A hybrid control system has been proposed for compressor surge, which combines the active method with the passive method. A bleed valve was selected as the actuator in the proposed system. As a submode of the hybrid system, a fuzzy logic based active controller was designed to extend the stability operating range of the compressor. Meanwhile, a surge avoidance controller was used as a backup-mode to improve the safety performance of the system. The simulation results showed that the compressor can operate steadily outside the surge line under active control mode and can be dragged back to inside the surge line by the passive control mode when the alternative fails. One advantage of the proposed control system is that it does not need a model of the compressor, and it works on any compression system. Passive surge control is a reliable and widely applied method in industrial compressors. The hybrid system makes the active control approach closer to the industrial implementation.
Skip Nav Destination
Article navigation
September 2014
Research-Article
Active/Passive Hybrid Control System for Compressor Surge Based on Fuzzy Logic
Hanlin Sheng,
Hanlin Sheng
Department of Power Engineering,
e-mail: dreamshl@nuaa.edu.cn
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016
, China
e-mail: dreamshl@nuaa.edu.cn
Search for other works by this author on:
Wei Huang,
Wei Huang
Department of Power Engineering,
e-mail: 181617040@qq.com
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016
, China
e-mail: 181617040@qq.com
Search for other works by this author on:
Tianhong Zhang,
Tianhong Zhang
1
Professor
Department of Power Engineering,
e-mail: thz@nuaa.edu.cn
Department of Power Engineering,
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016,
China
e-mail: thz@nuaa.edu.cn
1Corresponding author.
Search for other works by this author on:
Xianghua Huang
Xianghua Huang
Professor
Department of Power Engineering,
e-mail: xhhuang@nuaa.edu.cn
Department of Power Engineering,
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016,
China
e-mail: xhhuang@nuaa.edu.cn
Search for other works by this author on:
Hanlin Sheng
Department of Power Engineering,
e-mail: dreamshl@nuaa.edu.cn
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016
, China
e-mail: dreamshl@nuaa.edu.cn
Wei Huang
Department of Power Engineering,
e-mail: 181617040@qq.com
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016
, China
e-mail: 181617040@qq.com
Tianhong Zhang
Professor
Department of Power Engineering,
e-mail: thz@nuaa.edu.cn
Department of Power Engineering,
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016,
China
e-mail: thz@nuaa.edu.cn
Xianghua Huang
Professor
Department of Power Engineering,
e-mail: xhhuang@nuaa.edu.cn
Department of Power Engineering,
Nanjing University of Aeronautics and Astronautics (NUAA)
,Jiangsu 210016,
China
e-mail: xhhuang@nuaa.edu.cn
1Corresponding author.
Contributed by the Turbomachinery Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received February 14, 2014; final manuscript received February 21, 2014; published online March 21, 2014. Editor: David Wisler.
J. Eng. Gas Turbines Power. Sep 2014, 136(9): 092601 (8 pages)
Published Online: March 21, 2014
Article history
Received:
February 14, 2014
Revision Received:
February 21, 2014
Citation
Sheng, H., Huang, W., Zhang, T., and Huang, X. (March 21, 2014). "Active/Passive Hybrid Control System for Compressor Surge Based on Fuzzy Logic." ASME. J. Eng. Gas Turbines Power. September 2014; 136(9): 092601. https://doi.org/10.1115/1.4026953
Download citation file:
Get Email Alerts
Design and Manufacture of EBC Coated SiC/SiC Nozzle Guide Vanes for High-Pressure Turbines
J. Eng. Gas Turbines Power
Hydrogen & Ammonia Powered Turbofan Design Implications For Next Generation Of Aircraft Engines
J. Eng. Gas Turbines Power
Stability and Robustness Analysis and Optimization for Gain-Scheduled Control of Aero-Engines
J. Eng. Gas Turbines Power (December 2024)
Related Articles
Experimental Operating Range Extension of a Twin-Spool Turbofan Engine by Active Stability Control Measures
J. Eng. Gas Turbines Power (January,2006)
Experimental Evaluation of the Transient Behavior of a Compressor Station During Emergency Shutdowns
J. Eng. Gas Turbines Power (June,2010)
Application of Fuzzy Logic for Fault Isolation of Jet Engines
J. Eng. Gas Turbines Power (July,2003)
Single Versus Dual Recycle System Dynamics of High Pressure Ratio, Low Inertia Centrifugal Compressor Stations
J. Eng. Gas Turbines Power (December,2011)
Related Proceedings Papers
Related Chapters
Pulsation and Vibration Analysis of Compression and Pumping Systems
Pipeline Pumping and Compression Systems: A Practical Approach, Second Edition
Pulsation and Vibration Analysis of Compression and Pumping Systems
Pipeline Pumping and Compression System: A Practical Approach, Third Edition
Aerodynamic Performance Analysis
Axial-Flow Compressors