Propeller Control Loop Model Development and Simulation of Transient Behavior

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F09%3A%230000953" target="_blank" >RIV/00010669:_____/09:#0000953 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Propeller Control Loop Model Development and Simulation of Transient Behavior

Original language description

The article describes a propeller control loop model for the transient analysis of a small two shaft turboprop engines rated up to 500 kW and presents dynamic simulation results of a new conceptual control system solution. Mathematical models of each component are described with the aid of unsteady one-dimensional equations and steady-state components characteristics. The model is solved using MATLAB ? Simulink software package. Special efforts have been made to built realistic non-linear models both acontrolled system (it means mechanically linked a free turbine, a gear box and a propeller) and hydraulic elements of the control system. Simulated results demonstrate control loop behavior in different operational situations and conditions and determineparameters limits of control system components.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JT - Propulsion, engines and fuels

OECD FORD branch

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Project

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Continuities

R - Projekt Ramcoveho programu EK

Publication year

2009

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2/2009

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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