IP Library Granted Patent US 11,021,269
Granted Patent B2
US 11,021,269 · App. 15/778,164 · Granted Jun 1, 2021

System and method for representing a location of a fault in an aircraft cabin

Inventors: Tim Fagan (Beaconsfield, CA); Erin Murphy (Seattle, WA); Linsey Nancarrow (Seattle, WA); Jeff Bartenbach (Seattle, WA)
Assignee: BOMBARDIER INC.
B64F5/60B64D11/00B64D11/00155B64D45/00G05B23/0267H04L67/12H04L67/36H04L69/40B64D2045/0085
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,021,269
App. No.
15/778,164
Granted
Jun 1, 2021
Kind
B2
Abstract

A method and a distributed architecture for controlling functions of an aircraft comprising: a controller, an Input/Output (IO) node and a processor configured to display a graphical user interface component representing at least a portion of an aircraft cabin divided into at least two sections on the IO node and receive, by the IO node, a first and a second input from a user for selecting one of the at least two sections and selecting a preset of at least one controllable parameter respectively. Upon determining that the user requests a modification of the selected preset for the selected section, a preset setting menu including the at least one controllable parameter associated with the selected preset is displayed; a third input from the user for modifying the at least one controllable parameter is received and a modified preset based on the modified at least one controllable parameter is generated.

Claims (56)

1. A distributed architecture for controlling functions of an aircraft, the distributed architecture comprising:

a controller operatively connected to a processor;

an IO node operatively connected to the controller;

the processor being configured to perform:

displaying, on the IO node, a graphical user interface component representing at least a portion of an aircraft cabin divided into at least two aircraft cabin sections;

receiving, by the IO node, a first input from a user for selecting one of the at least two aircraft cabin sections;

receiving, by the IO node, a second input from the user for selecting a preset of at least one controllable parameter;

upon determining, by the processor, that a modification of the selected preset for the selected aircraft cabin section is requested by the user, executing:

displaying, on the IO node, a preset setting menu including the at least one controllable parameter associated with the selected preset, the at least one controllable parameter allowing modification of at least one of the functions of the aircraft cabin for the selected aircraft cabin section;

receiving, by the IO node, a third input from the user for modifying the at least one controllable parameter;

generating a modified preset based on the modified at least one controllable parameter; and

saving, in a memory associated with the distributed architecture, the modified preset.

2. The distributed architecture of claim 1 , wherein the IO node comprises at least one of a passenger IO node and a crew IO node.

3. The distributed architecture of claim 1 , wherein the processor is further configured to perform:

adjusting, by the controller, the selected aircraft cabin section in accordance with the modified preset.

4. The distributed architecture of claim 1 , wherein the at least one controllable parameter comprises at least one of light intensity, light, color, temperature and a degree of openness of a window shade.

5. The distributed architecture of claim 1 , wherein the at least one controllable parameter comprises a first controllable parameter associated with a light intensity, a second controllable parameter associated with a light color and a third controllable parameter associated with a degree of openness of a window shade.

6. The distributed architecture of claim 1 , wherein the preset menu comprises a first group of graphical user interface (GUI) components allowing modification of the first controllable parameter, a second group of GUI components allowing modification of the second controllable parameter and a third group of GUI components allowing modification of the third controllable parameter.

7. A method of modifying a preset of at least one controllable parameter associated with functions of an aircraft cabin for execution on a distributed architecture for multi-nodal control of the functions of the aircraft cabin, the method comprising:

displaying, on an IO node, a graphical user interface component representing at least a portion of an aircraft cabin divided into at least two aircraft cabin sections;

receiving, by the IO node, a first input from a user for selecting one of the at least two aircraft cabin sections;

receiving, by the IO node, a second input from the user for selecting the preset of the at least one controllable parameter;

upon determining, by a processor associated with the distributed architecture, that a modification of the selected preset for the selected aircraft cabin section is requested by the user, executing:

displaying, on the at least one of the passenger IO node and the crew IO node, a preset setting menu including the at least one controllable parameter associated with the selected preset, the at least one controllable parameter allowing modification of at least one of the functions of the aircraft cabin for the selected aircraft cabin section;

receiving, by the at least one of the passenger IO node and the crew IO node, a third input from the user for modifying the at least one controllable parameter;

generating a modified preset based on the modified at least one controllable parameter; and

saving, in a memory associated with the distributed architecture, the modified preset.

8. The method of claim 7 , wherein the IO node comprises at least one of a passenger IO node and a crew IO node.

9. The method of claim 7 , further comprising:

adjusting, by a controller associated with the distributed architecture, the selected aircraft cabin section in accordance with the modified preset.

10. The method of claim 7 , wherein the at least one controllable parameter comprises at least one of light intensity, light, color, temperature and a degree of openness of a window shade.

11. The method of claim 7 , wherein the at least one controllable parameter comprises a first controllable parameter associated with a light intensity, a second controllable parameter associated with a light color and a third controllable parameter associated with a degree of openness of a window shade.

12. The method of claim 7 , wherein the preset menu comprises a first group of graphical user interface (GUI) components allowing modification of the first controllable parameter, a second group of GUI components allowing modification of the second controllable parameter and a third group of GUI components allowing modification of the third controllable parameter.

13. A distributed architecture for controlling functions of an aircraft, the distributed architecture comprising:

a controller operatively connected to a processor;

an IO node operatively connected to the controller;

the processor being configured to perform:

displaying, on the IO node, a graphical user interface component representing at least a portion of an aircraft cabin divided into at least two aircraft cabin sections;

receiving, by the IO node, a first input from a user for selecting one of the at least two aircraft cabin sections;

receiving, by the IO node, a second input from the user for selecting a preset of controllable parameters;

determining, by the processor associated with the distributed architecture, a phase of a journey based at least on a function of time; and

dynamically adjusting, by the controller associated with the distributed architecture, at least one of the controllable parameters based on the selected preset and the determined phase of the journey for the selected aircraft cabin section.

14. The distributed architecture of claim 13 , wherein the IO node comprises at least one of a passenger IO node and a crew IO node.

15. The distributed architecture of claim 13 , wherein the at least one controllable parameter comprises at least one of light intensity, light, color, temperature and a degree of openness of a window shade.

16. The distributed architecture of claim 13 , wherein the phase of the journey defines an environment to be reproduced within the aircraft cabin section.

17. The distributed architecture of claim 16 , wherein the environment is one of a day environment, a work environment, a sunset environment, a relax environment, a sleep environment, a night environment, a sunrise environment and a work environment.

18. A method of dynamically adjusting a preset of controllable parameters associated with functions of an aircraft cabin for execution on a distributed architecture for multi-nodal control of the functions of the aircraft cabin, the method comprising:

displaying, on an IO node, a graphical user interface component representing at least a portion of an aircraft cabin divided into at least two aircraft cabin sections;

receiving, by the IO node, a first input from a user for selecting one of the at least two aircraft cabin sections;

receiving, by the IO node, a second input from the user for selecting the preset of controllable parameters;

determining, by a processor associated with the distributed architecture, a phase of a journey based at least on a function of time; and

dynamically adjusting, by a controller associated with the distributed architecture, at least one of the controllable parameters based on the selected preset and the determined phase of the journey for the selected aircraft cabin section.

19. The method of claim 18 , wherein the IO node comprises at least one of a passenger IO node and a crew IO node.

20. The method of claim 19 , wherein the phase of the journey defines an environment to be reproduced within the aircraft cabin section.

21. The method of claim 18 , wherein the at least one controllable parameter comprises at least one of light intensity, light, color, temperature and a degree of openness of a window shade.

22. The method of claim 21 , wherein the environment is one of a day environment, a work environment, a sunset environment, a relax environment, a sleep environment, a night environment, a sunrise environment and a work environment.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 28, 2018
From: FAGAN, TIM; MURPHY, ERIN; NANCARROW, LINSEY; BARTENBACH, JEFF
To: BOMBARDIER INC.
Reel/Frame 047610/0685 →
Continuity (3)
Continuation In Part 14165068 · Jan 27, 2014
Provisional Application 61759159 · Jan 31, 2013
Related Publication 20180281990A1 · Oct 4, 2018
Cited By (2)
US 12,282,650 US 12,450,997