Abstract: A lighting assembly that includes an outer housing defining an outer housing axis, an inner housing defining an inner housing axis and a light member positioned in the inner housing. The outer housing includes a front surface having a front opening and an inner surface that defines an adjustment cavity having a truncated spherical shape. The inner housing has a truncated spherical shape and is at least partially received within the adjustment cavity. The inner housing defines a light recess therein and includes a front cover having an aperture defined therein. The front cover at least partially defines the light recess. The light member defines a light axis. The light axis and the inner housing axis are not co-axial and not parallel and form an angle therebetween. The inner housing is adjustable between a home position and a plurality of adjustment positions.

Abstract: A partition configured to be positioned within an aircraft. The partition includes a first divider wall having a first wall portion and a first divider assembly. The first divider assembly includes a first lighted member and first lighting for illuminating the first lighted member. The partition also includes a second divider wall that is spaced apart from the first divider wall. The second divider wall includes a second wall portion and a second divider assembly that includes a second lighted member and second lighting for illuminating the second lighted member.

Abstract: A partition configured to be positioned within an aircraft. The partition includes a first divider assembly that includes a first wall portion having a first jamb member secured to an inboard surface thereof and a first door hingedly connected to the first jamb member. The first jamb member includes first lighting that illuminates the first door, and the first door is movable between a stowed position and a deployed position. The partition also includes a second divider assembly that includes a second wall portion having a second jamb member secured to an inboard surface thereof and a second door hingedly connected to the second jamb member. The second jamb member includes second lighting that illuminates the second door, and the second door is movable between a stowed position and a deployed position. The second door is spaced apart from the first door.

Abstract: A graphics display module that includes a frame with a front portion and a rear portion that cooperate to secure a hated panel having a front surface and a rear surface therebetween. The front portion defines a central opening through which the front surface of the lighted panel can be viewed, The front portion and rear portion cooperate to define a channel that includes lighting disposed therein that is configured to back light the lighted panel.

Abstract: A lavatory monument assembly that includes an enclosure having at least a front wall and that defines an enclosure interior, and a divider wall that extends rearwardly from the front wall. The divider wall includes a divider door that is movable between closed and open positions. In the closed position the divider door divides the enclosure interior into a first lavatory interior and a second lavatory interior. The front wall includes a first and second lavatory doors that are each movable between closed and open positions and provide access to the first lavatory interior and second lavatory interiors respectively. The front wall also includes a vertically extending center post. The second lavatory door is hingedly connected to the center post, and the center post and the second lavatory door are slidable to a stowed position when the second lavatory door is in the open position.

Abstract: A modular monument assembly configured to be positioned in an aircraft that includes an enclosure that includes a first module and a second module, and a circulation system that is adapted to receive water from a water source. The circulation system includes a circulation line for circulating water, a water heater, a circulation pump, first and second faucets and first and second lines that are in fluid communication with the first and second faucets. The first faucet is positioned in the first module and the second faucet is positioned in the second module.

Abstract: A lounge assembly configured to be positioned in the interior of an aircraft. The lounge assembly includes a first seat shell configured to at least partially surround a passenger seat, and an overhead storage bin assembly. The overhead storage bin assembly includes first and second posts configured to be secured to a floor of the aircraft, and an overhead bin housing supported by the first and second posts. The overhead bin housing includes at least a first overhead storage bin that is positioned generally above the first seat shell.

Abstract: A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.

Abstract: A lounge assembly configured to be positioned in the interior of an aircraft. The lounge assembly includes a first seat shell configured to at least partially surround a passenger seat, and an overhead storage bin assembly. The overhead storage bin assembly includes first and second posts configured to be secured to a floor of the aircraft, and an overhead bin housing supported by the first and second posts. The overhead bin housing includes at least a first overhead storage bin that is positioned generally above the first seat shell.

Abstract: A galley monument assembly that is configured to be positioned in the interior of an aircraft. The galley monument assembly includes a lower storage section that is adapted to receive at least one trolley cart and that includes a vertically oriented rear wall and two opposing side walls. The lower storage section defines a first storage depth. The galley monument assembly also includes an upper storage section that defines a second storage depth. The second storage depth is deeper than the first storage depth.

Abstract: A lavatory monument assembly configured to be positioned in the interior of an aircraft that includes a first wall and a second wall that are generally parallel to one another, and the second wall is longer than the first wall. The lavatory monument assembly further includes a third wall and a fourth wall, and the third wall and the fourth wall generally are perpendicular to the first wall and the second wall, and the third wall and the fourth wall connect to the first wall and the second wall to form a lavatory interior. The first portion of the fourth wall generally is parallel to the third wall, and a second portion of the fourth wall angles inwardly along generally straight lines into the lavatory interior, such that the area in the lavatory interior proximate the first wall is less than the area proximate the second wall.

Abstract: A damping mechanism that includes a housing with an inner circumferential surface defined by an assembly outer race, an axle shaft that is rotatable with respect to the housing, and a transmission assembly operatively associated with the axle shaft and disposed within the housing. The transmission assembly includes an assembly intermediate race. A fluid space that includes fluid therein is defined between the assembly intermediate race and the inner circumferential surface of the assembly outer race. A vane is disposed between the assembly intermediate race and the inner circumferential surface of the assembly outer race. The vane includes a restriction space defined therein. When the axle shaft rotates in the first direction, the transmission assembly transmits rotation from the axle shaft to the vane, and when the axle shaft rotates in the second direction, the transmission assembly transmits less rotation to the first vane than when the axle shaft rotates in the first direction.

Abstract: A lavatory monument assembly configured to be positioned in the interior of an aircraft that includes first, second, third and fourth walls that cooperate to define a lavatory interior, a door positioned on one of the first, second, third and fourth walls that allows access to the lavatory interior, and a toilet positioned within the lavatory interior. The toilet defines a first vertical plane that bifurcates the toilet and is positioned such that the first vertical plane is not parallel to the first wall. At least the first wall is pivotal between a stowed position and an expanded position. When the first wall is in the stowed position, the first, second, third and fourth walls define a first lavatory footprint and when it is in the expanded position, the first, second, third and fourth walls define a second lavatory footprint. The second lavatory footprint has a greater area than the first lavatory footprint.

Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated, with the first side panel and the bucket, and a second pivot mechanism operatively associated, with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along and are rotatable about a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

Abstract: A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.

Abstract: A damping mechanism that includes a housing having fluid disposed therein and an inner circumferential surface, an axle shaft that is rotatable with respect to the housing, and a first vane having a distal end and being pivotally associated with the axle shaft. When the axle shaft rotates in a first direction, the first vane pivots to a deployed position, and when the axle shaft rotates in a second direction, the first vane pivots to a stowed position. A first clearance is defined between the distal end of the first vane and the inner circumferential surface of the housing when the first vane is in the deployed position, and a second clearance is defined between the distal end of the first vane and the inner circumferential surface of the housing when the first vane is in the stowed position. The second clearance is greater than the first clearance.

Abstract: A monument assembly configured to be positioned interior of an aircraft that includes a galley module, a first lavatory module and a second lavatory module. The module is positioned between the first and second lavatory modules, and the first lavatory module and the galley module share a first inboard dividing wall that includes at least a first non-vertical wall section.

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.