| Issue |
EPJ Web of Conferences
Volume 92, 2015
EFM14 – Experimental Fluid Mechanics 2014
|
|
|---|---|---|
| Article Number | 02034 | |
| Number of page(s) | 4 | |
| Section | Contributions | |
| DOI | https://doi.org/10.1051/epjconf/20159202034 | |
| Published online | 06 May 2015 | |
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
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