Publication detail

Gas Generator Identification and Hydro-Mechanical Control Design for Turboshaft Engine

ZAKUCIA, J.

English title

Gas Generator Identification and Hydro-Mechanical Control Design for Turboshaft Engine

Type

Paper in proceedings (conference paper)

Language

en

Original abstract

Design of the gas turbine control system is a challenging process during the development of the gas turbine engine. In this article, we present identification and modeling of the gas generator for a 180 kW turboshaft engine, which is being developed in PBS VB (První brněnská strojírna Velká Bíteš, a.s.). The gas generator can be described as a nonlinear dynamic system, which comprises mechanical, thermodynamical and dynamical effects in various operational modes of the engine. This work also describes design and modeling of a hydro-mechanical backup fuel-control system. The hydro-mechanical backup fuel-control system is designed as a backup for a FADEC of the engine. Simulations of the identified model with the hydro-mechanical control system are also presented.

Keywords in English

system identification, gas generator modeling, hydro-mechanical fuel-control system

Released

2014-12-15

Publisher

Faculty of Aeronautics, Technical University of Košice

Location

Košice, Slovensko

ISBN

978-80-553-1650-5

ISSN

NEUVEDENO

Book

New Trends in Aviation Development 2014

Pages from–to

1–5

Pages count

5

BIBTEX


@inproceedings{BUT114382,
  author="Jozef {Zakucia}",
  title="Gas Generator Identification and Hydro-Mechanical Control Design for Turboshaft Engine",
  booktitle="New Trends in Aviation Development 2014",
  year="2014",
  pages="1--5",
  publisher="Faculty of Aeronautics, Technical University of Košice",
  address="Košice, Slovensko",
  isbn="978-80-553-1650-5",
  url="http://web.tuke.sk/lf/ntrl2014/index.php?name=2"
}