Design and Experiment of Test System for Simulating Aero-Engine Burn Fragments Fault

被引:0
|
作者
Huang Manguo [1 ,2 ]
Liu Wei [1 ,2 ]
Liu Defeng [1 ,2 ]
Wang Yanshan [1 ,2 ]
Li Xin [1 ,2 ]
机构
[1] AVIC Beijing Changcheng Aeronaut Measurement & Co, Adv Sensor Technol Ctr, Beijing, Peoples R China
[2] Aviat Key Lab Sci & Technol Special Condit Monito, Beijing, Peoples R China
关键词
aero-engine; gas path fault; burn fragments; electrostatic monitoring; simulation test system;
D O I
暂无
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The aero-engine gas path fault is the important aero-engine fault and has high frequency. This fault must be found timely and solved as early as possible to make sure the normal work of aero-engine and the safe flight of the airplane. The burn fragments fault is a common fault aero-engine gas path fault. The special aero-engine gas path fault simulation test system is necessary if we want to study the burn fragments fault efficiently and deeply. Based on the electrostatic monitoring technology, a kind of test system of aero-engine gas path fault was designed in this paper, and the burn fragments fault was simulated by the test system. Finally, the experiments for aero-engine gas path faults simulations were performed, and the effectiveness of simulation test system of aero-engine gas path fault was verified.
引用
收藏
页码:444 / 448
页数:5
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