Interior layout assembly of an aircraft cabin, and related method

Patent metadata

Field	Value
Publication number	US-9988149-B2
Application number	US-201615010722-A
Country	US
Kind code	B2
Filing date	Jan 29, 2016
Priority date	Feb 4, 2015
Publication date	Jun 5, 2018
Grant date	Jun 5, 2018

Abstract

An interior layout assembly of an aircraft cabin, and related method are provided. The assembly includes a table, a console defining a receiving housing and a cover mounted on the console. The cover in the closed configuration and the console define a passage slot between them. The assembly also includes a flap closing off the passage slot, movable by the table from an active configuration closing the passage slot to a retracted configuration freeing the passage slot during the passage of the table from its retracted position to the deployed position.

First claim

What is claimed is:

1. An interior layout assembly of an aircraft cabin comprising:
a table;
a console defining a housing for receiving the table, the receiving housing emerging through a deployment opening, the table being deployable through the deployment opening between a retracted position in the receiving housing and a deployed horizontal position;
a cover mounted on the console, the cover being movable between an open configuration for passage of the table and a closed configuration closing off the deployment opening, the cover in the closed configuration and the console defining a passage slot between them, to receive the table in the deployed horizontal position; and
a flap closing off the passage slot, the flap being movable by the table from an active configuration closing the passage slot to a retracted configuration freeing the passage slot during the passage of the table from the retracted position to the deployed position.

2. The assembly as recited in claim 1 further comprising at least one elastic returner for returning the closing flap to its active configuration.

3. The assembly as recited in claim 1 wherein the closing flap in the active closing configuration is situated above the closing flap in the retracted configuration.

4. The assembly as recited in claim 3 wherein the table is configured to bear on the closing flap during the passage of the table from the retracted position to the horizontal deployed position to push the closing flap downward in the retracted configuration under the effect of the weight of the table.

5. The assembly as recited in claim 1 wherein at least one of the closing flap and the table includes at least one slider for sliding of the table on the closing flap.

6. The assembly as recited in claim 1 wherein the closing flap is movable in translation between the active closing configuration and the retracted configuration.

7. The assembly as recited in claim 1 wherein the console has a stationary upper edge, downwardly defining the passage slot, the table bearing on sliders situated on the closing flap in the deployed horizontal position.

8. The assembly as recited in claim 7 wherein the table bears on the sliders without contact with the upper edge of the console.

9. The assembly as recited in claim 1 wherein the cover in the closed configuration is arranged above an upper surface of the table when the table is in the deployed horizontal position, the cover upwardly closing off the receiving housing.

10. The assembly as recited in claim 1 wherein the cover in the closed configuration is positioned above the closing flap when the table is in the retracted position, the cover upwardly closing off the receiving housing.

11. The assembly as recited in claim 1 wherein the console has an upper surface for bearing objects, an upper wall of the cover in the closed configuration being flush with the upper bearing surface.

12. The assembly as recited in claim 1 wherein the table includes a base panel and an additional panel articulated on the base panel, the additional panel being folded on the base panel during the passage of the table from the retracted position to the deployed horizontal position.

13. An interior layout method of an aircraft cabin comprising:
providing the assembly as recited in claim 1 , the table being in the retracted position in the receiving housing, the closing flap being in the active configuration for closing the passage slot;
deploying the table outside the receiving housing through the deployment opening toward the deployed position; and
moving the closing flap by the table during the deployment of the table to move the closing flap to the retracted configuration.

14. The method as recited in claim 13 further comprising:
retracting the table in the receiving housing through the deployment opening toward the retracted position; and
moving the closing flap from the retracted configuration to the active configuration closing the passage slot, under the effect of an elastic biaser of the closing flap toward its active closing configuration.

15. The method as recited in claim 13 wherein the table bears on the closing flap during the deployment of the table toward the deployed horizontal position, the movement of the closing flap by the table being generated by the weight of the table pressing on the closing flap.

Assignees

• Dassault Aviat

Inventors

• Maillaut Yann

Classifications

• B64D11/0638 Primary

  with foldable tables, trays or cup holders · CPC title

• B64D11/0605

  including tables or desks · CPC title