Abstract: A reduced profile legrest system has a legrest frame having at least two opposing edges, a width, and a centerline being a point that is half of the width. Also, at least two linkage mechanisms can each deploy and retract the legrest frame. Each linkage mechanism can have a first end and a second end. The second ends of the linkage mechanisms are attached to the legrest frame, and are offset from at least one of the two opposing edges toward the centerline. The offset can be a distance between the second ends and is approximately 15% to approximately 50% of the width. The offset can also be a distance between the second end and the centerline and is greater than 0.0 and less than or equal to 0.70 of the first distance.

Abstract: An aircraft seat that includes a seat bottom frame having a back, a seat back frame pivotally connected to the back of the seat bottom frame, and a seat back shell. The seat back shell has at least a front panel, a back panel opposite the front panel, and at least two side panels disposed between the front and back panels which connects the front panel to the back panel. The combination of the front, back, and side panels form a gap to receive the entire seat back frame.

Abstract: A vehicle seat having a bottom frame, a seat back connected to the frame, and an armrest capable of upward and downward movement. The armrest includes a seat bracket connecting the armrest to the frame and a vertically variable adjustment mechanism. The mechanism has a control disposed in the armrest, a lock actuated to an engaged or disengaged position by the control, a rack disposed in a generally vertical direction, and a one-way bearing acting as pinion and having two rotational states. The first rotational state is a locked state where the lock is engaged and prevents the one-way bearing from rotating, preventing the rack and armrest from a downward movement. The second rotational state is a free state where the lock is in the engaged position and a force is applied in the upward direction, the one-way bearing can rotate, allowing the rack and armrest an upward movement.

Abstract: An aircraft seat that includes a seat bottom frame having a back, a seat back frame pivotally connected to the back of the seat bottom frame, and a seat back shell. The seat back shell has at least a front panel, a back panel opposite the front panel, and at least two side panels disposed between the front and back panels which connects the front panel to the back panel. The combination of the front, back, and side panels form a gap to receive the entire seat back frame.

Abstract: A reduced profile legrest system has a legrest frame having at least two opposing edges, a width, and a centerline being a point that is half of the width. Also, at least two linkage mechanisms can each deploy and retract the legrest frame. Each linkage mechanism can have a first end and a second end. The second ends of the linkage mechanisms are attached to the legrest frame, and are offset from at least one of the two opposing edges toward the centerline. The offset can be a distance between the second ends and is approximately 15% to approximately 50% of the width. The offset can also be a distance between the second end and the centerline and is greater than 0.0 and less than or equal to 0.70 of the first distance.

Abstract: A vehicle passenger seat swivel mechanism connected between a seat frame and a seat base secured to a vehicle body. The swivel assembly can include a swivel axis around which the seat frame rotates and a tracking axis, approximately perpendicular to the swivel axis, along which the seat frame can translate. A guide plate can be disposed on the seat base and has a guide plate rail. A guide follower can be disposed on the seat frame having an engagement surface engaging the guide plate rail. As the seat frame swivels around the swivel axis, the guide follower is displaced along the translation axis, which causes at least the seat frame to displace in the same direction along the translation axis, to at least a first or a second clearance distance from the swivel axis, and the guide plate and the guide follower do not overlap along the swivel axis.

Abstract: A vehicle passenger seat swivel mechanism connected between a seat frame and a seat base secured to a vehicle body. The swivel assembly can include a swivel axis around which the seat frame rotates and a tracking axis, approximately perpendicular to the swivel axis, along which the seat frame can translate. A guide plate can be disposed on the seat base and has a guide plate rail. A guide follower can be disposed on the seat frame having an engagement surface engaging the guide plate rail. As the seat frame swivels around the swivel axis, the guide follower is displaced along the translation axis, which causes at least the seat frame to displace in the same direction along the translation axis, to at least a first or a second clearance distance from the swivel axis, and the guide plate and the guide follower do not overlap along the swivel axis.

Abstract: A vehicle seat having a bottom frame, a seat back connected to the frame, and an armrest capable of upward and downward movement. The armrest includes a seat bracket connecting the armrest to the frame and a vertically variable adjustment mechanism. The mechanism has a control disposed in the armrest, a lock actuated to an engaged or disengaged position by the control, a rack disposed in a generally vertical direction, and a one-way bearing acting as pinion and having two rotational states. The first rotational state is a locked state where the lock is engaged and prevents the one-way bearing from rotating, preventing the rack and armrest from a downward movement. The second rotational state is a free state where the lock is in the engaged position and a force is applied in the upward direction, the one-way bearing can rotate, allowing the rack and armrest an upward movement.

Abstract: An aircraft seat that includes a seat bottom frame having a back, a seat back frame pivotally connected to the back of the seat bottom frame, and a seat back shell. The seat back shell has at least a front panel, a back panel opposite the front panel, and at least two side panels disposed between the front and back panels which connects the front panel to the back panel. The combination of the front, back, and side panels form a gap to receive the entire seat back frame.

Abstract: A vehicle seat can include a seat bottom frame having a front, a back opposite the front, and enclosing a volume. Pivotally connected to the back of the seat bottom frame can be a seat back frame and pivotally connected to the front of the seat bottom frame can be a seat leg rest. The seat leg rest has a length. Mounted in the volume of the seat frame are at least two leg rest springs which are connected to the leg rest. When the leg rest springs are actuated, the seat leg rest can be directly pivoted approximately and incrementally parallel with the seat bottom frame. The two leg rest springs are mounted a first distance apart and the first distance is less than half of the length of the leg rest.

Abstract: An energy absorbing device for a seat containing an occupant includes a seat frame with legs, a seat pan, and a back member. Attached to the seat is an energy absorbing device fixed to the back member of the seat frame. The energy absorbing device includes an engagement portion fixing the energy absorbing device to the seat frame and an energy absorbing extension having a fixed end integral with the engagement portion, and a protruding end extending toward the seat pan. The seat has a seat belt for the occupant and the belt is attached to a belt support device which extends parallel to the energy absorbing extension. When the occupant is using the seatbelt and the seat undergoes lateral forces, the energy absorbing extension undergoes deformation, and when the occupant is not using the seatbelt and the seat undergoes lateral forces, the energy absorbing extension does not undergo deformation.

Abstract: A vehicle seat can include a seat bottom frame having a front, a back opposite the front, and enclosing a volume. Pivotally connected to the back of the seat bottom frame can be a seat back frame and pivotally connected to the front of the seat bottom frame can be a seat leg rest. The seat leg rest has a length. Mounted in the volume of the seat frame are at least two leg rest springs which are connected to the leg rest. When the leg rest springs are actuated, the seat leg rest can be directly pivoted approximately and incrementally parallel with the seat bottom frame. The two leg rest springs are mounted a first distance apart and the first distance is less than half of the length of the leg rest.

Abstract: An energy absorbing device for a seat containing an occupant includes a seat frame with legs, a seat pan, and a back member. Attached to the seat is an energy absorbing device fixed to the back member of the seat frame. The energy absorbing device includes an engagement portion fixing the energy absorbing device to the seat frame and an energy absorbing extension having a fixed end integral with the engagement portion, and a protruding end extending toward the seat pan. The seat has a seat belt for the occupant and the belt is attached to a belt support device which extends parallel to the energy absorbing extension. When the occupant is using the seatbelt and the seat undergoes lateral forces, the energy absorbing extension undergoes deformation, and when the occupant is not using the seatbelt and the seat undergoes lateral forces, the energy absorbing extension does not undergo deformation.

Abstract: An aircraft seat that includes a seat bottom frame having a back, a seat back frame pivotally connected to the back of the seat bottom frame, and a seat back shell. The seat back shell has at least a front panel, a back panel opposite the front panel, and at least two side panels disposed between the front and back panels which connects the front panel to the back panel. The combination of the front, back, and side panels form a gap to receive the entire seat back frame.

Abstract: An aircraft seat includes a seat bottom frame, a seat translation and rotation mechanism attached to the seat bottom frame allowing translation and rotational movement of the seat bottom frame. An armrest is removably attached to the side of the seat bottom frame, and can be set to different positions relative to the seat bottom. The armrest has a seat control mounted to an outside of the armrest, and an input transfer mechanism disposed inside the armrest. The input transfer mechanism has an end engaged to the seat control, and a receiver end. The input transfer mechanism is cable-less. A couple shaft is engaged with the receiver end and engaged with the seat translation and rotation mechanism. When the seat control is actuated, the input transfer mechanism causes the seat translation and rotation mechanism to allow the seat bottom frame to at least one of translate and rotate.

Abstract: An aircraft seat that includes a seat bottom frame having a back, a seat back frame pivotally connected to the back of the seat bottom frame, and a seat back shell. The seat back shell has at least a front panel, a back panel opposite the front panel, and at least two side panels disposed between the front and back panels which connects the front panel to the back panel. The combination of the front, back, and side panels form a gap to receive the entire seat back frame.