Abstract: An apparatus for dynamically tilting a seatpan in an aircraft passenger seating assembly includes a seat frame, seatback, seat cushion, and cushion support structure (e.g., a seatpan), the seat cushion and seatpan together having a forward end and a rear end and together supporting a passenger occupying the seating assembly. Accelerometers may detect an inertial event such as a rapid deceleration that may cause the passenger to pitch forward; dynamic seatpan actuators (e.g., airbags or ballistic devices) connected to the accelerometers react to the inertial event by detonating, driving the seatpan and seat cushion upward. As a result, the head path of the passenger may be redirected upward, alleviating the risk of passenger injury and component damage. Additional airbags may react to the inertial event by tightening the passenger seatbelt.

Abstract: An aircraft passenger seat having a dynamic breakover assembly includes a seat bottom frame and a seat back pivotally-mounted to the seat bottom frame that allows the angle of the seat back relative to the seat bottom frame to be varied from an upright taxi takeoff and landing (TTOL) position to a reclined position. The seat may include a means for sensing acceleration corresponding to a force indicative of an abnormal event; and a breakover mechanism coupled to the seat bottom frame and the seat back in which the means for sensing acceleration is coupled to the breakover mechanism. The breakover mechanism can prevent movement of the seat back in a forward direction past the TTOL position during normal use, and permit forward movement of at least a portion of the seat back in the forward direction past the TTOL position upon activation by the means for sensing acceleration.

Abstract: In an illustrative embodiment, a seat is oriented at an oblique angle with respect to a centerline of an aircraft fuselage, the seat having an Aircraft Passenger Restraint System (APRS) with a pre-tensioner and integral retractable shoulder and seat belt webbing. In an illustrative example, the ARPS may be a three-point restraint to control a seat occupant's upper body, head and torso area. In some embodiments, the ARPS may further control the forces on the lower spine and torso. In some applications, the ARPS may operate to control the Head Injury Criteria (HIC) levels for the seat occupant's head, as well as the neck twist and upper spinal forces, to meet aircraft certification requirements imposed by the Federal Aviation Administration (FAA) and/or European Aviation Safety Agency (EASA). In response to a deceleration event, the ARPS may rapidly retract the belt webbing to substantially remove slack.

Abstract: An apparatus for dynamically tilting a seatpan in an aircraft passenger seating assembly includes a seat frame, seatback, seat cushion, and cushion support structure (e.g., a seatpan), the seat cushion and seatpan together having a forward end and a rear end and together supporting a passenger occupying the seating assembly. Accelerometers may detect an inertial event such as a rapid deceleration that may cause the passenger to pitch forward; dynamic seatpan actuators (e.g., airbags or ballistic devices) connected to the accelerometers react to the inertial event by detonating, driving the seatpan and seat cushion upward. As a result, the head path of the passenger may be redirected upward, alleviating the risk of passenger injury and component damage. Additional airbags may react to the inertial event by tightening the passenger seatbelt.

Abstract: An aircraft passenger seat having a dynamic breakover assembly includes a seat bottom frame and a seat back pivotally-mounted to the seat bottom frame that allows the angle of the seat back relative to the seat bottom frame to be varied from an upright taxi takeoff and landing (TTOL) position to a reclined position. The seat may include a means for sensing acceleration corresponding to a force indicative of an abnormal event; and a breakover mechanism coupled to the seat bottom frame and the seat back in which the means for sensing acceleration is coupled to the breakover mechanism. The breakover mechanism can prevent movement of the seat back in a forward direction past the TTOL position during normal use, and permit forward movement of at least a portion of the seat back in the forward direction past the TTOL position upon activation by the means for sensing acceleration.

Abstract: In an illustrative embodiment, a seat is oriented at an oblique angle with respect to a centerline of an aircraft fuselage, the seat having an Aircraft Passenger Restraint System (APRS) with a pre-tensioner and integral retractable shoulder and seat belt webbing. In an illustrative example, the ARPS may be a three-point restraint to control a seat occupant's upper body, head and torso area. In some embodiments, the ARPS may further control the forces on the lower spine and torso. In some applications, the ARPS may operate to control the Head Injury Criteria (HIC) levels for the seat occupant's head, as well as the neck twist and upper spinal forces, to meet aircraft certification requirements imposed by the Federal Aviation Administration (FAA) and/or European Aviation Safety Agency (EASA). In response to a deceleration event, the ARPS may rapidly retract the belt webbing to substantially remove slack.

Abstract: An aircraft passenger restraint and protection system including an aircraft seat mounted at an oblique angle to a direction of forward travel, a multi-point seat belt associated with the aircraft seat, and a structural mounted airbag located forward of the aircraft seat.

Abstract: A class divider for an aircraft passenger cabin is provided. The class divider includes a partition positioned immediately aft of a rear row of seats in a first predetermined class area of the aircraft cabin and an aft-facing panel having a width and height generally corresponding to a width and height of the rear row of seats. One or more passenger convenience features selected from the group of video monitors, tray tables, and magazine storage pockets are provided on the aft-facing panel for use by passengers seated immediately aft of the partition in a front row of a second predetermined class area of the aircraft cabin.

Abstract: A class divider for an aircraft passenger cabin is provided. The class divider includes a partition positioned immediately aft of a rear row of seats in a first predetermined class area of the aircraft cabin and an aft-facing panel having a width and height generally corresponding to a width and height of the rear row of seats. One or more passenger convenience features selected from the group of video monitors, tray tables, and magazine storage pockets are provided on the aft-facing panel for use by passengers seated immediately aft of the partition in a front row of a second predetermined class area of the aircraft cabin.

Abstract: A passenger seat for a vehicle includes a seat bottom and a seat back mounted to a frame. The passenger seat includes at least one storage feature. One of the storage features may be a storage unit positioned underneath the seat bottom which is moveable between a first position in which the unit is readily accessible by a seated passenger, and a second position in which the unit is held upright or against a lower side of the seat bottom to reduce the intrusion of the unit into the under-seat space. Another storage feature may be a recess formed in the upper part of the seat bottom. The recess is covered by a moveable lid which forms part of the seating surface when closed.

Abstract: A seat bottom assembly for a passenger seat includes a flexible support panel having a left portion and a separate right portion, and a structural support member underlying the support panel. The structural support member is selectively moveable between a first, forward position in which the seat bottom assembly has a nominal length in a longitudinal direction, and a second, rearward position in which a forward portion of the support panel folds downward over the structural support member such that at least a portion of the seat bottom assembly has an effective length less than the nominal length. The effective length of the left portion and the right portion of the seat bottom assembly can be independently varied.

Abstract: A seat bottom assembly for a passenger seat, includes a flexible component; and a structural support member underlying the flexible component. The support member is selectively moveable between a first, forward position in which the seat bottom has a nominal length in a longitudinal direction, and a second, rearward position in which a portion of the flexible component bends downward over the structural component such that at least a portion of the seat bottom assembly has an effective length less than the nominal length. The left and right sides of the seat bottom assembly may be independently varied in length.

Abstract: An aircraft passenger seat includes a laterally extending support beam, a seat bottom frame rotatably mounted on the beam, a seat back frame, and a recline bracket carried on the seat bottom frame for attaching the seat back frame to the seat bottom frame. The recline bracket has an arcuate slot for receiving a laterally extending pin carried on the seat back frame and a pivot is spaced from the arcuate slot such that the seat bottom frame rotates on the beam and the seat back frame pivots about the pivot when the pin moves within the arcuate slot. The pin is positioned at the lower end of an elongate extension of the seat back frame and the pivot is positioned at the upper end of the extension. The passenger seat moves between a full upright position and a fully reclined position as the pin moves within the slot.

Abstract: A frame assembly for vehicle passenger seat, including at least one leg unit, including a cantilevered transverse main beam carried by a fore and aft-extending seat leg for being mounted to the floor of the vehicle, a transversely extending front beam positioned forward of the seat leg, a backshell attached to and carried by the transverse main beam, a seat back carried on the backshell, and a seat bottom carried by a perimeter frame mounted on the backshell.

Abstract: A passenger seat for a vehicle includes a seat back; and a seat bottom, which may be mounted to a fixed backshell. The seat bottom is selectively configurable such that at least a portion of one side thereof is higher than at least a portion of the opposite side thereof, relative to a floor of said vehicle, so as to support a passenger who is seated on said seat bottom in a rotated position wherein one of said passenger's hips is higher than the other hip relative to said floor.

Abstract: A passenger seat assembly convertible between a two-seat configuration and a three-seat configuration, and including a seat assembly base and first, second and third seats for carrying respective seat bottom and seat back cushions, the first and third seats defining outboard seats and the second seat defining a center seat. First and second armrests are mounted between the first and third outboard seats on opposing sides of the center seat and are moveable between an upright use position and a retracted storage position above the seat bottom of the center seat. A tray table is mounted for movement between a raised retracted position wherein a bottom surface of the tray table defines at least a portion of the seat back of the center seat, and a lowered use position wherein the tray table resides above the seat bottom of the center seat to provide additional seating space and a tray table for the occupants of the outboard seats.

Abstract: A passenger seat assembly convertible between a two-seat configuration and a three-seat configuration, and including a seat assembly base and first, second and third seats for carrying respective seat bottom and seat back cushions, the first and third seats defining outboard seats and the second seat defining a center seat. First and second armrests are mounted between the first and third outboard seats on opposing sides of the center seat and are moveable between an upright use position and a retracted storage position above the seat bottom of the center seat. A tray table is mounted for movement between a raised retracted position wherein a bottom surface of the tray table defines at least a portion of the seat back of the center seat, and a lowered use position wherein the tray table resides above the seat bottom of the center seat to provide additional seating space and a tray table for the occupants of the outboard seats.