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.

A group of seats for a passenger aircraft, which is configured as a rotating group of seats and by rotating the group of seats about the rotation axis a relocation of the position of the group of seats in relation to the initial position in the aircraft cabin is simultaneously achieved. The group of seats has a seat frame and at least one seat element. A support plate for fastening the group of seats to the aircraft structure is furthermore provided, the support plate having a rotating element which rotatably connects the support plate and the aircraft structure, the rotation axis of the rotating element being positioned in the region of the front half of the seat element, wherein the support plate is capable of being fastened to the aircraft structure by way of quick-release locks.

A seat configuration verification system and method for an internal cabin of a vehicle include a verification control unit that receives position data regarding positions of seat assemblies within the internal cabin. The verification control unit compares the position data with seat configuration data representative of the seat configuration to determine if the positions of the seat assemblies within the internal cabin conform to the seat configuration.

A passenger seating arrangement in an aircraft cabin, the passenger seating arrangement comprising exactly two rows of seat units and exactly one aisle, wherein a first row of seat units and a second row of seat units are separated by the aisle, and wherein the rows of seat units and the aisle all extend in a longitudinal direction parallel to a longitudinal axis of the aircraft cabin, each seat unit comprising a seat, an upper shell and a lower shell, the lower shell forming a footwell, wherein the seats are arranged in parallel to each other in a seating direction, wherein an upper shell of a first seat unit and a lower shell of a second seat unit, which, viewed in the longitudinal direction, is arranged behind the first seat unit, partially overlap in a vertical direction.

An aircraft passenger seating unit and aircraft seating arrangements including seating units, each seating unit configured as a window-facing seating unit or as an aisle-facing seating unit. Each individual seating unit including first and second laterally adjacent seats mounted on a common platform and oriented at an angle to a longitudinal aircraft axis. A forwardmost point of each of the first and second seats, when in an upright sitting position, resides along a plane common to both the first and second passenger seats perpendicular to the longitudinal aircraft axis to allow longitudinal alignment of rows and increased seating density.

The present invention relates to a console for a seat unit comprising: an upper wall forming a table surface on which a passenger can place objects, a cavity, an articulated arm fixed to an internal face of the cavity, said articulated arm comprising a holding device for a portable electronic device provided with a screen, said articulated arm being movable between a stored position, in which the articulated arm is located inside the cavity, and a extended position in which the articulated arm is at least in part outside the cavity.

Disclosed is an aircraft seat assembly provided as one continuous row generally including at least one passenger seat and a cabin attendant seat positioned at one end of the row, wherein the at least one passenger seat and the cabin attendant seat face in opposite directions. A transverse beam of the passenger seat frame portion of the assembly extends laterally outward to support a coupling assembly attached to the cabin attendant seat. In some cabin layouts, the aircraft seat assembly is positioned adjacent to a lateral passageway extending from a longitudinal aisle to an aircraft door such that the at least one passenger seat faces away from the lateral passageway and the cabin attendant seat faces toward the lateral passageway to position a seated cabin crew member with the passengers and proximate the aircraft door.

A passenger seat includes a seat frame, a plurality of legs extending down from the seat frame where each of the plurality of legs includes an upper end attached to the seat frame and a lower end, and at least one tube attached to the lower end of at least one of the plurality of legs. The at least one tube includes at least two attachments to a floor structure. The at least one tube includes at least one bent portion.

Child restraint system in a vehicle with features to support and ensconse the head and shoulders of an occupant during lateral impact to the vehicle.

An interior space for an aircraft includes a cockpit, a cockpit wall separating the cockpit from the remaining interior space, a cabin door arranged directly behind the cockpit wall for accessing the interior space of the aircraft from outside the fuselage, a modular installation space for installation equipment, a plurality of seat rows, a longitudinal aisle extending along the interior space through the seat rows to separate adjacent groups of seats from each other, and an access path for the cabin door. The access path extends from the cabin door to the longitudinal aisle to create an intersection region between the access path and the longitudinal aisle. The modular installation space is arranged directly forward of the seat rows. The access path extends at an angle of at least 100° to the longitudinal aisle in a forward direction.