Aircraft seat with moveable armrest

Patent metadata

Field	Value
Publication number	US-11999487-B2
Application number	US-202017617299-A
Country	US
Kind code	B2
Filing date	Jun 9, 2020
Priority date	Jun 11, 2019
Publication date	Jun 4, 2024
Grant date	Jun 4, 2024

Abstract

An aircraft seat (1) is disclosed. The aircraft seat (1) comprises a seating surface (51), an armrest (7), and a gas strut (9) configured such that the armrest (7) can be moved between a raised position a lowered position in which an armrest surface (71) is substantially level with the seating surface (51). The gas strut (9) comprises a switch (92) with an unlocked configuration in which the stroke of the gas strut (9) can be adjusted and a locked configuration for locking the stroke of the gas strut (9) so that the armrest (7) can be held at any position between the raised position and the lowered position. A trigger (117) is configured to move the switch (92) between the locked and unlocked configurations upon actuation of an actuatable member (111) that is located upon a surface of the aircraft seat (1).

First claim

The invention claimed is:

1. An aircraft seat comprising a seating surface, an armrest comprising an armrest surface, a mechanical linkage, and a gas strut, wherein:
the gas strut is coupled at a first end of the gas strut to the armrest and is coupled at a second end of the gas strut to a substructure of the aircraft seat such that the armrest can be moved between a raised position with respect to the seating surface and a lowered position in which the armrest surface is substantially level with the seating surface by extending and retracting the stroke of the gas strut;
the gas strut comprises a switch with an unlocked configuration in which the stroke of the gas strut can be adjusted, thereby allowing movement of the armrest to any position between the raised position and lowered position, and with a locked configuration for locking the stroke of the gas strut so that the armrest can be held at any position between the raised position and the lowered position;
the mechanical linkage comprises an actuatable member located on a surface of the aircraft seat, a trigger configured to move the switch between the locked configuration and the unlocked configuration, and a tension member coupled at a first end to the actuatable member and coupled at a second end to the trigger;
the tension member is coupled to and runs along an underside of the armrest surface;
the trigger is rotatably mounted to a bracket, and the bracket is mounted to the armrest; and
actuation of the actuatable member exerts a tensile force on the tension member and causes the tension member to pull and rotate the trigger into engagement with the gas strut switch to move the gas strut switch from the locked configuration to the unlocked configuration.

2. An aircraft seat according to claim 1 , wherein the armrest surface translates along an axis oriented substantially perpendicular to the armrest surface as the armrest is moved between the raised position and the lowered position.

3. An aircraft seat according to claim 1 , wherein the actuatable member is a button located on a surface of the armrest.

4. An aircraft seat according to claim 1 , wherein the tension member is a Bowden cable or a substantially rigid rod.

5. An aircraft seat according to claim 4 , wherein the bracket is a first bracket, the tension member is a Bowden cable, and the Bowden cable is held at a first end by the first bracket and held at a second end by a second bracket.

6. An aircraft seat according to claim 5 , wherein the first and second brackets are coupled to an underside of the armrest.

7. An aircraft seat according to claim 1 , wherein the mechanical linkage further comprises a pivot linkage coupled at a first end to the actuatable member and coupled at a second end to the tension member, wherein the pivot linkage is configured such that actuation of the actuatable member causes the pivot linkage to rotate and exert the tensile force on the tension member.

8. An aircraft seat according to claim 1 , wherein, at a first distal end of the gas strut, a piston rod of the gas strut is coupled to an underside of the armrest surface, and wherein, at a second, opposite distal end of the gas strut, a barrel of the gas strut is coupled to the substructure of the aircraft seat.

9. An aircraft seat according to claim 8 , wherein the gas strut switch is located on the piston rod, at the first distal end of the gas strut.

10. An aircraft seat according to claim 1 , the aircraft seat further comprising a backrest, wherein the gas strut is positioned between the actuatable member and the backrest.

11. An aircraft seat according to claim 1 , wherein the range of movement of the armrest surface between the raised and lowered positions is at least approximately 13 centimeters.

12. An aircraft seat comprising a seating surface, an armrest comprising an armrest surface, a mechanical linkage, and a gas strut, wherein:
the gas strut is coupled at a first end of the gas strut to the armrest and is coupled at a second end of the gas strut to a substructure of the aircraft seat such that the armrest can be moved between a raised position with respect to the seating surface and a lowered position in which the armrest surface is substantially level with the seating surface by extending and retracting the stroke of the gas strut;
the gas strut comprises a switch with an unlocked configuration in which the stroke of the gas strut can be adjusted, thereby allowing movement of the armrest to any position between the raised position and lowered position, and with a locked configuration for locking the stroke of the gas strut so that the armrest can be held at any position between the raised position and the lowered position;
the mechanical linkage comprises an actuatable member located on a surface of the aircraft seat, a trigger configured to move the switch between the locked configuration and the unlocked configuration, and a tension member coupled at a first end to the actuatable member and coupled at a second end to the trigger;
the tension member is coupled to and runs along an underside of the armrest surface;
actuation of the actuatable member exerts a tensile force on the tension member and causes the tension member to pull the trigger into engagement with the gas strut switch to move the gas strut switch from the locked configuration to the unlocked configuration; and
the mechanical linkage further comprises a pivot linkage coupled at a first end to the actuatable member and coupled at a second end to the tension member, wherein the pivot linkage is configured such that actuation of the actuatable member causes the pivot linkage to rotate and exert the tensile force on the tension member.

13. An aircraft seat comprising a seating surface, an armrest comprising an armrest surface, a mechanical linkage, and a gas strut, wherein:
the gas strut is coupled at a first end of the gas strut to the armrest and is coupled at a second end of the gas strut to a substructure of the aircraft seat such that the armrest can be moved between a raised position with respect to the seating surface and a lowered position in which the armrest surface is substantially level with the seating surface by extending and retracting the stroke of the gas strut;
the gas strut comprises a switch with an unlocked configuration in which the stroke of the gas strut can be adjusted, thereby allowing movement of the armrest to any position between the raised position and lowered position, and with a locked configuration for locking the stroke of the gas strut so that the armrest can be held at any position between the raised position and the lowered position;
the mechanical linkage comprises an actuatable member located on a surface of the aircraft seat, a trigger configured to move the switch between the locked configuration and the unlocked configuration, and a tension member coupled at a first end to the actuatable member and coupled at a second end to the trigger;
the tension member is coupled to and runs along an underside of the armrest surface;
actuation of the actuatable member exerts a tensile force on the tension member and causes the tension member to pull the trigger into engagement with the gas strut switch to move the gas strut switch from the locked configuration to the unlocked configuration; and
at a first distal end of the gas strut, a piston rod of the gas strut is coupled to an underside of the armrest surface, and, at a second, opposite distal end of the gas strut, a barrel of the gas strut is coupled to the substructure of the aircraft seat.

Assignees

• Safran Seats Gb Ltd

Inventors

• Chandra Naval
• Haikney Daniel

Classifications

• B64D11/0644 Primary

  Adjustable arm rests · CPC title

• A47C1/03

  the parts being arm-rests · CPC title

• A47C1/0303

  adjustable rectilinearly in vertical direction · CPC title

• B60N2/77

  Height adjustment · CPC title