Distributed electronic engine control architecture

摘要

A distributed electronic control system (100) for an aircraft includes an engine data controller (103) arranged on an airframe of the aircraft and a plurality of engine data concentrators (104-106) arranged proximate an engine of the aircraft in signal communication with the engine data controller. The engine data controller (103) is configured to process information related to the engine of the aircraft, the plurality of engine data concentrators (104-106) are configured to receive engine sensor information from a plurality of engine sensors (141-161), and the plurality of engine data concentrators (104-106) are further configured to transmit the engine sensor information to the engine data controller (103).