Telescoping arm restraint system

Patent metadata

Field	Value
Publication number	US-11338925-B2
Application number	US-202016988158-A
Country	US
Kind code	B2
Filing date	Aug 7, 2020
Priority date	Aug 7, 2020
Publication date	May 24, 2022
Grant date	May 24, 2022

Abstract

An ejection seat is disclosed. In various embodiments, the ejection seat includes a seat frame having a seat-back and a seat-pan adapted to support an occupant, the ejection seat further comprising a propulsion system configured to propel the ejection seat from an aircraft; and a backstop configured to deploy laterally outward from the seat-back to form a forward-facing surface, the backstop including a lower support arm and an upper support arm, the lower support arm and the upper support arm configured to telescope upon deployment of the ejection seat.

First claim

What is claimed is:

1. An ejection seat, comprising:
a seat frame having a seat-back and a seat-pan adapted to support an occupant, the ejection seat further comprising a propulsion system configured to propel the ejection seat from an aircraft; and
a backstop configured to deploy laterally outward from the seat-back to form a forward-facing surface, the backstop including a lower support arm and an upper support arm, the lower support arm and the upper support arm configured to telescope in response to deployment of the ejection seat.

2. The ejection seat of claim 1 , wherein the lower support arm includes a lower base member connected to the seat frame.

3. The ejection seat of claim 2 , wherein the lower support arm includes a first lower telescoping member slidably engaged with the lower base member.

4. The ejection seat of claim 3 , wherein the lower support arm includes a second lower telescoping member slidably engaged with the first lower telescoping member.

5. The ejection seat of claim 3 , wherein the lower support arm includes a shear pin extending through the lower base member and the first lower telescoping member.

6. The ejection seat of claim 3 , further comprising a ratcheting hinge connecting the lower base member to the seat frame.

7. The ejection seat of claim 3 , further comprising a pressure source, the pressure source configured to telescope the first lower telescoping member from the lower base member in response to deployment of the ejection seat.

8. The ejection seat of claim 6 , wherein the upper support arm includes an upper base member connected to the seat frame.

9. The ejection seat of claim 8 , wherein the upper support arm includes a first upper telescoping member slidably engaged with the upper base member.

10. The ejection seat of claim 9 , wherein the upper support arm includes a second upper telescoping member slidably engaged with the first upper telescoping member.

11. The ejection seat of claim 10 , further comprising a non-ratcheting hinge connecting the upper base member to the seat frame.

12. An ejection seat for an aircraft, comprising:
a seat frame having a seat-back and a seat-pan adapted to support an occupant; and
a backstop configured to deploy laterally outward from the seat-back to form a forward-facing surface, the backstop including
a lower support arm, the lower support arm configured to telescope in response to deployment of the ejection seat,
an upper support arm, the upper support arm configured to telescope in response to deployment of the ejection seat, and
a plurality of shrouds, the plurality of shrouds connected to the lower support arm and the upper support arm and configured to form the forward-facing surface in response to deployment of the ejection seat.

13. The ejection seat of claim 12 , wherein the lower support arm includes a lower base member connected to the seat frame and a first lower telescoping member slidably engaged with the lower base member.

14. The ejection seat of claim 13 , wherein the plurality of shrouds in connected to the first lower telescoping member.

15. The ejection seat of claim 13 , wherein the lower support arm includes a second lower telescoping member slidably engaged with the first lower telescoping member.

16. The ejection seat of claim 15 , wherein the plurality of shrouds in connected to the second lower telescoping member.

17. The ejection seat of claim 13 , wherein the upper support arm includes an upper base member connected to the seat frame and a first upper telescoping member slidably engaged with the upper base member.

18. The ejection seat of claim 17 , wherein the plurality of shrouds is connected to the first lower telescoping member and to the first upper telescoping member.

19. The ejection seat of claim 17 , wherein the upper support arm includes a second upper telescoping member slidably engaged with the first upper telescoping member and the lower support arm includes a second lower telescoping member slidably engaged with the first lower telescoping member and wherein the plurality of shrouds is connected to the second lower telescoping member and to the second upper telescoping member.

20. The ejection seat of claim 17 , wherein the lower support arm includes a first shear pin extending through the lower base member and the first lower telescoping member and the upper support arm includes a second shear pin extending through the lower base member and the first lower telescoping member.

Assignees

• Ami Ind Inc

Inventors

• Bharucha Nicholas K
• Holstine Steve
• Stribrny Casey Andrew

Classifications

• B64D25/10 Primary

  Ejector seats · CPC title

• B64D25/06

  Harnessing · CPC title

• B64D25/04 Primary

  Seat modifications · CPC title

• B64D11/06

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title

• B64D25/02 Primary

  Supports or holding means for living bodies · CPC title