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ANDRŠ, O. VETIŠKA, J. HOLUB, M. KOVÁŘ, J.
Originální název
Model Based Design of Fuel Pump Control
Typ
článek v časopise - ostatní, Jost
Jazyk
angličtina
Originální abstrakt
This paper presents a co-simulation method to design of speed controller for turbojet fuel pump. Expected fuel pump is used for small turbine engine concept with reducer driven by free turbine. The amount of injected fuel into the combustion chamber is based on the speed of the fuel pump which is controlled by the engine control unit. The final flow of fuel into the combustion chamber is restricted by fuel bypass which constricts the return fuel according to pressure in the nozzles. This back fuel bypass has nonlinear and fixed characteristic determined by its structure. The only way how to control the amount of incoming fuel to the engine is the pump speed control. Effect of the bypass represents a variable component in the fuel pump load and from the view of the speed controller it is a disturbance variable. This paper describes the co-simulation model based on the use of MATLAB/Simulink and MSC Adams environment. This simulation uses interconnection of Simulink controller design and simplified model of the fuel pump dynamics in Adams (without hydraulic modelling).
Klíčová slova
Co-Simulation ADAMS/MATLAB, Fuel Pump, Model Based Design, Motor Control
Autoři
ANDRŠ, O.; VETIŠKA, J.; HOLUB, M.; KOVÁŘ, J.
Vydáno
11. 1. 2016
Nakladatel
Trans Tech Publications
Místo
Switzerland
ISSN
1662-7482
Periodikum
Applied Mechanics and Materials
Ročník
2016
Číslo
821
Stát
Švýcarská konfederace
Strany od
601
Strany do
607
Strany počet
7
URL
http://www.scientific.net/AMM.821.601
BibTex
@article{BUT120620, author="Ondřej {Andrš} and Jan {Vetiška} and Michal {Holub} and Jiří {Kovář}", title="Model Based Design of Fuel Pump Control", journal="Applied Mechanics and Materials", year="2016", volume="2016", number="821", pages="601--607", doi="10.4028/www.scientific.net/AMM.821.601", issn="1662-7482", url="http://www.scientific.net/AMM.821.601" }