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 seat incorporating a path and follower mechanism for nonlinear deployment of a passenger leg rest is disclosed. The passenger seat incorporates lightweight tubular members linked to backrest linkages, the backrest linkages driven by a passenger occupying the seat, e.g., via a reclining motion of the seatback. The reclining motion drives the backrest linkages which in turn drive path followers through a curving path such that, as the path follower drives forward or backward, the leg rest deploys at a variable rate between undeployed and fully deployed configurations, consistently providing an optimally relaxing leg position at any point between.

A deployable ottoman extension fills the gap between the ottoman and fully reclined oblique aircraft seat. The deployable ottoman extension can pivot out from the ottoman about a pivot point and/or slide out along a rail. Alternatively, the ottoman extension may be hinged to the ottoman to deploy by flipping down. The deployable ottoman extension may include deployable support features that extend to the aircraft floor when deployed.

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.

Footrest assembly for a passenger seat having a saddle (22) and a post (16) pivotally coupled to a fastener (38) connected to the saddle. A ratcheting mechanism (86) with at least one tooth (88) is positioned on a first end (20) of the post and a pawl (90) is pivotally coupled to a pawl shaft (98) fixedly coupled to the saddle. A cam follower (96) is pivotally coupled to the fastener and positioned within a slot (106) formed in the end of the post in order to prevent the pawl from engaging with a tooth while pivoting in a direction of a fully deployed position of the assembly.

In various embodiments, a drive system with a motor rotary actuator driven linkage and an override system is provided. The override system may be a manually actuated override system that, in response to a power loss or outage, is configured to disengage one or more links of drive system 100 from the electric motor rotary actuator, allowing the disengaged link to be moved and/or repositioned. Moreover, drive system 100 and, more specifically, the override system may be configured to restore normal operation to the disengaged link in response to power being restored (i.e., by reengaging the link).

The invention relates to a seat assembly for a cabin of a means of transportation, having an aisle which is arranged in the longitudinal direction of the cabin, two mutually spaced cabin walls which are oriented parallel to the aisle at least in some regions and laterally delimit the cabin, two outer passenger seat regions which are separated from one another by the aisle and each of which adjoins one of the two cabin walls, wherein the outer passenger seat regions have at least one row of seats with a respective inner first seat module which faces the aisle, a central second seat module adjoining the first module, and an outer third seat module adjoining the respective cabin wall. Each of the seat modules has a seat and an ottoman paired with the seat or a foot rest at a distance from the respective seat, and the third seat module is offset to the second seat module in the longitudinal direction such that the seat of the third

The invention describes a passenger seat unit for an aircraft cabin, comprising a seat surface (10), a backrest (20) and a leg rest (30), and having: an upright configuration in which the backrest (20) and the leg rest (30) are in a first position, and a bed configuration in which the backrest (20) and the leg rest (30) are in a second position, the backrest (20), the seat surface (10) and the leg rest (30) forming a substantially plane and continuous surface,
characterised in that: the seat surface (10) is fixed, the backrest (20) is mounted mobile in rotation around a joint axis between the backrest and the seat surface (29), the leg rest (30) is mounted mobile in rotation around a joint axis between the leg rest and the seat surface (39).