An aircraft monument for use in a cabin of an aircraft includes a monument assembly and a seat assembly. The monument assembly includes a frame having a plurality of walls defining a compartment. The plurality of walls include a first end wall having a forward section at a forward plane of the frame. The compartment is defined rearward of the forward section. The seat assembly is forward of the frame. The seat assembly has a shell configured to at least partially surround a passenger seat. The shell has a rear rearward of the forward plane of the frame.

An aircraft passenger accommodation unit is disclosed. The aircraft passenger accommodation unit comprises a seat, a wall, an ottoman, and a console. An access path comprising a width is defined between the wall and the ottoman, the access path providing passenger access to the seat. The ottoman is moveably mounted with respect to the console and moveable between an extended position and a retracted position to change the width of the access path, and the ottoman is at least partially received within the console when the ottoman is in the retracted position.

A set of consolidated electronics packages for staggered aircraft seats may include a first consolidated electronics package and a second consolidated electronics package. The first consolidated electronics package and a second consolidated electronics package may be installed within a primary passenger compartment. The first consolidated electronics package and the second consolidated electronics package may be configured to provide electrical connectivity to the primary passenger compartment and an auxiliary passenger compartment including an auxiliary aircraft seat. A primary aircraft seat and the auxiliary aircraft seat may be installed in a staggered configuration within an aircraft cabin including the primary passenger compartment and the auxiliary passenger compartment.

The invention relates to a seat arrangement, in particular for an aircraft cabin, including: at least one first column of seats extending on one side of an aisle, at least one second column of seats extending on an opposite side of the aisle, the seats of the second column being disposed staggered with respect to the seats of the first column, this arrangement including at least one door that can move between a stowed position and a deployed position in which the door closes an upper space located above a console of the first column, the upper space being defined, on the one hand, by a shell associated with the console and, on the other hand, by a shell associated with a front seat, a lower space extending between the front end of the console and the shell of the front seat being left free, the lower space communicating with the upper space in order to form an access passage between the aisle and
a seat of the second column when the door is in the stowed position.

The invention relates to a passenger module for a vehicle cabin, the passenger module comprising a first side element, a second side element, a front partition wall, and two seats arranged between the first side element and the second side element, wherein the first side element and the second side element extending parallel to each other; the seats are arranged substantially one behind another and facing substantially in a same direction; wherein the front partition wall is arranged between the seats and connects the first side element and the second side element.

The invention relates to a passenger module for a vehicle cabin, the passenger module comprising a first side element, a second side element; and two seats arranged between the first side element and the second side element.

A removable privacy panel assembly (100) for a passenger seat includes a center panel (101) with a width approximately equal to a width of the passenger seat and at least one side panel (103, 104) with a connection to the center panel (101) where the at least one side panel extends approximately perpendicular to the center panel. The removable privacy panel assembly includes a deployed configuration where the removable privacy panel assembly is attached to the passenger seat and an uninstalled configuration where the removable privacy panel assembly is detached from the passenger seat. In the deployed configuration, the center panel is approximately aligned with a seatback (11) of the passenger seat and the at least one side panel (103, 104) extends forward from the center panel (101) beyond a seating surface of the passenger seat. In the deployed configuration, the at least one side panel (103, 104) is disposed adjacent to a headrest (15) of the passenger seat.

A multifunctional seat arrangement for a passenger cabin of a vehicle includes at least one first seat and one second seat which is laterally arranged directly adjacent to the at least one first seat. The second seat is narrower than the first seat, and the second seat has a pivotable seat surface extension which is pivotable into different positions relative to the seat surface of the second seat. Support functions and a child seat function or baby carrier function may be achieved thereby.

A slanted aircraft seat privacy panel may include a body. The body may be defined by a contour line along at least a portion of a height of the body. The contour line may be a straight line slanted at an angle relative to a vertical line. The vertical line may be defined relative to a floor of the aircraft cabin. The contour line being slanted may generate increased shoulder space in the passenger compartment in the aircraft cabin. The increased shoulder space in the passenger compartment may use a portion of non-fully utilized space in an adjacent passenger compartment in the aircraft cabin. The passenger compartment and the adjacent passenger compartment may be offset relative to an aisle in the aircraft cabin. A portion of each of the passenger compartment and the adjacent passenger compartment may be formed by the slanted aircraft seat privacy panel.

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.