https://doi.org/10.1051/epjconf/20159202034
Mathematical Model of the Jet Engine Fuel System
University of West Bohemia, Department of Power System Engineering, Univerzitni 8, 306 14 Pilsen, Czech Republic
a Corresponding author: klimko@kke.zcu.cz
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.
© Owned by the authors, published by EDP Sciences, 2015
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
