System and method for representing a location of a fault in an aircraft cabin
US11021269B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Nov 23, 2015 |
| Grant date | Jun 1, 2021 |
| Priority date | — |
| Expiry date | Oct 15, 2036 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D2045/0085
- WIPO fieldTransport
- WIPO sectorMechanical engineering
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.