IP Library Granted Patent US 12,466,562
Granted Patent B2
US 12,466,562 · App. 18/521,335 · Granted Nov 11, 2025

Aircraft cockpit seat with display integrated into the rear of the seat back, and cockpit provided with such a seat

Inventor: Jason Zaneboni (Blagnac, FR)
Assignee: Airbus (S.A.S.)
B64D11/00155B64D11/0689
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Quick Facts
Patent No.
US 12,466,562
App. No.
18/521,335
Granted
Nov 11, 2025
Kind
B2
Abstract

A cockpit seat comprising a seat back having a rear face and a cushion, wherein the seat back has equipment integrated into the rear face of the seat back and having at least one comfort parameter control and a display zone. Thus, the comfort parameter controls are easily visible and accessible on entering the cockpit, and the person entering can directly adapt his or her environment according to his or her wishes. A cockpit provided with such a seat and a method for controlling a comfort parameter from such a seat are disclosed.

Claims (44)

1 . A cockpit seat comprising a seat back comprising:

a rear face;

a cushion; and

equipment comprising:

a first part comprising at least one comfort parameter control, a display zone, and a touchscreen within the display zone, wherein the first part is secured to the cockpit seat on the rear face of the seat back; and

a removable part, which is removably attached to the first part and comprises at least a processor for processing data and at least one data storage zone, wherein the removable part is pre-programable with values for comfort parameters associated with a user before the user enters an aircraft where the cockpit seat is located;

wherein, when the removable part is connected to the first part on the cockpit seat, the comfort parameters are automatically adjusted to values for the comfort parameters that are preprogramed into the removable part.

2 . The cockpit seat according to claim 1 , wherein the comfort parameters comprise one or more of a position of the seat, a position of a portion of the seat, lighting in a cockpit where the cockpit seat is located, display of information associated with piloting, and a temperature in the cockpit.

3 . The cockpit seat according to claim 1 , wherein:

the seat back comprises a headrest; and

the equipment is integrated into the headrest, at least in part; or

wherein the at least one comfort parameter control is actuated by pressing on the touchscreen.

4 . The cockpit seat according to claim 1 , wherein:

the seat back comprises a shell;

the rear face of the seat back corresponds to a rear face of the shell; and

the equipment is integrated into an upper part of the shell, on a face of the shell that is inclined with respect to horizontal.

5 . An aircraft cockpit comprising:

the cockpit seat according to claim 1 ; and

an instrument panel having piloting controls, which are physically segregated from the equipment of the cockpit seat, such that the instrument panel is on an opposite side of the cockpit seat from the equipment of the cockpit seat.

6 . A method for controlling comfort parameters of a cockpit, the method comprising:

providing equipment comprising:

a first part comprising at least one comfort parameter control, a display zone, and a touchscreen within the display zone; and

a removable part comprising at least a processor for processing data and at least one data storage zone;

securing the first part of the equipment to a rear face of a seat back of at least one seat of the cockpit

attaching the removable part to the first part in a manner that allows for detachment of the removable part from the first part by a user during normal operation of an aircraft comprising the cockpit;

using the at least one comfort parameter control of the equipment to control the comfort parameters of the cockpit;

pre-programing the removable part with values for comfort parameters associated with the user before the user enters the cockpit; and

when the removable part is connected to the first part on the cockpit seat, automatically adjusting values to the comfort parameters that are preprogramed into the removable part.

7 . The method according to claim 6 , comprising controlling the display zone to provide temporary, alternative, or complementary lighting of the cockpit.

8 . The method according to claim 6 , wherein;

certain comfort controls are accessible from the equipment and also at a distance therefrom, in the cockpit outside an instrument panel; or

the equipment activates comfort controls associated with control parameters determined according to the user identified by recognition by the equipment.

9 . The method according to claim 6 , wherein the comfort parameters comprise one or more of a position of the seat, a position of a portion of the seat, lighting in a cockpit where the cockpit seat is located, display of information associated with piloting, and a temperature in the cockpit.

10 . A cockpit seat comprising:

a seat back comprising:

a rear face;

a cushion; and

equipment comprising:

at least one comfort parameter control, a display zone, and a touchscreen, all of which are attached to the cockpit seat on the rear face of the seat back; and

a removable part, which comprises at least some controls, a processor, and at least one data storage zone;

wherein the at least one comfort parameter control is actuated by pressing on the touchscreen;

a shell;

wherein the rear face of the seat back corresponds to a rear face of the shell; and

wherein the equipment is integrated into an upper part of the shell, on a face of the shell that is inclined with respect to horizontal.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 28, 2023
From: ZANEBONI, JASON
To: AIRBUS (S.A.S.)
Reel/Frame 065685/0185 →
Priority Claims (1)
FR 2212514 · Nov 29, 2022 · national
Continuity (1)
Related Publication 20240174363A1 · May 30, 2024
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