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Advanced Fuel Flow Measurement in Aero Engine Using MicrocontrollerBy M. J. Aarthi, K. Manikandan, M. Aravinthkumar, S. Bhuvaneshwari, D. Mohanapriya
Abstract: AbstractThe amount of fuel that must flow in an aircraft engine is an important parameter that must be considered while designing the fuel control unit in an aircraft engine. The amount of fuel supplied must be optimised as per the speed requirement of aircraft. The basic aim of this project is to solve the major problem of measurement of fuel flow rate in an aero engine. This project fulfils the …
Published in Journal of Operating Systems Development & Trends · Vol. 6, Issue 2, 2019 · pp. 6–13 Read article →