To explore the development path and future development trend of carrier-based advanced trainer engine
three development stages of advanced trainer engine were summarized
the technical performance requirements of carrier-based advanced trainer engine and the current situation of carrier-based advanced trainer engine abroad were emphatically analyzed. It was found that the carrier-based advanced trainer engine should be developed based on mature turbofan engines for long life
wide flight envelope
low fuel consumption
strong performance retention
easy maintenance and “sea adaptation”
or a mature carrier-based fighter power with lower status was chosen
according to the aircraft platform power demand. In the future it would be further developed in the aspects of higher weight ratio
lower fuel consumption
greater extraction power
longer service life and aircraft-engine integration design.
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
ptimum design of rotor structure layout and its mechanical properties
Aero-engine exhaust gas temperature prediction model based on IFOA-GRNN
Related Author
ZHU Jianqin
ZHAO Chaofan
QIU Lu
曹大录
白广忱
吕晶薇
肖翼
郭秩维
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics