Leg restraint device for side-facing seated vehicle occupants

Patent metadata

Field	Value
Publication number	US-9315271-B2
Application number	US-201514628431-A
Country	US
Kind code	B2
Filing date	Feb 23, 2015
Priority date	May 31, 2013
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A lower leg restraint for a side-facing passenger seat including a restraint panel configured to deploy from a first position proximate a seat to a second position forward of the seat in response to an abrupt deceleration event, an actuator arranged to push the panel from the first position to the second position, and a sensor and trigger assembly configured to signal the actuator to fire in response to the abrupt deceleration event. A side-facing aircraft passenger seat having a deployable lower leg restraint.

First claim

What is claimed is:

1. A lower leg restraint for a side-facing passenger seat, comprising:
(a) a restraint panel configured to deploy from a first position proximate a seat to a second position forward of the seat in response to an abrupt deceleration event;
(b) an actuator arranged to push the panel from the first position to the second position, the actuator comprising a pusher including a piston configured to rapidly extend;
(c) a sliding carriage, wherein the restraint panel is attached to the sliding carriage with one end of the sliding carriage arranged facing the piston such that piston extension pushes the sliding carriage away from the pusher in a direction of the second position; and
(d) a sensor and trigger assembly configured to signal the actuator to fire in response to the abrupt deceleration event.

2. The lower leg restraint of claim 1 , wherein the pusher is attached to one face of a fixed mounting plate further supporting at least one horizontally-oriented bearing spaced from the pusher for guiding linear movement of the sliding carriage, the restraint panel translating relative to the fixed mounting plate as the restraint panel moves between the first and second positions.

3. The lower leg restraint of claim 1 , further comprising a return spring arranged to return the restraint panel to the first position after the abrupt deceleration event, one end of the return spring attached to a fixed member and an opposite end of the return spring attached to one of the sliding carriage and the restraint panel.

4. The lower leg restraint of claim 1 , wherein the restraint panel deploys from within a housing adapted to be positioned under the seat.

5. The lower leg restraint of claim 1 , wherein the restraint panel deploys horizontally.

6. The lower leg restraint of claim 1 , further comprising a cushion attached to an inboard face of the restraint panel.

7. The lower leg restraint of claim 1 , wherein the restraint panel has a corrugated profile and a vertical dimension spanning between a floor supporting the seat and a seat pan of the seat.

8. The lower leg restraint of claim 1 , further comprising a decorative end plate attached to a forward end of the restraint panel.

9. A side-facing aircraft passenger seat having a deployable lower leg restraint, comprising:
(a) a seat bottom;
(b) a seat back
(c) a restraint panel configured to deploy from a first position under the seat bottom to a second position forward of the seat bottom in response to an abrupt deceleration event;
(d) an actuator comprising a pusher including a piston which extends to push the panel from the first position to the second position;
(e) a sensor and trigger assembly configured to signal the actuator to fire in response to the abrupt deceleration event; and
(f) a sliding carriage, wherein the restraint panel is attached to the sliding carriage with one end of the sliding carriage arranged facing the piston such that piston extension pushes the sliding carriage away from the pusher in a direction of the second position.

10. The seat of claim 9 , wherein the pusher is attached to one face of a fixed mounting plate further supporting at least one horizontally-oriented bearing spaced from the pusher for guiding linear movement of the sliding carriage, the restraint panel translating relative to the fixed mounting plate as the restraint panel moves between the first and second positions.

11. The seat of claim 9 , further comprising a return spring arranged to return the restraint panel to the first position after the abrupt deceleration event, one end of the return spring attached to a fixed member and an opposite end of the return spring attached to one of the sliding carriage and the restraint panel.

12. The seat of claim 9 , wherein the restraint panel deploys horizontally from within a housing positioned below the seat bottom.

13. The seat of claim 9 , further comprising a cushion attached to an inboard face of the restraint panel.

14. The seat of claim 9 , wherein the restraint panel has a corrugated profile and a vertical dimension spanning between the seat bottom and underlying floor.

15. The seat of claim 9 , further comprising a decorative end plate attached to a forward end of the restraint panel.

Assignees

• Be Aerospace Inc
• Takata Prot Systems Inc

Inventors

• Oleson Michael L
• Ho Hau
• Guyton Dave L
• Shimizu Norman
• Deevey Mark E
• Meister Pete C
• Farvet Michael J

Classifications

• B60N2/42727 Primary

  involving substantially rigid displacement · CPC title

• B64D11/0619 Primary

  with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash · CPC title

• B60R2021/0053

  Legs · CPC title

• B60N2/4235

  transversal · CPC title

• B64D25/04

  Seat modifications · CPC title