Aircraft passenger seat extended armrest

Patent metadata

Field	Value
Publication number	US-2019225342-A1
Application number	US-201815936497-A
Country	US
Kind code	A1
Filing date	Mar 27, 2018
Priority date	Jan 19, 2018
Publication date	Jul 25, 2019
Grant date	—

Abstract

An aircraft seat armrest includes an armrest portion and two extension elements coupled to the armrest portion on opposite sides thereof. A first of the two extension elements is rotatable from a first, closed, position where it is disposed below the armrest portion to a second, open, position wherein the first extension element is adjacent to the armrest portion. The arm rest also includes a first locking mechanism disposed on the first extension element that maintains the first extension element in the open position after it has been moved from the closed position to the open position.

First claim

What is claimed is:

1 . An aircraft seat armrest including:
an armrest portion; two extension elements coupled to the armrest portion on opposite sides thereof; wherein a first of the two extension elements is rotatable from a first, closed, position where it is disposed below the armrest portion to a second, open, position wherein the first extension element is adjacent to the armrest portion; and a first locking mechanism disposed on the first extension element that maintains the first extension element in the open position after it has been moved from the closed position to the open position.

2 . The aircraft seat armrest of claim 1 , wherein a second of the two extension elements is movable from the first, closed, position where it is disposed below the armrest portion and the second, open, position wherein the second extension element is adjacent to the armrest portion; and further comprising:
a second locking mechanism disposed on the second extension element that maintains the second extension element in the open position after it has been moved from the closed position to the open position.

3 . The aircraft seat armrest of claim 2 , wherein the first and second locking mechanisms are bolt latches.

4 . The aircraft seat armrest of claim 3 , wherein the first and second locking mechanisms include bolts that mate with a bolt retention element disposed on the armrest portion.

5 . The aircraft seat armrest of claim 4 , wherein the bolt retention element is a staple disposed on a bottom of the armrest portion.

6 . The aircraft seat armrest of claim 2 , further comprising:
a first arm extension retention element disposed on the first side of the first arm extension; and a second arm extension retention element disposed on the first side of the first arm extension.

7 . The aircraft seat armrest of claim 6 , further comprising:
a first extension retention element disposed on the armrest portion that mates with the first arm extension retention element that maintains the first extension element in the closed position; and a second extension retention element disposed on the bottom of the armrest portion that mates with the second arm extension retention element that maintains the second extension element in the closed position.

8 . The aircraft seat armrest of claim 7 , wherein the first and second arm extension retention elements are magnets and the first and second extension retention element are formed of magnetic material.

9 . The aircraft seat armrest of claim 7 , wherein the first and second arm extension retention elements are formed of magnetic material and the first and second extension retention element are magnets.

10 . The aircraft seat armrest of claim 1 , wherein the two extension elements are coupled to the armrest portion by hinges.

11 . A method of expanding an aircraft armrest, the method comprising:
providing an armrest portion; coupling two extension elements to the armrest portion on opposite sides thereof such that they can rotate relative to the armrest portion; wherein the two extension elements are coupled such that a first of the two extension elements can move from a first, closed, position where it is disposed below the armrest portion to a second, open, position wherein the first extension element is adjacent to the armrest portion; and providing the first extension element with a first locking mechanism disposed on the first extension element that can maintain the first extension element in the open position.

12 . The method of claim 11 , further comprising:
providing a second locking mechanism disposed on the second extension element that can maintain the second extension element in the open position after it has been moved from the closed position to the open position.

13 . The method of claim 12 , wherein the first and second locking mechanisms are bolt latches.

14 . The method of claim 13 , wherein the first and second locking mechanisms include bolts that mate with a bolt retention element disposed on the armrest portion.

15 . The method of claim 11 , further comprising:
providing a first arm extension retention element on the first arm extension; and providing a second arm extension retention element on the first arm extension.

16 . The method of claim 15 , further comprising:
providing a first extension retention element on the armrest portion that mates with the first arm extension retention element that maintains the first extension element in the closed position; and providing a second extension retention element on the armrest portion that mates with the second arm extension retention element that maintains the second extension element in the closed position.

Assignees

• Ami Ind Inc

Inventors

• Boddu Radha
• Sahay Gaurav

Classifications

• B64D11/0612 Primary

  specially adapted for children · CPC title

• B64D11/0646

  Seats characterised by special features of stationary arms, foot or head rests · 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

• B60N2/763

  adjustable · CPC title

• B60N2/753

  movable to an inoperative position · CPC title