×

FADEC and avionic component distributed architecture

  • US 8,825,227 B2
  • Filed: 08/20/2008
  • Issued: 09/02/2014
  • Est. Priority Date: 09/03/2007
  • Status: Active Grant
First Claim
Patent Images

1. A device for an engine-operated aircraft, the device comprising:

  • at least one avionic component positioned in the aircraft;

    at least one engine control positioned in or close to an engine of the aircraft; and

    at least one engine interface positioned in the aircraft, the at least one engine interface being adapted for exchanging data between the at least one avionic component and the at least one engine control, the at least one engine interface comprising a function to acquire data from different sources and functions of engine integration such as redundancy and verification of consistency of the data, the at least one engine interface being generic and adapted for communicating with engine controls of different types that can be mounted on the aircraft, and the at least one engine control being specific to one type of engine.

View all claims
  • 1 Assignment
Timeline View
Assignment View
    ×
    ×