A vehicle seat having at least one seat shell, the seat shell having a frame with two spaced-apart frame units and a shell surface arrangement extending from one of the frame units to the other frame unit. The shell surface arrangement has a net-like structure having a first fiber-reinforced plastic, and the seat shell has at least one holding element connected to a corresponding receiving element for fastening the seat shell.

The application relates to a fire-resistant textile composite having an upper surface and a lower surface. The composite contains a nonwoven layer and a knit layer. The nonwoven layer has a first and second side and contains a nonwoven textile. The nonwoven textile contains a plurality of first fire-resistant fibers, where the first fire-resistant fibers are non-thermoplastic. The nonwoven layer forms the lower surface of the textile composite. The knit layer contains a knit textile having a first and second side and the second side of the knit layer is adjacent to the first side of the nonwoven layer. The knit textile contains a plurality of second fire-resistant yarns, where the second fire-resistant yarns are non-thermoplastic. At least a portion of the first fire-resistant fibers from the nonwoven layer extend through the first side of the knit layer and form the upper surface of the textile composite.

A dual-occupancy aircraft minisuite incorporating a modular multiple-egress door assembly is disclosed. In embodiments, the dual-occupancy minisuite can accommodate two passengers in enhanced privacy. Access to (and egress from) the minisuite is through the modular multiple-egress door assembly, which provides forward and rear (relative to the egress gap between) sets of outer, intermediate, and inner doors. The outer doors translate laterally along rails in the intermediate doors, and the intermediate doors likewise translate laterally along rails in the inner doors, to open the minisuite for passenger access or direct view (or to close the minisuite for enhanced privacy). The forward and rear sets of doors are proportioned such that when any forward or rear translating door is jammed in a closed position, the remaining egress gap is of sufficient width to provide a distinct and independent emergency egress path for each occupying passenger of at least minimum required width.

A wheelchair securement system includes a first anchoring mechanism and a second anchoring mechanism. The first anchoring mechanism includes a first bar, a first set of seat track anchors, and a first set of adjustable strap anchors. The first bar extends between the first set of seat track anchors and is secured thereto. The first set of adjustable strap anchors is secured to the first bar, and the first set of adjustable strap anchors is configured to be securable to a wheelchair. The second anchoring mechanism includes a second bar, a second set of seat track anchors, and a second set of adjustable strap anchors. The second bar extends between the second set of seat track anchors and is secured thereto. The second set of adjustable strap anchors is secured to the second bar, and the second set of adjustable strap anchors is configured to be securable to the wheelchair.

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.

A ventilation assembly comprises a number of fan systems configured to purify air and a number of air distribution assemblies. Each air distribution assembly of the number of air distribution assemblies is configured to be removably installed on a seatback of a passenger seat. Each air distribution assembly of the number of air distribution assemblies comprises a pair of air distribution vents, ductwork configured to receive air from at least one fan system of the number of fan systems and direct air to the pair of air distribution vents, and a seat attachment device configured to removably couple the pair of air distribution vents to the seatback such that each air distribution vent is situated on opposite sides of the seatback for providing purified air to a seated passenger.

An aerial workstation which comprises a seat having a sitting portion, a backrest that is connected by a first articulation that allows the backrest to pivot relative to the sitting portion, and an arm configured to position the seat in various positions and orientations in space as required. The aerial workstation makes it possible to be able to translate the seat in a cockpit in an introduction direction, and to make it pivot about a pivot axis that coincides with the direction of introduction within the cockpit.

An aircraft seat fastening assembly, due to the use of electroactive polymers, facilitates the compensation of tolerances and the fastening of aircraft seats in the passenger cabin of the aircraft. A fixing actuator contains the electroactive polymer and can be switched electrically between a fixed state, in which a movement of a fastening region is not possible, and a non-fixed state, in which a movement of the fastening region is possible in a vertical direction. The aircraft seats can thereby be displaced in a continuously variable manner along the aircraft seat fastening rail. The aircraft seats can also be locked in a fully automated manner, and possibly from a central location. It is also conceivable to individually control the aircraft seats and/or the group(s) of seats.

Described are passenger seats having a seat frame and a seat bottom slidingly and pivotally attached to the seat frame that, when the passenger seats are reclined, are configured to articulate forward from an upright configuration of the passenger seat to a second seat position corresponding to a reclined configuration of the passenger seat. The seat bottom can include an aft articulating mechanism that defines a declining first path in an aft-to-forward direction to cause the aft end of the seat bottom to drop when the seat bottom articulates forward; and a forward articulating mechanism connected with the seat bottom near a forward end of the seat bottom that defines a second path shaped to cause the forward end of the seat bottom to move upward when the seat bottom articulates forward, such that the seat bottom tilts aft in response to articulating forward when the passenger seat is reclined.

A system to manage the sleep and/or the well-being of a passenger/user of an aircraft includes a chair to be installed in a cabin of the aircraft and interaction devices to interact with the user. The system further includes a user terminal configured to receive data relating to characteristics of a user profile of the user, and a control/command module connected to the user terminal, interaction devices and a database storing information relating to characteristics of a flight of the aircraft. The command/control module being configured to pilot the interaction devices according to the data relating to characteristics of the user profile and characteristics of the flight of the aircraft.