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http://dx.doi.org/10.5139/JKSAS.2014.42.3.237

Control System of Turbofan Engine with Variable Inlet Guide Vane  

Bae, Kyoungwook (Graduate School of Department of Aerospace Engineering, Pusan National University)
Min, Chanoh (Graduate School of Department of Aerospace Engineering, Pusan National University)
Cheon, Bongkyu (Graduate School of Department of Aerospace Engineering, Pusan National University)
Lee, Changyong (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.42, no.3, 2014 , pp. 237-242 More about this Journal
Abstract
Surge phenomenon can be occurred in a compressor when the performance of turbofan engine for an aircraft is changed considerably such as take-off phase. This study is aimed to avoid surge phenomenon. This paper propose the PID and Fuzzy control System for the turbofan engine with control inputs, the VIGV(Variable Inlet Guide Vane) in closed loop, and the fuel mass flow in open loop. We design the Dynamic modeling, NPSS S-function, which is connection block of simulink between NPSS(Engine analysis program) and Simulink. Finally, we certify the performance to prevent a serge phenomenon in the VIGV control system using the both methods, PID and fuzzy.
Keywords
Variable Inlet Guide Vane; Compressor; Turbofan Engine; Surge; Simulink;
Citations & Related Records
Times Cited By KSCI : 4  (Citation Analysis)
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