Abstract
The operating range of aerodynamic compressors is usually limited by a phenomenon known as surge. Active surge control has showed the ability to extend the operating range significantly. This study presents a solution to this problem based on classical PID regulator and a new PI fuzzy logic approach with three lines of protection. The fuzzy controller is designed to avoid the surge instability on a given compressor model. Simulation studies show promising results at different operating points compared to the results obtained using PID controller.
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Abbreviations
- w :
-
The mass flow (kg/s)
- w f :
-
The feed flow (kg/s)
- w r :
-
The recycle flow (kg/s)
- w t :
-
The throttle flow (kg/s)
- a p :
-
The speed of sound = 343 m/s
- c p :
-
Specific heat at constant pressure (1,005 (J/kg K))
- v 1 :
-
Suction plenum volume 0.05 m3
- v 2 :
-
Discharge plenum volume 0.1 m3
- P 01 :
-
ambient pressure 101,325 Pa
- P 1 :
-
Section plenum pressure (Pa)
- P 2 :
-
Discharge plenum pressure (Pa)
- T 01 :
-
ambient temperature 20 °C
- A :
-
Duct area 0.07 m
- L :
-
Duct length 2.85 m
- Ψc(w, Ω):
-
The pressure rise
- τd :
-
Drive torque
- τc :
-
Compressor torque
- μ :
-
Energy transfer coefficient 0.99
- r1 :
-
Inducer perimeter radius 0.0395 m
- r2 :
-
Impeller perimeter radius 0.0565 m
- a :
-
Constant of incidence loss
- k f :
-
Friction constant
- k :
-
Isentropic exponent
- c p :
-
Specific heat at constant pressure
- c v :
-
Specific heat at constant volume
- ξ :
-
1,000
- c f :
-
The percentage feed opening valve
- c r :
-
The percentage recycle opening valve Pressure of the feed valve
- Ω:
-
The speed (rad/s)
- J :
-
The impeller inertia 5e−4 kg m2
- P upstream :
-
Upstream pressure
- DSL:
-
Low deviation to the control line
- DSLL:
-
Low Low deviation to the control line
- SCL:
-
Surge control line
- DSH:
-
High deviation between operating point and control line (surge region)
References
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Chetate, B., Zamoum, R., Fegriche, A. et al. PID and Novel Approach of PI Fuzzy Logic Controllers for Active Surge in Centrifugal Compressor. Arab J Sci Eng 38, 1405–1414 (2013). https://doi.org/10.1007/s13369-013-0601-6
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DOI: https://doi.org/10.1007/s13369-013-0601-6