The Technical Research of PHM in Aeronautical Mechanical and Electronical System Based on IETM
The key parameters of aero-engine reflect the varieties of the system at a certain extent.The varieties will represent affirmatively when the system will or has appeared failure.Through the methods of modeling the key data which reflect aero-engine capability,vibration,and abrasion,the failure prognostics curves can be fit based on the working data in practice.By using the PHM curves to prognose the intending values,it has extraordinary meaning for predicting the aero-engine states in advance and making the maintenance steps available in order to avoid momentousness accidents.
IETM PHM Aviation mechatronics system
Fei Meng Jien Yang Hang Xu Xiaolei Li
The First Aeronautic Institute of Air Force, Xinyang, Henan, China
国际会议
西安
英文
133-139
2013-11-25（万方平台首次上网日期，不代表论文的发表时间）