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.

In a passenger seating arrangement in an aircraft cabin, the passenger seating arrangement has exactly two rows of seat units and exactly one aisle. A first row of seat units and a second row of seat units are separated by the aisle. 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 includes a seat, an upper shell and a lower shell, the lower shell forming a footwell. The seats are arranged in parallel to each other in a seating direction. 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.

A system and method for vehicle compartment item presence indication senses an item within a vehicle compartment and notifies a user if the item is expected or unexpected within the compartment based on a vehicle state. Should the item be expected in a compartment during a phase of flight where the compartment is expected to contain items, there is no abnormal indication. However, if a compartment is expected to be empty during a specific phase of flight and the sensors indicate an item is present, the system will alert the user to the unexpected item.

A bench seat assembly that includes a first seat that includes a seat portion and a back, a second seat that includes a seat portion and a back, and a center portion positioned between the first and second seats. The first seat is bifurcated by a first vertical plane, the second seat is bifurcated by a second vertical plane, and the center portion is bifurcated by a center vertical plane. The first seat is angled outwardly such that the first plane defines a first acute angle with the center plane and the second seat is angled outwardly such that the second plane defines a second acute angle with the center plane. The first acute angle and the second acute angle are approximately the same.

An aircraft seat for an aircraft passenger compartment suite is disclosed. In embodiments, the aircraft seat includes a primary section including a primary seatback portion and a primary seat base portion, and an auxiliary section including an auxiliary seatback portion and an auxiliary seat base portion. In embodiments, the aircraft seat may further include an actuatable element configured to actuate between an open position and a closed position. The actuatable element may include a first surface which defines at least a portion of the auxiliary seatback portion when the actuatable element is in the closed position, and a second surface which defines a surface of an armrest when the actuatable element is in the open position.

An aircraft seat for an aircraft passenger compartment suite may include a primary section with an upper actuatable portion and a lower actuatable portion. The primary section may be configured to actuate between a primary upright position and a primary lie-flat position. The aircraft seat may include an auxiliary section including an auxiliary seatback portion coupled to a privacy shell element of the aircraft passenger compartment suite and an auxiliary seat base portion configured to actuate between an auxiliary upright position and an auxiliary lie-flat position. The auxiliary seatback portion may include an actuatable element. The actuatable element may be configured to actuate between an open position and a closed position. The actuatable element may be configured to provide access to a stowage compartment when the actuatable element is in the open position.

The invention relates to an aircraft passenger seat comprising a support framework, the support framework being designed to be fastened to a floor in an aircraft passenger cabin, wherein the support framework has a seat divider and bars running transversely to the seating direction, the seat divider being supported by the bars. A housing comprises a structural component and the housing at least partly surrounds a backrest. According to the invention, the seat divider is connected to the structural component via a connecting device, the connecting device being designed as a plug-in connection.

A cabin of a vehicle for transporting passengers includes a plurality of units, each unit including a seat and a modular seat extension arranged staggered in the units. Each extension includes a shell having a front bottom and a rear opening determined by a hollow volume open towards the rear and a footrest area inside the hollow volume suitable for receiving the feet of a passenger. The shell of each extension includes an invariant portion and a modular portion located in front of the invariant portion. The modular portion making it possible during the fastening thereof to the invariant portion to obtain an extension with a length that can be modified between the opening and the bottom of the shell and, a width of passage towards the aisle between the seats and the extensions of the units is maintained constant during the use of the extensions by the passengers.

A seating module having a recessed grip for a vehicle, in particular an aircraft, and a seating arrangement that includes a seating module that has a recessed grip. The seating module includes a shell structure that defines the recessed grip in an upper area of the shell structure.

Described are consoles for use in a passenger seat row. The console may include a base of a support material. The base may include a top surface, a first side wall, and a second side wall opposite the first side wall. A tray may be configured to be releasably affixed to the top surface of the base. The tray be manufactured as a piece of molded plastic. The molded plastic may be molded to include one or more storage compartments. A bottom of the molded plastic may be configured to fittingly mate with the top surface of the base. The base may further include one or more straps configured to secure the base to a passenger seat cushion, passenger seat support structure, or a passenger seat restrain system. The one or more storage compartments may be a cupholder.