A passenger furniture device for a passenger seat provided within a vehicle cabin, in particular an aircraft cabin, including at least a base element having at least an upper utility surface for a passenger, a removable section element which is mounted to one side of the base element, and a simple latch mechanism. In particular, the latch mechanism may be a simple plug-in and clip device. The latch mechanism is an easy to handle releasable attachment and fixation device to release the removable section from the base element, particularly only by crew and service members of the aircraft. The latch mechanism is provided on the base element and the section element such that the section element is detachably mounted to the base element via the latch mechanism.

Passenger seats having improved comfort emergency egress solutions for mini suites or other types of passenger seats that have a privacy screen, wall, or sliding door that divides the passenger seat from the aisle area or other common area. Specific embodiments find particular use on-board passenger transportation vehicles, such as aircraft, where comfort and privacy must be balanced with safety and federal regulations.

An aircraft seating group including first and second laterally-adjacent seats, a center console positioned between the seats, a rear privacy shell positioned behind the seats and forming part of the center console, a vertical partition extending forward from the rear privacy shell to divide the center console, and a deployable shelf positioned to one side of the vertical partition, the shelf configured to hold a tablet for viewing by a passenger facing the shelf.

Described are seating arrangements having at least one set of columns that include an aisle column of seating units positioned adjacent a wall column of seating units. The aisle column is positioned adjacent an aisle, and the wall column is positioned adjacent an exterior wall. Each seating unit has a bed position having a head end and a foot end, wherein at least a height-limited portion of the foot end is less than a delineating height that separates a lower portion of the aisle from a upper portion of the aisle. The seating units in the adjacent columns are longitudinally aligned and positioned adjacent one another, as well as being angled with respect to each other. The height-limited portion of the foot ends in the aisle column is positioned adjacent the aisle, and the height-limited portion of the foot ends in the wall column is positioned within a concave portion of the exterior wall.

In an illustrative embodiment of an aircraft cabin passenger seating arrangement, first and second adjacent passenger seats are positioned at different angles with reference to a longitudinal axis of an aircraft, and longitudinally offset from each other such that the first seat is positioned forward of the second seat by an amount less than a length of the second passenger seat when in the lie-flat position. The first and second adjacent passenger seats may be longitudinally offset from a third passenger seat separated from the second passenger seat by an aisle, the third passenger seat disposed proximate a fourth passenger seat, such that a row of passenger seats includes two staggered groups of passenger seating. The first passenger seat may be vertically offset from the second passenger seat.

A vertical take-off and landing (VTOL) aircraft provides transportation to users of a network system. The network system may include multiple aircraft or other types of vehicles to provide multi-model transportation. An aircraft may include a fuselage, a truss coupled to the fuselage, and multiple distributed electric propellers coupled to the truss. The distributed electric propellers may be positioned on at least two different planes. The fuselage may include a cabin having one or more seats for the passengers arranged in a configuration that has a compact footprint, provides legroom, provides visibility to surroundings of the aircraft, or facilitates convenient ingress or egress of passengers. The aircraft may open a port cabin door and starboard cabin door for simultaneous ingress or egress of passengers.

An aircraft passenger seating system comprises an array of floor panels (4) fixed within an aircraft cabin deck section (1), the floor panels (4) providing an array of discrete fixing means for removable attachment of a plurality of passenger seating units. The seating units may be of mutually different configurations each having a common footprint, such that the different configurations are interchangeable without having to re-arrange other seating units. The common footprint may be provided by a common size and shape of floor panel (4) or the floor panels (4) may provide a regular array of discrete fixing means such that the configurations may be positioned regardless of the position of the floor panels (4).

A passenger cabin of an aircraft includes a seat arrangement that includes a number of seat assemblies. The seat assemblies include a seat structure having a seat backrest forming a backrest surface the and a seat cushion element forming a seat surface, and a passenger space partition, which spatially partitions a passenger space of the seat and which at least partially surrounds the seat structure and leaves open an access to the seat structure. The seat cushion element is moveable between a comfort position, in which the seat cushion element projects further into the access in order to provide a larger seat surface, and an access position in which the seat cushion element does not project as far or does not project at all into the access in order to make possible a wider access.

Described are seating arrangements having at least one set of columns that include an aisle column of seating units positioned adjacent a wall column of seating units. The aisle column is positioned adjacent an aisle, and the wall column is positioned adjacent an exterior wall. Each seating unit has a bed position having a head end and a foot end, wherein at least a height-limited portion of the foot end is less than a delineating height that separates a lower portion of the aisle from a upper portion of the aisle. The seating units in the adjacent columns are longitudinally aligned and positioned adjacent one another, as well as being angled with respect to each other. The height-limited portion of the foot ends in the aisle column is positioned adjacent the aisle, and the height-limited portion of the foot ends in the wall column is positioned within a concave portion of the exterior wall.

A method of determining a seating arrangement for an aircraft cabin includes entering configuration parameters into a processor including a cabin width, a quantity of aisles, a minimum aisle width, and a quantity of columns of seats, wherein each seat is movable between a seated configuration and a bed configuration. The method additionally includes entering seat parameters describing the taper in seat width from a main portion to a footrest, and entering configuration rules wherein in at least one column of an inboard column set and/or an outboard column set, the seats are reversed in direction and/or are staggered. The method further includes determining, using the processor, a seating arrangement including a column quantity in each column set, and a seat direction and/or a stagger for each column in the seating arrangement that results in a maximum seat width at a main portion of the seats.