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航空发动机叶尖间隙测量技术研究进展
引用本文:许欧阳,童杏林.航空发动机叶尖间隙测量技术研究进展[J].半导体光电,2020,41(6):774-778.
作者姓名:许欧阳  童杏林
作者单位:武汉理工大学 光纤传感技术国家工程实验室, 武汉 430070
基金项目:国家“863”项目(2015AA043505);湖北省重大技术创新项目(2017ACA167).通信作者:童杏林E-mail:tongxinglin@whut.edu.cn
摘    要:系统介绍了国内外航空发动机叶尖间隙测量技术的研究进展,分析了这些技术的原理、特点及具体应用,并指出了发展方向。在此基础上,提出了适用于航空发动机高转速叶片在线监测的新方法,并介绍了一种可实现航空发动机叶片故障监测的膜片式高温光纤F-P声发射传感测量系统。

关 键 词:航空发动机    叶尖间隙    高温光纤    研究进展
收稿时间:2020/6/15 0:00:00

Research Progress of Aero-engine Blade Tip Clearance Measurement Technology
XU Ouyang,TONG Xinglin.Research Progress of Aero-engine Blade Tip Clearance Measurement Technology[J].Semiconductor Optoelectronics,2020,41(6):774-778.
Authors:XU Ouyang  TONG Xinglin
Affiliation:National Engineering Laboratory for Optical Fiber Sensing Technology, Wuhan University of Technology, Wuhan 430070, CHN
Abstract:The research progresses of the techniques for measuring the tip clearance of aero-engine are introduced, and their principles, characteristics and specific applications are analyzed, and the development trends are pointed out. Based on this research, a new method for on-line monitoring of high-speed blades of aeroengines is proposed, and a diaphragm-type high-temperature optical fiber F-P acoustic emission sensing measurement system is introduced to achieve aero-engine blade fault monitoring.
Keywords:aero-engine  blade tip clearance  high temperature fiber  research progress
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