A modular bar made of bar modules includes a bar element and one or more seating elements pivotably attached to the bar element. The seating element(s) is moveable relative to the bar element between a stowed position and a seat position, the module configured to be arranged adjacent one or more other bar modules to form a bar.

The present disclosure provides a swivel stop comprising a rotating member, a first boss coupled to the rotating member and a second boss coupled to the rotating member, and a second plate having a first interference surface and a second interference surface. An interference between the first boss and the first interference surface and the second boss and the second interference surface tends to limit the rotation of the rotating member with respect to the second plate. The swivel stop may further comprise a rail wherein the second plate is configured to translate along the rail.

An aircraft passenger seat construction capable of in-flight rocking motion and berthing, wherein rocking motion and berthing are mutually exclusive features. The seat construction includes a fixed frame including spaced frame members each having a support surface to be rocked on, a rocking frame including a seat pan and spaced rockers, the spaced rockers positioned to rock on the support surfaces, guides carried on the spaced rockers engaged to travel within guide slots of the spaced frame members, a backrest pivotally attached to the rocking frame, and a leg rest pivotally attached to the rocking frame. The rocking frame may rock back-and-forth in-flight or may be locked at any given position based on passenger preference. The seat construction is compatible with or without other seat adjustment mechanisms such as tracking, swivel, lie-flat and recline adjustment mechanisms.

Described are crossbeam assemblies for installing a furnishing to a passenger compartment. The crossbeam assemblies can include a first structural member configured to span two floor-mounted channels in a passenger compartment, and at least two attachment elements that are slidingly connected with the first structural member. The attachment elements are repositionable along the first structural member to mate with the floor-mounted channels, and lockable to retain the first structural member with respect to the two floor-mounted channels when the first structural member is attached.

An orientation assembly includes a platform and a locking assembly engageable with the platform and positionable in a first state in which the platform is permitted to rotate about a lateral axis and inhibited from rotating about a longitudinal axis perpendicular to the lateral axis, and a second state in which the platform is permitted to rotate about the longitudinal axis and inhibited from rotating about the lateral axis.

An orientation assembly includes a platform and a locking assembly engageable with the platform and positionable in a first state in which the platform is permitted to rotate about a lateral axis and inhibited from rotating about a longitudinal axis perpendicular to the lateral axis, and a second state in which the platform is permitted to rotate about the longitudinal axis and inhibited from rotating about the lateral axis.

An airplane seat device includes at least one functional unit that is configured at least for a locking, a controlling and/or a movement of at least one airplane seat element, wherein the functional unit includes at least one actuatable shape-memory element.

A plinth attachment system for attachment to at least one track includes: a first plate having a first side configured for mounting to a longitudinally extending track, and a first mounting feature for mounting a first structure; and a second plate having a first side configured for mounting to the track, and a second mounting feature for mounting a second structure. When mounted on the track, at least one interlinking feature of the first side of the first plate and at least one interlinking feature of the first side of the second plate interlock at the track, and, the first mounting feature and second mounting feature are aligned at essentially equivalent longitudinal positions.

Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating and/or luggage placement is not coordinated. Among other advantages, dynamically assigning the VTOL aircraft payloads can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.

A vehicle seat including: a seat back; a seat pan; and one or more side support elements is disclosed. Each side support element is moveable with respect to the seat back between: a stowed configuration, in which the side support element is stowed flush with, or is stowed within or behind the seat back; and a deployed configuration, in which the side support element extends outwardly from the seat back, generally in the same direction that the seat back faces, so as to offer support to the side of a vehicle user sitting in the vehicle seat. A row of two or more such vehicles seats is also disclosed, in which all of the seats of the row face in the same direction, and adjacent seats within the row are connected to each other.