Abstract: An aircraft tray table may include a body with a defined interior cavity, a personal electronic device support, and a magnification lens. The personal electronic device support may be configured to hold a personal electronic device when the personal electronic device support is in a support deployed position. The magnification lens may be configured to fit within the interior cavity when the magnification lens is in a lens stowed position. The magnification lens may include a lens configured to magnify content displayed on the personal electronic device held by the personal electronic device support when the magnification lens is in a lens deployed position. The personal electronic device support may be parallel to the magnification lens when the personal electronic device is in the support deployed position and the magnification lens is in the lens deployed position.

Abstract: A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.

Abstract: A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.

Abstract: A seatback cover attachment system is disclosed. The attachment system may include a substrate configured to reversibly couple to a portion of a seatback frame. The substrate may include one or more surfaces that define a channel. The channel may be configured to receive a portion of the seatback frame. The attachment system may include a seatback cover sub-system. The seatback cover sub-system may include a dress cover. The seatback cover sub-system may include a side panel configured to couple to a portion of the substrate. The side panel may be configured to couple to one or more portions of the dress cover to form the seatback cover sub-system.

Abstract: A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.

Abstract: A compressible cushion may include a base structure and a plurality of foam layers positioned on a seat pan of the aircraft seat. The plurality of foam layers may include a first foam layer stacked on the base structure, and at least a second foam layer stacked on the first foam layer. A density of the at least a second foam layer may be less than a density of the first foam layer. The first foam layer and the at least a second foam layer may be cut at a length corresponding to a length of the seat pan when in an extended position. The first foam layer and the at least a second foam layer each may include a plurality of cuts, which may be configured to compress when the seat pan actuates between the extended position and a retracted position.

Abstract: A system may include a surface, a pocket member, and spring members. The pocket member may have a top portion, a bottom portion, an exterior side, and an interior side. Each spring member may be positioned vertically between the surface and the interior side of the pocket member. Each spring member may have a spring top portion and a spring bottom portion. Each of the spring top portions may be attached to the top portion of the pocket member. Each of the spring bottom portions may be attached to the surface at a location corresponding to a vertical position of the bottom portion of the pocket member. The surface, the pocket member, and the spring members may form a pocket configured to at a given time be one of: open at the top portion of the pocket member, open at the bottom portion of the pocket member, or closed.

Abstract: A system may include a surface, a pocket member, and spring members. The pocket member may have a top portion, a bottom portion, an exterior side, and an interior side. Each spring member may be positioned vertically between the surface and the interior side of the pocket member. Each spring member may have a spring top portion and a spring bottom portion. Each of the spring top portions may be attached to the top portion of the pocket member. Each of the spring bottom portions may be attached to the surface at a location corresponding to a vertical position of the bottom portion of the pocket member. The surface, the pocket member, and the spring members may form a pocket configured to at a given time be one of: open at the top portion of the pocket member, open at the bottom portion of the pocket member, or closed.

Abstract: A dress cover installable over a seatback of a passenger seat and having an integrated adjustable lumbar support device is disclosed. In embodiments, the dress cover includes a fabric outer shell and a seat cushion within the outer shell. The lumbar support device is disposed inside a pocket set into the dress cover and corresponding to the lumbar area of the seat occupant. The pocket extends laterally between left-side and right-side slots, each slot held closed by a zipper within which a slider tracks up and down to adjust the lumbar support device. As the slider tracks along the zipper it opens and closes the zipper within the body of the slider, maintaining its slot in a closed configuration. By adjusting the sliders up or down, the occupant may adjust the position of the lumbar support device through the dress cover.

Abstract: A vertical seat blocking/divider device includes a seat back connector and a seat cushion connector. The vertical seat blocking/divider device is disposed on the center of an aircraft seat to block occupancy of the aircraft seat and establish a barrier between neighboring seats. In a further aspect, the vertical seat blocking/divider device includes a spring element to apply a force to the fabric of the seat blocking/divider device. In a further aspect, the vertical seat blocking/divider device may include armrest connectors on opposing surfaces so that the vertical seat blocking/divider device can be disposed between occupied seats to create a barrier between passengers.

Abstract: An aircraft seat may include a support system including a seat frame, a cushion including at least one surface configured to conform to a corresponding surface of the support system, a seat cover configured to fit over a portion of the cushion, and a seat cover attachment system configured to secure the seat cover to the seat frame. The seat cover attachment system may include a seat frame element of the seat frame. The seat cover attachment system may include a seat cover extrusion element configured to couple to the at least one seat frame element. The seat cover attachment system may include a seat cover retain element configured to couple to the seat cover extrusion element. A portion of the seat cover may be secured between the seat cover extrusion element and the seat cover retain element.

Abstract: An aircraft tray table may include a body with a defined interior cavity, a personal electronic device support, and a magnification lens. The personal electronic device support may be configured to hold a personal electronic device when the personal electronic device support is in a support deployed position. The magnification lens may be configured to fit within the interior cavity when the magnification lens is in a lens stowed position. The magnification lens may include a lens configured to magnify content displayed on the personal electronic device held by the personal electronic device support when the magnification lens is in a lens deployed position. The personal electronic device support may be parallel to the magnification lens when the personal electronic device is in the support deployed position and the magnification lens is in the lens deployed position.

Abstract: A seat unibeam may include a defined cavity, a hole in an end of the seat unibeam, and an exterior surface. The defined cavity may be dimensioned to receive an electronics package inserted within the seat unibeam. The electronics package may include a plurality of electronics package sections. The hole may lead to the defined cavity. Each of the plurality of electronics package sections may be inserted into the cavity defined in the seat unibeam via the hole in the end of the seat unibeam. The exterior surface may be dimensioned to pass through at least one hole in a plurality of seat legs. The exterior surface may be dimensioned to pass through at least one hole in a plurality of spreaders including adjacent spreaders configured to support one or more components of an aircraft seat of the set of aircraft seats.