Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; 1992
DOI: 10.1115/92-gt-022
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Simplified Mathematical Representations of Single Shaft Gas Turbines in Mechanical Drive Service

Abstract: There have been several recent applications of large single shaft, heavy duty gas turbines in mechanical drive service, powering high horsepower, multi-casing compressors. This variable speed application of a traditional constant speed driver, with a more limited operating speed range, has created a need for simplified but accurate mathematical representations that can be incorporated into overall process simulations to allow interactive dynamic evaluation of the complete system.

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Cited by 138 publications
(80 citation statements)
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“…After this paper, the author proposed an upgrade to his model. The new model allowed the simulation of combined-cycle power plant, including variable stator vane (VSV) modeling and an acceleration control loop (Rowen 1992). The Rowen's model configuration and study are illustrated in Fig.…”
Section: Control Systemmentioning
confidence: 99%
“…After this paper, the author proposed an upgrade to his model. The new model allowed the simulation of combined-cycle power plant, including variable stator vane (VSV) modeling and an acceleration control loop (Rowen 1992). The Rowen's model configuration and study are illustrated in Fig.…”
Section: Control Systemmentioning
confidence: 99%
“…A robust controller for an identified model of a power plant gas turbine was designed by Najimi and Ramezani (2012). The applied model was built on the basis of Rowen's model (Rowen, 1992) and by using real data for tuning the GT parameters. Kolmanovsky et al (2012) developed a robust control system for aero gas turbines.…”
Section: White-box Modelsmentioning
confidence: 99%
“…Various mathematical and thermodynamic models have been proposed for gas turbines. They include, simple and applied models such as the Rowen model for a gas power plant [4] and for a combined cycle power plant [6], the aerothermodynamics model, the computational model, and the thermodynamic model [9]. The history of gas turbine modeling shows the simplified mathematical model consists of a set of algebraic equations and related temperature, speed and acceleration controllers is provided in [4,6].…”
Section: Gas Turbine Modelmentioning
confidence: 99%