The intercooled and recuperated processes were incorporated into the conventional high bypass turbofan engine thermodynamic cycle.Consequently
the intercooled recuperated aero-engine (IRA) simulation model was built and an overall performance simulation program was developed.Then
analysis on choosing and matching the thermodynamic cycle parameters of IRA was conducted.The result indicates that there are some thermodynamic cycle parameters such as intercooler effectiveness
recuperator effectiveness
bypass intercooling split
pressure ratio assignment between booster and high pressure compressor
overall pressure ratio and bypass ratio
which have significant influence on IRA performance.The turbofan engine performance can be improved with the proper use of intercooling
recuperation and the optimized matching of the thermodynamic cycle parameters.
Performance calculation and analysis of intercooled recuperated aero-engine
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Study on casing treatment stability extension and stator matching on multistage high-loading fan
Aero-engine cycle design approach for multiple operating conditions performance reliability
Related Author
KANG Yong
HUANG Hong-chao
LI Gang-tuan
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
Related Institution
China Gas Turbine Establishment, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics