By introducing and summarizing the traditional safety analysis method
a model-based safety analysis process and method for aero-engine were proposed. From the property of the aero-engine
unified safety analysis and performance design achieved the goal of balance between them. This could guarantee the consistency
integrity and objective of the analysis results. The three key technical breakthroughs during the safety analysis process and method are:(1) the description method of failure modes; (2) the classification and location methods of the key impact factors; (3) safety analysis verification methods.
Review of probabilistic risk assessment on aero-engine airworthiness
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
Civil turboshaft engine induction system icing test
Related Author
DING Shui-ting
ZHANG Gong
YU Duo-kui
ZHOU Yan-pei
WANG Xiaoming
GONG Lifeng
XIONG Qingyong
LUO Mingzhi
Related Institution
Airworthiness Technologies Research Center, National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China
Center of Aviation Safety Technology, Civil Aviation Administration of China