Passenger assistance device for passenger service unit

Abstract

An aircraft cabin passenger service assembly is disclosed that includes a passenger service assembly panel having a handle deployable from a stowed configuration, the handle configured to facilitate and increase maneuverability and stability of passengers in and out of passenger seats.

Description

Technical Field

[0001] The present disclosure generally relates to the field of aircraft cabin environment reservation. More specifically, the present disclosure relates to the field of passenger assistance devices located in the aircraft cabin environment. Background Art

[0002] Aircraft passenger seats in a passenger aircraft typically may include passenger seats, which may further include window seats adjacent to the outer wall of the passenger aircraft, aisle seats positioned adjacent to the aircraft cabin aisle, and center seats positioned between the window seats and the aisle seats. In a typical aircraft configuration, aisle seats generally provide the greatest convenience in terms of a passenger leaving and entering an aisle seat. For example, the proximity of the aisle seat to the aisle and the proximity of the aisle seat to the outer edge of the overhead bin above the aisle seat may provide such aisle seat passenger options in the form of an aircraft cabin adjacency structure that supports and / or assists an aisle seat passenger during the aisle seat passenger's entry into and exit from the aisle seat and otherwise facilitates the passenger's removal from and entry into the aisle passenger seat.

[0003] Center passenger seats and window passenger seats are generally located outside the convenient reach of any reliable structure that can assist a window seat passenger and a center seat passenger during entry into and exit from the window seat and the center seat without, for example, interfering with or relying on the seat directly in front of the window seat and / or center seat passenger.

[0004] Unless expressly so identified, nothing in this specification is admitted to be prior art merely by virtue of its inclusion in the technical field and / or background section. Summary of the Invention

[0005] This aspect relates to an aircraft cabin passenger service unit (hereinafter equivalently referred to as "PSU") slot cover assembly, which includes at least one cabin passenger service unit slot cover assembly panel in the passenger service unit slot cover assembly of an aircraft cabin, wherein the passenger service unit slot cover assembly is positioned outside the outer end of the overhead bin of the overhead bin, and wherein the passenger service unit slot cover assembly is further positioned inside the outer wall of the aircraft cabin. At least one cabin passenger service unit slot cover assembly panel includes an outer surface of the cabin passenger service unit slot cover assembly panel facing the aircraft cabin, and the outer surface of at least one cabin passenger service unit slot cover assembly panel includes a panel recessed area (hereinafter equivalently referred to as "recessed area" and "panel recess"), wherein the panel recessed area is at least partially defined by a panel recessed area bottom plate and a panel recessed area wall, wherein the size of the panel recessed area is formed to accommodate the handle of the cabin passenger service unit slot cover assembly panel in the handle retracted configuration of the cabin passenger service unit slot cover assembly panel, and wherein the passenger service unit slot cover assembly is configured to separate the passenger service unit slot from the aircraft cabin.

[0006] In another aspect, the cabin passenger service unit slot cover assembly further includes a plurality of cabin passenger service unit slot cover assembly panels.

[0007] In another aspect, the aircraft cabin passenger service unit slot cover assembly further includes at least one of a lighting panel, a passenger information panel, a spacer panel, an oxygen release panel, an air conditioning / blower vent, and a speaker panel.

[0008] In another aspect, the aircraft cabin passenger service unit slot cover assembly is a monolithic assembly.

[0009] In yet another aspect, the cabin passenger service unit slot cover assembly panel handle is configured to assist a passenger in performing at least one of entering and exiting a passenger seat.

[0010] In another aspect, the plurality of cabin passenger service unit slot cover assembly panels are discrete panels.

[0011] Another aspect relates to an aircraft cabin that includes an aircraft cabin passenger service unit slot cover assembly. The aircraft cabin passenger service unit slot cover assembly includes at least one cabin passenger service unit slot cover assembly panel of the passenger service unit slot cover assembly panels of the aircraft cabin. The passenger service unit slot cover assembly is positioned outside the outer end of an overhead bin of the overhead bin and further positioned inside the outer wall of the aircraft cabin. At least one cabin passenger service unit slot cover assembly panel includes an outer surface of the cabin passenger service unit slot cover assembly panel facing the aircraft cabin. The outer surface of at least one cabin passenger service unit slot cover assembly panel includes a panel recessed area. The panel recessed area is at least partially defined by a panel recessed area bottom plate and a panel recessed area wall. The panel recessed area is sized to accommodate the cabin passenger service unit slot cover assembly panel handle in a stowed configuration of the cabin passenger service unit slot cover assembly panel handle. The passenger service unit slot cover assembly is configured to separate the passenger service unit slot from the aircraft cabin.

[0012] On the other hand, it relates to an aircraft, which includes an aircraft cabin passenger service unit slot cover assembly. The aircraft cabin passenger service unit slot cover assembly includes at least one cabin passenger service unit slot cover assembly panel in the passenger service unit slot cover assembly panel of the aircraft cabin. The passenger service unit slot cover assembly is positioned outside the outer end of the overhead bin of the overhead bin, and the passenger service unit slot cover assembly is further positioned inside the outer wall of the aircraft cabin. At least one cabin passenger service unit slot cover assembly panel includes an outer surface of the cabin passenger service unit slot cover assembly panel facing the aircraft cabin. Among them, the outer surface of at least one cabin passenger service unit slot cover assembly panel includes a panel recessed area, which is at least partially defined by a panel recessed area bottom plate and a panel recessed area wall. The size of the panel recessed area is formed to accommodate the handle of the cabin passenger service unit slot cover assembly panel in the handle retracted configuration of the cabin passenger service unit slot cover assembly panel, and the passenger service unit slot cover assembly is configured to separate the passenger service unit slot from the aircraft cabin.

[0013] On the other hand, it relates to a panel of an aircraft cabin passenger service unit slot cover assembly. The panel of the aircraft cabin passenger service unit slot cover assembly includes an outer surface of the passenger service unit slot cover assembly panel. The outer surface of the passenger service unit slot cover assembly panel includes a recessed area, and the size of the recessed area is formed to accommodate the handle of the passenger service unit slot cover assembly panel in the handle retracted configuration of the passenger service unit slot cover assembly panel.

[0014] In another aspect, the panel of the aircraft cabin passenger service unit slot cover assembly is located inside the passenger service unit slot cover assembly of the aircraft cabin. The passenger service unit slot cover assembly is positioned outside the inner end of the overhead bin of the overhead bin, and the passenger service unit slot cover assembly is further positioned inside the outer wall of the aircraft cabin.

[0015] In another aspect, the handle of the passenger service unit slot cover assembly panel communicates with a signaling element, and the signaling element is configured to convey the state of the handle of the passenger service unit slot cover assembly panel to a display.

[0016] In another aspect, the outer surface of the passenger service unit slot cover assembly panel is illuminated.

[0017] In another aspect, the outer surface of the passenger service unit slot cover assembly panel further contains a luminescent material.

[0018] In another aspect, the outer surface of the passenger service unit slot cover assembly panel further contains a fluorescent material.

[0019] In another aspect, the outer surface of the passenger service unit slot cover assembly panel further contains a photoluminescent material.

[0020] In yet another aspect, the aircraft cabin passenger service unit slot cover assembly panel further includes an inner surface of the aircraft cabin passenger service unit slot cover assembly panel positioned adjacent to the support element of the aircraft cabin passenger service unit slot cover assembly panel, wherein the support element of the aircraft cabin passenger service unit slot cover assembly panel is configured to engage at least one of the handle of the aircraft cabin passenger service unit slot cover assembly panel and the inner surface of the aircraft cabin passenger service unit slot cover assembly panel.

[0021] In another aspect, at least one support element of the aircraft cabin passenger service unit slot cover assembly panel is further configured to support the weight applied to the handle of the aircraft cabin passenger service unit slot cover assembly panel.

[0022] In another aspect, at least one support element of the aircraft cabin passenger service unit slot cover assembly panel is further configured to support a weight in the range of about 350 pounds to about 500 pounds applied to the handle of the aircraft cabin passenger service unit slot cover assembly panel.

[0023] In another aspect, the aircraft cabin passenger service unit slot cover assembly panel is configured to engage at least one support element of the aircraft cabin passenger service unit slot cover assembly.

[0024] Yet another aspect relates to an aircraft cabin that includes an aircraft cabin passenger service unit slot cover assembly panel. The aircraft cabin passenger service unit slot cover assembly panel includes an outer surface of the aircraft cabin passenger service unit slot cover assembly panel. The outer surface of the aircraft cabin passenger service unit slot cover assembly panel includes a panel recessed area, wherein the panel recessed area is configured to accommodate the handle of the aircraft cabin passenger service unit slot cover assembly panel in a stowed configuration of the handle of the aircraft cabin passenger service unit slot cover assembly panel.

[0025] Another aspect relates to an aircraft that includes an aircraft cabin passenger service unit slot cover assembly panel. The aircraft cabin passenger service unit slot cover assembly panel includes an outer surface of the aircraft cabin passenger service unit slot cover assembly panel. The outer surface of the aircraft cabin passenger service unit slot cover assembly panel includes a recessed area, wherein the recessed area is configured to be sized to accommodate the handle of the aircraft cabin passenger service unit slot cover assembly panel in a stowed configuration of the handle of the aircraft cabin passenger service unit slot cover assembly panel.

[0026] In another aspect, the structural support element of the aircraft cabin passenger service unit slot cover assembly is at least one of an AC rail (airconditioning rail) and a passenger service unit rail.

[0027] In another aspect, the aircraft cabin passenger service unit slot cover assembly panel is configured to engage the AC rail, and the aircraft cabin passenger service unit slot cover assembly panel is further configured to also engage the passenger service unit rail.

[0028] In yet another aspect, the structural support element of the aircraft cabin passenger service unit slot cover assembly is configured to support the aircraft cabin passenger service unit slot cover assembly.

[0029] On the other hand, it relates to a method for modifying a passenger service unit slot cover assembly in an aircraft cabin, the method comprising: positioning a passenger service unit slot cover assembly panel in the passenger service unit slot cover assembly in the aircraft cabin; wherein the passenger service unit slot cover assembly is positioned outside the outer end of the overhead bin in the overhead bin of the aircraft cabin, wherein the passenger service unit slot cover assembly is further positioned inside the outer wall of the aircraft cabin, wherein the passenger service unit slot cover assembly panel includes an outer surface of the passenger service unit slot cover assembly panel facing the aircraft cabin, wherein the outer surface of the passenger service unit slot cover assembly panel includes a panel recessed area, wherein the panel recessed area is at least partially defined by a panel recessed area bottom plate and a panel recessed area wall, and wherein the panel recessed area is sized to accommodate a passenger service unit slot cover assembly panel handle in a passenger service unit slot cover assembly panel handle retracted configuration.

[0030] In yet another aspect, the method for modifying a passenger service unit slot cover assembly in an aircraft cabin further comprises engaging the passenger service unit slot cover assembly panel with at least one passenger service unit slot cover assembly structural support element, wherein the at least one passenger service unit slot cover assembly structural support element is configured to support the passenger service unit slot cover assembly panel, and wherein the passenger service unit slot cover assembly structural support element is further configured to support the weight applied to the passenger service unit slot cover assembly panel handle.

[0031] On the other hand, it relates to a method for assisting / stabilizing a passenger to enter and leave an aircraft passenger seat assembly, the method comprising deploying a passenger service unit slot cover assembly panel handle from the passenger service unit slot cover assembly panel, wherein the passenger service unit slot cover assembly panel handle is deployed from a passenger service unit slot cover assembly panel handle retracted configuration to a passenger service unit slot cover assembly panel handle deployed configuration.

[0032] In another aspect, the passenger service unit slot cover assembly panel is positioned in the aircraft cabin at a location outside the outer end of the overhead bin in the overhead bin and further at a location inside the outer wall of the aircraft cabin, wherein the passenger service unit slot cover assembly panel includes an outer surface of the passenger service unit slot cover assembly panel facing the aircraft cabin, the outer surface of the passenger service unit slot cover assembly panel includes a panel recessed area, and wherein the panel recessed area is sized to accommodate a passenger service unit slot cover assembly panel handle in a passenger service unit slot cover assembly panel handle retracted configuration.

[0033] In another aspect, a method further comprises: engaging the passenger service unit slot cover assembly panel handle with the weight load of the passenger during at least one of the passenger entering the passenger seat assembly and the passenger leaving the passenger seat assembly; and stabilizing the passenger during at least one of the passenger entering the passenger seat assembly and the passenger leaving the passenger seat assembly.

[0034] On the other hand, the present invention relates to an overhead passenger seat access stabilizer for an aircraft cabin, which includes an overhead panel located in the aircraft cabin and at the aircraft passenger position, wherein the overhead passenger seat access stabilizer for the aircraft cabin is positioned outside the outer end of the luggage compartment, wherein the overhead passenger seat access stabilizer for the aircraft cabin is further positioned inside the outer wall of the aircraft cabin, wherein the overhead panel includes an outer surface of the overhead panel facing the aircraft cabin, wherein the outer surface of the overhead panel includes a panel recessed area, wherein the panel recessed area is at least partially defined by a panel recessed area bottom plate and a panel recessed area wall, and wherein the panel recessed area is sized to accommodate an overhead panel handle in an overhead panel handle stowed configuration. The overhead panel handle of the overhead passenger seat access stabilizer for the aircraft cabin is configured to at least support and / or stabilize a passenger during entry and exit from the passenger seat.

[0035] On the other hand, it relates to an aircraft including an overhead passenger seat access stabilizer for an aircraft cabin.

[0036] The features, functions, and advantages that have been discussed can be implemented independently in various aspects or can be combined in other aspects, and further details thereof can be seen with reference to the following description and drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] Therefore, variations of the present disclosure have been generally described, and now reference will be made to the drawings, which are not necessarily drawn to scale, and in which:

[0038] Figure 1 is an illustration of a vehicle in the form of an aircraft according to this aspect;

[0039] Figure 2A is an illustration of a partial cross-sectional rear view as viewed from inside the aircraft cabin of a vehicle of the type shown according to this aspect; Figure 1 is an illustration of a partial cross-sectional front view as viewed from inside the aircraft cabin of a vehicle of the type shown according to this aspect;

[0040] Figure 2B is an illustration of a partial cross-sectional front view as viewed from inside the aircraft cabin of a vehicle of the type shown according to this aspect; Figure 1 is an illustration of a partial cross-sectional front view as viewed from inside the aircraft cabin of a vehicle of the type shown according to this aspect;

[0041] Figure 3 is an illustration of a partial cross-sectional front view as viewed from inside the aircraft cabin of a vehicle of the type shown according to this aspect; Figure 1 is a further illustration of a partial cross-sectional front view as viewed from inside the aircraft cabin of a vehicle of the type shown according to this aspect;

[0042] Figure 4 is an illustration of an outer perspective view as viewed from the aisle inside the aircraft cabin of a vehicle of the type shown according to this aspect; Figure 1 is an illustration of an outer perspective view as viewed from the aisle inside the aircraft cabin of a vehicle of the type shown according to this aspect;

[0043] Figure 5 is a partial perspective view of a PSU slot cover assembly inside the aircraft cabin according to this aspect;

[0044] Figure 6 is a partial exposed view of the interior of an aircraft cabin, further showing an exposed view of an aircraft cabin PSU slot and a PSU slot cover assembly according to this aspect;

[0045] Figure 7 is an enlarged partial exposed view of the interior of an aircraft cabin, further showing an exposed view of an aircraft cabin PSU slot and a PSU slot cover assembly that can be of the type shown in Figure 6 ;

[0046] Figure 8A is an enlarged plan view of a PSU slot cover assembly panel according to this aspect including an integral handle in an extended orientation;

[0047] Figure 8B is an enlarged plan view of a PSU slot cover assembly panel according to this aspect including an integral handle in a retracted orientation within a recess of the integral PSU slot cover assembly panel;

[0048] Figure 8C is an enlarged perspective view of a PSU slot cover assembly panel according to this aspect including an integral handle in a retracted orientation within a recess of the integral PSU slot cover assembly panel;

[0049] Figure 9 is an enlarged perspective view of a PSU slot cover assembly panel according to this aspect including an integral handle in an extended orientation within a recess of the integral PSU slot cover assembly panel;

[0050] Figure 10 is a cross-sectional side view of a PSU slot cover assembly panel according to this aspect including an integral handle in an extended orientation within a recess of the PSU slot cover assembly panel;

[0051] Figure 11 is an internal perspective view of a PSU slot cover assembly panel according to this aspect including a PSU slot cover assembly panel support element fastened to the PSU slot cover assembly panel;

[0052] Figure 12 is a flowchart outlining a method according to this aspect; and

[0053] Figure 13 is a flowchart outlining a method according to this aspect. Detailed Description

[0054] Entering (equivalently referred to herein as "accessing") and exiting (equivalently referred to herein as "departing") an aircraft passenger seat can require a great deal of independent physical flexibility, especially for a person sitting in a window seat and / or a center seat of an aircraft passenger seat assembly. In addition, the time required for an aircraft passenger to access a seat in the aircraft and the time required for a passenger to deplane from the aircraft can result in significant lost time (e.g., including delayed takeoff times and ground turn-around times, etc.), which can cause or otherwise result in cumulative significant delays, increased aviation costs, and increased passenger inconvenience.

[0055] In addition, passengers who can be considered persons with reduced mobility (equivalently referred to as "PRMs") and / or passengers with diminished physical strength and / or physical ability may find it difficult to independently maneuver into and out of a window seat and / or a center seat because there is typically nothing for such a passenger to "grab" to provide seating and "un-seating" assistance and stability.

[0056] This aspect relates to the arrangement of passenger assistance and stabilization devices in the vicinity of and within reach of a passenger seated and / or to be seated in a window seat and / or a center seat of a passenger cabin of a commercial aircraft. For example, the present device can significantly increase passenger independence, passenger stability, and passenger mobility in entering and exiting center and window aircraft passenger seats, which mobility would not be possible without significant additional passenger assistance from, for example, aircraft personnel, other passengers, etc. That is, according to the present aspect, significantly increased passenger self-help and self-stabilization (e.g., assistance and stability achieved under the "own strength" and / or physical exertion of the passenger, etc.) is conveniently and reliably provided to a passenger, which passenger includes passengers seated in window passenger seats and center passenger seats.

[0057] Figure 1 is a perspective view of a vehicle in the form of an aircraft 10, the aircraft 10 including a fuselage 12 and an aircraft passenger cabin 14 located within an aircraft passenger wall capable of communicating with the fuselage.

[0058] Figure 2A is a rearward view looking into the aircraft passenger cabin 14 (equivalently referred to herein as "cabin 14") of the aircraft 10, wherein the aircraft passenger cabin outer wall 18 is located on the inner side within the fuselage 12 and otherwise communicates with the fuselage. As Figure 2A shown, the illustrated seat assembly 16 is a three-seat assembly having an aisle seat 16a adjacent to an aisle 17, a window seat 16c adjacent to the aircraft passenger cabin outer wall 18, and a center seat 16b positioned between the aisle seat and the window seat (16a and 16c, respectively). Each seat in the passenger seat assembly 16 also includes a seat headrest 16d.

[0059] As Figure 2AFurther shown, the overhead bin 20 is positioned in the aircraft cabin, typically above one or more of the aisle passenger seats and the center passenger seats, where the overhead bin has an inner end 20a of the overhead bin (which can be opened and accessed by a passenger, for example, standing in the aisle 17) and an outer end 20b of the overhead bin, and the outer end 20b of the overhead bin can typically be suspended above, for example, the center seat.

[0060] The area on the inner side of the outer side of the outer end 20b of the overhead bin and the inner side of the fuselage interior (and the inner side of the outer wall that can communicate with the fuselage) is generally referred to as the passenger service unit (PSU) slot 40, and the passenger service unit slot can extend longitudinally along the length of the passenger aircraft cabin and can be at least partially defined by the outer end 20b of the overhead bin, the fuselage 12, or the outer wall 18 of the aircraft cabin, and the PSU slot cover assembly 30. The PSU slot 40 is an area inside the aircraft that can accommodate and otherwise include various devices, components, component parts, etc., and can include, for example, electrical auxiliary components and component parts, and the component parts can further include, for example, speaker assemblies, lighting assemblies, illuminated passenger information / warning indicator assemblies, passenger assistance call assemblies, vent assemblies, air conditioners, etc. The PSU slot can also include oxygen delivery components, oxygen tanks, fire extinguishing delivery devices, etc.

[0061] The PSU slot cover assembly 30 can be modified to allow visual and tactile access by passengers located near a specific area (usually below the specific area) of the slot cover assembly. The PSU slot cover assembly can include a plurality of separate PSU slot cover assembly panels that can form the PSU slot cover assembly 30 when in contact with each other and / or when attached together (including, for example, fixedly attached together). Various PSU slot cover assembly panels can be dedicated panels that can be selected and dedicated to delivering selected passenger target functions and / or comfort (including, for example, visual signaling, sound / verbal information / music, oxygen delivery, air circulation delivery, air conditioning delivery, crew assistance notification, etc.).

[0062] For example, the position of one or more PSU components within the PSU slot can coexist with a PSU slot cover assembly of the type of PSU slot cover assembly panel located proximally. The PSU panel can include, for example: 1) an opening for facilitating the passage of sound from a proximally located sound speaker; 2) an opening in the form of a ventilation opening that communicates with an air delivery component, for example, a "blower" including a blower for delivering conditioned air and recirculated air; 3) a lens for facilitating the passage of light when the indicator is powered; 4) a lens for facilitating illumination for reading and / or cabin lighting; 4) oxygen delivery for delivering oxygen in cases where auxiliary oxygen is required in the cabin environment; and other modifications, etc.

[0063] In addition, in the case where there are no functional components along and at the position within the PSU slot, a "spacer" PSU panel can be incorporated into the PSU slot cover assembly. In addition to providing continuity, structural consistency, etc. to the PSU slot cover assembly and overall aesthetic design and / or overall cabin environment, such a "spacer" panel generally performs or does not facilitate auxiliary functions.

[0064] This aspect relates to specialized modifications and increased functionality of the PSU slot cover assembly panel, which can be a PSU spacer panel for increasing passenger independence and the comfort and mobility of entering and exiting the passenger seat. According to this aspect, the PSU slot cover assembly panel is incorporated with a handle, which can be a retractable handle that is accommodated within a recess of the PSU slot cover assembly panel when in a stowed configuration. According to this aspect, the PSU slot cover assembly panel is incorporated with a retractable handle that is capable of moving from the stowed configuration to a deployed configuration that can be "grasped" and / or otherwise engaged by a passenger. The PSU slot cover assembly panel handle can be a load-bearing handle and assembly configured to support a downward force, such as in the form of a passenger weight in the range of approximately 250 pounds to approximately 350 pounds or greater. In another example, the PSU slot cover assembly panel handle can be a load-bearing handle and assembly configured to support a downward force in the form of a passenger weight in the range of, for example, from about 350 pounds to about 500 pounds.

[0065] Returning to the drawings, Figure 2A A cross-sectional end view of a PSU slot cover assembly 30 is shown, having an outer surface 30a of the PSU slot cover assembly facing the cabin 14 and an inner surface 30b of the PSU slot cover assembly facing the PSU slot 40. Figure 2A A cross-sectional end view of a PSU slot cover assembly panel 31 is also shown, having an outer surface 31a of the PSU slot cover assembly panel facing the cabin 14 and an inner surface 31b of the PSU slot cover assembly panel facing the PSU slot 40. The PSU slot cover assembly panel 31 further includes a PSU slot cover assembly panel recess 32 (equally referred to herein as "panel recess 32"), the dimensions of the PSU slot cover assembly panel recess being configured to accommodate the PSU slot cover assembly panel handle 34 in a stowed configuration within the PSU slot cover assembly panel recess 32 (equally referred to herein as "recess 32" and "recessed area 32").

[0066] As Figure 2A shown, when the PSU slot cover assembly panel handle 34 moves from the stowed configuration within the panel recess 32 towards the deployed configuration ( Figure 2AWhen moving as shown), the handle 34 of the PSU slot cover assembly panel can pivot about a handle attachment point (which can attach the handle to at least one of the panel and / or the panel support element, and the panel and / or the panel support element can be adjacent to and / or otherwise communicate with the inner surface 31b of the PSU slot cover assembly panel), where the handle 34 extends downward from the panel recess 32 and into the aircraft cabin and extends toward the passenger seat assembly 16. According to this aspect, the PSU slot cover assembly 30 is held in an elevated position in the aircraft cabin and can be suspended from and otherwise communicate with and / or fixedly attached to the PSU slot cover assembly support 22, and the PSU slot cover assembly support 22 can be an air conditioning push-out rail (equivalently referred to herein as the "AC rail" 24) that can extend longitudinally along and within the PSU slot 40. The PSU slot cover assembly 30 can further be held in an elevated position in the aircraft cabin and can be suspended from and otherwise communicate with and / or fixedly attached to the PSU slot cover assembly support 22, and the PSU slot cover assembly support 22 can be the PSU rail 26 adjacent to the outer end 20b of the overhead bin and can also extend longitudinally along and within the PSU slot 40.

[0067] Figure 2B is from Figure 1 and Figure 2A A forward view looking into the aircraft cabin 14 of an aircraft 10 of the type shown, where the outer wall 18 of the aircraft cabin is located on the inner side of the interior of the fuselage 12 and otherwise communicates with the fuselage. As Figure 2B shown, the seat assembly 16 shown is a three-seat assembly having an aisle seat 16a adjacent to the aisle 17, a window seat 16c adjacent to the outer wall 18 of the cabin, and a center seat 16b positioned between the aisle seat and the window seat (16a and 16c respectively). Each seat in the passenger seat assembly 16 also includes a seat headrest 16d.

[0068] As Figure 2B Further shown, the overhead bin 20 is typically positioned in the aircraft cabin 14 above one or more of the aisle passenger seats and the center passenger seats, where the overhead bin has an inner end 20a of the overhead bin (which can be opened and accessed by a passenger standing in the aisle 17 for example) and an outer end 20b of the overhead bin, and the outer end of the overhead bin can be typically suspended above the center seat for example. Figure 2B Also shown are the AC rail 24 and the PSU rail 26 of the type of the PSU slot cover assembly support element 22, and the PSU slot cover assembly support element is configured to support and suspend the PSU slot cover assembly 30 in place within the aircraft cabin 14.

[0069] Similar to Figure 2B , Figure 3 is another view looking forward from within the aircraft cabin 14 of the aircraft 10, where the outer wall 18 of the aircraft cabin is located on the inner side inside the fuselage 12 and otherwise communicates with the fuselage. As Figure 3 shown, the deployable oxygen assembly 28a is positioned in the region within the PSU slot 40 and further positioned adjacent to the PSU slot cover assembly 30, where the oxygen assembly 28a represents any assembly that can occupy the PSU slot 40 and is configured to be placed adjacent to or integral with the PSU slot cover assembly panel 30 and deliver services, comfort, and / or information, etc. to passengers, including, for example, vision signaling, sound / spoken information / music, oxygen delivery, air circulation delivery, air conditioning delivery, crew assistance notification, etc., as described herein.

[0070] Figure 4 is from Figure 1 , Figure 2A , Figure 2B , Figure 3 an outer view observed from within the aircraft cabin 14 of an aircraft 10 of the type shown in Figure 4 (e.g., an inner position observable from the aisle 17). Figure 4 shows the cabin outer wall 18, the seat assembly 16, and the aircraft cabin window 19. Figure 4 also shows the PSU slot cover assembly outer surface 30a of the PSU slot cover assembly 30 and the PSU slot cover assembly panel outer surfaces 31a of the various PSU slot cover assembly panels 31, which together form the PSU slot cover assembly 30. Figure 4 also shows the present dedicated and / or modified spacer panel in the form of the PSU slot cover assembly panel 31c, which also includes a panel recess 32 and a PSU slot cover assembly panel handle 34 extending downward from the panel recess 32, where the shown PSU slot cover assembly panel handle 34 is in a deployed configuration (e.g., extending downward from the panel recess 32 and partially "protruding" visible from the panel recess 32).

[0071] Figure 5 is a partial front view of the aircraft cabin 14 of the aircraft 10, where Figure 5 shows the seat assembly 16, where the window seat 16c is positioned adjacent to the cabin outer wall 18, the window seat 16c and the center seat 16b are substantially positioned below the PSU slot cover assembly panel 31c, and the position of the PSU slot cover assembly panel 31c is positioned within reach of a passenger who may occupy the seats 16c, 16b. As Figure 5As shown, the PSU slot cover assembly panel 31c includes a panel recess 32 and a PSU slot cover assembly panel handle 34 that extends downwardly from the panel recess 32, and the PSU slot cover assembly panel handle 34 is shown in a deployed configuration (e.g., extending downwardly from the panel recess 32 and partially "protruding" visible from the panel recess 32).

[0072] Figure 6 and Figure 7 are partial exposed views from above the PSU slot 40 of the aircraft 10 and into the PSU slot 40 of the aircraft 10. Figure 6 A partial view of the aircraft cabin 14 is shown as viewed from the outside of the aircraft 10, where the fuselage section has been removed to expose the aircraft cabin outer wall 18 and the aircraft cabin window 19. The aircraft crown ( Figure 6 not shown in the figure) has also been removed to expose the PSU slot 40, where the inner surface 30b of the PSU slot cover assembly of the PSU slot cover assembly 30 faces the PSU slot 40, and the inner surface 31b of the PSU slot cover assembly panel of the PSU slot cover assembly panel 31 faces the PSU slot 40. Figure 6 Also shown is the present special and / or modified spacer panel in the form of the PSU slot cover assembly panel 31c, which is a reverse view of the PSU slot cover assembly panel 31c compared to the Figure 4 view shown, and shows the inner surface 31b of the PSU slot cover assembly panel facing the PSU slot 40.

[0073] Figure 6 Also shown is a raised area 32a of the panel 31c facing the PSU slot 40, where the raised area 32a on the inner surface 31b of the PSU slot cover of the panel 31c corresponds to a recessed area or recessed areas 32 on the outer surface 31a of the PSU slot cover assembly panel of the PSU slot cover assembly panel 31c (facing into the aircraft cabin 14), the recessed area or recessed areas forming the panel recess 32 and sized and otherwise configured to receive the slot cover assembly panel handle 34, as described herein. As Figure 6 shown, the PSU slot cover assembly panel 31c can be strengthened to withstand a downward weight load that other PSU slot cover assembly panels 31 would not withstand.

[0074] As Figure 6As shown, the PSU slot cover assembly panel 31c is shown fixedly attached via fasteners 38 to a PSU slot cover assembly panel support element 35 that engages or is otherwise fixedly attached to a PSU slot cover assembly support element 22 (e.g., which may be in the form of an AC rail 24 and a PSU rail 26). As explained herein, in one example, the PSU slot cover assembly panel support element 35 provides a degree of support to the PSU slot cover assembly panel 31c to which the support element is attached. According to one example, the degree of support provided by the PSU slot cover assembly panel support element 35 to the panel 31c is configured to be able to withstand at least a downward bearing load (e.g., "passenger weight") in the range of about 350 lbs to about 500 lbs on the PSU slot cover assembly panel 31c.

[0075] Figure 7 is an exposed top view of the aircraft 10 and another part of the PSU slot 40 and the aircraft cabin 14 as viewed from the outside. In the aircraft 10, a fuselage section is removed to expose the aircraft cabin outer wall 18 and the aircraft cabin window 19, and a section of the aircraft crown is removed to expose the PSU slot 40, where the inner surface 30b of the PSU slot cover assembly 30 of the PSU slot cover assembly is exposed and faces the PSU slot 40 (and where the inner surface 31b of the PSU slot cover assembly panel 31 of the PSU slot cover assembly faces into the PSU slot 40). Further shown is the PSU slot cover assembly panel support element 35 fixedly attached via fasteners 38 to the slot cover assembly panel 31c, similar to Figure 6 that shown and described herein in the view. Figure 7 Also shown is a PSU assembly that may be positioned adjacent to or integrally formed with the PSU slot cover assembly and panel, where the PSU assembly is shown as a deployable oxygen assembly 28a, a lighting assembly 28b, a passenger notification assembly 28c, a speaker 28d, and may further include, for example, a vent (e.g., a ventilation vent). A blower vent assembly, not shown in the figure). Other PSU assemblies not specifically shown may include, for example, an air conditioner and / or a recirculation air blower and / or a vent, etc.

[0076] Figure 8A 、 Figure 8B 、 Figure 8C 、 Figure 9 、 Figure 10 and Figure 11 is an enlarged plan view of the PSU slot cover assembly panel 31c according to this aspect. As Figure 8AAs shown, the PSU slot cover assembly panel 31 is the PSU slot cover assembly panel 31c, which according to the PSU slot cover assembly panel of this aspect includes a PSU slot cover assembly panel recess 32 (equivalently referred to herein as "panel recess 32"), and the PSU slot cover assembly panel handle 34 (equivalently referred to herein as "panel handle 34") is shown pivotally engaged within the panel recess 32, and the panel handle 34 is shown in the deployed configuration where the panel handle 34 extends from the panel recess 32. The PSU slot cover assembly panel 31c further includes a PSU slot cover assembly panel outer surface 31a, which (when the panel is in place and integrally formed into the PSU slot cover assembly) faces the aircraft cabin as described herein.

[0077] As Figure 8A shown, and when in place within the PSU slot cover assembly, the PSU slot cover assembly panel 31c is configured to engage at least one PSU slot cover assembly support element 22, and the at least one PSU slot cover assembly support element can be at least one of an AC rail 24 and a PSU rail 26. In another example, the PSU slot cover assembly 30 and the PSU slot cover assembly panel 31 are configured to engage more than one PSU slot cover assembly support element 22 and can engage both the AC rail 24 and the PSU rail 26. Figure 8A The panel recess 32, which is at least partially defined by a panel recessed floor 33a and a panel recessed wall 33b, is further shown.

[0078] Figure 8B Shown as Figure 8A the features of the PSU slot cover assembly panel 31c as shown, where the PSU slot cover assembly panel handle 34 is in the stowed configuration, and where the PSU slot cover assembly panel handle 34 is configured to rest within the PSU slot cover assembly panel recess 32 and substantially adjacent to the panel recessed floor 33a, and where the PSU slot cover assembly panel handle 34 is in the stowed configuration within the panel recess 32, where the PSU slot cover assembly panel handle is configured to pivot rotatably from the deployed configuration ( Figure 8A shown in Figure 8B to the stowed configuration shown in

[0079] As Figure 8BAs shown, the PSU slot cover assembly panel handle 34 is configured to retract towards a stowed configuration and into the stowed configuration (e.g., from a deployed configuration), and can be in communication with a retaining and / or retracting mechanism to hold the PSU slot cover assembly panel handle in the stowed configuration. The retaining and / or retracting mechanism (not shown in the figures) can be, for example, a spring-loaded mechanism or other mechanism configured to deliver a force, which can be a reaction force or a "return force" that can resist a manual "downward" force applied to the handle by, for example, a passenger, and is required to move the PSU slot cover assembly panel handle out of the stowed configuration and towards and into the deployed configuration.

[0080] Figure 8C is a top view (from the "bottom side" or from "below") of the PSU slot cover assembly panel 31c, which can be a view of the position of the PSU slot cover assembly panel 31c in, for example, the PSU slot cover assembly 30. The PSU slot cover assembly is configured to "cover" or at least partially "define" the PSU slot 40 when the PSU slot cover assembly 30 and the component panel 31 (shown in Figure 8A 、 Figure 8B 、 Figure 8C as including the handle 34 and also referred to herein as the modified panel 31 of the PSU slot cover assembly panel 31c) are installed in place and supported in place. As shown in Figure 8A 、 Figure 8B and Figure 8C , the PSU slot cover assembly panel 31c is installed in place and supported in place, for example, by the PSU slot cover assembly support elements 22, which can be the AC rails 24 and the PSU rails 26. The AC rails and the PSU rails extend longitudinally and are otherwise longitudinally disposed within the PSU slot 40 along a selected length of the PSU slot.

[0081] As shown in Figure 8C , the PSU slot cover assembly panel handle 34 is in the stowed configuration, and the PSU slot cover assembly panel handle 34 is substantially completely held or "accommodated" within the PSU slot cover assembly panel recess 32. As shown at least in Figure 8B and Figure 8C , when the PSU slot cover assembly panel handle 34 is in the stowed configuration and is substantially completely held or "accommodated" within the PSU slot cover assembly panel recess 32, the PSU slot cover assembly panel handle 34 is configured not to extend beyond the plane of the PSU slot cover assembly panel outer surface 31a.

[0082] Figure 9 is an illustration of the PSU slot cover assembly panel 31c shown at least in Figure 8A 、 Figure 8B 、 Figure 8C , wherein Figure 9Shows a top view (from the "bottom side" or from "below") of the PSU slot cover assembly panel 31c, which can be a view of the position of the PSU slot cover assembly panel 31c in, for example, the PSU slot cover assembly 30. The PSU slot cover assembly is configured to "cover" or at least partially "define" the PSU slot 40 when the PSU slot cover assembly 30 and the assembly panel 31c are installed in place and supported, for example, by the PSU slot cover assembly support elements 22. The support elements can be the AC rail 24 and the PSU rail 26 that extend longitudinally within and along a selected length of the PSU slot 40. As Figure 9 shown, the PSU slot cover assembly panel handle 34 is in the deployed configuration, and the PSU slot cover assembly panel handle 34 is configured to extend a selected distance from the PSU slot cover assembly panel recess 32 and is configured to extend beyond the plane of the PSU slot cover assembly panel outer surface 31a (in the deployed configuration).

[0083] Figure 10 is an enlarged cross-sectional side view of the PSU slot cover assembly panel 31c having a PSU slot cover assembly panel outer surface 31a (e.g., facing the passenger compartment) and a PSU slot cover assembly panel inner surface 31b (e.g., facing the PSU slot). As Figure 10 shown, the PSU slot cover assembly panel support element 35 is communicatively connected or otherwise fixedly attached to the PSU slot cover assembly panel 31c, for example, by fasteners 38. The fasteners 38 and the PSU slot cover assembly panel support element 35 are configured to withstand a load bearing (e.g., "downward") gravity in the range from about 350 pounds to about 500 pounds, such as when such a downward force is applied to the PSU slot cover assembly panel handle 34 or otherwise applied. As Figure 10 shown, the PSU slot cover assembly panel support element 35 can be in the shape of an "I" beam that can extend across the width of the PSU slot cover assembly panel 31c and can be connected from one PSU slot cover assembly support element 22 (e.g., the "first" PSU slot cover assembly support element 22, which can be in the form of, for example, the AC rail 24, etc.) to another PSU slot cover assembly support element 22 (e.g., the "second" PSU slot cover assembly support element 22, which can be in the form of, for example, the PSU rail 26, etc.).

[0084] As Figure 10As shown, the PSU slot cover assembly panel 31c can be discretely supported by one or more PSU slot cover assembly support elements 22 or as part of the PSU slot cover assembly 30. The one or more PSU slot cover assembly support elements 22 can be the AC rail 24 and the PSU rail 26. The one or more PSU slot cover assembly support elements 22 are configured to extend longitudinally and otherwise be longitudinally disposed within the PSU slot 40 along a selected length of the PSU slot, and the one or more PSU slot cover assembly support elements 22 can communicate with additional aircraft support elements, such as various frame / support elements that are not necessarily shown in the figure. In this aspect, the PSU slot cover assembly panel support element 35 can be a discrete element fixedly attached to the PSU slot cover assembly panel 31c. In another example, the PSU slot cover assembly panel support element 35 can be integrally formed with the PSU slot cover assembly panel 31c such that the PSU slot cover assembly panel support element 35 and the PSU slot cover assembly panel 31c are a one-piece structure.

[0085] Figure 11 is a view of the PSU slot cover assembly panel 31c according to this aspect, for example, looking down into the PSU slot. Figure 11 The PSU slot cover assembly panel 31c having the inner surface 31b of the PSU slot cover assembly panel is shown, and the PSU slot cover assembly panel support element 35 communicates with and is otherwise fixedly attached to the PSU slot cover assembly panel 31c via, for example, fasteners 38, where the fasteners 38 and the PSU slot cover assembly panel support element 35 are configured to withstand a load bearing (e.g., "downward") gravity in the range of about 350 pounds to about 500 pounds, for example, when such a force is applied to the PSU slot cover assembly panel handle 34 or otherwise applied, such as when a passenger is moving into or out of a seat and the PSU slot cover assembly panel handle supports the body weight. According to this aspect, the weight load applied to the PSU slot cover assembly panel handle is configured to be at least partially transferred from the PSU slot cover assembly panel support element 35 to one or more of the PSU slot cover assembly support elements 22.

[0086] Figure 11 The PSU slot cover assembly panel 31c supported by one or more PSU slot cover assembly support elements 22 is also shown. The one or more PSU slot cover assembly support elements can be the AC rail 24 and the PSU rail 26. The one or more PSU slot cover assembly support elements 22 are configured to extend longitudinally and otherwise be longitudinally disposed within the PSU slot 40 along a selected length of the PSU slot, and the one or more PSU slot cover assembly support elements can communicate with additional aircraft support elements, such as various frame / support elements that are not necessarily shown in the figure. As Figure 10 and Figure 11As shown, the PSU slot cover assembly panel support element 35 is fixedly attached to and otherwise supported by one or more PSU slot cover assembly support elements 22, which may be the AC rail 24 and the PSU rail 26.

[0087] Figure 10 and Figure 11 An elevated area along the contour of the inner surface 31b of the PSU slot cover assembly panel is also shown. This elevated area is the recessed elevated area 32a of the PSU slot cover assembly panel, which corresponds to the opposite or inner side (e.g., the inner surface) of the PSU slot cover assembly panel recess 32 present on the outer surface 31a of the PSU slot cover assembly panel (e.g., at least as Figure 8A , Figure 8B , Figure 8C and Figure 9 shown).

[0088] Figure 12 and Figure 13 are flowcharts outlining methods according to other aspects of the present invention. As Figure 12 outlined, this aspect relates to a method 100 for modifying a passenger service unit slot cover assembly 30 in an aircraft cabin. The method includes step 102: positioning a passenger service unit slot cover assembly panel 31 in a passenger service unit slot cover assembly 30 of an aircraft cabin 14 of an aircraft 10; wherein the passenger service unit slot cover assembly is located outside the outer end 20b of an overhead bin 20, and wherein the passenger service unit slot cover assembly 30 is further located inside the outer wall 18 of the aircraft cabin. The passenger service unit slot cover assembly panel includes an outer surface 31a facing the passenger service unit slot cover assembly in the aircraft cabin. The outer surface 31a of the passenger service unit slot cover assembly panel includes a panel recess 32, and the recessed area of the panel recess 32 is sized to accommodate a passenger service unit slot cover assembly panel handle 34 in a retracted configuration of the passenger service unit slot cover assembly panel handle.

[0089] In yet another aspect, the method 100 for modifying a passenger service unit slot cover assembly 30 in an aircraft cabin further includes step 104: engaging the passenger service unit slot cover assembly panel 31 with at least one passenger service unit slot cover assembly structural support element 22, wherein the at least one passenger service unit slot cover assembly structural support element is configured to support the passenger service unit slot cover assembly panel, and wherein the passenger service unit slot cover assembly structural support element is further configured to support the weight applied to the passenger service unit slot cover assembly panel handle.

[0090] As Figure 13As shown, on the other hand, there is provided a method 200 for assisting / stabilizing a passenger to enter and exit an aircraft passenger seat assembly. The method 200 includes: step 202 of providing a PSU slot cover panel in a stowed configuration; and step 204 of deploying a passenger service unit slot cover assembly panel handle 34 from a stowed configuration of the passenger service unit slot cover assembly panel to a deployed configuration. The passenger service unit slot cover assembly panel is located at an outer position of the outer end 20b of the overhead bin 20 in the aircraft cabin 14 of the aircraft 10 and further at an inner position of the outer wall 18 of the aircraft cabin. The passenger service unit slot cover assembly panel includes an outer surface 30a of the passenger service unit slot cover assembly panel facing the aircraft cabin. The outer surface of the passenger service unit slot cover assembly panel includes a panel recess 32, and the panel recess 22 is sized to receive the passenger service unit slot cover assembly panel handle 34 in the stowed configuration of the passenger service unit slot cover assembly panel handle.

[0091] On the other hand, the method 200 further includes: step 206 of engaging the passenger service unit slot cover assembly panel handle with the weight load of the passenger during at least one of entering the passenger seat assembly 16 by the passenger and exiting the passenger seat assembly 16 by the passenger; and step 208 of stabilizing the passenger during at least one of entering the passenger seat assembly 16 by the passenger and exiting the passenger seat assembly 16 by the passenger.

[0092] Figure 12 and Figure 13 The methods 100, 200 outlined herein and disclosed herein may include the devices disclosed herein, and the devices may be Figure 1 、 Figure 2A 、 Figure 2B 、 Figure 3 、 Figure 4 、 Figure 5 、 Figure 6 、 Figure 7 、 Figure 8A 、 Figure 8B 、 Figure 8C 、 Figure 9 、 Figure 10 and / or Figure 11 of the type shown in at least one of

[0093] As described herein, the device provides increased passenger comfort, mobility, and independence at least during entry and exit from the passenger seat where mobility is typically restricted. According to a further aspect herein, the ability of the PSU slot cover assembly handle to retract or return to a stowed position (e.g., stowed configuration) within the panel recess ensures that the line of sight throughout the cabin remains unobstructed and is not hindered by any component elements that may descend from the slot cover assembly and block such cabin line of sight.

[0094] In addition, this aspect also contemplates that the PSU slot cover assembly handle is arranged to communicate with a signaling device (equivalently referred to herein as a "signaling element") to at least convey or transmit information about the condition of the handle dedicated to a particular aircraft cabin seat position (e.g., the handle is in a stowed configuration or a deployed configuration, etc.) to at least one of a receiver, a controller, and / or a display, so as to, for example, during takeoff, landing, etc., warn the flight crew that a particular passenger is correctly or incorrectly occupying a particular seat.

[0095] In other aspects, the PSU slot cover assembly panel handle, the panel recess, and / or the panel itself may include a light source, which may be a light-emitting component, to facilitate a passenger's confirmation of the handle position and / or to signal when a particular handle is used (e.g., deployed, etc.). Such a light source may be a light-emitting component (e.g., including LEDs, etc.) included within the panel, the handle, the recess, etc., or the light source may be located near the handle, and its light beam is configured to illuminate the handle. In addition, the PSU slot cover assembly panel and / or the panel handle may further include one or more layers of luminescent material, e.g., which may absorb light energy in the presence of light and may release the absorbed light energy in the absence of light to present "illumination" for a selected duration.

[0096] As stated herein, the PSU slot cover assembly may include an integral or one-piece assembly having various integrally formed panels associated with various PSU functions, and the various PSU functions include, for example, a light-emitting component, a passenger information unit component, an oxygen release component, an air-conditioning / blower vent component, and a speaker component, etc. In addition, this aspect relates to a PSU slot cover assembly that includes a plurality of associated discrete panels, which combinatorially form the PSU slot cover assembly, wherein the discrete panels are configured to be used with a selected dedicated function, and the discrete panels may include, for example, a passenger information unit component panel, an oxygen release component panel, an air-conditioning / blower vent component panel, a speaker component panel, and a spacer panel without a specific component function assigned to the panel. This aspect may facilitate the retrofit of the PSU slot cover assembly, for example, by replacing the spacer panel with a PSU slot cover assembly panel including the PSU slot cover assembly panel handle currently disclosed.

[0097] Although the drawings show an outer PSU slot (associated with the PSU slot cover assembly) positioned adjacent to the outer wall of the aircraft cabin or otherwise positioned within the aircraft cabin, additionally aspects of the present invention relate to a center panel PSU slot and an associated PSU slot cover assembly positioned at or near the center of the aircraft and / or at least positioned on the inner side of one or more aircraft aisles, wherein the cover assembly panel equipped with the PSU slot cover assembly panel handle disclosed herein is at least located, for example, above a central seat located at or near the center of the aircraft in a seat assembly, adjacent to the central seat, and / or otherwise accessible from the central seat.

[0098] As used herein, the terms "substantially", "substantially adjacent", "substantially received therein", etc. mean that a particular physical element is almost completely, almost completely positioned or adjacent and / or almost completely received within another stated element.

[0099] Of course, without departing from the basic characteristics of the present disclosure, this aspect may be implemented in other ways different from those specifically set forth herein. This aspect is considered illustrative rather than restrictive in all respects, and all changes falling within the meaning and equivalents of the appended claims are intended to be included therein.

Claims

1. An aircraft cabin passenger service unit slot cover assembly (30), comprising: At least one cabin passenger service unit slot cover assembly panel (31) is located in the aircraft cabin passenger service unit slot cover assembly (30) of the aircraft cabin (14), the aircraft cabin passenger service unit slot cover assembly (30) is positioned outside the overhead luggage box inner end (20a) of the overhead luggage box (20), the aircraft cabin passenger service unit slot cover assembly (30) is further positioned inside the aircraft cabin outer wall (18), the at least one cabin passenger service unit slot cover assembly panel includes a cabin passenger service unit slot cover assembly panel outer surface (31a) facing the aircraft cabin, at least one of the cabin passenger service unit slot cover assembly panel outer surfaces includes a recessed area (32), the recessed area is sized to accommodate a cabin passenger service unit slot cover assembly panel handle (34) in a cabin passenger service unit slot cover assembly panel handle retracted configuration; and The passenger service unit slot cover assembly is configured to separate the passenger service unit slot from the aircraft cabin (14).

2. The aircraft cabin passenger service unit slot cover assembly according to claim 1, further comprising a plurality of cabin passenger service unit slot cover assembly panels.

3. The aircraft cabin passenger service unit slot cover assembly of claim 1, further comprising at least one of a light panel, a passenger information panel, a partition panel, an oxygen release panel, and a speaker panel.

4. The aircraft cabin passenger service unit slot cover assembly according to claim 1, wherein: The aircraft cabin passenger service unit slot cover assembly (30) is an integral assembly.

5. The aircraft cabin passenger service unit slot cover assembly according to claim 1, wherein: The cabin passenger service unit slot cover assembly panel handle is configured to assist a passenger in performing at least one of passenger entry into a passenger seat and passenger exit from a passenger seat.

6. An aircraft cabin (14) comprising an aircraft cabin passenger service unit slot cover assembly according to claim 1.

7. An aircraft (10) comprising an aircraft cabin passenger service unit slot cover assembly according to claim 1.

8. A slot cover assembly panel (31) of an aircraft cabin passenger service unit, comprising: a passenger service unit slot cover assembly panel exterior surface (31a), the passenger service unit slot cover assembly panel exterior surface comprising a recessed area (32) configured and sized to accommodate a passenger service unit slot cover assembly panel handle (34) in a passenger service unit slot cover assembly panel handle stowed configuration; The aircraft cabin passenger service unit slot cover assembly panel (31) is located in a passenger service unit slot cover assembly (30) of an aircraft cabin (14), the passenger service unit slot cover assembly is positioned outside an overhead luggage box inner end (20a) of an overhead luggage box (20), and the passenger service unit slot cover assembly (30) is further positioned inside an aircraft cabin outer wall (18).

9. The aircraft cabin passenger service unit slot cover assembly panel according to claim 8, wherein: The passenger service unit slot cover assembly panel handle is in communication with a signaling element configured to communicate a status of the passenger service unit slot cover assembly panel handle to a display.

10. The aircraft cabin passenger service unit slot cover assembly panel according to claim 8, wherein: At least one of the passenger service unit slot cover assembly panel exterior surface, the panel recess, and the passenger service unit slot cover assembly is illuminated.

11. The aircraft cabin passenger service unit slot cover assembly panel according to claim 8, wherein: The outer surface of the panel of the passenger service unit slot cover assembly also contains luminescent material.

12. The aircraft cabin passenger service unit slot cover assembly panel according to claim 8, further comprising: The passenger service unit slot cover assembly panel inner surface (31b) is positioned adjacent to a passenger service unit slot cover assembly panel support element (35), wherein the passenger service unit slot cover assembly panel support element (35) is configured to engage at least one of the passenger service unit slot cover assembly panel inner surface (31b) and the passenger service unit slot cover assembly panel handle (34).

13. The aircraft cabin passenger service unit slot cover assembly panel according to claim 12, wherein: The passenger service unit slot cover assembly panel support element is further configured to support weight applied to the passenger service unit slot cover assembly panel handle.

14. The aircraft cabin passenger service unit slot cover assembly panel according to claim 13, wherein: The weight applied to the aircraft cabin passenger service unit slot cover assembly panel ranges from about 350 pounds to about 500 pounds.

15. The aircraft cabin passenger service unit slot cover assembly panel according to claim 8, wherein: The passenger service unit slot cover assembly panel (31) is configured to engage at least one passenger service unit slot cover assembly structural support element (22).

16. The aircraft cabin passenger service unit slot cover assembly panel according to claim 15, wherein: The at least one passenger service unit slot cover assembly structural support element (22) is at least one of an air conditioning rail (24) and a passenger service unit rail (26).

17. The aircraft cabin passenger service unit slot cover assembly panel according to claim 16, wherein: The passenger service unit slot cover assembly panel (31) is configured to engage the air conditioning rail (24), and the passenger service unit slot cover assembly panel is further configured to also engage the passenger service unit rail (26).

18. The aircraft cabin passenger service unit slot cover assembly panel according to claim 16, wherein: The passenger service unit slot cover assembly structural support element (22) is configured to support the passenger service unit slot cover assembly (30).

19. An aircraft cabin (14) comprising an aircraft cabin passenger service unit slot cover assembly panel according to claim 8.

20. An aircraft (10) comprising an aircraft cabin passenger service unit slot cover assembly panel according to claim 8.

21. A method (100) comprising: Step (102), positioning at least one passenger service unit slot cover assembly panel (31) in the passenger service unit slot cover assembly (30) of an aircraft cabin (14), the passenger service unit slot cover assembly being positioned outside an overhead luggage box inner end (20a) of an overhead luggage box (20), the passenger service unit slot cover assembly (30) being further positioned inside an aircraft cabin outer wall (18), the at least one passenger service unit slot cover assembly panel comprising a passenger service unit slot cover assembly panel outer surface (31a) facing the aircraft cabin, the passenger service unit slot cover assembly panel outer surface (31a) comprising a recessed area (32), the recessed area being sized to accommodate a passenger service unit slot cover assembly panel handle (34) in a retracted configuration of the passenger service unit slot cover assembly panel handle.

22. The method of claim 20, wherein the at least one passenger service unit slot cover assembly panel further comprises a passenger service unit slot cover assembly panel inner surface (31b) positioned proximate to a passenger service unit slot cover assembly panel structural support element (35), the passenger service unit slot cover assembly panel structural support element being fixedly attached to at least one of the passenger service unit slot cover assembly panel handle (34) and the at least one passenger service unit slot cover assembly panel inner surface (31b), the method further comprising: Step (104), coupling the at least one passenger service unit slot cover assembly panel (31) to at least one passenger service unit slot cover assembly structural support element (22), wherein the at least one passenger service unit slot cover assembly structural support element is configured to support the at least one passenger service unit slot cover assembly panel, and the at least one passenger service unit slot cover assembly structural support element is further configured to support weight applied to a handle of the passenger service unit slot cover assembly panel.

23. The method according to claim 15, wherein: The at least one passenger service unit slot cover assembly structural support element (22) is at least one of an air conditioning rail (24) and a passenger service unit rail (26).

24. A method (200) comprising: The invention relates to a step (204) of deploying a passenger service unit slot cover assembly panel handle (34) from a passenger service unit slot cover assembly panel, the passenger service unit slot cover assembly panel handle being deployed from a passenger service unit slot cover assembly panel handle stowed configuration to a passenger service unit slot cover assembly panel handle deployed configuration, the passenger service unit slot cover assembly panel being positioned in an aircraft cabin (14) at a position outside an overhead luggage bin inner end (20a) of an overhead luggage bin (20), and the passenger service unit slot cover assembly panel being further positioned at a position inside an aircraft cabin outer wall (18), the passenger service unit slot cover assembly panel including a passenger service unit slot cover assembly panel outer surface (30a) facing the aircraft cabin, the passenger service unit slot cover assembly panel outer surface including a recessed area (32) sized to accommodate the passenger service unit slot cover assembly panel handle (34) in the passenger service unit slot cover assembly panel handle stowed configuration: The step (206) of engaging the passenger service unit slot cover assembly panel handle with the weight load of the passenger during at least one of passenger entry into the passenger seat assembly (16) and passenger exit from the passenger seat assembly (16); and The step (208) of stabilizing a passenger during at least one of passenger entry into the passenger seat assembly (16) and passenger exit from the passenger seat assembly (16).

Images