scholarly journals Dynamic performance simulation and control of gas turbines used for hybrid gas/wind energy applications

2019 ◽  
Vol 147 ◽  
pp. 122-142 ◽  
Author(s):  
Elias Tsoutsanis ◽  
Nader Meskin
2012 ◽  
Vol 616-618 ◽  
pp. 1922-1925
Author(s):  
Kai Peng ◽  
Ding Fan ◽  
Lei Zhang ◽  
Qiu Xia Wang

Turbine blade tip clearance continues to be a concern in the design and control of gas turbines. Ever increasing demands for improved efficiency and higher operating temperatures require more stringent tolerances on turbine tip clearance. An implicit active generalized predictive control with AR error modification and fuzzy adjustment on control horizon of aero-engine turbine tip clearance is presented and evaluated. The results show the resultant active tip clearance control system has good steady and dynamic performance and benefits of increased efficiency, reduced specific fuel consumption, and additional service life.


1993 ◽  
Vol 17 ◽  
pp. S299-S304
Author(s):  
G. Heyen ◽  
K. Murphy ◽  
D. Marchio ◽  
P. Kalata ◽  
B. Kalitventzeff

1994 ◽  
Vol 18 (11-12) ◽  
pp. 1071-1082 ◽  
Author(s):  
G. Heyen ◽  
K. Murphy ◽  
D. Marchio ◽  
P. Kalata ◽  
B. Kalitventzeff ◽  
...  

2014 ◽  
Vol 672-674 ◽  
pp. 1531-1534
Author(s):  
Kai Peng ◽  
Ding Fan ◽  
Ran Ran Wu ◽  
Yu Qiang Teng

Active control of turbine blade tip clearance continues to be a concern in design and control of gas turbines. Ever increasing demands for improved efficiency and higher operating temperatures require more stringent tolerances on turbine tip clearance. In this paper, a turbine tip clearance control apparatus and a model of turbine tip clearance are proposed. The active clearance control (ACC) of aero-engine turbine tip clearance is evaluated in a lapse-rate take-off transient, along with the comparative and quantitative analysis. The results show that the resultant active tip clearance control system has favorable steady-state and dynamic performance and benefits of increased efficiency, reduced specific fuel consumption, and additional service life.


Author(s):  
A. Traverso

In recent years microturbines and, more generally, small radial turbomachinery have been of great interest to the power industry due to their possible integration with advanced energy systems involving very high-tech components, such as high temperature fuel cells, high temperature ceramic heat exchangers and air saturators, which are still under development. Even if microturbine technology is already commercially available, when such an engine is inserted into a more complex plant there are at least two difficulties to be faced: firstly, guaranteeing the safe operation of the microturbine at all the operating points, including start-up and shut-down; and secondly, ensuring the proper feeding conditions to the main components of the cycle. In fact, additional components bring new variables to be monitored and require additional control devices and control systems. As a result, a flexible and modular simulation tool is extremely useful for the actual development of new cycles, where attention is mainly paid to the interaction of quasi-conventional turbomachinery with advanced components integrated in the same cycle. The TRANSEO code is a MATLAB-based modular tool for the transient performance simulation of conventional and advanced energy systems based on gas turbine and microturbine technology. This paper presents the theoretical background and the organization of the tool, showing the validation of results for a conventional recuperated microturbine.


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