Turbofan Motor Hareketli Yüzey Kontrol Ünitesi ve Aktüatörleri Tasarımı

Moving surface control unit and actuators will be designed to be integrated into the domestic and national turbofan engine that will power the Kızılelma aircraft platform. It is aimed to control the variable angle stator blades and exhaust nozzle in the turbofan engine with high oil pressure actuators. An electrohydromechanical control unit will be designed to control the actuators with the command received from the control system. A robust control algorithm will be created by examining the effect of the actuators' positions on the engine performance.