AIRCRAFT OCCUPANT RESTRAINT PRETENSIONING DEVICES, SYSTEMS AND METHODS

• US 20150158590A1
• Filed: 12/09/2014
• Published: 06/11/2015
• Est. Priority Date: 12/09/2013
• Status: Abandoned Application

• Current Assignee: AmSafe, Inc. (Transdigm Group Incorporated)
• Original Assignee: AmSafe, Inc. (Transdigm Group Incorporated)
• Inventors: Gehret, William J., Gullotto, Giuseppe, Scott, Robert
• Application Number:
  US14/565,207
• Publication Number:
  US 20150158590A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B60R 22/1952 Transmission of tensioning power by cable; Return motion locking means therefor
• CPC Class Codes: B60R 22/1954 characterised by fluid actuators, e.g. pyrotechnic gas generators actuating a cable B60R22/1952
• CPC Class Codes: B64D 11/062 Belts or other passenger restraint means for passenger seats

Abstract

Occupant restraint systems for use with aircraft occupant restraint systems and other restraint systems, and associated devices and methods are disclosed herein. In one embodiment, an occupant restraint system can include a flexible web configured to extend across at least a portion of a lap of an occupant positioned on a seat of an aircraft, and an electronically-actuated pretensioner operably coupled to an end portion of the web. The system can also include a sensor assembly operably coupled to the pretensioner, wherein the sensor assembly is configured to send an electrical signal to the pretensioner in response to an aircraft acceleration or deceleration above a preset magnitude, and wherein, in response to receiving the electrical signal from the sensor assembly, the pretensioner is configured to automatically increase tension on the web.

Claims

1. An occupant restraint system for use in an aircraft, the occupant restraint system comprising:

a flexible and elongate web configured to extend across at least a portion of an occupant seated in a seat;

an electronically-actuated pretensioner operably coupled to an end portion of the web; and

a sensor assembly operably connected to the pretensioner, wherein the sensor assembly is configured to send an electrical signal to the pretensioner in response to an aircraft acceleration or deceleration above a preset magnitude, and wherein, in response to receiving the electrical signal from the sensor assembly, the pretensioner is configured to automatically increase tension in the web.

2. The occupant restraint system of claim 1 wherein:

the pretensioner includes a housing and a cable;

the cable has a first cable portion positioned within the housing and a second cable portion extending from the housing and operably coupled to the end portion of the web; and

in response to receiving the electrical signal from the sensor assembly, the pretensioner is configured to retract the cable into the housing and increase tension in the web.

3. The occupant restraint system of claim 2 wherein the pretensioner further includes a piston slidably disposed within the housing and operably coupled to the first cable portion, and wherein in response to receiving the electrical signal from the sensor assembly, the piston is driven into the housing to retract the cable and increase tension in the web.

4. The occupant restraint system of claim 2 wherein the pretensioner further includes a piston slidably disposed within the housing and a rotatable spool, wherein the first cable portion is operably coupled to the piston and the second cable portion is operably coupled to the spool, and wherein in response to receiving the electrical signal from the sensor assembly, the piston is driven into the housing to retract the cable, whereby the cable rotates the spool to increase tension in the web.

5. The occupant restraint system of claim 1 wherein the pretensioner includes a flexible connecting member extending from a pretensioner body, wherein the connecting member has a distal end portion coupled to the end portion of the web, wherein the connecting member extends along a tensioning axis between the pretensioner body and the web when the web is secured around the occupant, and wherein the tensioning axis extends at an angle that is greater than 10 degrees and less than 45 degrees relative to a horizontal axis of the seat.

6. The occupant restraint system of claim 5 wherein the seat is mounted to a floor surface of the aircraft, and wherein the horizontal axis of the seat extends parallel to the floor surface.

7. The occupant restraint system of claim 6 wherein:

the tensioning axis extends at an angle that is between about 15 degrees and about 40 degrees relative to the horizontal axis of the seat.

8. The occupant restraint system of claim 6 wherein:

the tensioning axis extends at an angle of about 35 degrees relative to the horizontal axis of the seat.

9. The occupant restraint system of claim 1 wherein:

the web includes;

a first web portion having a first distal end and a first proximal end operably coupled to the pretensioner; and

a second web portion have a second distal end and a second proximal end;

and wherein the first distal end is releasably coupleable to the second distal end via a buckle.

10. The occupant restraint system of claim 1 wherein the pretensioner is positioned toward a first side of the seat, and wherein the occupant restraint system further comprises a web retractor positioned toward an opposite, second side of the seat, wherein the end portion of the web is a first end portion, and wherein the web further comprises a second end portion, opposite the first end portion and operably coupled to the web retractor.

11. The occupant restraint system of claim 1 wherein the pretensioner is a linear pretensioner.

12. The occupant restraint system of claim 1 wherein the pretensioner is a rotary pretensioner.

13. The occupant restraint system of claim 1 wherein the occupant restraint system is a two-point occupant restraint system.

14. The occupant restraint system of claim 1 wherein the web is configured to extend across a lap of the occupant.

15. The occupant restraint system of claim 1 wherein the web is configured to extend across a lap of the occupant, and wherein the web is the sole restraint web included in the occupant restraint system.

16. The occupant restraint system of claim 1 wherein the occupant restraint system is a three-point occupant restraint system.

17. A seating system for use in an aircraft, the seating system comprising:

an aircraft seat, wherein the seat is mounted to a floor that defines a horizontal axis of the seat;

a flexible and elongate web configured to extend across a lap of an occupant seated on the seat, wherein the web includes—

a first web portion having a first distal end portion and a first proximal end portion;

a second web portion have a second distal end portion and a second proximal end portion; and

wherein the first distal end portion is releasably coupleable to the second distal portion via a buckle; and

an electronically-actuated pretensioner fixedly mounted proximate the seat, the pretensioner including—

a housing; and

a cable, wherein the cable has a first cable portion extending within the housing and a second cable portion extending between the housing and the first web portion, wherein the second cable portion is coupled to the first proximal end portion of the first web portion, wherein the second cable portion extends along a tensioning axis, and wherein the tensioning axis extends at an angle that is less than 45 degrees relative to the horizontal axis of the seat when the web extends across the lap of the seat occupant.

18. The seating system of claim 17 wherein the angle is between about 15 degrees and about 40 degrees.

19. The seating system of claim 17 wherein the angle is between about 30 degrees and about 40 degrees.

20. The seating system of claim 17 wherein the angle is about 35 degrees.

21. The seating system of claim 17, further comprising a sensor assembly operably connected to the pretensioner, wherein the sensor assembly is configured to send an electrical signal to the pretensioner in response to an aircraft acceleration or deceleration above a preset magnitude, and wherein, in response to receiving the electrical signal from the sensor assembly, the pretensioner is configured to automatically increase tension in the web.

22. The seating system of claim 17 wherein the pretensioner is a linear pretensioner.

23. The seating system of claim 17, further comprising a web retractor coupled to the second proximal end portion of the second web portion.