Force absorbing shoulder belt assemblies especially useful for aircraft occupant seats
Force absorbing shoulder belt assemblies for vehicle seats, especially aircraft seats, are provided. The shoulder belt assemblies will include a box structure defining an interior space having an open rear end and adapted to being fixed to adjacent vehicle structure, a block of a compressible material positioned within the interior space of the box structure, a rear plate in pressing contact with the rear face of the block of compressible material, and an inertial reel assembly carried by the rear plate and including a shoulder web strap which extends through the rear plate, the block of compressible material and the box structure. When a deceleration force of predetermined magnitude is exerted on the shoulder web strap of the inertial reel, the rear plate will responsively be forcibly pressed against the block of compressible material thereby compressively crushing the compressible material within the box structure to thereby absorb shock force of the shoulder web strap against vehicle seat occupant's torso.
1. A force absorbing shoulder belt assembly for a vehicle seat comprising:
a box structure adapted to being fixed to adjacent vehicle structure, the box structure having an interior space and includes a forward side wall defining an elongate slot and an open rear end opposite the forward side wall;
a block of a compressible material positioned within the interior space of the box structure defining an elongate channel therethrough which is aligned with the elongate slot of the forward side wall of the box structure;
a rear plate in contact with a rear face of the block of compressible material at the open end of the box structure and defining an elongate passageway therethrough; and
an inertial reel assembly carried by the rear plate and including a shoulder web strap extending through the elongate passageway of the rear plate, the elongate channel of the block of compressible material and the elongate slot of the forward side wall of the box structure, wherein
a deceleration force of predetermined magnitude exerted on the shoulder web strap along a force vector causes the inertial reel to forcibly move the rear plate forwardly against the block of compressible material to compressively crush the compressible material within the box structure to thereby absorb shock force of the shoulder web strap against a torso of an occupant of the vehicle seat.
2. The force absorbing shoulder belt assembly according to claim 1 , wherein the block of compressible material comprises a block of compressible metal honeycomb.
3. The force absorbing shoulder belt assembly according to claim 2 , wherein the block of compressible metal honeycomb is an aluminum honeycomb.
4. The force absorbing shoulder belt assembly according to claim 3 , wherein the block of aluminum honeycomb comprises elongate cells that are aligned substantially with the force vector.
5. The force absorbing shoulder belt assembly according to claim 3 , wherein the elongate slot of the forward side wall includes opposed edges and elongate anti-chafing grommets operatively associated with the opposed edges.
6. The force absorbing shoulder belt assembly according to claim 1 , further comprising a pair of L-shaped press pads connected to the box structure and engaged with the rear plate so as to positionally restrain the rear plate within the box structure.
7. The force absorbing shoulder belt assembly according to claim 6 , wherein
the box structure includes a pair of opposed side walls each having a connection lobes, and wherein
the L-shaped press pads are connected to a respective connection lobe of the opposed side walls.
8. The force absorbing shoulder belt assembly according to claim 1 , wherein the rear plate includes a mounting arm projecting aftwardly away from the rear plate, and wherein the inertial reel assembly is connected to the mounting arm so as to be carried by the rear plate.
9. A vehicle seat which comprises the force absorbing shoulder belt assembly according to claim 1 .
10. The vehicle seat according to claim 9 , wherein the vehicle seat is an aircraft seat.
11. An aircraft seat comprising:
an aircraft seat assembly adapted to support a seated occupant therein; and
a force absorbing should belt assembly rigidly connected to adjacent aircraft structure; wherein the force absorbing shoulder belt assembly comprises:
(i) a box structure adapted to being fixed to adjacent vehicle structure which defines an interior space having a forward side wall having an elongate slot and an open rear end opposite the forward side wall;
(ii) a block of a compressible material positioned within the interior space of the box structure defining an elongate channel therethrough which is aligned with the elongate slot of the forward side wall of the box structure;
(iii) a rear plate in contact with a rear face of the block of compressible material at the open end of the box structure and defining an elongate passageway therethrough; and
(iv) an inertial reel assembly carried by the rear plate and including a shoulder web strap extending through the elongate passageway of the rear plate, the elongate channel of the block of compressible material and the elongate slot of the forward side wall of the box structure, wherein
a deceleration force of predetermined magnitude exerted on the shoulder web strap along a force vector causes the inertial reel to forcibly move the rear plate forwardly against the block of compressible material to compressively crush the compressible material within the box structure to thereby absorb shock force of the shoulder web strap against a torso of an occupant of the vehicle seat.
12. The aircraft seat according to claim 1 , wherein the block of compressible material comprises a block of compressible metal honeycomb.
13. The aircraft seat according to claim 12 , wherein the block of compressible metal honeycomb is an aluminum honeycomb.
14. The aircraft seat according to claim 13 , wherein the block of aluminum honeycomb comprises elongate cells that are aligned substantially with the force vector.
15. The aircraft seat according to claim 11 , wherein the elongate slot of the forward side wall includes opposed edges and an elongate anti-chafing grommet operatively associated with the opposed edges.
16. The aircraft seat according to claim 1 , further comprising a pair of L-shaped press pads connected to the box structure and engaged with the rear plate so as to positionally restrain the rear plate within the box structure.
17. The aircraft seat according to claim 16 , wherein
the box structure includes a pair of opposed side walls each having a connection lobes, and wherein
the L-shaped press pads are connected to a respective connection lobe of the opposed side walls.
18. The aircraft seat according to claim 11 , wherein the rear plate includes a mounting arm projecting aftwardly away from the rear plate, and wherein the inertial reel assembly is connected to the mounting arm so as to be carried by the rear plate.