Inflatable restraint systems for ejection seats

• US 6,422,512 B1
• Filed: 08/30/2000
• Issued: 07/23/2002
• Est. Priority Date: 08/31/1999
• Status: Expired due to Term

• Current Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Baker, Jeffrey Allyn, Butt, Steven K., Karigiri, Shyam S., Hailstone, Steven R., Lewis, Donald J., Merrifield, Terry W.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US09/651,477
• Time in Patent Office: 692 Days
• Field of Search: 244/141, 244/121, 244/118.5, 244/118.6, 244/122.AG, 280/728.1, 280/768, 280/769, 280/751, 297/464-465, 297/487-488
• US Class Current: 244/121
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use
• CPC Class Codes: B64D 25/02 Supports or holding means for living bodies
• CPC Class Codes: B64D 25/06 Harnessing
• CPC Class Codes: B64D 25/10 Ejector seats

Abstract

An inflatable restraint system for holding and securing an aircrew member in his seat during ejection from an aircraft has one or more members forming a shield around him or her. The system is controlled to inflate after the aircrew member has started the sequence of ejection and before the rockets that power the seat from the aircraft are ignited. The forces of windblast are deflected by the inflatable restraint from the aircrew member as the aircrew member enters into and remains in the windblast and in his seat.

Claims

1. An inflatable restraint system for protecting an aircrew member during ejection from the aircraft, the system comprising:

an aircrew member'"'"'s seat mounted in an aircraft and adaptable to be ejected from the aircraft;

a central L-shaped tubular member having the vertical arm of said “

L”

extending from the ankles and in front of the legs to above the knees and the horizontal arm of said “

L”

extending toward the chest of the aircrew member;

at least one pair of tubular members extending from either side of said central tubular member and extending along said aircraft seat, said pair of tubular members in fluid communication with said central tubular member;

a tubular manifold member secured to said vertical arm of said “

L”

shaped central tubular member and positioned between the ankles and the knees of the aircrew member and between said central tubular member and said aircraft seat, said manifold member in fluid communication with said central tubular member and having an inflation inlet;

a sheet member connected to said central tubular member and said pair of tubular members and operable to enclose the arms and the legs of the aircrew member prior to entering into the windblast during ejection; and

a source of inflating fluid connected to said inflation inlet and operable upon command to inflate said tubular members and along with said sheet member for forming a shield around the aircrew member and said aircrew member'"'"'s seat.

2. An inflatable restraint system according to claim 1 additionally including a second pair of tubular members extending from either side of said central tubular member,

wherein one of said first and second pair tubular members is operable to extend along said aircraft seat in front of and along the arms of the aircrew member, and

the other of said first and second pair of tubular members is operable to extend in front of and along the sides of the legs and said aircrew member'"'"'s seat.

3. An inflatable restraint system according to claim 2 wherein said sheet member is connected to each of said first and second pair of tubular members and extends from said central tubular member across said first and second tubular members forming a shield around the aircrew member and said aircrew member'"'"'s seat for deflecting the windblast during ejection.

4. An inflatable restraint system according to claim 1 wherein said horizontal arm of said central L-shaped tubular member has an orthogonally extending tubular member extending away from said horizontal arm and from the helmet of the aircrew member for deflecting the windblast during ejection.

5. An inflatable restraint system according to claim 2 wherein one of said first and second tubular members extends from said central tubular member and around the foot and ankles of the aircrew member for restraining the foot and leg of the aircrew member in front of said aircrew member'"'"'s seat during ejection.

6. An inflatable restraint system according to claim 5 wherein the other of said first and second tubular members extends from said central tubular member and around the hands and arms of the aircrew member for restraining the hands and arms of the aircrew member during ejection.

7. An inflatable restraint system according to claim 1 wherein said manifold member and said central L-shaped tubular member inflates prior to said at least one pair of tubular members.

8. An inflatable restraint system according to claim 7 wherein said sheet member is a perforated sheet.

9. An inflatable restraint system for protecting an aircrew member during ejection, the system comprising:

an aircrew member'"'"'s seat mounted in an aircraft and adaptable to be ejected from the aircraft;

a first inflatable member adapted to be inflated;

a second inflatable member operable to extend orthogonal from said first inflatable member and then rearward along the side of said aircrew member'"'"'s seat;

a third inflatable member spaced along said first member from said second member and operable to extend orthogonal from said first inflatable and then rearward along the side of said aircrew member'"'"'s seat;

a frangible cover storing said first, second and third inflatable members;

an inflator connected to said first inflatable member and operative to supply an inflating gas to said inflatable members and to breakaway said frangible cover to extend said first inflatable member in front of the aircrew member from a bottom edge intermediate the knees and the feet of the aircrew member to a top edge intermediate the aircrew member'"'"'s waist and shoulders and said second and third inflatable members from said first inflatable member in front of the aircrew member and along the sides of said aircrew member'"'"'s seat;

said first, second and third inflatables forming an inflated unshaped member enclosing the aircrew member'"'"'s seat providing a shield to the windblast when the aircrew member is ejected.

10. An inflatable restraint system according to claim 9 wherein said first, second and third inflatables are in fluid communication with said inflator.

11. An inflatable restraint system according to claim 9 additionally including a mast member connected to said first inflatable member and responsive to said inflator for rigidly extending from the bottom of said seat between the aircrew member'"'"'s legs.

12. An inflatable restraint system according to claim 11 wherein said mast member is normally inflated substantially simultaneously with said first inflatable member.

13. An inflatable restraint system according to claim 9 wherein the inflation pressure of said inflator is less than thirty-five psi.

14. An inflatable restraint system according to claim 13 wherein the inflation pressure of said inflator is between fifteen and twenty-five psi.

15. An inflatable restraint system according to claim 9 wherein said first inflatable member is fully inflated within three hundred milliseconds from the initial actuation of said inflator.

16. An inflatable restraint system according to claim 11 wherein said mast is telescopically stored in said frangible cover before inflation.

17. An inflatable restraint system according to claim 11 wherein said mast and said first inflatable member are fully inflated within three hundred milliseconds from the initial actuation of said inflator.

18. An inflatable restraint system according to claim 9 wherein the material of said first, second and third inflatables is 420 denier, urethane coated material.