Electronic engine control software reconfiguration for distributed eec operation

A method of configuring a full authority digital engine controller (FADEC) for use with an engine and an airframe combination, the method comprising:

• receiving a data entry plug configured for the engine and the airframe combination into an airframe data concentrator (ADC) attached to the airframe;
• directing the ADC to recall configuration data from a data storage device within the ADC, the configuration data corresponding to the engine and the airframe combination of the data entry plug;
• recalling the configuration data from the data storage device as directed by the data entry plug;
• transmitting the recalled configuration data from the ADC over a digital bus to an electronic engine controller (EEC), the EEC being attached to the engine;
• and
• configuring the EEC using the transmitted configuration data.

A system for configuring and controlling an aircraft engine attached to an airframe, the system comprising:

• a plurality of airframe sensors attached to the airframe to produce airframe sensor signals;
• an airframe data concentrator (ADC) attached to the airframe and electrically connected to the plurality of airframe sensors to convert the airframe sensor signals to airframe sensor digital data, the ADC comprising:
• a data entry plug socket;
• and
• a data storage device;
• and
• a fuel metering unit (FMU) attached to the engine, the FMU comprising:
• an effector;
• and
• an electronic engine controller (EEC);
• an engine sensor;
• a digital bus connecting the ADC to the EEC;
• and
• a data entry plug inserted into the data entry plug socket to direct the ADC to recall configuration data from the data storage device for the engine and the airframe combination and send the configuration data over the digital bus to the EEC;
• the data entry plug comprising electrical components configured for the engine and the airframe combination;
• wherein the engine sensor is electrically connected to the EEC to provide an engine sensor signal to the EEC;
• the effector is electrically connected to the EEC to adjust a rate of fuel flowing into the engine in response to a control signal sent from the EEC;
• and the control signal sent from the EEC is responsive to the airframe sensor digital data sent by the ADC over the digital bus and the engine sensor signal.