In order to make the error of aero-engine reliability model smaller
error analysis was made for traditional aero-engine reliability model
the reason that reliability indexes over expand was pointed out
and the aero-engine reliability model based on failure modes in structural system considering aero-engine structural system and the failure mechanics characteristics was established. The reliability calculation method of each layer was given. Structural system reliability model of aero-engine based on failure modes
which considers relative independence
timeliness and time varying of failure rate
can avoid problems such as missing important failure modes and over expansion of reliability index
Research status and development trend of condition monitoring on main⁃shaft bearings used in aircraft engines
Development path and future trend of carrier-based advanced trainer engine
Method of failure mode analysis and test verification for fiber reinforced composites turbo-shaft structure
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Related Author
Peng LIU
Liqin WANG
Chuanwei ZHANG
Dezhi ZHENG
PENG Yunlong
WU Xiong
DING Ting
LUO Li
Related Institution
Ministry of Industry and Information Technology Key Laboratory of Aerospace Bearing Technology and Equipment,Harbin Institute of Technology
State Key Laboratory of Robotics and System,Harbin Institute of Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics