Seat cushion length adjuster for ejection seat

Patent metadata

Field	Value
Publication number	US-11623755-B2
Application number	US-202117180571-A
Country	US
Kind code	B2
Filing date	Feb 19, 2021
Priority date	Apr 7, 2020
Publication date	Apr 11, 2023
Grant date	Apr 11, 2023

Abstract

A cushion length adjusting system for use in an ejection seat of an aircraft may include a seat pan and first cushion length adjuster coupled to the seat pan. The cushion length adjuster may be hingedly or slidingly coupled to the seat pan. The cushion length adjuster may be configured to adjust a leg support length for greater ergonomics for a pilot of an aircraft.

First claim

What is claimed is:

1. A cushion length adjusting system for use in an ejection seat of an aircraft, comprising:
a seat pan comprising a first slot disposed at a front end of the seat pan and a second slot disposed at the front end;
a first cushion length adjuster slidingly coupled to the seat pan, the first slot configured to receive the first cushion length adjuster;
a second cushion length adjuster slidingly coupled to the seat pan, the second slot configured to receive the second cushion length adjuster; and
an ejection handle disposed between the first cushion length adjuster and the second cushion length adjuster proximate the front end of the seat pan.

2. The cushion length adjusting system of claim 1 , wherein the first cushion length adjuster further comprises a first track disposed on a first side of the first cushion length adjuster and a second track disposed on a second side of the first cushion length adjuster, the first track and the second track configured to slidingly engage the seat pan.

3. The cushion length adjusting system of claim 1 , further comprising a handle coupled to the first cushion length adjuster.

4. The cushion length adjusting system of claim 1 , wherein the seat pan is configured to house the first cushion length adjuster when the first cushion length adjuster is in a retracted state.

5. A cushion length adjusting system for use in an ejection seat of an aircraft, comprising:
a seat pan;
a first cushion length adjuster hingedly coupled to the seat pan, the first cushion length adjuster defining a pivot axis;
a second cushion length adjuster nested with the first cushion length adjuster and hingedly coupled to the seat pan, wherein in response to pivoting the second cushion length adjuster, the first cushion length adjuster and the second cushion length adjuster pivot; and
a third cushion length adjuster nested with the second cushion length adjuster and the first cushion length adjuster.

6. The cushion length adjusting system of claim 5 , wherein in response to pivoting the first cushion length adjuster, only the first cushion length adjuster pivots.

7. The cushion length adjusting system of claim 5 , wherein in response to pivoting the third cushion length adjuster, the second cushion length adjuster and the first cushion length adjuster pivot.

8. The cushion length adjusting system of claim 5 , wherein the first cushion length adjuster has a first width extending away from the pivot axis, wherein the second cushion length adjuster has a second width extending away from the pivot axis, and wherein the second width is greater than the first width.

9. The cushion length adjusting system of claim 5 , further comprising a first tab coupled to the first cushion length adjuster and a second tab coupled to the second cushion length adjuster.

10. The cushion length adjusting system of claim 5 , wherein the cushion length adjusting system is configured to adjust a length of support from extending away from the seat pan.

11. An aircraft ejection seat, comprising:
a seat pan extending from a first side to a second side and defining a front side;
a seat back coupled to the seat pan;
a cushion length adjusting system comprising a first cushion length adjuster and a second cushion length adjuster, the cushion length adjusting system configured to vary a support length measured from the front side of the seat pan; and
an ejection handle disposed between the first cushion length adjuster and the second cushion length adjuster, wherein the ejection handle is configured to expel the aircraft ejection seat in response to being pulled.

12. The aircraft ejection seat of claim 11 , wherein the first cushion length adjuster is hingedly coupled to the front side of the seat pan.

13. The aircraft ejection seat of claim 12 , wherein the second cushion length adjuster is hingedly coupled to the front side of the seat pan, wherein the first cushion length adjuster and the second cushion length adjuster are configured to pivot in concert when the second cushion length adjuster is pivoted, and wherein the first cushion length adjuster is configured to pivot alone when the first cushion length adjuster is pivoted.

14. The aircraft ejection seat of claim 11 , wherein the first cushion length adjuster is slidingly coupled to the seat pan.

15. The aircraft ejection seat of claim 14 , wherein the seat pan further comprises a slot disposed at the front side, wherein the slot is configured to receive the first cushion length adjuster.

16. The aircraft ejection seat of claim 14 , wherein the second cushion length adjuster is slidingly coupled to the seat pan and the ejection handle.

Assignees

• Ami Ind Inc

Inventors

• Shaw Glen
• Fahey Tyler
• Holstine Steve

Classifications

• B64D11/0689

  specially adapted for pilots · CPC title

• B64D25/10 Primary

  Ejector seats · CPC title

• B64D11/0639

  with features for adjustment or converting of seats · CPC title