Mathematical Model of the Jet Engine Fuel System
University of West Bohemia, Department of Power System Engineering, Univerzitni 8, 306 14 Pilsen, Czech Republic
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Published online: 6 May 2015
The paper discusses the design of a simplified mathematical model of the jet (turbo-compressor) engine fuel system. The solution will be based on the regulation law, where the control parameter is a fuel mass flow rate and the regulated parameter is the rotational speed. A differential equation of the jet engine and also differential equations of other fuel system components (fuel pump, throttle valve, pressure regulator) will be described, with respect to advanced predetermined simplifications.
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