A leg assembly for a passenger seat for a vehicle such as an aircraft includes a forward leg and an aft leg. The forward leg includes a top end and a bottom end opposite the top end, and the top end of the forward leg includes a forward aperture for receiving a first base frame tube of the passenger seat. The aft leg includes a top end, a bottom end, a forward side, and an aft side, and the top end of the aft leg includes an aft aperture for receiving a second base frame tube of the passenger seat. The forward side at the aft aperture of the aft leg may be a forward-most portion of the aft leg, and the aft leg is indirectly connected to the forward leg.

A rotorcraft seating assembly includes a seat base supporting a seat bucket, the seat base having left- and right-side panel portions. Each side panel portion has a linear bucket guide channel set into its inside face (including an upper portion for adjusting the seat bucket relative to the seat base for pilots of varying heights, and a lower portion for energy attenuation (EA) stroking in response to a crash event) and a bucket guide slot set into its outside face (including a linear upper portion corresponding to the range of adjustment of the seat bucket and a curved lower portion allowing the seat bucket to translate forward and away from the seat base during EA stroking). The curved outer bucket guide slot allows for the required EA stroking distance within a minimal vertical space between the seat bucket and the flight deck floor.

Described is a frame component for a passenger seat assembly. The frame includes a tubular frame component having a first portion and a second portion. The bent portion bends the frame at a non-zero angle within a plane. The tubular frame component includes a variable inner diameter such that the first portion of the tubular frame component has a first wall thickness and the bent portion of the tubular frame component has a second wall thickness that is different from the first wall thickness.

In-aircraft seats include plastic components having anti-microbial, metallic reinforcing fibers such as copper or silver. Copper or silver wires are embedded into the plastic at the time or molding to provide both structural reinforcement and anti-microbial properties. At the time of molding, copper or silver wires are disposed in a plastic mold prior to plastic application to ensure the metallic wires are generally disposed toward the surface of the molded part.

A seat back for an aircraft seat includes a first side wall, a second side wall and a support wall for supporting a passenger leaning against the seat back. The first side wall and the second side wall each include a front edge and a rear edge. At least part of the support wall is positioned adjacent the front edge of the first side wall and the second side wall. The first side wall and the second side wall each include an aperture for receiving a bolt and the support wall includes one or more shaped surfaces to allow (i) insertion of a bolt through the aperture in each of the side walls from a position which is between the first and second side walls and in front of the shaped surface, and (ii) adjustment of the or each bolt from the front of the seat back.

Seat assemblies (200) including structural components (212, 222, 232) made of foam are described. A seat sub-assembly (210, 220, 230) can include a frame (214, 224, 234) and a foam support (212, 222, 232). The foam support (212, 222, 232) can be coupled to the frame (214, 224, 234) for receiving a load on the seat sub-assembly (210, 220, 230), dissipating at least half of the load, and dispersing the load through the frame (214, 224, 234).

Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

Described are privacy screens and privacy assemblies for passenger seats including a frame defining a perimeter of the privacy screen and shaped to partially wrap around a portion of a passenger seat, a textile shell connected with and surrounding the frame, and a sound-absorbing layer positioned within the frame and surrounded by the textile shell for conferring physical, visual, and sound privacy for an occupant.

Vehicle seat assemblies including support structures having at least two supports parts coupled at an articulating joint and a pneumatic actuator system including at least one pneumatic chamber inflated and deflated to articulate the articulating joint to move one support part relative to the other or to synchronize movement of two support parts. Support structures can include a backrest coupled to a seat bottom or leg rest coupled to a seat bottom, wherein articulation of the joint causes movement of the backrest or leg rest along a non-hinged trajectory to change a sitting position of the support structure, change seat orientation, and generally improve seat comfort.

An upholstery cover retention assembly is disclosed. In embodiments, the upholstery cover retention assembly includes an upholstered article including an upholstered surface, a bezel including a bezel lip proximate to the upholstered article, and a retention flange disposed on a peripheral surface of the upholstered article. In embodiments, the upholstery cover retention assembly further includes a dress cover assembly including a dress cover configured to at least partially cover the upholstered surface of the upholstered article, and an assembled edge configured to be disposed within a groove formed between the peripheral surface of the upholstered article and the bezel. In embodiments, assembled edge is configured to be secured within the groove by engaging a lower engagement surface of the retention flange and a lower surface of the bezel lip with the assembled edge.