In order to meet the urgent needs of developing large commercial aero-engines which satisfies the airworthiness requirments
the fundamental methodology and development progress of probabilistic risk assessment (PRA) of life limited parts in recent years were discussed. The PRA technologies
including their processes and characteristics
were described to show their compliance with the life-limited parts requirements set forth in section 33.70 of federal aviation regulations (FAR). Moreover
the core methodology and basic database structure of PRA were analyzed. It indicates that the PRA methodology should be established on the basis of combining the probabilistic fracture mechanism with accurate databases.
Research on model-based safety analysis for aero-engine
Probabilistic failure risk assessment method of turbine engine life limited parts for airworthiness requirements
Development history of civil turbine engine endurance test requirements
Speed prediction for power turbine rotors of turboshaft engine on loss-of-load
Aero-engine stall/surge airworthiness certification method under the influence of crosswind
Related Author
BAO Meng-yao
LI Guo
DING Shui-ting
ZHANG Gong
ZHOU Yan-pei
DING Shui-ting
WANG Xiaoming
GONG Lifeng
Related Institution
Department of Aircraft Airworthiness Certification, Civil Aviation Management Institute 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
Engine Certification Center, Civil Aviation Administration of China
Aeroengine Airworthiness Certification Center Preparatory Office, China Academy of Civil Aviation Science and Technology
School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics