In order to analyze the oil systems characteristics and study the coperative working and design problems involving aero-engine
a general simulation block library for its components was developed in MATLAB/Simulink based on flow rate
pressure and heat transfer characteristics. Then a full-system simulation model was established
including supply
return, air and thermal system. Taking a certain turbofan engine and its oil system as example
the main working parameters of the oil system were calculated under high temperature taking off condition. Compared with the calculated values of Flowmaster model
the relative error was less than 3.8%. Through the extension ability of the full-system simulation model
a co-simulation with GasTurb engine model was successfully implemented and the oil systems design parameters were optimized through genetic algorithm. The highest temperature of return oil decreased by 4.12% by changing the oil supply ratio. This method can provided a reference for oil system design and improvement.
Quasi-steady flow model of slot-type casing treatments Ⅱ: design optimization of casing treatment for a transonic rotor
Steady Pressure Model of the Aeroengine Oil System
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Related Author
FAN Lin
NING Fang-fei
LIU Huo-xing
MA Zhuang
CHENG Li
PENG Yunlong
WU Xiong
DING Ting
Related Institution
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Air Force Engineering University
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics