DUAL FUEL AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD FOR OPERATING SAME

摘要

A dual fuel engine control system 900 is disclosed including a first fuel control system 700 for controlling the flow of a first fuel 11 to an aircraft gas turbine engine 101 and a second fuel control system 800 for controlling the flow of a second fuel 11 to the aircraft gas turbine engine 101. A method of operating a dual fuel aircraft engine control system 900 is disclosed comprising the steps of: activating a first fuel control system 700 for controlling the flow of a first fuel 11 to an aircraft gas turbine engine 101; and activating a second fuel control system 800 for controlling the flow of a second fuel 12 to the aircraft gas turbine engine 101.