A method and apparatus for holding a book or other hand-held object is disclosed. The book holder comprises an encasement portion and a book holder support platform attached thereto. The book holder support platform may be vertically lowered or raised to fit the needs of the user. The encasement portion comprises material that easily stretches over or around a seatback or other substantially vertically upright support structure.

The present application relates to securing a mattress within an aircraft including a pliable enclosure configured for enclosing a cushion including a fastener system for providing access to an interior of the pliable enclosure when the fastener system is in an open state and for restraining the mattress when the fastener system is in a closed state and wherein the pliable enclosure has a top surface and a bottom surface and a strapping system affixed to the bottom surface wherein the strapping system includes a strap extension affixed to the strapping system wherein the strap extension is configured to be received by a retention clip secured to a bed support platform.

Disclosed is a flame protection fabric provided for vehicle cushions, in particular for aircraft cushions, the flame protection fabric including the following layers: at least one first abrasion-resistant layer as an abrasion layer including at least one textile material with high abrasion resistance of at least one fiber type, and at least one second layer as a barrier layer including at least one fibrous fleece of at least one flame-proof fiber type. The at least one abrasion layer is provided as a first layer on at least one side of the at least one barrier layer as a second layer.

A method and apparatus for holding a book or other hand-held object is disclosed. The book holder comprises an encasement portion and a book holder support platform attached thereto. The book holder support platform may be vertically lowered or raised to fit the needs of the user. The encasement portion comprises material that easily stretches over or around a seatback or other substantially vertically upright support structure.

A retention system for an aircraft seat dress cover defines a cable channel sewn around the periphery of a back portion. A cable in the cable channel is tightened to tighten the aircraft seat dress cover around an aircraft seat back. Adjustable buckles at terminals of the cable interlock and allow the cable to be tightened. A midpoint strap is disposed on opposing sides of the periphery to allow the aircraft seat dress cover to more fully conform to the structure of the aircraft seat.

A modular seatback cover attachment system is disclosed. The modular seatback cover attachment system may include one or more trim caps including one or more tabs configured to reversibly couple the one or more trim caps to one or more portions of a seatback frame. The one or more tabs may include at least one of one or more hook tabs or one or more panel tabs. The modular seatback cover attachment system may include an interlocking assembly configured to interlock the one or more trim caps when the one or more trim caps are coupled to the seatback frame. The modular seatback cover attachment system may include a fastening assembly configured to couple the one or more trim caps to a portion of the dress cover.

A seating module having a recessed grip for a vehicle, in particular an aircraft, and a seating arrangement that includes a seating module that has a recessed grip. The seating module includes a shell structure that defines the recessed grip in an upper area of the shell structure.

A passenger seat includes a spreader with one or more open slot. The slot may be positioned on a lateral side of the spreader and may receive a portion of a seat base of the passenger seat within the slot. In some aspects, the slot may be elongated, and an insertion opening for the slot is provided in a top side of the spreader.

An aircraft seat may include a backrest and a seat pan coupled to the backrest. The backrest may include a plurality of backrest panels. A set of backrest panels of the plurality of backrest panels may be coupled via a coil hinge. The coil hinge may include a first plurality of holes formed in a first backrest panel of the set of backrest panels. The coil hinge may include a second plurality of holes formed in a second backrest panel of the set of backrest panels. The coil hinge may include a coil spring wound through the first plurality of holes and the second plurality of holes. The first backrest panel and the second backrest panel may be configured to rotate about an axis through the coil hinge when the seat pan and the backrest actuate between a stowed position and a deployed position.

A seat control system of an air vehicle for urban air mobility (UAM)UAM is provided. When the air vehicle turns strongly to one side during rotor failure of the air vehicle for UAM, side pads and air cells prevent the head and the body of a passenger seated on a seat in the air vehicle from being sharply tilted to the one side. Additionally, air bags of the side pads prevent and cushion impact energy applied to the head of the passenger at the moment when the air vehicle lands on the ground.