A passenger seat assembly includes a riser attached to an upper surface of a floor of the vehicle, a seat attached to an upper surface of the riser, and at least one shell portion attached to the upper surface of the riser. The riser includes at least one door for accessing an interior volume of the riser. At least a portion of the interior volume of the riser is a luggage storage volume.

A removable closure device for a space inside an aircraft includes: a frame comprising at least one upright said frame comprising at least one fixation interface including a structural element, a curtain assembly comprising a flexible curtain and at least one guiding device or ensuring a translational guiding of the flexible curtain with respect to the upright so that the flexible curtain s able to be moved in a direction of movement parallel to a longitudinal direction of the upright between a stowed position, in which the flexible curtain s released from the space, and a deployed position, in which the flexible curtain closes the space.

An aircraft seat device with at least one shell element, with at least one table unit, with at least one support device that is configured to obliquely connect the at least one table unit to the shell element at least in a stowage position, the support device comprising at least one rotational bearing unit, which is configured for pivoting the table unit between the stowage position and at least one intermediate position that is situated substantially in a horizontal plane, the support device comprising at least one linear bearing unit, which is configured for traversing the table unit between the intermediate position and at least one completely deployed usage position that is close to a seat.

Described are examples of a seating arrangement for an aircraft with a first seat in a first accommodation space and a second seat in a second accommodation space, wherein the first and second accommodation spaces are configured to share a common floor space at a floor level of the aircraft. One seating arrangement includes a divider screen located between the first and second accommodation spaces, moveable, by sliding in a direction along the common floor space, between a stowed position permitting passenger egress between the first and second accommodation spaces across the common floor space, and a deployed position preventing passenger egress between the first and second accommodation spaces across the common floor space.

An adjustable table assembly for use in a passenger cabin environment such as an aircraft passenger suite including a passenger seat. The table assembly includes a fixed rail assembly attached to a monument, a support column rotatably mounted on the rail assembly, and a table mounted on the support column, the table having a stowed position and deployed positions in a first direction generally toward the passenger seat from the stowed position. The table has a predetermined stowage orientation at which the support column and table are movable along the rail assembly in a second direction opposite the first direction to the stowed position, and the rail assembly prevents the table from moving into the stowed position when the table is rotated out of the predetermined stowage orientation.

An aircraft passenger compartment suite may include at least one single passenger compartment including at least one single aircraft seat. The at least one single aircraft seat may be configured to seat a single passenger. The aircraft passenger compartment suite may include a combined divan passenger compartment with a combined divan aircraft seat. The combined divan aircraft seat may be configured to seat at least one passenger. The combined divan aircraft seat may have a width greater than a width of the at least one single aircraft seat. The combined divan passenger compartment may include a stowage compartment configured to stow large passenger amenities in a substantially vertical orientation. The aircraft passenger compartment suite may include a privacy divider separating the combined divan passenger compartment and the at least one single passenger compartment.

The present invention relates essentially to an arrangement of individual seats intended to be installed in an aircraft cabin and characterised in that the first seat faces inwards in the direction of the axis of the aircraft cabin and the second seat faces outwards away from the axis of the aircraft cabin and in that at least a portion of the first seat and of the corresponding first footwell are capable of defining at least a portion of a first bed surface which faces outwards away from the axis of the aircraft cabin and in that at least a portion of the second seat and of the corresponding second footwell are capable of defining at least a portion of a second bed surface which faces inwards in the direction of the axis of the aircraft cabin.

A travel suite arrangement for an aircraft cabin, such as a business class cabin, including at least one longitudinal aisle dividing sections, with each section including at least one four-suite unit. Each four-suite unit generally includes an angled first seat positioned directly adjacent the longitudinal aisle forward-facing, a second angled seat positioned directly adjacent the longitudinal aisle rearward-facing, a third angled seat positioned apart from the longitudinal aisle, to one side of the first seat and rearward-facing, and a fourth angled seat positioned apart from the longitudinal aisle, to one side of the second seat and forward-facing. Aisle seats are accessed directly from the aisle while outboard seats share access passageways.

A variety of seats and seating arrangements are disclosed for use in transport vehicles such as airliners. The seats can have specific features and/or be arranged at specific angles adjacent to each other to combine high capacity with passenger comfort and safety.

The present invention provides a divider screen assembly for an aircraft seating arrangement, the divider screen assembly comprising a divider screen moveable between a lower height in a stowed configuration, and an upper height in a deployed configuration, a first actuation mechanism being actuable to allow movement of the divider screen between the upper height and an intermediate height in between the upper height and the lower height, a second actuation mechanism being actuable to allow movement of the divider screen between the intermediate height and the lower height, wherein the second actuation mechanism is actuable only when the screen has been lowered to the intermediate height. The present invention also provides an aircraft accommodation arrangement, a method of stowing a divider screen and a method of deploying a divider screen.