AIRBAG SYSTEM WITH IMPROVED PERFORMANCE FOR A WIDE RANGE OF LOADS

• US 20110011973A1
• Filed: 03/17/2009
• Published: 01/20/2011
• Est. Priority Date: 03/17/2008
• Status: Abandoned Application

• Current Assignee: Rafael Advanced Defense Systems Limited (Government of Israel)
• Original Assignee: Rafael Advanced Defense Systems Limited (Government of Israel)
• Inventors: Shahar, Rahav, Albagli, David, Ben Moshe, Alon, Ben-Soussan, Mordechai
• Application Number:
  US12/922,854
• Publication Number:
  US 20110011973A1
• Time in Patent Office: Days
• US Class Current: 244/100.A
• CPC Class Codes: B60R 21/239 characterised by their venting means
• CPC Class Codes: B64C 2025/325 specially adapted for helicopters
• CPC Class Codes: B64C 27/57 automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use

Abstract

An airbag system according to any one individual feature or combination of features as described herein.

Claims

1-3. -3. (canceled)

4. An air bag system comprising an airbag having at least one pressure release vent sealed by a sealing diaphragm wherein a variation of one of a diameter of said pressure release vent and a thickness of said sealing diaphragm determined a breaching pressure of said sealing diaphragm.

5. The airbag system of claim 4, wherein said at least one pressure release vent is configured as an array of pressure release vents.

6. The airbag system of claim 5, wherein some of said pressure release vents in said array have diameters that are different from other said pressure release vents in said array.

7. The airbag system of claim 6, wherein said differing pressure release vent diameters are configured to provide a plurality of pressure release stages.

8. The airbag system of claim 6, wherein said differing pressure release vent diameters are configured to provide a continuous pressure release range.

9. The airbag system of claim 4, wherein at least a portion of an edge of said pressure release vent is configured with a controlled breaching mechanism.

10. The airbag system of claim 9, wherein said controlled breaching mechanism includes said edge of said pressure release vent being configured as a jagged edge.

11. A method for holding an overpressure state in an airbag, the method comprising:

(a) providing the airbag with an array of bursting pressure release vents having various breaching pressures; and

(b) introducing a residual flow of gases into the airbag after initial inflation.

12. The method of claim 11, further including holding the overpressure state for a period of time longer than 500 mS.

13. A method for folding an airbag having bursting pressure release vents, the method comprising folding the airbag in a modified accordion pattern, such that the bursting pressure release vents are placed in the final folds, so as to mitigate heat and pressure waves caused by an inflation system before said heat and pressure waves reach said bursting pressure release vents, thus preventing an early breach of the bursting pressure release vents.