Patent application number | Description | Published |
20110084168 | REMOVABLE BACK SHELL FOR AN AIRCRAFT SEAT - 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. | 04-14-2011 |
20110084527 | AIRCRAFT SEAT CONTROL INPUT TRANSFER AND DISCONNECT MECHANISM - 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. | 04-14-2011 |
20130154329 | REMOVABLE BACK SHELL FOR AN AIRCRAFT SEAT - 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. | 06-20-2013 |
20130241256 | AIRCRAFT SEAT CONTROL INPUT TRANSFER AND DISCONNECT MECHANISM - 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. | 09-19-2013 |
20130328371 | REMOVABLE BACK SHELL FOR AN AIRCRAFT SEAT - 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. | 12-12-2013 |
20140239683 | AIRCRAFT SEAT ENERGY ABSORBING DEVICE FOR OCCUPANT RESTRAINT - 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. | 08-28-2014 |
20140265511 | DOUBLE SPRING LEG REST - 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. | 09-18-2014 |
20150158591 | REMOVABLE BACK SHELL FOR AN AIRCRAFT SEAT - 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. | 06-11-2015 |