Deployable door-mounted seat

Patent metadata

Field	Value
Publication number	US-2017106983-A1
Application number	US-201514884661-A
Country	US
Kind code	A1
Filing date	Oct 15, 2015
Priority date	Oct 15, 2015
Publication date	Apr 20, 2017
Grant date	—

Abstract

A seat system may include a door and a locking mechanism. The door may be movable between an open position and a closed position. The seat system may include a seat mounted to the door and including a seat bottom that may be movable between a stowed position and a deployed position. The seat system may further include a locking mechanism operatively coupled to the seat bottom and configured such that movement of the seat bottom from the stowed position to the deployed position when the door is in the closed position causes the locking mechanism to engage fixed door-frame structure located adjacent the door and to immobilize the door against movement from the closed position. Movement of the seat bottom from the deployed position to the stowed position may cause the locking mechanism to disengage from the fixed door-frame structure and to allow the door to be moved from the closed position.

First claim

What is claimed is:

1 . A seat system, comprising:
a door including a locking mechanism, the door being movable between an open position and a closed position; a seat mounted to the door and including a seat bottom movable between a stowed position and a deployed position; and the locking mechanism operatively coupled to the seat bottom and configured such that movement of the seat bottom from the stowed position to the deployed position when the door is in the closed position causes the locking mechanism to engage fixed door-frame structure located adjacent the door and to immobilize the door against movement from the closed position, and movement of the seat bottom from the deployed position to the stowed position causes the locking mechanism to disengage from the fixed door-frame structure and to allow the door to be moved from the closed position.

2 . The seat system of claim 1 , wherein:
the locking mechanism is at least one of mechanically-actuated and electrically-actuated in response to movement of the seat bottom to the deployed position when the door is in the closed position.

3 . The seat system of claim 1 , wherein:
the locking mechanism includes a plurality of translatable pins extendable from a door edge into engagement with the fixed door-frame structure.

4 . The seat system of claim 1 , wherein:
the locking mechanism includes at least one cam mounted to the seat bottom and connected to at least one translatable pin by a connecting rod; and the at least one cam moving with the seat bottom between the stowed position and the deployed position causing the locking mechanism to respectively disengage and engage with the fixed door-frame structure.

5 . The seat system of claim 1 , wherein:
the fixed door-frame structure comprises at least one of a door threshold and a seat track included with a floor of a vehicle.

6 . The seat system of claim 1 , wherein:
the fixed door-frame structure comprises a door sill mounted above a door upper portion.

7 . The seat system of claim 1 , wherein:
the locking mechanism includes a structural frame coupled to the door and configured to transfer at least one of lateral loads and vertical loads from the seat to the locking mechanism.

8 . The seat system of claim 7 , wherein:
the locking mechanism and structural frame are configured to support at least one of lateral loads and vertical loads imposed on the door by a mass of an occupant seated on the seat bottom.

9 . The seat system of claim 1 , wherein:
the door is a door in an interior of a vehicle.

10 . The seat system of claim 9 , wherein:
the vehicle is an aircraft cabin having at least one main aisle; and the seat being generally aligned with the main aisle.

11 . The seat system of claim 9 , wherein:
the seat facing in one of a forward direction and an aft direction relative to a direction of forward motion of the vehicle when the door is in the closed position.

12 . An aircraft including a cabin having a lavatory, comprising:
a lavatory door including a locking mechanism and movable between an open position and a closed position; a seat mounted to the lavatory door and including a seat bottom having a folding mechanism allowing movement of the seat bottom between a stowed position and a deployed position; and the locking mechanism operatively coupled to the seat bottom and configured such that movement of the seat bottom from the stowed position to the deployed position when the lavatory door is in the closed position causes the locking mechanism to engage fixed door-frame structure located adjacent the lavatory door and to immobilize the lavatory door against movement from the closed position, and movement of the seat bottom from the deployed position to the stowed position causes the locking mechanism to disengage from the fixed door-frame structure and to allow the lavatory door to be moved from the closed position.

13 . A method of supporting a seat mounted to a door, comprising the steps of:
moving a seat bottom of a door-mounted seat to a deployed position with the door in a closed position; engaging a locking mechanism of the door to a fixed door-frame structure located adjacent to the door in response to moving the seat bottom to the deployed position; and immobilizing the door against movement in response to engagement of the locking mechanism to the fixed door-frame structure.

14 . The method of claim 13 , further including:
transferring, using the locking mechanism, a structural load from the seat to the fixed door-frame structure.

15 . The method of claim 14 , wherein the locking mechanism includes a structural frame coupled to the door, the step of transferring the structural load from the seat to the fixed door-frame structure includes:
transferring the structural load from the seat into the structural frame; transferring the structural load from the structural frame to the locking mechanism; and transferring the structural load from the locking mechanism to the fixed door-frame structure.

16 . The method of claim 14 , wherein the step of transferring the structural load includes:
transferring at least one of lateral loads and vertical loads into the fixed door-frame structure.

17 . The method of claim 13 , wherein the step of engaging the locking mechanism of the door to the fixed door-frame structure includes:
at least one of mechanically actuating and electrically actuating the locking mechanism into engagement with the fixed door-frame structure upon movement of the seat bottom to the deployed position.

18 . The method of claim 13 , wherein the step of engaging the locking mechanism of the door to the fixed door-frame structure includes:
extending one or more translatable pins from a door upper portion into a door sill mounted above the door upper portion.

19 . The method of claim 13 , wherein the step of engaging the locking mechanism of the door to the fixed door-frame structure includes:
extending one or more translatable pins from a door lower portion into at least one of a door threshold and a seat track included with a floor of a vehicle.

20 . The method of claim 13 , wherein the seat bottom includes at least one cam mounted on at least one of opposing seat sides, the cam coupled to a translatable pin using a connecting rod, the step of engaging the locking mechanism of the door to the fixed door-frame structure including:
rotating the cam with movement of the seat bottom to the deployed position; and extending the translatable pin into the fixed door-frame structure in response to rotating the cam.

Assignees

• Boeing Co

Inventors

• Castanos Carmen J
• Starks Hugh A
• Nix Jeffrey R

Classifications

• B64D11/06

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

• B64D11/0691 Primary

  specially adapted for cabin crew · CPC title

• B64C1/1423

  Passenger doors · CPC title

• B64D11/02

  Toilet fittings · CPC title

• B64D11/0639

  with features for adjustment or converting of seats · CPC title