An aircraft passenger seat construction capable of in-flight rocking motion and berthing, wherein rocking motion and berthing are mutually exclusive features. The seat construction includes a fixed frame including spaced frame members each having a support surface to be rocked on, a rocking frame including a seat pan and spaced rockers, the spaced rockers positioned to rock on the support surfaces, guides carried on the spaced rockers engaged to travel within guide slots of the spaced frame members, a backrest pivotally attached to the rocking frame, and a leg rest pivotally attached to the rocking frame. The rocking frame may rock back-and-forth in-flight or may be locked at any given position based on passenger preference. The seat construction is compatible with or without other seat adjustment mechanisms such as tracking, swivel, lie-flat and recline adjustment mechanisms.

A reversible seat assembly for use with an airplane. The reversible seat comprises a base assembly and a vertical assembly. The base assembly and the vertical assembly are connected to a support structure and are collectively disposable into and out of a first travel position, a second travel position, and a third travel position. In the first and second travel positions a user or passenger may assume a usual sitting position. In the third travel position the user may assume a reverse sitting position. The base assembly comprises a right segment and a left segment connected and rotationally movable to a central segment. The vertical assembly comprises a lower segment and an upper segment connected to and rotationally movable a middle segment. The reversible seat assembly may further comprise a back armrest connected to an opposite side of said middle segment and structure to provide support to the arms of the user.

A seat bottom assembly, movable between stowed and deployed configurations, includes a seat pan plate having a front side, a rear side, a left side, a right side, a top surface, and a bottom surface. The seat pan plate is configured to move between stowed and deployed positions. The assembly also includes a pair of beam braces configured to engage a seat frame of a seat; a pair of front links operationally connecting the beam braces and the seat pan plate; and a pair of rear links operationally connecting the beam braces and the seat pan plate. Each of the front links is disposed on an opposite side of the seat pan plate from the other front link; and each of the rear links is disposed on an opposite side of the seat pan plate from the other rear link. The assembly also includes a seat cushion having a first top portion, a second top portion, and a bottom portion. The bottom portion of the seat cushion is generally disposed on the top surface of the seat pan plate. The bottom portion of the seat cushion and the seat pan plate are equally inclined when the seat pan plate is in the stowed and deployed positions. The second top portion is generally horizontal when the seat bottom assembly is in the deployed configuration, and negatively inclined relative to horizontal when the seat bottom assembly is in the stowed configuration.

The invention relates to a seating system (10) for a passenger aircraft, comprising at least one aircraft seat (12) having at least one sensor device (24) which is configured to detect a seat load on the aircraft seat (12) by a passenger (22) sitting thereon, an evaluation device (32) which is configured to determine a recommendation for a change in a sitting posture depending on the detected seat load and a display device (36) which is configured to display the recommendation.

Furthermore, the invention relates to a method, a program product and a sleeping system for a passenger aircraft.

An aircraft cabin is provided. The aircraft cabin comprises a first seat unit and a second seat unit, the first and second seat units being in a first row of seat units and being separated by an aisle. The cabin comprises a partition movable between a stowed position and a deployed position in which the partition is positioned at least partially in the aisle between the first and second seat units thereby at least partially blocking the aisle. The cabin further comprises an item of furniture movable between a stowed position and a deployed position in which the item of furniture is positioned in the aisle between the first and second seat units.

In a first aspect, provided is a cushion for an aircraft seat including at least one cushion having an upper side and a lower side of at least one plastic foam; at least one sensor system, where at least one sensor system is arranged in a region of the cushion adjacent the bottom surface of the cushion; and at least one flame retardant fabric covering at least one side of the at least one cushion. In a second aspect, provided is a cushion for an aircraft seat including at least one pad made of at least one plastic; at least one stabilizing means embedded in the at least one plastic; and at least one sensor system arranged on the at least one stabilizing means.

An aircraft cabin is provided. The aircraft cabin comprises a first row of seat units extending across the cabin between a first outboard sidewall of the cabin and a second opposite outboard sidewall of the cabin, a first aisle extending along the cabin, and a second aisle extending along the cabin. The first row of seats units comprises a first seat unit, a second seat unit, a third seat unit and no further seat units. The first aisle is positioned adjacent the first outboard sidewall and separates the first outboard sidewall and the first seat unit, the second seat unit is positioned adjacent the first seat unit, and the third seat unit is spaced apart from the second seat unit by the second aisle, the third seat unit being positioned adjacent the second outboard sidewall. The first row of seat units further comprises a privacy screen movable between a stowed position and a deployed position in which the privacy screen provides a barrier at least partially partitioning the first seat unit and second seat unit.

In a first aspect, provided is a cushion for an aircraft seat including at least one cushion having an upper side and a lower side of at least one plastic foam; at least one sensor system, where at least one sensor system is arranged in a region of the cushion adjacent the bottom surface of the cushion; and at least one flame retardant fabric covering at least one side of the at least one cushion. In a second aspect, provided is a cushion for an aircraft seat including at least one pad made of at least one plastic; at least one stabilizing means embedded in the at least one plastic; and at least one sensor system arranged on the at least one stabilizing means.

A seat configured to support an occupant may include a urine-based power generator and an adjustable cushion. The urine-based power generator includes a urine accumulation reservoir configured to receive urine from the occupant, and the urine-based power generator is configured to provide power to the adjustable cushion. The seat may be an ejection seat, and the urine-based power generator and the adjustable cushion may be mounted to the seat such that the urine-based power generator and the adjustable cushion are configured to be ejected with the ejection seat.

A portable leg lift device for an airplane seat with a seat panel, a movable leg lift panel, a stationary panel, an inflatable chamber, an inflation tube, an outer foldable outer panel and a inner foldable panel. The outer foldable panel is attached to the seat panel and the movable leg lift panel. The inner foldable panel is attached to the stationary panel. The inner foldable panel is also attached to the outer foldable panel. The inflatable chamber is attached on its distal surface to the inner wall of the movable leg lift panel and on its proximal surface to the stationary panel. The seat panel rests on the surface of an airplane seat. The inflation chamber can be inflated thereby lifting the movable leg panel and raising the lower legs of a person sitting on the seat panel.