Closed Loop Control of an Afterburning F100 Gas Turbine Engine

1986 ◽  
Author(s):  
Soraya A. Eisa ◽  
Henry P. Tyler
Author(s):  
Amit Pandey ◽  
Maurício de Oliveira ◽  
Chad M. Holcomb

Several techniques have recently been proposed to identify open-loop system models from input-output data obtained while the plant is operating under closed-loop control. So called multi-stage identification techniques are particularly useful in industrial applications where obtaining input-output information in the absence of closed-loop control is often difficult. These open-loop system models can then be employed in the design of more sophisticated closed-loop controllers. This paper introduces a methodology to identify linear open-loop models of gas turbine engines using a multi-stage identification procedure. The procedure utilizes closed-loop data to identify a closed-loop sensitivity function in the first stage and extracts the open-loop plant model in the second stage. The closed-loop data can be obtained by any sufficiently informative experiment from a plant in operation or simulation. We present simulation results here. This is the logical process to follow since using experimentation is often prohibitively expensive and unpractical. Both identification stages use standard open-loop identification techniques. We then propose a series of techniques to validate the accuracy of the identified models against first principles simulations in both the time and frequency domains. Finally, the potential to use these models for control design is discussed.


Author(s):  
Mehrdad Pakmehr ◽  
Nathan Fitzgerald ◽  
Eric M. Feron ◽  
Jeff S. Shamma ◽  
Alireza Behbahani

A stable gain scheduled controller for a gas turbine engine that drives a variable pitch propeller is developed and described. A stability proof is developed for gain scheduled closed-loop system using global linearization and linear matrix inequality (LMI) techniques. Using convex optimization tools, a single quadratic Lyapunov function is computed for multiple linearizations near equilibrium and nonequilibrium points of the nonlinear closed-loop system. This approach guarantees stability of the closed-loop gas turbine engine system. To verify the stability of the closed-loop system on-line, an optimization problem is proposed, which is solvable using convex optimization tools. Simulation results show that the developed gain scheduled controller is capable to regulate a turboshaft engine for large thrust commands in a stable fashion with proper tracking performance.


Author(s):  
Mehrdad Pakmehr ◽  
Nathan Fitzgerald ◽  
Eric M. Feron ◽  
Jeff S. Shamma ◽  
Alireza Behbahani

We develop and describe a stable gain scheduling controller for a gas turbine engine that drives a variable pitch propeller. A stability proof is developed for gain scheduled closed-loop system using global linearization and linear matrix inequality (LMI) techniques. Using convex optimization tools, a single quadratic Lyapunov function is computed for multiple linearizations near equilibrium and non-equilibrium points of the nonlinear closed-loop system. This approach guarantees stability of the closed-loop gas turbine engine system. Simulation results show the developed gain scheduling controller is capable of regulating a turboshaft engine for large thrust commands in a stable fashion with proper tracking performance.


Author(s):  
B. M. Antkowiak ◽  
F. C. Nelson

This paper summarizes the development of a finite element rotordynamic solution used in a closed loop simulation for a magnetic bearing rotor system in a gas turbine engine. A magnetic bearing controlled rotor is analyzed, and the state dynamics matrix [A], the shaft control influence matrix [B], and the sensor matrix [C] are constructed. Bode plots of the state-space transfer function are also constructed and compared to the results of the rotor dynamic model.


2021 ◽  
Author(s):  
Robert T. Fievisohn ◽  
John Hoke ◽  
Ryan T. Battelle ◽  
Christopher Klingshirn ◽  
Adam T. Holley ◽  
...  

Author(s):  
Xiao-Yi Zhang

The market requirements with regard to transient operation capabilities of gas turbines (GT) in utility use are becoming stringent. Besides normal frequency support features, gas turbines in local electrical grids are often required to maintain the grid frequency under various situations, including emergencies, such as, loss of national grid connection or trip of a large consumer, etc. These requirements demand high performance and stability of GT control. On the other hand, the environmental aspects are becoming increasingly a public concern. In the past decades, remarkable progress has been made in combustion technologies of heavy-duty gas turbines. Lean premixing is a preferred technology for NOx emission reduction. Because of its flashback and extinction limits, a premix flame has usually a much narrower operation range compared to a diffusional one, adding tight constraint on GT control. This paper demonstrates a successful implementation of a model-based predictor, a proven control technique, in the closed loop control of the ALSTOM GT11N2 gas turbine. First, an online GT model, which is integrated into the GT control algorithm, was developed. By applying appropriate assumption and simplification, this model is capable of simulating the GT process over the whole load operation range with high dynamic accuracy. Secondly, a model-based predictor for accelerating slow measured signals was implemented. It dynamically compensates the system delays in the GT process and in the measuring instruments. Thirdly, the predictor was applied to the GT core control by replacing the measured signals with the accelerated signals. The original control structure was kept unchanged. In order to verify its performance and stability, the new control technique was validated on a real engine. Successful engine tests proved that the model-based predictor improves GT transient operation capabilities.


Author(s):  
J. S. Weisert

Allison Gas Turbine Division of General Motors Corporation has manufactured industrial and marine gas turbines for nearly 30 years. The selection of a viable control system is critical for any gas turbine installation, and especially for marine applications. This paper will describe the hydromechanical control system previously used on Allison 501-K marine gas turbines, and the electronic closed loop control system currently used. The discussions of these control systems will include schematics; a description of the components; and a description of the operation of each system. The two systems will be compared, and the newer closed loop control system will be shown as a significant improvement.


1998 ◽  
Vol 120 (3) ◽  
pp. 621-625 ◽  
Author(s):  
B. M. Antkowiak ◽  
F. C. Nelson

This paper summarizes the development of a finite element rotordynamic solution used in a closed loop simulation for a magnetic bearing rotor system in a gas, turbine engine. A magnetic bearing controlled rotor is analyzed, and the state dynamics matrix [A], the shaft control influence matrix [B], and the sensor matrix [C] are constructed. Bode plots of the state-space transfer function are also constructed and compared to the results of the rotor dynamic model.


Sign in / Sign up

Export Citation Format

Share Document