Hybrid architecture for an aircraft system
US9470549B2 · kind B2 · utility
Assignees
Inventors
Key dates
| Filing date | Dec 23, 2013 |
| Grant date | Oct 18, 2016 |
| Priority date | — |
| Expiry date | Dec 23, 2033 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG08G5/21
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A method of configuring an aircraft management system comprising the following steps, implemented by a configuration module integrated into the avionic system of the aircraft cockpit: obtaining at least one item of computation data for computing at least one configuration parameter of the management system, sending, to a computation module that is independent from the avionic system of the aircraft cockpit, a request for computing said at least one parameter on the basis of said at least one item of computation data, receiving, from said computation module, said at least one computed parameter, and configuring said management system with said at least one received computed parameter.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.