Configurable control panel for an aircraft cockpit and method of configuration for such a panel

Patent metadata

Field	Value
Publication number	US-10279890-B2
Application number	US-201615179580-A
Country	US
Kind code	B2
Filing date	Jun 10, 2016
Priority date	Jun 11, 2015
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

A configurable control panel for an aircraft cockpit includes a set of universal control modules each comprising at least one screen including at least one manually manipulable control key. Each of the control modules further includes at least one master control module, and at least one universal slave module associated with the master module, and including a screen and at least one control key. The at least one master module is configured to control the screen and the at least one control key of the at least one universal slave module.

First claim

What is claimed is:

1. A configurable control panel for an aircraft cockpit, comprising:
a master interface comprising a master controller, a screen, and one or more mechanical or electro-mechanical controls for receiving user input; and
two or more slave interfaces, including first and second slave interfaces, electrically coupled with the master interface, each slave interface comprising: a screen, one or more mechanical or electro-mechanical controls for receiving user input, and a slave controller to configure the screen and the one or more mechanical or electro-mechanical controls of the slave interface based on a control signal from the master controller,
wherein:
the master controller is configured to, in response to receiving a user input for display of a first functional system of an aircraft:
display first information for the first functional system of the aircraft; and
send a control signal to the respective slave controllers of the first and second slave interfaces to display the first functional system of the aircraft; and

the control signal causes the respective slave controllers of the first and second slave interfaces to configure the respective screens of the first and second slave interfaces for displaying second information for the first functional system of the aircraft, wherein the second information displayed by the first and second slave interfaces details the first information displayed by the master interface for the first functional system of the aircraft, the second information including additional functionalities relating to the first functional system not included in the first information.

2. The control panel of claim 1 , wherein:
the first information for the first functional system of the aircraft indicates an overall state of the first functional system; and
the second information for the first functional system of the aircraft includes information for first and second distinct components of the first functional system.

3. The control panel of claim 2 , wherein the control signal further causes the respective slave controllers of the first and second slave interfaces to configure behavior of the one or more mechanical or electro-mechanical controls of the first and second slave interfaces for the displayed second information.

4. The control panel of claim 3 , wherein the one or more mechanical or electro-mechanical controls of the first and second slave interfaces are used to control the first and second distinct components of the first functional system, respectively.

5. The control panel of claim 1 , further comprising another interface to control a second functional system of the aircraft.

6. The control panel of claim 1 , wherein the screen of the master interface and the screen of each slave interface are touch-sensitive.

7. The control panel of claim 1 , wherein the first functional system of the aircraft is selected from the group consisting of: a system for supplying the aircraft with fuel, and a system for supplying the aircraft with electricity.

8. A method comprising:
at a control system for an aircraft, the control system including: (i) a master interface comprising a master controller, a screen, and one or more mechanical or electro-mechanical controls for receiving user input, and (ii) two or more slave interfaces, including first and second slave interfaces, electrically coupled with the master interface, each slave interface comprising: a screen, one or more mechanical or electro-mechanical controls for receiving user input, and a slave controller to configure the screen and the one or more mechanical or electro-mechanical controls of the slave interface based on a control signal from the master controller:
receiving, at the master interface, a user input for display of a first functional system of the aircraft;
in response to receiving the user input:
displaying, on the screen of the master interface, first information for the first functional system of the aircraft; and
sending, by the master controller, a control signal to the respective slave controllers of the first and second slave interfaces to display the first functional system of the aircraft; and

in response to sending the control signal:
configuring, by the respective slave controllers of the first and second slave interfaces, the respective screens of the first and second slave interfaces for displaying second information for the first functional system of the aircraft, wherein the second information displayed by the first and second slave interfaces details the first information displayed by the master interface for the first functional system of the aircraft, the second information including additional functionalities relating to the first functional system not included in the first information.

9. The method of claim 8 , wherein:
the first information for the first functional system of the aircraft indicates an overall state of the first functional system; and
the second information for the first functional system of the aircraft includes information for first and second distinct components of the first functional system.

10. The method of claim 9 , further comprising:
in response to sending the control signal:
configuring, by the respective slave controllers of the first and second slave interfaces, behavior of the one or more mechanical or electro-mechanical controls of the first and second slave interfaces for the displayed second information.

11. The method of claim 10 , wherein the one or more mechanical or electro-mechanical controls of the first and second slave interfaces are used to control the first and second distinct components of the first functional system, respectively.

12. The method of claim 8 , wherein the control system further comprises another interface to control a second functional system of the aircraft.

13. The method of claim 8 , wherein the screen of the master interface and the screen of each slave interface are touch-sensitive.

14. The method of claim 8 , wherein the first functional system of the aircraft is selected from the group consisting of: a system for supplying the aircraft with fuel, and a system for supplying the aircraft with electricity.

Assignees

• Zodiac Aero Electric

Inventors

• De Bossoreille Romain
• Nahmiyace Michael

Classifications

• B64C13/042 Primary

  operated by hand · CPC title

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title

• G06F3/041

  Digitisers, e.g. for touch screens or touch pads, characterised by the transducing means · CPC title

• G01C23/00

  Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

• G06F3/1423

  controlling a plurality of local displays, e.g. CRT and flat panel display · CPC title