Microturbines have a less complex mechanical design than large-size gas turbines that should make it possible to fit them with a more straightforward control system. However, these systems have very low shaft mechanical inertia and a fast response to external disturbances, such as load trip, that make this very difficult to do. Furthermore, the presence of the recuperator requires smooth variations to the Turbine Outlet Temperature (TOT), when possible, to ensure reduced thermal stresses to the metallic matrix. This paper, after a brief overview of microturbine control systems and typical transients, presents the expected transient behavior of two advanced cycles: the Externally Fired micro Gas Turbine (EFmGT) cycle, where the aim is to develop a proper control system set-up to manage safe part-load operations at constant rotational speed, and a solar Closed Brayton Cycle (CBC), whose control system has to ensure the maximum efficiency at constant rotational speed and constant Turbine Inlet Temperature (TIT).
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ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference
June 16–19, 2003
Atlanta, Georgia, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-3686-X
PROCEEDINGS PAPER
Transient Analysis of and Control System for Advanced Cycles Based on Micro Gas Turbine Technology Available to Purchase
Alberto Traverso,
Alberto Traverso
Universita` di Genova, Genova, Italy
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Federico Calzolari,
Federico Calzolari
Universita` di Genova, Genova, Italy
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Aristide Massardo
Aristide Massardo
Universita` di Genova, Genova, Italy
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Alberto Traverso
Universita` di Genova, Genova, Italy
Federico Calzolari
Universita` di Genova, Genova, Italy
Aristide Massardo
Universita` di Genova, Genova, Italy
Paper No:
GT2003-38269, pp. 201-209; 9 pages
Published Online:
February 4, 2009
Citation
Traverso, A, Calzolari, F, & Massardo, A. "Transient Analysis of and Control System for Advanced Cycles Based on Micro Gas Turbine Technology." Proceedings of the ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference. Volume 3: Turbo Expo 2003. Atlanta, Georgia, USA. June 16–19, 2003. pp. 201-209. ASME. https://doi.org/10.1115/GT2003-38269
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