volatile memory, hard drives, CD ROMs, DVDs, flash drives, disks, and other known physical storage media.

[0061] The present disclosure and examples should be considered as illustrative only, and the true scope and spirit of the disclosed embodiments are defined based on the following claims.

Claims

1. An aircraft disinfection system comprising: a safety belt having a first portion attached to a first fabric portion thereof and a second portion attached to a second fabric portion of the safety belt, the first fabric portion being configured to receive the second portion and fasten the safety belt; a first storage casing for completely enclosing the first portion, the first storage casing comprising: a first inner wall for enclosing an outer surface of the first portion; a first set of ultraviolet (UV) light emitting diodes (LEDs) attached to the first inner wall for disinfecting the outer surface of the first portion; a plate-like member having one end fixed to the first inner wall and the other end disposed inside the first storage casing away from the first inner wall, the plate-like member being configured to lift a flap of the first portion when the first portion of the safety belt is completely enclosed inside the first storage casing in cooperation with the first portion of the safety belt; a second set of UV LEDs attached to a surface of the tong for disinfecting an inner surface of the first portion, and further comprising: a second storage casing for enclosing the second portion, the second storage casing comprising: a second inner wall for enclosing the second portion; a third set of UV LEDs attached to the second inner wall for disinfecting the second portion; An aircraft disinfection system

2. The aircraft disinfection system according to claim 1, wherein: the first storage casing further comprises a first slit configured to receive the first fabric portion, the first slit comprising: a first pair of rollers cooperating with the first fabric portion, the first pair of rollers enabling the first portion to be enclosed by sliding the first storage casing over the first fabric portion, the first fabric portion being configured to pass through the first storage casing via the first slit; and further, the second storage casing further comprises a second slit configured to receive the second fabric portion, the second slit comprising: a second pair of rollers cooperating with the second fabric portion, the second pair of rollers enabling the second portion to be enclosed by sliding the second storage casing over the second fabric portion, the second fabric portion being configured to pass through the second storage casing via the second slit.

3. The aircraft disinfection system according to claim 2, wherein; The first storage casing further includes a first electric mechanism coupled to a first pair of rollers, and the first electric mechanism is configured to slide the first storage casing on the first fabric portion by operating the first pair of rollers; furthermore, the second storage casing further includes a second electric mechanism coupled to a second pair of rollers, and the second electric mechanism is configured to slide the second storage casing on the second fabric portion by operating the second pair of rollers, an aircraft disinfection system.

4. The aircraft disinfection system according to claim 3, further comprising: a first set of sensors disposed within the first storage casing, the first set of sensors being configured to determine a complete containment of the first portion by the first storage casing; a second set of sensors disposed within the second storage casing, the second set of sensors being configured to determine a complete containment of the second portion by the second storage casing; a controller communicatively connected to each of the first set of UV LEDs, the second set of UV LEDs, the third set of UV LEDs, the first set of sensors, the second set of sensors, the first electric mechanism, and the second electric mechanism, the controller: gives an instruction to the first electric mechanism in response to a disinfection execution signal to slide on the first fabric portion, thereby enclosing the first storage casing; gives an instruction to the second electric mechanism in response to the disinfection execution signal to slide on the second fabric portion, thereby enclosing the second storage casing; activates the first set of UV LEDs and the second set of UV LEDs respectively in response to the first set of sensors determining a complete containment of the first portion by the first storage casing; furthermore, an aircraft disinfection system configured to activate the third set of UV LEDs in response to the second set of sensors determining a complete containment of the second portion by the second storage casing.

5. The aircraft disinfection system according to claim 4, wherein the controller: gives an instruction to the first electric mechanism after a predetermined period has elapsed to slide the first storage casing on the first fabric portion, thereby exposing the first portion; furthermore, An aircraft disinfection system configured to give an instruction to the second electric mechanism to slide the second storage casing on the second cloth portion after the expiration of the predetermined period, thereby exposing the second portion.

6. The aircraft disinfection system according to claim 4, wherein the controller: in response to the first set of sensors determining that the first portion is only partially enclosed by the first storage casing, turns off each of the first set of UV LEDs and the second set of UV LEDs; and further, an aircraft disinfection system configured to turn off the third set of UV LEDs in response to the second set of sensors determining that the second portion is only partially enclosed by the second storage casing.

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