Multi-function credenza

Patent metadata

Field	Value
Publication number	US-11066173-B2
Application number	US-201715797769-A
Country	US
Kind code	B2
Filing date	Oct 30, 2017
Priority date	Oct 31, 2016
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

First claim

We claim:

1. An aircraft multi-function credenza system, comprising:
an interchangeable multi-function credenza, comprising:
at least one cabinet having a first top surface and a first front panel;
a seat adjacent the cabinet, the seat having a seat bottom and a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed;
a second front panel flush with the first front panel for concealing the seat when the seat is stowed, the second front panel being retractable for retracting beneath the seat when the seat is deployed, wherein the second front panel is substantially perpendicular to the second top surface when the seat is stowed; and
a predetermined footprint abutting a fuselage wall within an aircraft cabin of for a particular type of aircraft; and

common attachment mechanisms disposed in common attachment points that are located beneath the multi-function credenza for attaching to a floor of the aircraft, such that the interchangeable multi-function credenza is adapted for installation in the same location abutting the inner fuselage wall in any aircraft cabin of the particular type of aircraft.

2. The aircraft multi-function credenza system of claim 1 , wherein the first top surface is adapted as a lid for opening to access the at least one cabinet.

3. The aircraft multi-function credenza system of claim 2 , wherein the first top surface, when closed, lies substantially flush with the second top surface when the seat is stowed to form a substantially continuous working surface.

4. The aircraft multi-function credenza system of claim 1 , wherein the seat back includes a first side that is cushioned for seating and a second side adapted as the second top surface when the seat is stowed.

5. The aircraft multi-function credenza system of claim 1 , wherein the first front panel is configured for concealing the at least one cabinet, and the first front panel is slidable for accessing an interior of the at least one cabinet.

6. The aircraft multi-function credenza system of claim 1 , the second front panel being retractable for retracting from a substantially upright orientation for concealing the seat to a substantially horizontal orientation for stowing beneath the seat.

7. The aircraft multi-function credenza system of claim 6 , wherein the second front panel includes a notch for accessing a handle enabling a user to initiate retraction from the substantially upright orientation for concealing the seat to the substantially horizontal orientation for stowing beneath the seat.

8. The aircraft multi-function credenza system of claim 1 , further comprising a first bearing and slide mechanism for enabling rotating and stowing of the seat back, such that the seat back stows behind and partially below the seat bottom, and a second bearing and slide mechanism enabling retracting and stowing of the second front panel beneath the seat.

9. The aircraft multi-function credenza system of claim 1 , wherein the at least one cabinet includes a sink located in the first top surface.

10. A multi-function credenza in an aircraft cabin, comprising:
a first cabinet having a first inboard panel and a first top surface;
a second cabinet having a second inboard panel aligned with the first inboard panel, and a second top surface aligned with the first top surface;
a stowable seat located between the first cabinet and the second cabinet, the seat having a convertible seat back for converting to a third top surface when the seat is stowed, and a third inboard panel for concealing the seat when the seat is stowed, the third inboard panel being retractable for retracting beneath the seat when the seat is deployed, wherein the third inboard panel is substantially perpendicular to the third top surface when the seat is stowed;
a predetermined footprint abutting an inner fuselage wall in the aircraft cabin;
common attachment mechanisms disposed at common attachment points beneath the multi-function credenza for attaching to a floor of the aircraft against the inner fuselage wall of the aircraft, such that the multi-function credenza is adapted for installation in the same location against the inner fuselage wall in the aircraft cabin for a particular type of aircraft.

11. The multi-function credenza of claim 10 , wherein the stowable seat is convertible between a seating mode and a stowed mode, the stowable seat comprising:
a seat bottom, in the seating mode, having a cushioned top surface exposed for seating;
a seat back having a cushioned side and an opposing side;
the seat back, in the seating mode, having the cushioned side exposed for seating and the opposing side extends behind and partially below the seat bottom such that no gap exists between the cushioned top surface of the seat bottom and the cushioned side of the seat back;
the seat back, in the stowed mode, having the opposing side form a third top surface, the third top surface being positioned between the first top surface and the second top surface;
a third inboard panel, in the seating mode, positioned beneath the seat bottom;
the third inboard panel, in the stowed mode, positioned between the first inboard panel and the second inboard panel; and
the third inboard panel and the third top surface, in the stowed mode, conceal the stowable seat.

12. The multi-function credenza of claim 11 , wherein the third top surface, in the stowed mode, is substantially flush with the first top surface and the second top surface to form a substantially continuous working surface.

13. The multi-function credenza of claim 11 , wherein the third inboard panel, in the stowed mode, is substantially flush with the first inboard panel and the second inboard panel to form a uniform façade.

14. An exchangeable multi-function credenza system, comprising:
a first credenza configured for installation against an inner fuselage wall of an aircraft cabin, the first credenza comprising:
a first functional feature and a second functional feature each accessible for use when the first credenza is installed in the aircraft cabin;
wherein the first functional feature is a stowable seat, comprising:
a seat back having a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode; the seatback articulates between the first mode and the second mode for deploying and stowing the seat, respectively; and a front panel for concealing the seat when the seat is stowed, the front panel being retractable for retracting beneath the seat when the seat is deployed, wherein the front panel is substantially perpendicular to the seatback when the seat is stowed;

a plurality of common attachment mechanisms configured for securely attaching to a floor at a predetermined location against the fuselage wall in any aircraft cabin of a given aircraft type; and
a predetermined footprint adapted for installation in any aircraft cabin of the given aircraft type; and

a second credenza comprising:
a third functional feature accessible for use when the second credenza is installed in the aircraft cabin; and
a plurality of common attachment mechanisms configured for securely attaching to the floor at the predetermined location against the fuselage wall; and
the predetermined footprint such that the second credenza is exchangeable with the first credenza at the predetermined location against the fuselage wall.

15. The system of claim 14 , wherein the second functional feature is a storage cabinet and the third functional feature is a sink.

16. The system of claim 14 , wherein the second

Assignees

• Textron Aviation Inc
• Textron Innovations Inc

Inventors

• Davis David Wayne
• Rowe Frank Joseph
• Decker Jason Michael
• Harrell Matthew Robert

Classifications

• B64D11/0627 Primary

  Seats combined with storage means · CPC title

• A47B85/08

  Convertible cupboards · CPC title

• A47B85/04

  Tables convertible into chairs · CPC title

• A47B83/00

  Combinations comprising two or more pieces of furniture of different kinds · CPC title

• B64D11/064 Primary

  Adjustable inclination or position of seats · CPC title