Turbofan Motor Yağlama Sistemi Mimarisi ve Alt Komponent Tasarımı

The lubrication system architecture will be designed to be integrated into the domestic and national turbofan engine that will power the Kızılelma aircraft platform. Subcomponents such as sensors, oil tank, oil pump, oil filter and valves, hydraulic actuators will be designed according to the requirements of the designed architecture. System parameters such as pressure, flow rate, speed and losses will be calculated and oil flow analysis will be performed.