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http://dx.doi.org/10.5139/JKSAS.2013.41.7.539

Surge Control of Turbofan Engine Compressor with the Variable Inlet Guide Vane  

Bae, Kyoungwook (Graduate School of Department of Aerospace Engineering, Pusan National University)
Kim, Sangjo (Graduate School of Department of Aerospace Engineering, Pusan National University)
Han, Dongin (Graduate School of Department of Aerospace Engineering, Pusan National University)
Min, Chanoh (Graduate School of Department of Aerospace Engineering, Pusan National University)
Lee, Daewoo (Department of Aerospace Engineering, Pusan National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.41, no.7, 2013 , pp. 539-546 More about this Journal
Abstract
Surge phenomenon can be occurred in a compressor when compressor performance of turbofan engine for an aircraft is changed considerably in a short time on the cases like take-off phase and changing of RPM from idle to maximum, because performance of aircraft engine is changed suddenly. This study is aimed to avoid surge in a compressor. Dynamic simulation in a compressor is modeled by simulink in specific condition. Fuel flow is control input, rpm and air mass flow are expressed in terms of transfer function. Surge margin is obtained by using compressor performance map from NPSS. VIGV(Variable Inlet Guide Vane) is controlled by PD controller with difference between surge margin and reference. Finally this paper verifies IGV can prevent surge phenomenon in a compressor.
Keywords
Variable Inlet Guide Vane; Compressor; Turbofan Engine; Surge; Simulink;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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