An aircraft seat may include a seat back coupled to a shell of one or more passenger compartment shell sections of a passenger compartment installed within an aircraft cabin. The aircraft seat may include a seat pan coupled to a floor of the aircraft cabin proximate to an ottoman installed within the passenger compartment. The seat back may be in contact with a surface of the seat pan when the aircraft seat is in a first position. The seat back may be separated from the surface of the seat pan when the aircraft seat is in a second position. The seat back may be configured to move independently of the seat pan when the aircraft seat transitions between the first position and the second position.

An aircraft seat includes an actuator and a movement transmission device. The transmission device includes a frame provided with an immobilizing portion and a drive shaft. The transmission device further includes a gear wheel provided with coupling teeth having inclined side walls and a sleeve with an immobilizing portion complementary to the immobilizing portion of the frame, and coupling teeth having inclined side walls. The transmission device also has an elastic member configured to push the sleeve. The stiffness of the elastic member and the inclination of the side walls of the coupling teeth of the gear wheel and sleeve are chosen such that, when a torque greater than a threshold torque is applied to the gear wheel, the sleeve slides on the drive shaft from a position of coupling the sleeve to the gear wheel to a position of immobilizing the sleeve relative to the frame.

A safety system includes a safety response device positioned proximal to an aircraft seat. The safety response device is operable to deploy thereby controlling the leg extension condition of legs of an occupant of the aircraft seat. A triggering system is operable to activate the safety response device when a deceleration is detected. The safety response device can be operable to maintain the legs of a seated occupant in an un-extended condition thereby protecting the legs from extending when a rapid deceleration occurs. The safety response device can be operable to transition the legs of a seated occupant from an un-extended condition to an extended condition at a predetermined rate. The safety response device can be, for example, and airbag or a kick plate. The device may automatically return to a stowed condition a predetermined time after deployment to permit egress from the seat and aircraft.

A passenger seat incorporating a path and follower mechanism for nonlinear deployment of a passenger leg rest is disclosed. The passenger seat incorporates lightweight tubular members linked to backrest linkages, the backrest linkages driven by a passenger occupying the seat, e.g., via a reclining motion of the seatback. The reclining motion drives the backrest linkages which in turn drive path followers through a curving path such that, as the path follower drives forward or backward, the leg rest deploys at a variable rate between undeployed and fully deployed configurations, consistently providing an optimally relaxing leg position at any point between.

A seat drivetrain assembly for an aircraft seat is disclosed. The assembly may include a seatback drivetrain sub-assembly configured to actuate a seatback frame of a seat frame of the aircraft seat between a first position and at least a second position. The assembly may include a seat pan drivetrain sub-assembly configured to actuate a seat pan frame of the seat frame of the aircraft seat between a first position and at least a second position. The assembly may include an actuator sub-assembly configured to cause one of the seatback drivetrain sub-assembly or the seat pan drivetrain sub-assembly to actuate one of the seatback frame or the seat pan frame of the aircraft seat between the first position and the at least second position.

A standee transit pod having a padded backrest supported by a vertically reclined roll bar and a rear brace bar. The backrest is reclined from vertical by about 8 degrees over a range of 5 to 15 degrees. Additionally there is a safety restraint apparatus for a standee, a platform, a lower rear portion of the brace, which is attached proximate to a mid rear edge of the platform therein providing a right rear open space and a left rear open space on the platform. Where, in a row of transit pods, every other transit pod is staggered rearward about half a length of the platform, therein creating adjoining right rear open spaces and left rear open spaces with the adjacent transit pods, therein providing an aisle for a passenger to walk past the row of the plurality of transit pods.

A configurable interior fixture for a vehicle includes a base assembly, a table assembly and an ottoman cushion. The base assembly is positionable between a lowered position and a raised position. The table assembly includes a center leaf section supported on the base assembly and a side leaf section that is moveable between a stowed position and a use position. The ottoman cushion includes a base frame with a cavity for receiving the table assembly and a cushion assembly attached to the base frame. The interior fixture may be configured as a foot rest by lowering the base assembly, folding the table assembly and attaching the ottoman cushion to the table assembly. The interior fixture may be configured as a table by raising the base assembly, detaching the ottoman cushion from the table assembly and the unfolding the table assembly into the use position.

Example lie-flat passenger seat configurations for transportation are described. A non-elevated passenger seat includes a seat base and a seatback pivotably connected to the sliding bar. The seat base may be opened upwardly or downwardly. The seatback may be opened sideway such that a space originally used for seat base and seatback is converted to a passage accessible by the passenger. An elevated-height passenger seat also includes a seat base, a seatback pivotably connected to the seat base, and a hinge at an upper portion of the seatback. The elevated-height passenger seat may rotate upwardly around the hinge. When the elevated-height passenger seat rotates upwardly, the elevated-height passenger seat transitions from a seating position to an elevated position with the seat base and the seatback forming a flat bed such that the passenger can lie flat on the flat bed formed by the seat base and the seatback.

A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.

An aircraft passenger compartment suite may include a privacy shell element proximate to an aircraft seat installed within the aircraft passenger compartment suite. The privacy shell element may include a first section configured to conform to a primary section of the aircraft seat, and a second section configured to conform to an auxiliary section of the aircraft seat. The privacy shell element may include a first profile configured to conform with the aircraft seat when the aircraft seat is in a first position, and a second profile configured to conform with the aircraft seat when the aircraft seat is in a second position. The second profile of the privacy shell element may be configured to occupy a greater amount of passenger aircraft living space surrounding the aircraft passenger compartment suite than an amount of passenger aircraft living space occupied by the first profile of the privacy shell element.