Passenger suite with table mechanism with vertical, translational and rotational adjustment

Patent metadata

Field	Value
Publication number	US-11230381-B2
Application number	US-201916542725-A
Country	US
Kind code	B2
Filing date	Aug 16, 2019
Priority date	May 7, 2019
Publication date	Jan 25, 2022
Grant date	Jan 25, 2022

Abstract

An adjustable table assembly for use in a passenger cabin environment such as an aircraft passenger suite including a passenger seat. The table assembly includes a fixed rail assembly attached to a monument, a support column rotatably mounted on the rail assembly, and a table mounted on the support column, the table having a stowed position and deployed positions in a first direction generally toward the passenger seat from the stowed position. The table has a predetermined stowage orientation at which the support column and table are movable along the rail assembly in a second direction opposite the first direction to the stowed position, and the rail assembly prevents the table from moving into the stowed position when the table is rotated out of the predetermined stowage orientation.

First claim

What is claimed is:

1. An aircraft passenger suite defined by at least one privacy wall, comprising:
a passenger seat;
a fixed rail assembly attached to a monument;
a support column rotatably mounted on the rail assembly; and
a table mounted on the support column, the table having a stowed position, and the table having deployed positions in a first direction generally toward the passenger seat from the stowed position;
wherein the table has a predetermined stowage orientation in which the support column and table are movable along the rail assembly in a second direction opposite the first direction to the stowed position, and the rail assembly prevents the table from moving into the stowed position when the table is rotated out of the predetermined stowage orientation; and
wherein the rail assembly comprises a control rail having a first portion extending in the first direction and along which the support column and table are rotatable around a vertical axis defined by the support column, and a second portion extending in the second direction and along which the support column and table are not rotatable around the vertical axis.

2. The aircraft passenger suite of claim 1 , wherein:
the first portion of the control rail has a first lateral width;
the second portion of the control rail has a second lateral width greater than the first lateral width; and
the support column has a radially reduced portion that faces the control rail when the table is in the predetermined stowage orientation.

3. The aircraft passenger suite of claim 2 , wherein at least a portion of the support column has a vertical circular cylindrical wall having a radius.

4. The aircraft passenger suite of claim 3 , wherein the radially reduced portion is formed by a chord surface.

5. The aircraft passenger suite of claim 1 , further comprising a brake that automatically prevents movement of the support column and table along the rail assembly in a braked condition, wherein, when a user applies force in the first direction or second direction, the brake is switched to a freed condition permitting movement of the table along the rail assembly.

6. The aircraft passenger suite of claim 1 , wherein a vertical position of the table is adjustable.

7. The aircraft passenger suite of claim 1 , wherein the table comprises a base panel mounted on the support column, and a first folding panel pivotally attached to the base panel, wherein the first folding panel is pivotable relative to the base panel between a folded position and an unfolded position.

8. The aircraft passenger suite of claim 7 , wherein the table comprises a second folding panel pivotally attached to the base panel.

9. The aircraft passenger suite of claim 7 , further comprising a wall positioned forward of the passenger seat in the second direction, wherein the base panel has a first linear end to which the first folding panel is pivotally attached, and wherein the predetermined stowage orientation is defined by the first linear end facing the wall.

10. The aircraft passenger suite of claim 9 , wherein, in the stowed position of the table, the first folding panel is in the folded position and the first linear end of the base panel faces, and is adjacent, the wall.

11. The aircraft passenger suite of claim 1 , wherein the monument comprises a bed.

12. An adjustable table assembly installable in a passenger cabin environment, the table assembly comprising:
a fixed rail assembly attachable to a fixed structure in a passenger cabin;
a support column rotatably mounted on the rail assembly; and
a table mounted on the support column, the table having a stowed position, and the table having deployed positions in a first direction from the stowed position;
wherein the table has a predetermined stowage orientation in which the support column and table are movable along the rail assembly in a second direction opposite the first direction to the stowed position, and the rail assembly prevents the table from moving into the stowed position when the table is rotated out of the predetermined stowage orientation;
wherein the table comprises a base panel mounted on the support column, and a first folding panel pivotally attached to the base panel, wherein the first folding panel is pivotable relative to the base panel between a folded position and an unfolded position; and
wherein the base panel has a first linear end to which the first folding panel is pivotally attached, and wherein the predetermined stowage orientation is defined by the first linear end facing the second direction or the first direction.

13. The table assembly of claim 12 , wherein the rail assembly comprises a control rail having a first portion extending in the first direction and along which the support column and table are rotatable around a vertical axis defined by the support column, and a second portion extending in the second direction and along which the support column and table are not rotatable around the vertical axis.

14. The adjustable table assembly of claim 13 , wherein:
the first portion of the control rail has a first lateral width;
the second portion of the control rail has a second lateral width greater than the first lateral width; and
the support column has a radially reduced portion that faces the control rail when the table is in the predetermined stowage orientation.

15. The adjustable table assembly of claim 14 , wherein at least a portion of the support column has a vertical circular cylindrical wall having a radius.

16. The adjustable table assembly of claim 12 , further comprising a brake that automatically prevents movement of the support column and table along the rail assembly in a braked condition, wherein, when a user applies force in the first direction or second direction, the brake is switched to a freed condition permitting movement of the table along the rail assembly.

17. The adjustable table assembly of claim 12 , wherein a vertical position of the table is adjustable.

Assignees

• Be Aerospace Inc

Inventors

• Frost Ian L
• Overhiser Gerry J

Classifications

• B64D11/0604

  including a bed, e.g. cocoon type passenger seat modules · CPC title

• B64D11/0606

  with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title

• B60N3/001

  of tables or trays · CPC title

• B64D2011/0046

  Modular or preassembled units for creating cabin interior structures · CPC title

• B64D2011/0084

  Bed units for passengers attached to the ceiling of the fuselage · CPC title