Armrest for aircraft seat, associated seat and process

Patent metadata

Field	Value
Publication number	US-2017297722-A1
Application number	US-201715489680-A
Country	US
Kind code	A1
Filing date	Apr 17, 2017
Priority date	Apr 18, 2016
Publication date	Oct 19, 2017
Grant date	—

Abstract

Armrest for aircraft seat, associated seat and process are provided. The armrest includes a stationary part ( 12 ) intended to be connected to the seat, a moving part ( 14 ) movable relative to the stationary part ( 12 ), between a high position in which the moving part ( 14 ) is intended to protrude above a seat bottom of the seat and a low position, and a maneuvering mechanism ( 18 ) able to guide the movement of the moving part ( 14 ) between the high position and the low position. The maneuvering mechanism ( 18 ) includes at least a first connecting rod ( 26 ) and a second connecting rod ( 27 ), each independently connecting the stationary part ( 12 ) to the moving part ( 14 ), the first connecting rod ( 26 ) and the second connecting rod ( 27 ) being arranged parallel to one another during the movement of the moving part ( 14 ) between the high position and the low position.

First claim

What is claimed is:

1 . An armrest for an aircraft seat comprising:
a stationary part configured to be connected to the seat; a movable part movable relative to the stationary part, between a high position in which the moving part is intended to protrude above a seat bottom of the seat and a low position; a maneuvering mechanism configured to guide the movement of the movable part between the high position and the low position, the maneuvering mechanism including at least a first connecting rod and a second connecting rod, each independently connecting the stationary part to the movable part, the first connecting rod and the second connecting rod being arranged parallel to one another during the movement of the movable part between the high position and the low position.

2 . The armrest according to claim 1 , wherein the maneuvering mechanism includes a third connecting rod connecting the stationary part to the movable part, the third connecting rod being arranged parallel to the first connecting rod and the second connecting rod during the movement of the movable part between the high position and the low position.

3 . The armrest according to claim 2 , wherein the first connecting rod, the second connecting rod and the third connecting rod are mounted rotatingly on the stationary part respectively around a first rotation axis, a second rotation axis and a third rotation axis, the third rotation axis being situated separated from a plane containing the first rotation axis and the second rotation axis.

4 . The armrest according to claim 1 , wherein the maneuvering mechanism includes a member stressing the movable part toward the high position.

5 . The armrest according to claim 4 , wherein, from an intermediate position between the high position and the low position, the member stressing the movable part is configured to stress the movable part toward the low position.

6 . The armrest according to claim 4 , wherein the stressing member includes a pneumatic cylinder connected at a first end to the movable part, and at a second end to one of the first connecting rod or the second connecting rod.

7 . The armrest according to claim 6 , wherein the second end of the pneumatic cylinder is articulated to one end of the first connecting rod or the second connecting rod, the second end of the pneumatic cylinder being rotatable jointly with the end of the connecting rod.

8 . The armrest according to claim 1 , including a trim cover defining an upper surface for bearing of a user's arm, the trim cover being supported by the movable part and hiding the stationary part and the maneuvering mechanism.

9 . The armrest according to claim 8 , wherein the movable part defines a central recess, the trim cover defining a through opening coinciding with the central recess, the maneuvering mechanism and the stationary part being situated separated from the central recess and the through opening.

10 . The armrest according to claim 1 , including at least one connection configured to connect the stationary part to the seat, the movable part defining a passage aperture for the connection connecting the stationary part to the seat, during the movement of the movable part between the high position and the low position.

11 . The armrest according to claim 10 , wherein the passage aperture is in the form of an arc of circle.

12 . The armrest according to claim 1 , further comprising a releasable locking system for locking the movable part in the high position and/or the low position.

13 . The armrest according to claim 1 , wherein the stationary part is L-shaped.

14 . An aircraft seat, including:
a framework, a seat bottom mounted on the framework, a seatback mounted on the framework, and at least one of the armrest according to claim 1 , the stationary part being fastened on the framework.

15 . A method for maneuvering an armrest according to claim 1 comprising:
moving, from the low position of the movable part, the movable part toward the high position via the maneuvering mechanism, the first connecting rod and the second connecting rod remaining parallel to one another between the low position and the high position.

16 . The method according to claim 15 , the armrest including a member stressing the movable part toward the high position, the method including, from the high position of the movable part, the following steps:
moving the movable part toward the low position, by exerting a force against the stressing member, to an intermediate position between the high position and the low position, and past the intermediate position, stressing the movable part toward the low position via the stressing member.

Assignees

• Dassault Aviat

Inventors

• Mihai Michel
• LAMOTHE Gaëtan

Classifications

• B60N2/753

  movable to an inoperative position · CPC title

• B64D11/0644 Primary

  Adjustable arm rests · CPC title