Constant area vent for external crash attenuation airbag

• US 9,045,222 B2
• Filed: 03/30/2011
• Issued: 06/02/2015
• Est. Priority Date: 03/30/2011
• Status: Active Grant

• Current Assignee: Textron Innovations Incorporated (Textron Inc)
• Original Assignee: Textron Innovations Incorporated (Textron Inc)
• Inventors: Lu, Zi, Tho, Cheng-Ho, Smith, Michael R., Hill, Andrew T., Rajan, Samgeeth
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Giczy, Alexander V
• Application Number:
  US13/699,758
• Publication Number:
  US 20130068883A1
• Time in Patent Office: 1,525 Days
• Field of Search: 244/100.A, 244/105, 244/107, 244/101, 244/121
• US Class Current: 1/1
• CPC Class Codes: B64C 27/006 Safety devices
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use
• CPC Class Codes: B64D 25/00 Emergency apparatus or devices, not otherwise provided for parachutes B64D17/00, B64D19/00; jettisoning of fuel tanks or fuel per se B64D37/00; specially adapted for protection against criminal attack, e.g. anti-hijacking systems B64D45/0015 ; safety belts or body harnesses in general A62B35/00; safety belts or body harnesses for land vehicles B60R22/00; jettisonable parts of fuselage facilitating emergency escape B64C

Abstract

The external crash attenuation airbag includes an inflatable bladder which is inflatable to an exterior of an aircraft, so that the inflatable bladder is generally located between the aircraft and a crash surface when inflated. The airbag includes a vent configured to burst at a predefined burst pressure, the vent being located along a side portion of the inflatable bladder. The airbag also includes a vent support located approximate the vent, the vent support being configured to prevent deformation and therefore maintain the effectiveness of a venting area of the vent, and the vent support being rigid and annular and includes an upper portion and a lower portion that are hinged together around the vent.

Claims

1. An external airbag for an aircraft, the external airbag comprising:

an inflatable bladder configured to be inflated exterior of the aircraft;

a vent integrated with and coupled to the inflatable bladder, the vent having a vent opening configured to release pressure within the inflatable bladder in order to dissipate energy; and

a vent support coupled to the inflatable bladder and located near the vent, the vent support being configured to prevent deformation of the vent opening due to hoop stresses as pressure within the inflatable bladder increases;

wherein the vent support is rigid and is annular; and

wherein the vent support includes an upper portion and a lower portion;

wherein the upper portion and the lower portion of the vent support are hinged together around the vent.

2. The external airbag according to claim 1, wherein the vent support is hexagonally shaped.

3. The external airbag according to claim 1, wherein the vent support is circular.

4. The external airbag according to claim 1, wherein the inflatable bladder is cylindrically shaped.

5. The external airbag according to claim 1, wherein the inflatable bladder has a first cylinder and a second cylinder, the first and second cylinders connected to form a dual cylindrical shape.

6. The external airbag according to claim 1, wherein the vent support is metallic.

7. The external airbag according to claim 1, wherein further the vent support is attached to the inflatable bladder by a fabric, the fabric being attached to the inflatable bladder thereby entrapping the vent support.

8. The external airbag according to claim 7, wherein the vent support is attached to the inflatable bladder through a stitching process.

9. The external airbag according to claim 7, wherein the vent support is attached to the inflatable bladder through a thermal bonding process.

10. The external airbag according to claim 1, wherein the vent support is attached to the inflatable airbag with an adhesive.

11. An external airbag for an aircraft, the external airbag comprising:

an inflatable bladder which is inflatable to an exterior of an aircraft so that the inflatable bladder is generally located between the aircraft and a crash surface when inflated;

a vent configured to burst at a predefined burst pressure, the vent being located along a side portion of the inflatable bladder;

a vent support located approximate the vent, the vent support being configured to prevent deformation of a venting area of the vent;

wherein the vent support is rigid and is annular; and

wherein the vent support includes an upper portion and a lower portion;

wherein the upper portion and the lower portion of the vent support are hinged together around the vent.

12. The external airbag according to claim 11, wherein the inflatable bladder is cylindrically shaped.

13. The external airbag according to claim 11, wherein the inflatable bladder is pressurized between 1 psi and 15 psi prior to an impact.

14. The external airbag according to claim 11, wherein the vent includes a burst portion, the predefined burst pressure is between 3 psi and 25 psi.

15. The external airbag according to claim 11, wherein the vent support is configured to provide structural integrity around the vent.

16. An aircraft having a crash attenuation system, comprising:

a fuselage;

a rotor system;

an airbag assembly located near a lower portion of the fuselage, the airbag assembly comprising;

an airbag bladder which is inflatable to an exterior of the fuselage;

a vent located in the airbag bladder, the vent configured so as to extend to the exterior of the fuselage with the airbag bladder as the airbag bladder is inflated, the vent being configured to burst at a predefined pressure;

a rigid vent support located approximate the vent, the vent support being configured to resist deformation of the vent during compression of the airbag bladder;

wherein the rigid vent support is annular shaped; and

wherein the rigid vent support includes an upper portion and a lower portion;

wherein the upper portion and the lower portion of the rigid vent support are hinged together around the vent.

17. The aircraft according to claim 16, wherein the airbag bladder is at least partially cylindrically shaped.