A seat system for a passenger aircraft. The seat system includes a passenger seat frame (i) a plurality of spreader bars and (ii) a plurality of laterally extending spar tubes connecting the plurality of spreader bars to one another and at least one canted leg assembly connected to the seat frame for attachment to fixed, spaced apart attachment points on a supporting surface of the passenger aircraft. The canted leg assembly includes: (i) a front leg portion including a front joint clamp for receiving one of the plurality of laterally extending spar tubes in a non-perpendicular attachment point; and (ii) an aft leg portion including an aft joint clamp for receiving another one of the plurality of laterally extending spar tubes in a non-perpendicular attachment point, whereby the seat system is adapted to be laterally positioned and attached to provide different spaced apart passenger seating configurations. A seat back tray table may be attached to the back of the passenger seat frame.

A floor mounted aircraft seat seal frame includes a frame, displacing elements connecting the frame to the posterior of the seat, and fabric tensioning elements that keep a gap covering fabric connected to the posterior surface of the seat in tension around the frame. The frame displacing elements, which may be leaf springs, coil springs, or manually adjustable element, allow the frame to conform to a wall behind the seat, regardless of the tapering of the wall.

A seat skate assembly is configured to be secured to a fitting of a seat assembly. The seat skate assembly includes a pin-retaining guide including a plurality of pin cavities configured to receive and retain one or more pins of the fitting, one or more wheel couplers, and one or more wheel members rotatably coupled to the wheel coupler(s). The wheel member(s) allow the seat assembly to be moved.

A conventional passenger vehicle has a lower deck and an upper deck on both sides of its aisle to double its seating areas. Each deck has ceiling and seat heights about the same as that in sedans, and hence without substantially increasing the vehicle height. Both decks are divided into seating sections with partition walls, and in a seating section each deck contains only a row of power reclining seats. Each seat has a power footrest mounted separately on the partition wall in front of the seat for sitting comfort and forming a bed with the seat. The footrest can also be placed to higher elevations to use as a table for eating or working. The footrest is stored vertically to allow more leg room for the seat. In some section of the vehicle each seating section may mount two rows of sitting-only seats to increase the vehicle capacity.

Disclosed is an aircraft seat assembly provided as one continuous row generally including at least one passenger seat and a cabin attendant seat positioned at one end of the row, wherein the at least one passenger seat and the cabin attendant seat face in opposite directions. A transverse beam of the passenger seat frame portion of the assembly extends laterally outward to support a coupling assembly attached to the cabin attendant seat. In some cabin layouts, the aircraft seat assembly is positioned adjacent to a lateral passageway extending from a longitudinal aisle to an aircraft door such that the at least one passenger seat faces away from the lateral passageway and the cabin attendant seat faces toward the lateral passageway to position a seated cabin crew member with the passengers and proximate the aircraft door.

A passenger seat includes a seat frame, a plurality of legs extending down from the seat frame where each of the plurality of legs includes an upper end attached to the seat frame and a lower end, and at least one tube attached to the lower end of at least one of the plurality of legs. The at least one tube includes at least two attachments to a floor structure. The at least one tube includes at least one bent portion.

Described are passenger seats (102) having a seat bottom (122) connected to the seat frame (108) at a hinge (130) at an aft portion of the seat bottom (122), and having a release mechanism (132) operably connected with the seat bottom (122) that, when actuated by a user, cause the seat bottom (122) to be released from a locked configuration to an unlocked configuration, whereby the seat bottom (122) is free to rotate downward, independent of a seat back (142), about the hinge (130) to a tilted position in order to increase a range of available angles between the seat bottom (122) and seat back (130).

A passenger seat includes a bottom support to be connected to the aircraft floor, a seat pan frame, and a support structure interconnecting the seat pan frame to the bottom support. A front support member defines a frontmost portion of the support structure, and has a top end connected to a front end of the seat pan frame and a bottom end connected to the bottom support. The front end of the seat pan frame is forwardly offset from a front end of the bottom support and the top end of the front support member is forwardly offset from its bottom end such that an empty space is defined across a width of the seat between the seat pan frame and the floor, forwardly of the support structure, forwardly of the bottom support, and rearwardly of a vertical plane aligned with the front end of the seat pan frame.

A central frame assembly for a passenger seat of a vehicle includes a spreader member (201) and a lower frame member (101) comprising at least one clamp member (121) for securing the lower frame member (101) relative to the spreader member (201). The lower frame member (101) may include a vertical portion (102) with a forward lower attachment portion (102.1) and an aft portion (103) with an aft lower attachment portion (103.1). The spreader member (201) and the lower frame member (101) may be aligned such that a centerline of the spreader member (201) and a centerline of the lower frame member (101) are approximately coplanar.

Transformable seat assembly includes a seat support structure and a seat connected to the seat support structure with a first hinge having a first axis of rotation. A back support structure is connected to the seat support structure with the back support structure positioned on a back side portion of the seat support structure and the first hinge is positioned on an opposing front side portion of the seat support structure. A wall member having a first end portion connected to the back support structure with a second hinge having a second axis of rotation, wherein the seat is rotatable about the first axis of rotation from an occupant support position to a deployed position and the wall member is rotatable about the second axis of rotation from an overlying position with respect to the back support structure to the wall member extending away from the back support structure.