The choice of compressor characteristics of turbogroups is of decisive importance for the stable behavior of circuits during transients. It is shown how compressor surge at dangerous speeds during rapid shutdown can be suppressed by combining a compressor having a steep characteristic and low reaction with a compressor having a flat characteristic and high reaction. This combination is also well suited with respect to loss of load and startup. In addition, very favourable properties are obtained during positive load steps executed for the purpose of frequency support. Beside providing a machine design with inherent safety, a control system must be supplied which is not only redundant but exhibits inherent safety from malfunction and failures which could endanger the power plant. Because of the importance of these problems, the design and operation of such a control system are presented in this paper.
Skip Nav Destination
Article navigation
October 1974
This article was originally published in
Journal of Engineering for Power
Research Papers
Ensuring Stable Circuit Conditions of Direct Cycle Helium Gas Turbine System
H. U. Frutschi
H. U. Frutschi
Gas Turbine Engineering, BST Brown Boveri-Sulzer Turbomachinery Ltd., Zurich, Switzerland
Search for other works by this author on:
H. U. Frutschi
Gas Turbine Engineering, BST Brown Boveri-Sulzer Turbomachinery Ltd., Zurich, Switzerland
J. Eng. Power. Oct 1974, 96(4): 435-439 (5 pages)
Published Online: October 1, 1974
Article history
Received:
November 27, 1973
Online:
July 14, 2010
Citation
Frutschi, H. U. (October 1, 1974). "Ensuring Stable Circuit Conditions of Direct Cycle Helium Gas Turbine System." ASME. J. Eng. Power. October 1974; 96(4): 435–439. https://doi.org/10.1115/1.3445872
Download citation file:
7
Views
Get Email Alerts
Cited By
An Efficient Uncertainty Quantification Method Based on Inter-Blade Decoupling for Compressors
J. Eng. Gas Turbines Power
Experimental Design Validation of A Swirl-Stabilized Burner with Fluidically Variable Swirl Number
J. Eng. Gas Turbines Power
Experimental Characterization of A Bladeless Air Compressor
J. Eng. Gas Turbines Power
Related Articles
Heat Exchanger Design Considerations for Gas Turbine HTGR Power Plant
J. Eng. Power (April,1977)
Experimental Operating Range Extension of a Twin-Spool Turbofan Engine by Active Stability Control Measures
J. Eng. Gas Turbines Power (January,2006)
Analyses of the Load Following Capabilities of Brayton Helium Gas Turbine Cycles for Generation IV Nuclear Power Plants
ASME J of Nuclear Rad Sci (October,2017)
Dynamic Modeling of a Cogenerating Nuclear Gas Turbine Plant—Part II: Dynamic Behavior and Control
J. Eng. Gas Turbines Power (July,2002)
Related Chapters
The Special Characteristics of Closed-Cycle Gas Turbines
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Studies Performed
Closed-Cycle Gas Turbines: Operating Experience and Future Potential