Illuminated luggage box assembly within a transporter

By designing a wirelessly controlled suitcase system and using sensors and optical devices to achieve automatic control, the problem of the luggage in the prior art that cannot be operated unmanned and difficult to prohibit passengers from opening in a specific flight stage is solved, improving flight safety and passenger experience.

JP7658709B2Active Publication Date: 2025-04-08THE BOEING CO
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Patent Information

Application Number
JP2018040356
Authority / Receiving Office
JP · JP
Patent Type
Patents
Current Assignee / Owner
Priority Date
2017-06-15
Filing Date
2018-03-07
Publication Date
2025-04-08
Estimated Expiration
2038-03-07

AI Technical Summary

Technical Problem

The prior art is difficult to implement unmanned luggage control systems inside the aircraft, and it is difficult to prohibit passengers from opening the suitcase during specific flight stages (such as takeoff, landing and turbulence), resulting in safety hazards.

Method used

A wireless control system including a combination of main control equipment and suitcases is designed. The main control equipment controls the opening and closing and locking state of the suitcase through a wireless connection, and is equipped with sensors and optical devices to automatically control and monitor the suitcase status.

Benefits of technology

Unmanned open and closed and automatic locking of the suitcase are realized, ensuring that passengers are prohibited from opening the suitcase during specific flight stages, improving flight safety and passenger experience.

✦ Generated by Eureka AI based on patent content.

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Abstract

To provide, interior cabins within vehicles such as commercial aircraft, and particularly, electronic stowage bin control systems and methods within interior cabins of vehicles.SOLUTION: A stowage bin assembly 502 within an interior cabin of a vehicle comprises: one or more interior light-emitting elements 528 configured to illuminate a baggage retaining chamber of the stowage bin assembly. The interior light-emitting elements 528 are disposed within the baggage retaining chamber of the stowage bin assembly 502. The one or more interior light-emitting elements 528 illuminate the baggage retaining chamber when the stowage bin assembly 502 is in an open position, and are deactivated when the stowage bin assembly 502 is in a closed position.SELECTED DRAWING: Figure 10
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Description

[Technical field]

[0001] FIELD OF THE DISCLOSURE This disclosure relates generally to interior cabins within a vehicle, such as a commercial aircraft, and more particularly to a system and method for electronic luggage bin control within the interior cabin of a vehicle. [Background technology]

[0002] Commercial aircraft typically include an interior cabin that may be divided into multiple zones. The cockpit is generally separated from the cabin, which may include a first class zone, a business class zone, and an economy class zone. The cabin may also include one or more flight crew work areas, such as a galley, which may have food and beverage storage structures. One or more corridors run through the cabin, connecting each passenger zone to one or more pathways that lead to one or more doors on the aircraft.

[0003] Overhead luggage bins are typically located above rows of seats in commercial aircraft. Each overhead luggage bin is configured to move between an open position and a closed position. In the open position, passengers may place carry-on baggage into the movable bin or bucket. Before the aircraft leaves the terminal, flight attendants ensure that each bin is securely closed.

[0004] To open a luggage box, an individual (such as a passenger or flight attendant) physically contacts the luggage box latch. For example, to operate the luggage box to an open position, the individual first grasps and pulls the latch. As can be appreciated, luggage box latches are contacted many times by many individuals. Ultimately, if the latches are not cleaned regularly, various germs and bacteria may be present on the latches. Furthermore, certain individuals may have difficulty grasping and operating the latches.

[0005] Furthermore, it is usually not possible for flight attendants to prevent passengers from opening their luggage bins during flight. Even when passengers should be securely buckled in their seats (such as during takeoff, landing, or turbulence), passengers may often stand up and open their luggage bins. This can lead to dangerous situations. For example, during periods of turbulence, the contents of an open luggage bin may fall into the aisle or even onto passengers. Summary of the Invention

[0006] There is a need for a luggage box assembly that can be opened and closed without contact by individuals.There is a need for a luggage box assembly that can be controlled by flight crew.There is a need for a system and method that prevents passengers from opening the luggage box assembly during limited periods during flight, such as takeoff, landing, and during turbulence.

[0007] In light of those needs, certain embodiments of the present disclosure provide a luggage box control system for a transporter, the luggage box control system including at least one luggage box assembly configured to selectively move between an open position and a closed position, a master control device separate and distinct from the luggage box assembly, the master control device communicatively coupled to the luggage box assembly via a wireless connection and configured to operate the luggage box assembly.

[0008] In at least one embodiment, a master control device is configured to automatically move the luggage box assemblies between the open and closed positions. Each luggage box assembly includes a latch configured to selectively lock and unlock the luggage box assembly. The master control device is configured to automatically lock and unlock the latch. The latch is operatively connected to one or more latching mechanisms.

[0009] In at least one embodiment, the master control device includes a master luggage box control unit in communication with the luggage box assemblies. One or more of the luggage box assemblies may include luggage box control units in communication with the master luggage box control unit. The master control device may include a user interface configured to allow an individual to input commands.

[0010] In at least one embodiment, multiple luggage box assemblies are communicatively coupled to a master control device. The master control device may open or close multiple luggage box assemblies simultaneously. The master control device may open or close multiple luggage box assemblies in an alternating manner. The master control device may synchronize the opening or closing of the luggage box assemblies with lighting effects, sounds, graphics, and / or animation. In at least one embodiment, the master control device is configured to transition the luggage box assembly into a manual override mode in response to receiving one or more error signals from the luggage box assembly, where a user can manually open or close the luggage box assembly.

[0011] The luggage box assembly may be configured to output a report signal to the master control device, the report signal including data regarding operational health or status.

[0012] The luggage box assembly may include a proximity sensor configured to detect the presence of an object within a detection range. The proximity sensor may be mounted to an exterior surface of the luggage box assembly. The proximity sensor may be configured to selectively switch the luggage box assembly between a locked state and an unlocked state.

[0013] The luggage box assembly may include one or more exterior light-emitting elements configured to emit light indicative of a current status of the luggage box assembly. The (one or more) exterior light-emitting elements may be proximate to a latch of the luggage box assembly.

[0014] The luggage box assembly may include a motion sensor configured to detect motion within a detection range. The motion sensor may be proximate to a latch of the luggage box assembly. The motion sensor may be configured to participate in automatically opening or closing the luggage box assembly without an individual contacting the luggage box assembly.

[0015] The luggage box assembly may include one or more inner light-emitting elements. The inner light-emitting element(s) may be disposed within a luggage-holding compartment of the luggage box assembly. The inner light-emitting element(s) may be configured to illuminate the luggage-holding compartment of the luggage box assembly. The inner light-emitting element(s) may be configured to illuminate the luggage-holding compartment when the luggage box assembly is in an open position and may be deactivated when the luggage box assembly is in a closed position. In at least one embodiment, the inner light-emitting element(s) emits light that gradually increases in intensity as the luggage box opens and emits light that gradually decreases in intensity as the luggage box closes.

[0016] The luggage box assembly may include a box position sensor configured to detect a position of the luggage box assembly.

[0017] The luggage box assembly may include a weight sensor configured to detect a weight of the luggage box assembly.

[0018] The luggage box assembly may include at least one touch sensor configured to be contacted to lock, unlock, close, and / or open the luggage box assembly.

[0019] In at least one embodiment, a luggage box assembly includes a bucket having a front panel connected to a forward end panel and an aft end panel, the front panel, the forward end panel, and the aft end panel defining, at least in part, a luggage holding compartment, the front panel may include an arched panel having a curved outer surface.

[0020] Certain embodiments of the present disclosure provide a vehicle including an interior cabin and a luggage box control system. The luggage box control system includes at least one luggage box assembly within the interior cabin. The luggage box assembly is configured to selectively move between an open position and a closed position. A master control device is separate and distinct from the luggage box assembly. The master control device is wirelessly coupled to the luggage box assembly and configured to operate the luggage box assembly.

[0021] Certain embodiments of the present disclosure provide a method of luggage box control for a vehicle, the method including wirelessly connecting a master control device to at least one luggage box assembly within the vehicle, and operating the luggage box assembly using the master control device.

[0022] Certain embodiments of the present disclosure provide a luggage box assembly for a transporter. The luggage box assembly includes a latch configured to selectively lock and unlock the luggage box assembly. The luggage box assembly also includes one or more of a proximity sensor configured to detect the presence of an object, a motion sensor configured to detect motion within a detection range, or at least one touch sensor configured to be contacted to lock, unlock, close, and / or open the luggage box assembly.

[0023] The luggage box assembly may also include one or more exterior light emitting elements configured to emit light indicative of a current status of the luggage box assembly.

[0024] The luggage box assembly may also include one or more interior light-emitting elements configured to illuminate a luggage-holding compartment of the luggage box assembly, a box position sensor configured to detect a position of the luggage box assembly, and / or a weight sensor configured to detect a weight of the luggage box assembly.

[0025] Certain embodiments of the present disclosure provide a luggage box assembly that includes a latch configured to selectively lock and unlock the luggage box assembly, and a sensor in communication with the latch, the sensor configured to participate in locking, unlocking, opening, and / or closing the luggage box assembly without the latch or sensor being contacted.

[0026] In at least one embodiment, the sensor includes a proximity sensor configured to detect the presence of an object within a detection range.In at least one embodiment, the sensor includes a motion sensor configured to detect motion within the detection range.

[0027] Certain embodiments of the present disclosure provide a method of operating a luggage box assembly, the method including communicatively connecting a latch configured to selectively lock and unlock the luggage box assembly to a sensor, and engaging the sensor in one or more of locking, unlocking, opening, or closing the luggage box assembly without the latch or sensor being contacted.

[0028] Certain embodiments of the present disclosure provide a luggage box assembly including one or more interior light-emitting elements configured to illuminate a luggage-holding compartment of the luggage box assembly. The interior light-emitting elements may be disposed within the luggage-holding compartment of the luggage box assembly.

[0029] In at least one embodiment, an inner light-emitting element is configured to illuminate the luggage holding compartment when the luggage box assembly is in an open position, and one or more inner light-emitting elements are deactivated when the luggage box assembly is in a closed position. The inner light-emitting elements may emit light that gradually increases in intensity as the luggage box assembly opens and gradually decreases in intensity as the luggage box closes.

[0030] Certain embodiments of the present disclosure provide a method of operating a luggage box assembly, the method including illuminating a luggage-holding compartment of the luggage box assembly with one or more interior light-emitting elements.

[0031] Certain embodiments of the present disclosure provide a luggage box assembly that includes a weight sensor configured to detect a weight of the luggage box assembly.

[0032] Certain embodiments of the present disclosure provide a method of operating a luggage box assembly that includes detecting a weight of the luggage box assembly using a weight sensor in the luggage box assembly. [Brief description of the drawings]

[0033] [Figure 1] FIG. 1 illustrates a front perspective view of an aircraft according to one embodiment of the disclosure. [Figure 2A] FIG. 1 illustrates a top view of an interior cabin of an aircraft, according to one embodiment of the disclosure. [Figure 2B] FIG. 1 illustrates a top view of an interior cabin of an aircraft, according to one embodiment of the disclosure. [Diagram 3] 1 illustrates an interior perspective view of an interior cabin of an aircraft, according to one embodiment of the disclosure. [Figure 4] 1 illustrates a front perspective view of a luggage box assembly in a closed position within an interior passenger compartment according to one embodiment of the present disclosure. [Diagram 5] 1 illustrates a front perspective view of a luggage box assembly in an open position within an interior passenger compartment according to one embodiment of the present disclosure. [Figure 6] 1 illustrates a side perspective view of a row of seats within an interior cabin of a vehicle according to one embodiment of the disclosure. [Figure 7] 1 illustrates a front view of a latch for a luggage box assembly according to one embodiment of the present disclosure. [Figure 8] 1 illustrates a latching mechanism for a luggage box assembly according to one embodiment of the present disclosure. [Figure 9] FIG. 1 illustrates a block diagram of a luggage box control system according to one embodiment of the present disclosure. [Figure 10] FIG. 1 illustrates a block diagram of a luggage box assembly according to one embodiment of the present disclosure. [Figure 11] 1 illustrates a front view of a latch according to one embodiment of the present disclosure. [Figure 12]1 illustrates a circuit diagram of a luggage box control unit connected to a latch according to one embodiment of the present disclosure. [Figure 13] 1 illustrates a flowchart of a luggage box control method according to one embodiment of the present disclosure. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0034] The above summary, as well as the following detailed description of certain embodiments, will be better understood when read in conjunction with the accompanying drawings. As used herein, it is to be understood that the use of "a" or "an" in the singular form of an element or step does not necessarily exclude a plurality of such elements or steps. Moreover, references to "one embodiment" should not be interpreted as excluding the existence of additional embodiments that incorporate the features described herein. Additionally, unless expressly stated to the contrary, an embodiment "comprising," "including," or "having" one or more elements having a particular property may include additional elements that do not have that property.

[0035] Certain embodiments of the present disclosure provide touchless activated luggage box assemblies. The luggage box assemblies may be selectively moved between open and closed positions without an individual physically contacting them. Additionally, the luggage box assemblies may be controlled by one or more luggage box control units. The luggage box control units may be operated by aircraft crew (e.g., pilots or flight attendants) and may prevent passengers from opening the luggage box assemblies during limited periods of time (e.g., takeoff, landing, during turbulence, etc.).

[0036] In at least one embodiment, the luggage box assembly includes an electronic latch configured to automatically lock and open. In at least one embodiment, the latch includes a sensor (such as a proximity or motion sensor) configured to detect hand movement within a predefined detection range (such as within 3 or 4 inches from the sensor). In this manner, when an individual moves their hand within a proximate range of the latch (such as within 6 inches or less), the latch can be operatively engaged without physically contacting the latch. An individual can automatically open the luggage box assembly by simply waving their hand in front of the latch.

[0037] A luggage box control unit in communication with the latches of the luggage box assembly (such as through one or more wired or wireless connections) may be used to lock the latches and prevent the latches from switching to an open state. In this manner, aircraft crew can lock the latches to prevent passengers from opening the luggage box assembly. The luggage box control unit may be in a computer onboard the aircraft, such as in a workstation or control panel in the galley or cockpit. In at least one other embodiment, the luggage box control unit may be in a handheld device, such as a handheld smart device or cell phone.

[0038] In at least one embodiment, the latch can be set to a locked state when the flight crew swipes their badge in front of the latch. The latch can include one or more light-emitting elements (such as light-emitting diodes - LEDs) that indicate whether the latch is locked or not. For example, in the locked state, the light-emitting element can emit a red light. In the unlocked state, the light-emitting element can emit a green light.

[0039] Certain embodiments of the present disclosure provide a wirelessly controllable electronic luggage box system. The luggage box system includes a luggage box assembly having a latching mechanism coupled to a door, an electric button on or near the luggage box assembly for controlling the electric latch, and an electric drive system for at least assisting the force required to manipulate the luggage box through at least a portion of the luggage box's range of motion. In at least one embodiment, aircraft crew can control one or all of the luggage box assemblies from a control panel or a portable electronic device (PED), such as a handheld control device, electronic tablet, cell phone, or other such smart device. Passengers may also control overhead luggage box assemblies from their PEDs in limited circumstances.

[0040] Certain embodiments of the present disclosure provide an overhead luggage box system including a plurality of wirelessly controlled features. The overhead luggage box system includes a plurality of luggage box assemblies. One or more of the luggage box assemblies include a powered latch, a powered actuator, and an electronic proximal control. An electronic control device may be used to control the wirelessly controlled features of the luggage box assemblies.

[0041] Wireless connection of the various components of the luggage box system provides a luggage box assembly that is light and not bulky; routing multiple wires within the luggage box assembly requires space and can add weight.

[0042] In at least one embodiment, one or more of the luggage box assemblies includes an electronic light source (such as one or more LEDs). The light source may be within an enclosed area of ​​the luggage box assembly. The light source may be configured to gradually illuminate or gradually fade light in synchronization with each opening and closing movement of the box. The luggage box assembly may also include a sensor for determining the instantaneous position, such as the rotational position, of the box relative to the aircraft.

[0043] The system may include pre-programmed control sequences for all or some of the features, including choreographed opening / closing of the box and automatic locking of the box during certain parts of a trip, at least some of the pre-programmed control sequences ensure compliance with safety and security requirements promulgated by the Federal Aviation Administration (FAA).

[0044] In at least one embodiment, the box defaults to a manual override mode that allows the user to manually open and close the box by physically manipulating the box.

[0045] In at least one embodiment, the luggage bin assembly is programmable (e.g., the latches can be programmed to lock or unlock at various times). As one example, the luggage bin assembly may be programmed to open and close in a wave-like motion, synchronized with cabin lighting, sound schemes, etc.

[0046] The proximity control button may be a light-emitting capacitive touch surface. In at least one other embodiment, the proximity control button may include a proximity or motion sensor, such as one that is activated by waving a hand. In at least one other embodiment, the proximity control button may be configured for voice control.

[0047] Each luggage box assembly can be configured to report information to the master control unit to indicate its operational health and / or status, such as box volume status, maintenance needs, and utilization data that can speed up loading and unloading procedures.

[0048] In at least one embodiment, at least a portion of the system is powered from a power strip and / or a data strip.

[0049] The disclosed embodiments provide luggage bin systems, methods, and assemblies that provide a variety of advantages: improved accessibility for people with reduced mobility, improved passenger experience, low-cost and lightweight design, efficient, safe, aesthetically pleasing, and ergonomic aircraft interiors, less aircraft downtime, faster turnaround times, faster boarding and disembarking, increased bin capacity (not limited by ergonomics / varying human strength limitations), easier crew work, better on-board service, e.g., reduced repetitive physical pushing to close luggage bins, and improved on-board health care.

[0050] 1 illustrates a front perspective view of a vehicle, such as an aircraft 10, according to one embodiment of the disclosure. For example, the aircraft 10 includes a propulsion system 12, which may include two turbofan engines 14. Optionally, the propulsion system 12 may include more engines 14 than are shown. The engines 14 are carried by wings 16 of the aircraft 10. In other embodiments, the engines 14 may be carried by a fuselage 18 and / or a tail 20. The tail 20 may also support a horizontal stabilizer 22 and a vertical stabilizer 24.

[0051] The fuselage 18 of the aircraft 10 defines an interior cabin, which may include a cockpit, one or more work areas (e.g., a galley, a crew baggage area, etc.), one or more passenger areas (e.g., first class, business class, economy class), and an aft area. Each of the areas may be separated by a cabin transition area. Overhead baggage bin assemblies are located throughout the interior cabin.

[0052] Alternatively, instead of aircraft, embodiments of the present disclosure may be used in a variety of other vehicles, such as automobiles, buses, locomotives and trains, ships, spacecraft, and the like.

[0053] FIG. 2A illustrates a top view of an interior cabin 30 of an aircraft, according to one embodiment of the disclosure. The interior cabin 30 may be within a fuselage 32 of the aircraft. For example, one or more fuselage wall members may define the interior cabin 30. The interior cabin 30 includes multiple zones, including a forward zone 33, a first class zone 34, a business class zone 36, a forward galley 38, an extended economy or coach zone 40, a standard economy or coach zone 42, and an aft zone 44, which may include multiple lavatories and galleys. It should be understood that the interior cabin 30 may include more or fewer zones than shown. For example, the interior cabin 30 may not include a first class zone and may include more or fewer galleys than shown. Each of the zones may be separated by a cabin transition area 46, which may include a class divider assembly between the aisles 48.

[0054] 2A, the interior passenger compartment 30 includes two passageways 50 and 52 that lead to the aft section 44. Optionally, the interior passenger compartment 30 may have fewer or more passageways than shown. For example, the interior passenger compartment 30 may include a single passageway extending through the center of the interior passenger compartment 30 that leads to the aft section 44.

[0055] One or more electrical signal feed systems 200 may be secured to one or more structural components within the interior cabin 30. As shown, each electrical signal feed system 200 may extend parallel to the longitudinal axis 47 of the interior cabin 30. Optionally, the electrical signal feed systems 200 may not be parallel to the longitudinal axis 47. For example, at least one electrical signal feed system 200 may traverse the interior cabin 30, whereby at least one electrical signal feed system 200 may be perpendicular to the longitudinal axis 47. However, the interior cabin 30 may include more or fewer electrical signal feed systems 200 than shown. For example, an electrical signal feed system 200 may be disposed across each longitudinal section of a seat installed in the aircraft.

[0056] The electrical signal distribution system 200 may span from the front or forward area 33 to the rear area 44. The electrical signal distribution system 200 may span the entire length of the interior passenger compartment 30. Optionally, the electrical signal distribution system 200 may span less than the entire length of the interior passenger compartment 30.

[0057] The electrical signal distribution system 200 may be secured to various structural components within the interior cabin 30. For example, the electrical signal distribution system 200 may be securely attached to a strongback, a passenger service unit (PSU) trough, a luggage bin, a PSU rail, a floor member structure, a ceiling structure, a wall member structure, etc. The electrical signal distribution system 200 is configured to provide electrical signals, such as power signals and / or data signals, to various electrical devices within the interior cabin, as described below.

[0058] The electrical signal supply system 200 is further described by background reference to U.S. patent application Ser. No. 15 / 287,949, entitled "Systems and Methods for Providing Electrical Signals to Electrical Devices Within an Interior Cabin of a Vehicle."

[0059] 2B illustrates a top view of an interior cabin 80 of an aircraft, according to one embodiment of the disclosure. The interior cabin 80 may be within a fuselage 81 of the aircraft. For example, one or more fuselage wall members may define the interior cabin 80. The interior cabin 80 includes multiple sections, including a main cabin 82 having passenger seats 83 and an aft section 85 behind the main cabin 82. It should be understood that the interior cabin 80 may include more or fewer sections than shown.

[0060] The interior cabin 80 may include a single passageway 84 that leads to the aft section 85. The single passageway 84 may extend through a center of the interior cabin 80 that leads to the aft section 85. For example, the single passageway 84 may be aligned coaxially with a central longitudinal plane 86 of the interior cabin 80. One or more electrical signal distribution systems 200 may be secured to structural components within the interior cabin 80.

[0061] FIGURE 3 illustrates an interior perspective view of an interior cabin 100 of an aircraft, in accordance with one embodiment of the disclosure. The interior cabin 100 includes an outboard wall member 102 and a ceiling 104, which may include a number of ceiling panels. Windows 106 may be formed in the outboard wall member 102. A floor member 108 supports a row of seats 110. As shown in FIGURE 3, the row 112 may include two seats 110 on either side of an aisle 113. However, the row 112 may include more or fewer seats 110 than shown. Additionally, the interior cabin 100 may include more aisles than shown.

[0062] Electrical devices such as PSUs 114 are secured between the outboard wall members 102 and the ceiling 104 on either side of the aisle 113. The PSUs 114 extend between the forward and aft ends of the interior cabin 100. For example, a PSU 114 may be located above each seat 110 in the row 112. Each PSU 114 may include a housing 116 generally above each seat 110 (or group of seats) in the row 112 that may include passenger vents, reading lights, an oxygen delivery system (such as an oxygen bag drop panel), a flight attendant request button, and other such controls.

[0063] Overhead luggage bin assemblies 118 are secured to structure on either side of the aisle 113, above and inboard from the PSU 114, near the ceiling 104 and / or outboard wall members 102. The overhead luggage bin assemblies 118 are secured above the seats 110. The overhead luggage bin assemblies 118 extend between the forward and aft ends of the interior cabin 100. Each luggage bin assembly 118 may include a swivel box or bucket 120 pivotally secured to a strongback (hidden from view in FIG. 3). The overhead luggage bin assemblies 118 may be located above and inboard from the underside of the PSU 114. The overhead luggage bin assemblies 118 are configured to pivot open, for example, to receive passenger baggage and personal items.

[0064] As used herein, the term "outboard" means a location further away from the central longitudinal plane 122 of the interior passenger compartment 100 compared to another component. The term "inboard" means a location closer to the central longitudinal plane 122 of the interior passenger compartment 100 compared to another component. For example, the lower surface of the PSU 114 may be outboard relative to the luggage box assembly 118.

[0065] At least one electrical signal distribution system 200 (shown in FIGS. 2A and 2B but hidden from view in FIG. 3) may extend the entire length of the interior cabin 100 and run parallel to the longitudinal surface 122. For example, the electrical signal distribution system 200 may be attached to a strongback of the luggage box assembly 118. Optionally, the electrical signal distribution system 200 may be attached to a PSU rail that secures the PSU 114 in place. As another example, the electrical signal distribution system 200 may be attached to a floor section or ceiling structure.

[0066] An electrical device 125 may be mounted on the bucket 120 of the luggage box assembly 118. As shown, the electrical device 125 may be secured to an exterior surface of the bucket 120. Optionally, the electrical device 125 may be secured to an interior surface of the bucket 120. In at least one embodiment, the electrical device 125 may be embedded within the bucket 120. The electrical device 125 may be one or more of a power latch or lock, a speaker, a lighting assembly (such as one or more light emitting diodes), a monitor (such as a video screen and / or touch screen), a fan, one or more sensors, and the like. The electrical device may also be located within the PSU trough, for example adjacent to a reading light panel.

[0067] The electrical device 125 in the form of an electric latch may be located in various areas of the bucket 120. For example, the latch may be located at or near the center of the front of the bucket 120, at or near the top, bottom, side portions, etc. In at least one embodiment, the latch may not be on the bucket 120, but may be on a structural feature to which the luggage box assembly 118 is secured.

[0068] 4 illustrates a front perspective view of a luggage box assembly 118 in a closed position within the interior passenger compartment 100, according to one embodiment of the disclosure. The luggage box assembly 118 includes a bucket 120 having a front panel 126 coupled to forward and aft end panels (hidden from view in FIG. 4). As shown, the front panel 126 may be an arched panel having a curved outer surface that curves downward toward the outboard wall member 102. As such, an upper end portion 128 of the front panel 126 is more inboard than a lower portion 130. An electrical device 125 may be fixed and / or embedded within the front panel 126. As noted, the electrical device 125 may be an electric latch, a proximity control member (such as a button), a proximity or motion sensor, or the like.

[0069] FIG. 5 illustrates a front perspective view of the luggage box assembly 118 in an open position within the interior cabin 100, according to one embodiment of the present disclosure. As shown, the front panel 126 is secured to a forward end panel 132 and an aft end panel 134, which may be generally opposed and parallel to one another. The front panel 126 and the end panels 132 and 134 may also be connected to a bottom panel 136. For example, the bottom panel 136 may be an inwardly curved portion of the front panel 126. In at least one embodiment, a closeout bracket 138 may extend between the end panels 132 and 134 to provide rigid bracing support therebetween. The front panel 126 may be thicker than the end panels 132 and 134 because the front panel 126 is configured to directly support the weight of an overhead bag. As such, the front panel 126 may have an increased thickness to provide additional support strength and rigidity.

[0070] A cargo holding compartment 140 is defined between the front panel 126, the end panels 132 and 134, and the bottom panel 136. The cargo holding compartment 140 is configured to receive cargo 142 when the cargo box assembly 118 is in the open position.

[0071] End panels 132 and 134 are each pivotally secured to a fixed panel 144, such as a fixed panel of a strongback. That is, fixed panel 144 may be part of a strongback within interior passenger compartment 100.

[0072] A background art example of a luggage bin assembly is described in U.S. patent application Ser. No. 14 / 682,217, entitled "Overhead Stowage Bin Assembly for a Vehicle." However, as can be appreciated, various other types of luggage bin assemblies can be used with the embodiments of the present disclosure. As with U.S. patent application Ser. No. 14 / 682,217, the luggage bin assembly 118 shown in Figures 4 and 5 is merely exemplary.

[0073] 6 illustrates a side perspective view of a row of seats 300 in an interior cabin 302 of a vehicle 304, according to one embodiment of the disclosure. The interior cabin 302 may include a first electrical signal distribution system 200a mounted to an interior cabin floor member 305, a second electrical signal distribution system 200b mounted to a PSU rail 306 that supports a PSU 308 below a luggage box assembly 310, and a third electrical signal distribution system 200c mounted to a ceiling 308 of the interior cabin 302. Optionally, the interior cabin 302 may include less than all of the electrical signal distribution systems 200a, 200b, and 200c.

[0074] As shown, electrical signal feed systems 200a, 200b, and 200c extend along the length of interior cabin 302. Electrical signal feed systems 200a, 200b, and 200c are parallel to a central longitudinal axis 311 of interior cabin 302, or at least a portion of the central longitudinal axis 311 of interior cabin 302. Optionally, one or more electrical signal feed systems may be oriented transversely relative to interior cabin 302, whereby one or more electrical signal feed systems may be perpendicular to central longitudinal axis 311.

[0075] Various electrical devices may be connected to the outlets 210 of the electrical signal supply systems 200a, 200b, and 200c. For example, a console 212a on the armrest 320 of the seat 300 may be electrically connected to the electrical signal supply system 200a. The console 212a may be or include a display, such as a monitor, touch screen, etc. Optionally, the console 212a may be mounted on the back of the seat. The PSU 308 and the luggage box latch 212b may be electrically connected to the electrical signal supply system 200b. An accent lighting assembly 212c and a speaker may be electrically connected to the electrical signal supply system 200c. Additionally, a lighting assembly 212d may be electrically connected to the electrical signal supply system 200b.

[0076] Additionally, microphones 212e may be electrically connected to the electrical signal supply system 200b. The microphones 212e may be positioned throughout the interior cabin 702 to allow flight attendants to broadcast messages during the flight.

[0077] The electrical signal delivery systems 200a-c replace the wiring and bundled structures traditionally used to connect electrical devices to power and data sources. Receptacles 210 regularly spaced on the PCB 208 allow quick and easy connections to a variety of electrical devices throughout the interior cabin 302.

[0078] 7 shows a front view of a latch 350 of a luggage box assembly 351, according to one embodiment of the disclosure. Latch 350 is an example of latch 212b shown in FIG. 6. Latch 350 is mounted on a front panel 355 of luggage box assembly 351. Optionally, latch 350 may be mounted on other portions of luggage box assembly 351. Latch 350 includes an activation button 360 within the latch button that includes an electrical switch connected to a latching mechanism (not shown in FIG. 7).

[0079] FIG. 8 illustrates a latching mechanism 400 for a luggage box assembly 351 according to one embodiment of the disclosure. The latching mechanism 400 may be mounted on a side wall 410 of a bucket (such as the bucket 120 shown in FIGS. 4 and 5), on a strongback, or the like. The latching mechanism 400 includes a solenoid drive member 420 that pushes open the aircraft luggage box door upon activation, and may also include a latching element used to hold the door closed when a passenger or airline flight attendant pushes the door closed. A cable 430 may be connected between an electronic switch in the latch 350 (shown in FIG. 3) and the latching mechanism 400. Optionally, the electronic switch in the latch 350 and the latching mechanism may communicate through a wireless connection.

[0080] 7 and 8, when latch 350 is activated by a passenger or airline flight attendant, an electrical signal is passed from latch 350 to latching mechanism 400 via conductors in cable 430, causing latching mechanism 400 to push open the door or bucket of luggage box assembly 351.

[0081] Background art examples of latches 350 and latching mechanism 400 are further described in U.S. patent application Ser. No. 14 / 542,265, entitled "Self-Contained Electronic Stowage Bin System." As described in U.S. patent application Ser. No. 14 / 542,265, the luggage bin assembly may include an energy utilization system and energy storage configured to provide power to latches 350 and / or latching mechanism 400. In at least one other embodiment, latches 350 and / or latching mechanism 400 may be configured to receive power and / or data from electrical signal supply system 200 (shown in FIGS. 2A, 2B, and 6), as described in U.S. patent application Ser. No. 15 / 287,949, entitled "Systems and Methods for Providing Electrical Signals to Electrical Devices Within an Interior Cabin of a Vehicle." As another background example, latch 350 and / or latching mechanism 400 may be configured to receive power and / or data via the systems and methods described in U.S. patent application Ser. No. 15 / 281,263, entitled "Systems and Methods for Wirelessly Transmitting Electrical Signals to an Overhead Stowage Bin Assembly of a Vehicle." Alternatively, latch 350 and / or latching mechanism 400 may be configured to receive power and / or data through one or more wired connections.

[0082] FIG. 9 illustrates a block diagram of a luggage box control system 500 according to one embodiment of the disclosure. The luggage box control system 500 includes a plurality of luggage box assemblies 502 (such as any of those described herein) in communication with a master control device 501 that is separate and distinct from the luggage box assemblies 502. The luggage box assemblies 502 may be located within a vehicle, such as those described herein. The master control device 501 may also be located within the vehicle, such as in a cockpit, a galley, etc. In at least one embodiment, the master control device 501 may be or be part of a control panel and / or computer station within the vehicle. In at least one other embodiment, the master control device 501 may be or be part of a handheld device, such as a handheld control device, a smart device, a smart phone, a tablet, etc.

[0083] In at least one embodiment, a master control device 501 is communicatively connected to all of the luggage box assemblies 502 in the transport. In at least one embodiment, a single master control device 501 is used to control the operation of multiple luggage box assemblies 502. Optionally, the master control device 501 may communicate with less than all of the luggage box assemblies 502 in the transport. A transport may include more or fewer luggage box assemblies 502 than are shown in FIG.

[0084] At least one of the luggage box assemblies 502 includes a latch 506, a luggage box control unit 508, and a communication device 510. The luggage box control unit 508 is communicatively coupled to the latch 506 and the communication device 510 through one or more wired or wireless connections. Optionally, the luggage box assembly 502 may not include the luggage box control unit 508.

[0085] Latch 506 is operably connected to one or more latching mechanisms (such as latching mechanism 400 shown in FIG. 8) configured to latch luggage box assembly 502 into a closed position. For example, latch 506 may be operably connected to two latching mechanisms at opposite ends of luggage box assembly 502. Optionally, latch 506 may be operably connected to a single latching mechanism. Further, optionally, latch 506 may be operably connected to three or more latching mechanisms.

[0086] The latch 506 may be in various locations on the luggage box assembly 502. For example, the latch 506 may be in the center of the front panel, above the front panel, below the front panel, to the side of the front panel, etc. In at least one embodiment, the latch 506 may be located on a structural feature that is separate and distinct from the luggage box assembly 502.

[0087] The master control device 501 includes a housing 512 including a master bin control unit 514 communicatively connected to a display 516, a user interface 518, and a communication device 518, such as through one or more wired or wireless connections. The display 516 may include a monitor, such as a touch screen monitor, an LED monitor, a liquid crystal display (LCD) monitor, a plasma monitor, etc. Optionally, the master control device 501 may not include a display 516. The user interface 518 may be or include a touch screen surface of a display, a separate touch screen surface, a keyboard, one or more buttons, etc. The user interface 518 allows an individual to input commands to the master control device 501. The display 516 is configured to allow an individual to interact with the master control device 501 to input commands, view the status of the system, etc.

[0088] The luggage box assembly 502 is communicatively coupled to the master control device 501 via communication device 510 and communication device 518 of the master control unit 514 through one or more wired or wireless connections. The communication devices 510 and 518 may be or include antennas (such as radio antennas), transceivers, other wireless communication systems (such as WiFi), etc. configured to enable wireless communication between the master control device 501 and the luggage box assembly 502. Alternatively, the master control device 501 may communicate with the luggage box assembly 502 through one or more wired connections.

[0089] In at least one embodiment, the master control device 501 communicates with the luggage box assemblies 502 in the aircraft through a wireless connection. By wirelessly connecting the master control device 501 with the luggage box assemblies 502, the aircraft is made substantially lighter because there is no need to route bundles of wires between the master control device 501 and the various luggage box assemblies 502. Ultimately, a lighter aircraft consumes less fuel, thereby saving costs. Furthermore, because there are no bundles of wires routed between the master control device 501 and the luggage box assemblies 502, space is saved within the aircraft. Furthermore, because there are no wires routed between the master control device 501 and the luggage box assemblies 502, the process of manufacturing is easier and less expensive.

[0090] In operation, an individual (such as an aircraft crew member) may control the operation of the luggage box assemblies 502 via the master control device 501. For example, the individual may input a locking command into the master control device 501 via the user interface 518. The master luggage box control unit 514 receives the locking command and transmits locking control signals to one or more of the luggage box assemblies 502 based on the locking command input into the master control device 501. For example, the individual may input a locking command to lock all of the luggage box assemblies 502 or a subset of the luggage box assemblies 502.

[0091] The luggage box assembly 502 receives a locking control signal from a master luggage box control unit 514 via the communication device 510. In response to the received control signal, the luggage box control unit 508 operates a latch 506 to lock the luggage box assembly 502, thereby preventing a passenger from opening the luggage box assembly 502. Optionally, the luggage box assembly 502 may not include a separate and distinct luggage box control unit 508. Instead, the master luggage box control unit 514 may control the latch 506 without an intermediate luggage box control unit 508.

[0092] In another embodiment, an individual may input an unlock command into the master control device 501 via the user interface 518. The master box control unit 514 receives the unlock command and transmits an unlock control signal to one or more of the box assemblies 502 based on the unlock command input into the master control device 501.

[0093] The luggage box assembly 502 receives an unlocking control signal from the master luggage box control unit 514 via the communication device 510. In response to the received control signal, the luggage box control unit 508 operates the latch 506 to unlock the luggage box assembly 502, thereby allowing the passenger to open the luggage box assembly 502.

[0094] In another embodiment, an individual may input an open command to the master control device 501 via the user interface 518. The master box control unit 514 receives the open command and transmits an open control signal to one or more of the box assemblies 502 based on the open command input to the master control device 501.

[0095] The luggage box assembly 502 receives an opening control signal from a master luggage box control unit 514 via the communication device 510. In response to the received control signal, the luggage box control unit 508 automatically opens the luggage box assembly 502. For example, the luggage box assembly 502 may include an actuator 520 (which may include the locking mechanism 400 shown in FIG. 8, one or more motors, a hydraulic subsystem, a pneumatic subsystem, an electrical opening system, etc.) configured to automatically open the luggage box assembly 502 upon receiving a command. The actuator 520 is communicatively coupled to the luggage box control unit 508, which controls the operation of the actuator 520. In at least one other embodiment, the actuator 520 may be configured to be directly controlled by the master luggage box control unit 514 based on the control signal received from the master luggage box control unit 514.

[0096] In another embodiment, an individual may input a close command to the master control device 501 via the user interface 518. The master bin control unit 514 receives the close command and transmits a close control signal to one or more of the bin assemblies 502 based on the close command input to the master control device 501.

[0097] The luggage box assembly 502 receives a close control signal from the master luggage box control unit 514 via the communication device 510. In response to the received control signal, the luggage box control unit 508 automatically closes the luggage box assembly 502. For example, the luggage box assembly 502 may control the actuator 520 to automatically close the luggage box assembly 502 upon receiving the command.

[0098] In at least one embodiment, the master baggage bin control unit 514 may be programmed to automatically lock, unlock, open, and close the baggage bin assembly 502. For example, the master baggage bin control unit 514 may communicate with a flight computer and operate the master baggage bin control unit 514 based on various phases of travel (such as takeoff, landing, periods of turbulence, taxiing, parking at a gate, etc.).

[0099] The master luggage box control unit 514 and / or luggage box control unit 508 may be programmed with control sequences for all or some of the functions described herein, including choreographed box opening / closing and automatic locking of boxes during certain parts of the trip. For example, the master luggage box control unit 514 may operate to simultaneously open and / or close all of the luggage box assemblies 502 on board the transport. In at least one other embodiment, the master luggage box control unit may operate to open and / or close in a synchronized and / or alternating manner. In this manner, all of the luggage box assemblies 502 may not be closed or opened at the same time, which may consume increased amounts of energy and / or generate increased amounts of noise. In at least one embodiment, the master control device 501 and / or luggage box assemblies 502 are programmed to open and close in a wave-like motion, which may or may not be synchronized with cabin lighting, sound schemes, etc. For example, the luggage box assembly 502 may open and close in conjunction with lighting effects emitted by interior cabin lights, audio signals emitted by interior speakers, and / or moving images or graphics displayed on one or more monitors or displays within the interior cabin. Additionally, preprogrammed control sequences ensure compliance with safety and security requirements promulgated by the U.S. Federal Aviation Administration (FAA).

[0100] In at least one embodiment, the system 500 defaults to a manual override mode that allows a user to manually open and close the box. For example, if the master box control unit 514 receives an error signal from one or more of the box control units 508, the master box control unit 514 may set the box assembly 502 to the default mode.

[0101] The luggage box control unit 508 of each luggage box assembly 502 may be configured to report information to the master luggage box control unit 514 to indicate a health or status, such as a box's capacity status, maintenance needs, and / or utilization data that may speed up loading and unloading procedures. For example, the luggage box control unit 508 may monitor the luggage box assemblies 502 and output a report signal to the master luggage box control unit 514. The report signal includes data regarding the operational health or status of the luggage box assembly 502.

[0102] As used herein, terms such as "controller," "device," "central processing unit," "CPU," "computer," and the like, may include any processor-based or microprocessor-based system, including systems using microcontrollers, reduced instruction set computers (RISC), application specific integrated circuits (ASICs), logic circuits, and any other circuits or processors, including hardware, software, or combinations thereof, capable of performing the functions described herein. The above examples are illustrative only, and thus are not intended to limit in any way the definition and / or meaning of such terms. For example, master bin control unit 514 and bin control unit 508 may be or include one or more processors configured to control operations as described herein.

[0103] Each of the master bin control unit 514 and the bin control unit 508 is configured to execute a set of instructions stored in one or more data storage units or elements (such as one or more memories) to process data. For example, each of the master bin control unit 514 and the bin control unit 508 may include or be connected to one or more memories. The data storage units may also store data or other information as desired or needed. The data storage units may take the form of an information source or a physical memory element within a processing machine.

[0104] The set of instructions may include various commands that instruct each of the master bin control unit 514 and the bin control unit 508 to perform certain operations as processing machines, such as the methods and processes of various embodiments of the subject matter described herein. The set of instructions may take the form of a software program. The software may be in various forms such as system software or application software. Further, the software may take the form of a collection of separate programs, a subset of a program within a larger program, or a portion of a program. The software may also include modular programming in the form of object oriented programming. The processing of input data by the processing machine may be in response to user commands, or in response to results of previous processing, or in response to a request made by another processing machine.

[0105] The diagrams of the embodiments herein may show one or more control or processing units, such as the master bin control unit 514 and the bin control unit 508. It should be understood that the processing or control units represent circuitry that may be implemented as hardware, or portions thereof, including associated instructions (e.g., software stored in a tangible and non-transitory computer-readable storage medium, such as a computer hard drive, ROM, RAM, etc.) to perform the operations described herein. The hardware may include state machine circuitry hardwired to perform the functions described herein. Optionally, the hardware may include electronic circuitry including and / or connected to one or more logic-based devices, such as a microprocessor, processor, controller, etc. Optionally, each of the master bin control unit 514 and the bin control unit 508 may represent processing circuitry, such as one or more of a field programmable gate array (FPGA), an application specific integrated circuit (ASIC), microprocessor(s), etc. The circuitry of various embodiments may be configured to execute one or more algorithms to perform the functions described herein. Such one or more algorithms, whether or not explicitly identified in a flowchart or method, may include aspects of the embodiments disclosed herein.

[0106] As used herein, the terms "software" and "firmware" are used interchangeably and include any computer program stored in a data storage unit (e.g., one or more memories) for execution by a computer. Data storage units include RAM memory, ROM memory, EPROM memory, EEPROM memory, and non-volatile RAM (NVRAM) memory. The types of data storage units listed above are merely exemplary and thus not limiting as to the types of memory that may be used for storage of computer programs.

[0107] Figure 10 illustrates a block diagram of a luggage box assembly 502, according to one embodiment of the disclosure. The luggage box assembly 502 is an example of the luggage box assembly described above in connection with Figures 1 through 9. The luggage box assembly 502 may or may not be communicatively connected to the master control device 501 shown in Figure 9.

[0108] In at least one embodiment, luggage box assembly 502 includes a proximity sensor 522 configured to detect the presence of an object within a vicinity, such as within a detection range of less than six inches. Proximity sensor 522 may be mounted on an exterior surface of luggage box assembly 502, such as on front panel 126 of bucket 120 (shown in FIG. 4). In at least one embodiment, proximity sensor 522 may be a radio frequency identification sensor and / or reader. Proximity sensor 522 may be mounted on luggage box assembly 502 in proximity to latch 506. In at least one embodiment, proximity sensor 522 contacts or forms a portion of latch 506.

[0109] In at least one embodiment, a flight crew member may place a badge, such as an RFID badge, within the detection range of the proximity sensor 522. The flight crew member may move the RFID badge within the proximity sensor 522 to set the latch 506 to a locked state, thereby preventing the luggage box assembly 502 from being opened. When in the locked state, one or more exterior light-emitting elements 524 (such as LEDs) that may be in proximity to or connected to the latch 506 may emit a light of a particular color indicating the locked state. For example, when a passenger attempts to open the luggage box assembly 502, such as by pressing the latch 506, the light-emitting element(s) 524 may emit a red light. In at least one other embodiment, the light-emitting element 524 may be disposed on a display and configured to emit light in a text pattern. For example, the light-emitting element 524 may be operative to show an illuminated "locked" message.

[0110] To allow the passenger to open the luggage box assembly 502, the flight attendant can again swipe the RFID badge near the proximity sensor 522 to return the latch 506 to the unlocked state. The exterior light-emitting element(s) 524 can then emit a light (such as a green light) or text (such as "Unlocked") to indicate that the luggage box assembly 502 is unlocked. Optionally, the luggage box assembly 502 may not include a proximity sensor 522.

[0111] In at least one embodiment, the luggage box assembly 502 may include a motion sensor 526 proximate to the latch 506. The motion sensor 526 may be connected to or attached to the latch 506. The motion sensor 526 is configured to detect motion within a detection range, such as within six inches of the latch 506. The motion sensor 526 may be an ultrasonic sensor, an infrared sensor, or the like.

[0112] In operation, the motion sensor 526 may be responsible for automatically opening the luggage box assembly 502 without an individual touching the latch 506 or another part of the luggage box assembly 502. For example, when an individual waves their hand within the detection range of the motion sensor 526, the motion sensor 526 sends an open signal to the luggage box control unit 508, the actuator 520, and / or the latch 506. The open signal causes the actuator 520 to open the luggage box assembly 502 without manual intervention. In at least one embodiment, when the luggage box assembly 502 is in the open state, if an object (such as a hand) passes within the detection range of the motion sensor 526, the actuator 520 automatically closes the luggage box assembly 502 without manual intervention. Optionally, the luggage box assembly 502 may not include the motion sensor 526.

[0113] In at least one embodiment, the luggage box assembly 502 may include one or more inner light-emitting elements 528, such as one or more LEDs. In at least one embodiment, the luggage box control unit 508 is configured to operate the inner light-emitting elements 528 (and / or the outer light-emitting elements 524). The inner light-emitting elements 528 may be within the luggage box assembly 502, such as within the luggage-holding compartment 144 shown in FIG. 5, secured to a strongback or the like. The inner light-emitting elements 528 are configured to illuminate the luggage-holding compartment 144. For example, when the luggage box assembly 502 is open, the inner light-emitting elements 528 may illuminate the interior of the open luggage box assembly 502. When the luggage box assembly 502 is closed, the light-emitting elements 528 are deactivated. The luggage box control unit 508 may be configured to operate the inner light-emitting elements 528 based on whether the luggage box assembly 502 is open or closed. In at least one other embodiment, the inner light-emitting element 528 may be controlled by a switch in communication with the actuator 520 and / or the latch 506 .

[0114] In at least one embodiment, the inner light emitting element 528 may emit light that gradually increases in intensity as the luggage box assembly 502 opens. Additionally, the inner light emitting element 528 may emit light that gradually attenuates and disappears as the luggage box assembly 502 closes. Optionally, the luggage box assembly 502 may not include the inner light emitting element(s) 528.

[0115] In at least one embodiment, the luggage box assembly 502 may include a box position sensor 530 in communication with the luggage box control unit 508, such as through one or more wired or wireless connections. The box position sensor 530 may be one or more of an accelerometer, an encoder, an angular position detector, a load sensor, a spatial integrator sensor, etc. configured to detect the position of the luggage box assembly 502 (such as whether it is closed or open). The luggage box control unit 508 receives one or more signals from the box position sensor 530 to determine the position of the luggage box assembly 502. A master control device 501 (shown in FIG. 9 ) may communicate with the luggage box control unit 508 to determine the position of the luggage box assembly 502 and other luggage box assemblies within the transporter. Optionally, the luggage box assembly 502 may not include the box position sensor 530.

[0116] In at least one embodiment, the luggage box assembly 502 may include a weight sensor 532, such as an electronic scale, communicatively coupled to the luggage box control unit 508, such as through one or more wired or wireless connections. The weight sensor 532 is configured to detect the weight of the luggage box assembly 502. The luggage box control unit 508 (and / or the master luggage box control unit 514 shown in FIG. 9) monitors the signals output by the weight sensor 532 and compares them to one or more weight thresholds stored in memory. For example, if the weight of the luggage box assembly 502 exceeds a maximum weight threshold (due to the amount of luggage in the luggage box assembly 502), the luggage box control unit 508 may output an alert, such as to the master control device 501 (shown in FIG. 9), indicating that at least some contents in the luggage box assembly 502 should be removed. In another embodiment, in response to the weight of luggage box assembly 502 being within a predetermined range of a maximum weight threshold, luggage box control unit 508 may operate actuator 520 to automatically close luggage box assembly 502 and operate latch 506 to a locked position.

[0117] In at least one embodiment, the weight sensor 522 is securely coupled to a portion of the luggage box assembly 502. For example, the weight sensor 522 may be attached to the front panel 126 (e.g., shown in FIG. 5 ), the end panels 132 and / or 134 (e.g., shown in FIG. 5 ). The weight sensor 522 may be securely attached to an inner or outer surface of the front panel 126, the end panels 132 and / or 134. In at least one embodiment, the weight sensor 522 may be embedded within a portion of the luggage box assembly 502, such as the front panel 126, the end panel 132, and / or the end panel 134.

[0118] In at least one embodiment, the luggage box assembly 502 may also include at least one touch sensor 534, such as a touch screen interface, a capacitance sensor, a sonic sensor, etc. The touch sensor 534 is communicatively coupled to one or both of the luggage box control unit 508 and / or the latch 506 and configured to be contacted (such as via pressing, swiping, etc.). When contacted, the touch sensor 534 transmits a signal to the luggage box control unit 508 and / or the latch 506 that selectively locks the latch 506, unlocks the latch 506, or opens the luggage box assembly 502.

[0119] Figure 11 illustrates a front view of a latch 506, according to one embodiment of the present disclosure. Figure 11 illustrates one implementation of the latch 506. However, the latch 506 may have a different size and shape than that shown in Figure 11. For example, the latch 350 shown in Figure 7 may be used.

[0120] The latch 507 may include an engagement button 507 secured within a frame or housing 509. A cover 511 and / or space above the engagement button 507 may include and / or cover a motion sensor 526, a proximity sensor 522, and / or an outer light emitting element(s) 524, as shown and described in connection with FIG. 10. In at least one embodiment, the light emitting element(s) 524 may be mounted within the engagement button 507.

[0121] 12 illustrates a circuit diagram of a luggage box control unit 508 connected to latch 506, according to one embodiment of the disclosure. Latch 506 may include or be otherwise connected to one or more latching mechanisms, such as latching mechanisms 600 and 602. For example, a luggage box assembly may include a left or front latching mechanism and a right or rear latching mechanism. Latching mechanisms 600 and 602 may include respective solenoids 604 and 606 connected to respective switches 608 and 610. Luggage box control unit 508 is configured to operate solenoids 604 and 606 to open the luggage box assembly based on an input command.

[0122] Luggage box control unit 508 may monitor signals received from latching mechanisms 600 and 602 to determine whether luggage box assembly 502 is in a desired position. For example, if luggage box assembly 502 should be in an open position but luggage box assembly 502 receives conflicting signals from latching mechanisms 600 and 602, luggage box control unit 508 may determine an error condition (such as a malfunctioning latching mechanism). Luggage box control unit 508 may output an error signal to master control device 501. The error signal may be indicated on luggage box assembly 502 (such as via exterior light-emitting elements 524).

[0123] 12 illustrates one example of a luggage box control unit 508 associated with the latch 506. The luggage box control unit 508 may be operatively connected to the latch in a variety of other ways. For example, the latch 506 may include only or be connected to a single latching mechanism. In at least one other embodiment, instead of or in addition to a solenoid, the latching mechanism may include a motor configured to open and close the luggage box assembly 502.

[0124] 9 and 13, the method begins at 700 where a master control device 501 is communicatively connected to a plurality of luggage box assemblies 502. For example, a master luggage box control unit 514 of the master control device 501 communicates with a luggage box control unit 508 of the luggage box assemblies, such as through a wireless connection.

[0125] Next, at 702, master control device 501 monitors the status of luggage box assembly 502. For example, master luggage box control unit 514 receives signals output from luggage box assembly 502 (e.g., via luggage box control unit 508) to determine whether latch 506 is locked or unlocked, whether luggage box assembly 502 is open or closed, etc., to determine the capacity of luggage box assembly 502, etc.

[0126] At 704, the master bin control unit 514 determines whether one or more of the bin assemblies 502 should be locked. For example, the flight crew may input a locking command to the master bin control unit 514, or the master bin control unit 514 may detect a condition (such as during a particular defined phase of flight) that triggers a locking command. At 706, if the bin assemblies should be locked, the master bin control unit 514 outputs a lock command signal that automatically locks one or more of the bin assemblies 502. The method then returns to 702.

[0127] However, if the bin assemblies 502 do not need to be actuated to a locked position (e.g., if they are already locked) or if the bin assemblies 502 do not need to be locked at 704, the method proceeds to 708, where the master bin control unit 514 determines whether the bin assemblies should be unlocked. For example, a flight crew may input an unlock command to the master bin control unit 514, or the master bin control unit 514 may detect a condition (such as the aircraft parking at the gate) that triggers an unlock command.

[0128] At 708, if any of the luggage box assemblies 502 are to be unlocked, the method proceeds to 710 where the master luggage box control unit 514 automatically unlocks one or more of the luggage box assemblies 502. The method then returns to 702.

[0129] At 708, if the luggage bin assemblies are already unlocked or do not need to be unlocked, the method proceeds to 712 where the master luggage bin control unit 514 determines whether the luggage bin assemblies 502 should be automatically opened, such as when the aircraft is parked at the gate. If the luggage bin assemblies 502 should be opened, the method proceeds to 714 where the master luggage bin control unit 514 automatically opens one or more of the luggage bin assemblies 502. The method then returns to 702.

[0130] At 712, if the luggage box assemblies are already open or do not need to be opened, the method proceeds to 716, where the master luggage box control unit 514 determines whether the luggage box assemblies 502 should be automatically closed, such as when the aircraft is taxiing to a runway for takeoff. If the luggage box assemblies 502 should be closed, the method proceeds to 718, where the master luggage box control unit 514 automatically closes one or more of the luggage box assemblies 502. The method then returns to 702. However, if the luggage box assemblies 502 should not be closed, the method returns to 702.

[0131] Steps 704, 708, 712, and 716 may occur in a different order than shown. For example, the master bin control unit 514 may analyze steps 704, 708, 712, and 716 simultaneously.

[0132] Furthermore, the present disclosure includes embodiments according to the following clauses: Clause 1 A luggage box assembly (502) within an interior passenger compartment (30) of a vehicle, comprising: A luggage box assembly (502) comprising one or more interior light-emitting elements configured to illuminate a luggage-holding compartment of said luggage box assembly (502). Clause 2 2. The luggage box assembly (502) of claim 1, wherein the one or more interior light emitting elements are disposed within the luggage holding compartment of the luggage box assembly (502). Clause 3 The luggage box assembly (502) of claim 1, wherein the one or more internal light-emitting elements are configured to illuminate the luggage holding compartment when the luggage box assembly (502) is in an open position, and the one or more internal light-emitting elements are deactivated when the luggage box assembly (502) is in a closed position. Clause 4 The luggage box assembly (502) of claim 1, wherein the one or more inner light-emitting elements emit light that gradually increases in intensity as the luggage box assembly (502) opens, and the one or more inner light-emitting elements emit light that gradually decreases in intensity as the luggage box assembly (502) closes. Clause 5 2. The luggage box assembly (502) of claim 1, further comprising a bucket having a front panel connected to a forward end panel and an aft end panel, wherein a luggage holding compartment is defined, at least in part, between said front panel, said forward end panel, and said aft end panel. Clause 6 6. The luggage box assembly (502) of claim 5, wherein the front panel comprises an arched panel having a curved outer surface. Clause 7 2. The luggage box assembly (502) of claim 1, further comprising one or more exterior light emitting elements. Clause 8 8. The luggage box assembly (502) of clause 7, wherein the one or more exterior light-emitting elements are configured to emit light indicative of a current status of the luggage box assembly (502). Clause 9 The luggage box assembly (502) of clause 1, further comprising a luggage box control unit in communication with the one or more interior light-emitting elements, the luggage box control unit (508) being configured to operate the one or more interior light-emitting elements. Clause 10 A method of operating a luggage box assembly (502) within an interior compartment (30) of a vehicle, comprising: illuminating a luggage-holding compartment of said luggage box assembly (502) with one or more interior light-emitting elements. Clause 11 11. The method of claim 10, wherein the one or more interior light-emitting elements are disposed within the luggage-holding compartment of the luggage box assembly (502). Clause 12 The illuminating illuminating the luggage compartment with the one or more interior light-emitting elements when the luggage box assembly (502) is in an open position; and 11. The method of claim 10, comprising deactivating the one or more interior light-emitting elements when the luggage box assembly (502) is in a closed position. Clause 13 The illuminating emitting a light that gradually increases in intensity as the luggage box assembly (502) is opened; and 11. The method of claim 10, comprising emitting a gradually attenuating light as the luggage box assembly (502) closes. Clause 14 11. The method of claim 10, further comprising emitting light from one or more exterior light-emitting elements secured to the luggage box assembly (502). Clause 15 15. The method of claim 14, wherein emitting light from the one or more exterior light-emitting elements includes emitting light indicative of a current status of the luggage box assembly (502). Clause 16 11. The method of claim 10, further comprising operating the one or more interior light-emitting elements using a luggage box control unit (508). Clause 17 Interior passenger compartment (30), and A vehicle comprising a plurality of luggage box assemblies (502) within said interior compartment (30), At least one of the plurality of luggage box assemblies (502) comprises one or more interior light-emitting elements configured to illuminate a luggage holding compartment of the at least one of the plurality of luggage box assemblies (502). Clause 18 18. The vehicle of claim 17, wherein the one or more interior light emitting elements are disposed within the luggage carrying compartment of the luggage box assembly (502). Clause 19 The transport vehicle described in clause 17, wherein the one or more interior light-emitting elements are configured to illuminate the luggage holding compartment when the at least one of the plurality of luggage box assemblies (502) is in an open position, and the one or more interior light-emitting elements are deactivated when the at least one of the plurality of luggage box assemblies (502) is in a closed position. Clause 20 The transporter described in clause 17, wherein the one or more inner light-emitting elements emit light that gradually increases in intensity as the at least one of the plurality of luggage box assemblies (502) opens, and the one or more inner light-emitting elements emit light that gradually decreases in intensity as the at least one of the plurality of luggage box assemblies (502) closes.

[0133] As discussed above, certain embodiments of the present disclosure provide a luggage box assembly that can be opened and closed without contact by an individual. Certain embodiments of the present disclosure provide a luggage box assembly that can be controlled by the flight crew. Certain embodiments of the present disclosure provide systems and methods that prevent passengers from opening the luggage box assembly during limited periods of flight, such as during takeoff, landing, and turbulence.

[0134] For purposes of describing the embodiments of the present disclosure, various spatial and directional terms may be used, such as top, bottom, lower, center, lateral, horizontal, vertical, front, etc., but it should be understood that such terms are used only relative to the orientation shown in the drawings. The orientation may be flipped, rotated, or otherwise changed so that top becomes bottom and bottom becomes top, horizontal becomes vertical, etc.

[0135] As used herein, a structure, limitation, or element that is "configured to" perform a task or process is structurally formed, configured, or adapted to specifically correspond to the task or process. For clarity and to avoid doubt, an object that is merely modifiable to perform a task or process is not "configured to" perform a task or process as used herein.

[0136] It should be understood that the above description is intended to be illustrative, not limiting. For example, the above-described embodiments (and / or aspects thereof) can be used in combination with each other. In addition, many modifications can be made to the teachings of the various embodiments of the present disclosure to adapt to a particular situation or material without departing from the scope of the various embodiments of the present disclosure. The geometries and types of materials described herein are intended to define the parameters of the various embodiments of the present disclosure, but these embodiments are exemplary rather than limiting. Many other embodiments will be apparent to those skilled in the art upon review of the present invention. The scope of the various embodiments of the present disclosure should be determined with reference to the appended claims, along with the full scope of equivalents to which such claims are entitled. In the appended claims, the words "including" and "in which" are used as obvious synonyms of the words "comprising" and "wherein," respectively. Additionally, the words "first," "second," "third," and the like are used merely as labels and are not intended to impose numerical requirements on their objects. Moreover, the following claim limitations are not written in means-plus-function format and are not to be construed under 35 U.S.C. 112(f) unless such claim limitations expressly use the phrase "means for" followed by a recitation of a function without further structure.

[0137] The description set forth herein uses examples to disclose various embodiments of the present disclosure, including the best mode, and to enable any person skilled in the art to practice various embodiments of the present disclosure, including making and using any device or system, and performing any methods incorporated therein. The patentable scope of the various embodiments of the present disclosure is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if the examples have structural elements that do not differ from the literal language of the claims, or if the examples include equivalent structural elements that differ only insignificantly from the literal language of the claims.

Claims

1. A luggage box assembly (502) within an interior passenger compartment (30) of a vehicle, comprising: a latch configured to selectively lock and unlock the luggage box assembly; a sensor in communication with the latch, the sensor being configured to participate in one or more of locking, unlocking, opening, or closing the luggage box assembly without the latch or the sensor being contacted; Strong Back; a bucket movably connected to the strongback, a luggage holding compartment defined, at least in part, by the bucket, the luggage holding compartment sized and configured to receive and hold carry-on baggage; and one or more internal light-emitting elements configured to illuminate the luggage compartment; the opening or closing of the luggage box assembly is synchronized with sound, graphics, and / or video; The luggage box assembly (502), wherein the sensor is a motion sensor configured to detect motion within a detection range.

2. 2. The luggage box assembly (502) of claim 1, wherein the one or more interior light emitting elements are disposed within the luggage holding compartment of the luggage box assembly (502).

3. 3. The luggage box assembly (502) of claim 1 or 2, wherein the one or more interior light-emitting elements are configured to illuminate the luggage holding compartment when the luggage box assembly (502) is in an open position, and the one or more interior light-emitting elements are deactivated when the luggage box assembly (502) is in a closed position.

4. 4. The luggage box assembly (502) of claim 1, wherein the one or more inner light-emitting elements emit light that gradually increases in intensity as the luggage box assembly (502) opens, and the one or more inner light-emitting elements emit light that gradually decreases in intensity as the luggage box assembly (502) closes.

5. 5. The luggage box assembly (502) of any one of claims 1 to 4, further comprising a bucket having a front panel connected to a forward end panel and an aft end panel, the luggage holding compartment being defined, at least in part, between the front panel, the forward end panel, and the aft end panel.

6. 6. The luggage box assembly (502) of claim 5, wherein said front panel comprises an arched panel having a curved outer surface.

7. The luggage box assembly (502) of any one of claims 1 to 6, further comprising one or more exterior light emitting elements.

8. 8. The luggage box assembly (502) of claim 7, wherein the one or more exterior light-emitting elements are configured to emit light indicative of a current status of the luggage box assembly (502).

9. 9. The luggage box assembly (502) of any one of claims 1 to 8, further comprising a luggage box control unit in communication with the one or more interior light-emitting elements, the luggage box control unit (508) configured to operate the one or more interior light-emitting elements.

10. A method of operating a luggage box assembly (502) within an interior passenger compartment (30) of a vehicle, comprising: illuminating a luggage carrying compartment of said luggage box assembly (502) with one or more interior light emitting elements; the luggage box assembly having a latch configured to selectively lock and unlock the luggage box assembly, a sensor in communication with the latch, the sensor configured to participate in one or more of locking, unlocking, opening, or closing the luggage box assembly without contacting the latch or the sensor, a strong back, and a bucket movably connected to the strong back, the luggage holding compartment being defined at least in part by the bucket, the luggage holding compartment being sized and configured to receive and hold carry-on baggage, and the opening or closing of the luggage box assembly being synchronized with audio, graphics, and / or video; The method, wherein the sensor is a motion sensor configured to detect motion within a detection range.

11. The method of claim 10, wherein the one or more interior light emitting elements are disposed within the luggage carrying compartment of the luggage box assembly (502).

12. The illuminating illuminating the luggage compartment with the one or more interior light-emitting elements when the luggage box assembly (502) is in an open position; and 12. The method of claim 10 or 11, comprising deactivating the one or more interior light-emitting elements when the luggage box assembly (502) is in a closed position.

13. The illuminating emitting a light that gradually increases in intensity as the luggage box assembly (502) is opened; and 13. The method of any one of claims 10 to 12, comprising emitting a light that gradually attenuates as the luggage box assembly (502) closes.

14. 14. The method of any one of claims 10 to 13, further comprising emitting light from one or more exterior light emitting elements secured to the luggage box assembly (502).

15. 15. The method of claim 14, wherein emitting light from the one or more exterior light-emitting elements comprises emitting light indicative of a current status of the luggage box assembly (502).

16. 16. The method of any one of claims 10 to 15, further comprising operating the one or more interior light-emitting elements using a luggage box control unit (508).

17. An interior passenger compartment (30); and A vehicle comprising a plurality of luggage box assemblies (502) within said interior passenger compartment (30), At least one of the plurality of luggage box assemblies (502) a latch configured to selectively lock and unlock the luggage box assembly; a sensor in communication with the latch, the sensor being configured to participate in one or more of locking, unlocking, opening, or closing the luggage box assembly without the latch or the sensor being contacted; Strong Back; a bucket movably connected to the strongback, a luggage holding compartment defined, at least in part, by the bucket, the luggage holding compartment sized and configured to receive and hold carry-on baggage; and one or more internal light emitting elements configured to illuminate the luggage compartment; the opening or closing of the luggage box assembly is synchronized with sound, graphics, and / or video; The vehicle, wherein the sensor is a motion sensor configured to detect motion within a detection range.

18. 20. The vehicle of claim 17, wherein the one or more interior light emitting elements are disposed within the luggage carrying compartment of the luggage box assembly (502).

19. 19. The transport vehicle of claim 17 or 18, wherein the one or more interior light-emitting elements are configured to illuminate the luggage holding compartment when the at least one of the plurality of luggage box assemblies (502) is in an open position, and the one or more interior light-emitting elements are deactivated when the at least one of the plurality of luggage box assemblies (502) is in a closed position.

20. 20. The transporter of any one of claims 17 to 19, wherein the one or more inner light-emitting elements emit light that gradually increases in intensity as the at least one of the plurality of luggage box assemblies (502) opens, and the one or more inner light-emitting elements emit light that gradually decreases in intensity as the at least one of the plurality of luggage box assemblies (502) closes.

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