Study on multi-loop control strategy of three-shaft gas turbine for electricity generation

Purpose This paper aims to develop a dynamic performance model of three-shaft gas turbine for electricity generation and to study a multi-loop control strategy of three-shaft gas turbine for electricity generation. Design/methodology/approach In this paper, the dynamic performance model of the three...

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Veröffentlicht in:Aircraft engineering 2019-08, Vol.91 (7), p.1002-1010
Hauptverfasser: Zhang, Zilai, Zang, Shusheng, Ge, Bing
Format: Artikel
Sprache:eng
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Zusammenfassung:Purpose This paper aims to develop a dynamic performance model of three-shaft gas turbine for electricity generation and to study a multi-loop control strategy of three-shaft gas turbine for electricity generation. Design/methodology/approach In this paper, the dynamic performance model of the three-shaft gas turbine is established and developed. A novel approach, variable partial differential coefficient deviation linearization method is used to simulate the dynamic performance of the three-shaft gas turbine. Single-loop control system, feed-forward feedback control system and cascade system are assessed to control the engine during transient operation. Findings A novel approach, variable partial differential coefficient deviation linearization method is used to simulate the dynamic performance of the three-shaft gas turbine. According to the results shown, the cascade control system is most satisfactory due to its fastest response and the best stability and robustness. Originality/value The method of variable partial linearization is adopted to make the dynamic simulation of the model achieve higher precision, better steady state and less computation time. This paper provides a theoretical study for the multi-loop control system of a marine three-shaft gas turbine.
ISSN:1748-8842
1758-4213
DOI:10.1108/AEAT-05-2018-0149