The present invention relates to an assembly of individual seats intended to be installed in an aircraft cabin, the assembly comprising: —a first seat and a second seat, a central console arranged between the first seat and the second seat, the central console comprising a first foot area and a second foot area extending in two opposite directions, —a seat surface width of the first seat being smaller in a portion of the seat opposite the second foot area in relation to a width of a portion of the seat surface opposite the first foot area so as to increase a space between the seat surface of the first seat and the second foot area.

The invention relates to a passenger module (M) for a vehicle cabin (3), in particular an aircraft cabin, comprising two seats (1, 2) arranged between a first side element (FE) and a second side element (SE), wherein the first side element (FE) and the second side element (SE) extending parallel to each other, the seats (1, 2) are arranged substantially one behind another and facing substantially in a same direction, wherein a front seat (1) is positioned angled by a predefined first angle (α) around its vertical axis (sz) in a direction towards the first side element (FE), and
a rear seat (2) is positioned angled by a predefined second angle (β) around its vertical axis (sz′) in a direction towards the second side element (SE). Further, the invention relates to a passenger seating arrangement (PA) for a vehicle cabin (3).

The present application relates to securing a mattress within an aircraft including a pliable enclosure configured for enclosing a cushion including a fastener system for providing access to an interior of the pliable enclosure when the fastener system is in an open state and for restraining the mattress when the fastener system is in a closed state and wherein the pliable enclosure has a top surface and a bottom surface and a strapping system affixed to the bottom surface wherein the strapping system includes a strap extension affixed to the strapping system wherein the strap extension is configured to be received by a retention clip secured to a bed support platform.

An economy class (Y class) private suite includes a continuous seatback and a stowable aisle-side panel. The continuous seatback covers the gaps between seats of a 3-seat or 4-seat PAX and the stowable aisle-side panel slides to close off the PAX from the aisle when desirable. Each seat in the PAX includes an extension element to extend from the anterior surface of the seat cushion and establish a substantially flat surface including the seat cushions and extension elements. A separate padded element may be placed over the substantially flat surface. Each seatback cushion in the PAX is removable and reconfigurable as a reclining support or expanded armrest.

Child restraint system in a vehicle with features to support and ensconse the head and shoulders of an occupant during lateral impact to the vehicle.

Improved seating arrangements for a vehicle cabin of a passenger transport system, in particular of an aircraft are disclosed. Examples herein provide improved seating arrangements providing a high density of seats and increased PAX numbers while ensuring privacy, comfort and a direct aisle access to each passenger. For example, the seating arrangements provided herein are applicable to narrow body aircrafts and wide body aircrafts, in particular in view of business class solutions.

The present invention relates to a suite, in particular for an aircraft cabin, comprising: a seat, an ottoman, and a storage cupboard, the suite further comprising a movable table capable of assuming: a stowed state in which the movable table extends in a vertical plane, in which the movable table is arranged between the cupboard and the ottoman, and a deployed state in which the movable table extends in a horizontal plane.

The invention relates to an aircraft seat assembly (14a; 14b; 14c; 14d) comprising at least one aircraft seat device (46a; 46b; 46c; 46d) and at least one additional aircraft seat device (48a; 48b; 48c; 48d) which are arranged at least partly next to one another in at least one common column of seats (36a; 36b; 36c; 36d) and each of which can be adjusted between a sitting position and a lying position. According to the invention, the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) is oriented in the opposite direction to another lying direction (96a; 96b; 96c; 96d) of the at least one other aircraft seat device (48a; 48b; 48c; 48d).

The invention relates to a seat arrangement, in particular designed to be installed in an airplane cabin, comprising: at least one “front” seat and at least one “rear” seat, positioned one behind the other along a longitudinal axis of the airplane cabin and comprising respectively at least one seat that can pass from a “seating” position to a “bunk” position, a transverse passage arranged between the “front” seat and the “rear” seat to allow access to an aisle, characterized in that the seat arrangement comprises movable closure means that can at least partially close off the transverse passage when the closure means are deployed.

A vehicular seating suite configuration may include a plurality of vertically stacked seating suites configured to be positioned within a vehicle. Each seating suite may include an elongated generally horizontal seating surface angled away from a longitudinal axis of a vehicle and a generally vertical backrest portion adjacent to a proximal end of the elongated generally horizontal seating surface. The elongated generally horizontal seating surface and the generally vertical backrest portion may be configured to accommodate a person in a sitting position and the elongated generally horizontal seating surface may be configured to accommodate a person in a lying position.