The Technical Research of PHM in Aeronautical Mechanical and Electronical System Based on IETM

被引：38
|
作者：
Meng, Fei [1 ]
Yang, Jien [1 ]
Xu, Hang [1 ]
Li, Xiaolei [1 ]
机构：
[1] First Aeronaut Inst Air Force, Xinyang, Henan, Peoples R China
来源：
PROCEEDINGS OF THE FIRST SYMPOSIUM ON AVIATION MAINTENANCE AND MANAGEMENT, VOL I | 2014年 / 296卷
关键词：
IETM; PHM; Aviation mechatronics system;
D O I：
10.1007/978-3-642-54236-7_15
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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.
引用
收藏
页码：133 / 139
页数：7
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