Safety restraint protection for aircraft occupants seated facing the side of the aircraft
View Patent ↗A restraint system ( 120, 120 a ) for protecting at least one aircraft occupant, the aircraft including a cabin having at least one seat ( 54, 56, 58 ) facing a longitudinal center line of the aircraft, the restraint system including a first airbag ( 162 ) inflatable from a stored position to an inflated position, the airbag when inflated being adjacent the seated occupant and located on a side of the occupant facing the front of the aircraft, the airbag reducing occupant movement toward the front of the aircraft and cushioning the occupant from any impact, the system also includes a mechanism ( 222, 240 ) to lessen movement of the lower legs of the occupant.
1. A restraint system ( 120 , 120 a ) on an aircraft for protecting at least one aircraft occupant, the aircraft including a cabin having at least one center facing seat ( 54 , 56 , 58 ) facing a longitudinal center line of the aircraft, the restraint system including a first airbag ( 160 , 162 , 164 ) inflatable from a stored position to an inflated position, the airbag when deployed and inflated being adjacent a forward facing side of the center facing seat to protect the seated occupant, the deployed and inflated airbag being located on a side of the occupant closer to the front of the aircraft, the airbag reducing occupant movement toward the front of the aircraft and cushioning the occupant from any impact.
2. The systems according to claim 1 wherein the center facing seat ( 54 , 56 , 58 ) has seating for one or more occupants, and the restraint system includes additional first airbags ( 160 , 162 , 164 ) between each forward facing side of each center facing seat to protect each seated occupant.
3. The system according to claim 1 including a second airbag inflatable from a stored position to an inflated position, the airbag when deployed and inflated being adjacent a rearward facing side of the center facing seat to protect the seated occupant, the deployed and inflated second airbag being located on a side of the occupant closer to facing the rear of the aircraft, the second airbag reducing occupant movement toward the rear of the aircraft and cushioning the occupant from any impact.
4. The system according to claim 1 wherein each first airbag, in its stored position is stored in one of a bulkhead ( 62 ), a permanent aircraft structure, a roof of the aircraft or a side of a seat back or an armrest of the center facing seat and configured to deploy therefrom.
5. The system according to claim 1 wherein each second airbag, in its stored position is stored in one of a bulkhead ( 62 ), permanent aircraft structure ( 64 ), roof ( 200 ) of the aircraft or a side of a seat back or an armrest of the center facing seat and configured to deploy therefrom.
6. The system according to claim 1 including a controller sensitive to an activation signal to activate the first or second airbag or both during an emergency which requires activation of the airbags.
7. The system according to claim 1 including a weight sensor installed in the seat to detect the presence of a seated occupant, the system configured not to activate an airbag or airbags associated with an unoccupied seat.
8. The system according to claim 1 including a 2-point seat belt system securable about the occupant's lower torso.
9. The system according to claim 1 including a 3-point seat belt system securable about the occupant's torso.
10. The system according to claim 1 including a leg protection ( 222 , 224 , 242 ) mechanism configured to deploy to reduce induced motion of the lower leg or tibia of the occupant in the event of a crash or accident.
11. The systems according to claim 10 wherein the leg protection mechanism includes one of an inflatable airbag ( 222 , 224 ) or movable piston ( 240 ).