Development status and trends of aero-engine containment case were reviewed in respect of the containment capability definition
case material
design concept and method
validity testing
numerical simulation
failure and deformation patterns of case and released blade.Requirements of lightweight fan case with high containment capability for the development of high bypass pressure ratio turbofan engine have been illustrated.Therefore
different structure designs of fan case of in-service and developing aero-engine for large airplane were presented
and researches on containment capability of fiber reinforced composite fan case were reviewed.The development directions of containment case for Chinese high thrust/weight engine and low-pollution civilian engine were proposed
respectively
with regard to structure improvement
low-cost manufacturing technology for composite fan case
winding pattern of full composite case
high temperature composite case
multi-disciplinary simulation of engine blade out event and smart containment case.
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
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
ptimum design of rotor structure layout and its mechanical properties
Related Author
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
QIU Lu
曹大录
白广忱
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