Abstract: Disclosed are embodiments of monuments for installation in an aircraft passenger cabin. Each monument is multi-use in that the monument serves to accommodate a wheelchair and provide at least one additional function. In embodiments, the monument includes an interior space dedicated for receiving and positioning a wheelchair in an unfolded state, for instance an occupied wheelchair during taxi-takeoff, and landing (TTOL) and during flight. In embodiments, the monuments include storage compartments, direct access to an exterior window, tray table assemblies, etc. In embodiments, the monuments are configured to be positioned adjacent to at least one aisle for accessibility, and to a seat row including a passenger seat reserved for a caregiver. The monuments disclosed herein enhance the travel experience for a passenger with reduced mobilities (PRM), as well as increase flexibility in cabin designs.

Abstract: A self-deploying counter for an aircraft monument is disclosed. In embodiments, the monument is installable adjacent to a cabin space within an aircraft passenger cabin (e.g., on either side of an exit door) and the self-deploying counter includes a partition door capable of being pivoted between a default closed position and an open position extending into the cabin space. The self-deploying counter has a horizontal top surface and an undersurface. When the partition door is deployed, the counter pivots in concert with the door's deployment, the fully deployed position corresponding to the open position of the partition door.

Abstract: An in-seat mini-bar assembly, apparatus and method of manufacture is provided. The assembly includes a housing that is insertable into a compartment of the seating module and includes a container with an interior cavity that is conductively cooled by thermo-electric elements of a micro-chiller unit mounted on a conductive rear plate that forms an exterior side of the container. A vent is configured proximate to a front section of the housing to receive outside air forward of the housing for channeling the outside air to a rear section of the housing using a duct attached to the vent at the front section. The duct is shaped for a fluidic intake of the outside air by a frontal flange having a wide cross-sectional area that is gradually tapered to a circular cross-sectional area to direct the airflow in a uniform manner.

Abstract: A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.

Abstract: An implementation of a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.

Abstract: A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.

Abstract: An aircraft interior structure may include a primary monument, an auxiliary monument, and a passenger seating section. The primary monument may include one or more storage compartments and a primary panel configured to actuate between a primary panel stowed position and a primary panel deployed position. The auxiliary monument may be spaced a select distance from the primary monument across a floor area of an aircraft cabin, and may include an auxiliary panel configured to actuate between an auxiliary panel stowed position and an auxiliary panel deployed position. The passenger seating section may include a footwell at least partially within the primary monument and proximate to the one or more storage compartments. The footwell may correspond to an aircraft seat. The aircraft seat may be configured to form a bed surface with at least a portion being within the footwell when the aircraft seat is in a lie-flat position.

Abstract: A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.

Abstract: A slim aircraft monument is installable in an aircraft cabin adjacent to an aisle and has an upper portion, a lower portion, and a middle portion between the upper and lower portions. The monument includes a storage compartment accessible from a first side and a door on an adjacent side, the door deployable into the adjacent aisle or cabin space to reveal folding interconnected panels also deployable into the cabin space. The interconnected panels unfold into a horizontal workspace and, beneath the workspace, a series of vertically stacked storage bays capable of accommodating storage drawers and a cart bay configured for temporary accommodation of a half-size galley cart.

Abstract: A hand drying system for an aircraft lavatory includes a hand blower tap with an inlet configured to connect to an aircraft environmental control system (ECS) to receive a flow of conditioned air from the ECS. A valve is operatively connected to the inlet to selectively block flow from the ECS and allow flow from the ECS through the hand blower tap.

Abstract: An aircraft interior structure for an aircraft cabin may include a main body with a plurality of walls, where at least one wall of the plurality of walls may be shared with an adjacent passenger suite including an aircraft seat. The passenger suite may be installed at an angle relative to an aisle of the aircraft cabin. The aircraft interior structure may include a cavity defined within the main body. The cavity may be a trapezoidal shape defined at least in part by the angle at which the passenger suite is installed in the aircraft cabin. The cavity may be configured to receive a plurality of galley carts. A length of each of the plurality of galley carts may be dependent on a depth of the cavity at respective locations in the trapezoidal shape.

Abstract: An aircraft lavatory complex incorporating lavatories accessible to passengers of reduced mobility (PRM) is disclosed. Left-side and right-side full service lavatory units are accessible via left-side and right-side lavatory access doors opening in opposing directions. The left-side and right-side full service lavatory units are separated by a common central partition repositionable by cabin crewmembers (but protected from independent repositioning by occupants of either lavatory unit) to enlarge either of the left-side or right-side lavatory units for enhanced PRM accessibility.

Abstract: A modular aft galley and lavatory complex is disclosed. The galley complex is situated aft of an aircraft passenger cabin and incorporates left-side, right-side, and aft galley structures together partially enclosing an interior workspace, the left-side and right-side galley structures separated by a center aisle. Each galley structure includes trolley bays capable of securing trolleys therewithin. Each trolley can be removed from its trolley bay into the interior workspace or central aisle for use in catering or service operations inflight. Each galley structure includes storage bays accessible from the interior workspace. Between the upper and lower portions are flat workdecks and galley insert bays capable of accepting ovens, chillers, beverage makers, and other galley insert devices. Either the left or right galley structure includes a lavatory complex adjacent to the passenger cabin, incorporating aft lavatory units and a galley extension housing additional storage and cart space.

Abstract: A female urinary relief device is disclosed. The device may include an intimate interface device (IID) configured to be positioned intimate with a user's body. The IID may include a tray including a raised perimeter forming a seal between the user's body and the tray. The IID may include a fluid cavity configured to capture fluid from the user's body. The IID may include a pad including a slot configured to provide an unobstructed route to the fluid cavity. The device may include a fluid removal system configured to remove the fluid from the fluid cavity and route the fluid to a storage device. The fluid removal system may include a suction sub-system configured to pull the fluid against gravity to remove the fluid from the fluid cavity. The fluid removal system may include discharge hoses configured to fluidically and mechanically couple the IID to the storage device.

Abstract: A slanted aircraft seat privacy panel may include a body. The body may be defined by a contour line along at least a portion of a height of the body. The contour line may be a straight line slanted at an angle relative to a vertical line. The vertical line may be defined relative to a floor of the aircraft cabin. The contour line being slanted may generate increased shoulder space in the passenger compartment in the aircraft cabin. The increased shoulder space in the passenger compartment may use a portion of non-fully utilized space in an adjacent passenger compartment in the aircraft cabin. The passenger compartment and the adjacent passenger compartment may be offset relative to an aisle in the aircraft cabin. A portion of each of the passenger compartment and the adjacent passenger compartment may be formed by the slanted aircraft seat privacy panel.

Abstract: A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.

Abstract: An aircraft interior structure may include a primary monument, an auxiliary monument, and a passenger seating section. The primary monument may include one or more storage compartments and a primary panel configured to actuate between a primary panel stowed position and a primary panel deployed position. The auxiliary monument may be spaced a select distance from the primary monument across a floor area of an aircraft cabin, and may include an auxiliary panel configured to actuate between an auxiliary panel stowed position and an auxiliary panel deployed position. The passenger seating section may include a footwell at least partially within the primary monument and proximate to the one or more storage compartments. The footwell may correspond to an aircraft seat. The aircraft seat may be configured to form a bed surface with at least a portion being within the footwell when the aircraft seat is in a lie-flat position.

Abstract: A slim aircraft monument is installable in an aircraft cabin adjacent to an aisle and has an upper portion, a lower portion, and a middle portion between the upper and lower portions. The monument includes a storage compartment accessible from a first side and a door on an adjacent side, the door deployable into the adjacent aisle or cabin space to reveal folding interconnected panels also deployable into the cabin space. The interconnected panels unfold into a horizontal workspace and, beneath the workspace, a series of vertically stacked storage bays capable of accommodating storage drawers and a cart bay configured for temporary accommodation of a half-size galley cart.

Abstract: A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.