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基于电涡流位移传感器的钛合金叶片振动疲劳试验研究
引用本文:张龙,邱荣凯,刘春辉,程俊,刘秉斌,廖文林.基于电涡流位移传感器的钛合金叶片振动疲劳试验研究[J].推进技术,2022,43(2):349-355.
作者姓名:张龙  邱荣凯  刘春辉  程俊  刘秉斌  廖文林
作者单位:1.中国空气动力研究与发展中心,四川 绵阳 621000;2.中国航空工业空气动力研究院,辽宁 沈阳 110034
基金项目:国家自然科学基金(51605476);全军装备军内科研项目(JK20202A040525)。
摘    要:为了研究钛合金叶片振动疲劳特性,基于电磁振动测试平台和非接触式电涡流位移传感器,开展了试验工装和试验程序设计。通过本文的传感器标定和振动应力标定方法研究,发展了基于电涡流位移传感器的非接触测量式钛合金叶片振动疲劳试验手段,进而完成了疲劳考核试验和裂纹扩展试验,研究了裂纹长度和固有频率随疲劳循环数累积的变化规律。试验结果表明,钛合金叶片具有较好的抗疲劳特性,疲劳裂纹萌生寿命较长,但裂纹扩展寿命较短。

关 键 词:钛合金叶片  振动疲劳  标定方法  振动应力  裂纹扩展
收稿时间:2021/1/6 0:00:00
修稿时间:2021/4/23 0:00:00

Experimental Study on Vibration Fatigue of Titanium Blades Using Eddy Current Displacement Sensor
ZHANG Long,QIU Rong-kai,LIU Chun-hui,CHENG Jun,LIU Bing-bin,LIAO Wen-lin.Experimental Study on Vibration Fatigue of Titanium Blades Using Eddy Current Displacement Sensor[J].Journal of Propulsion Technology,2022,43(2):349-355.
Authors:ZHANG Long  QIU Rong-kai  LIU Chun-hui  CHENG Jun  LIU Bing-bin  LIAO Wen-lin
Institution:1.China Aerodynamics Research and Development Center,Mianyang 621000,China;2.AVIC Aerodynamics Research Institute,Shenyang 110034,China
Abstract:In order to investigate the vibration fatigue characteristics of titanium alloy blades, experimental apparatus and procedures were designed on the basis of electromagnetic vibration platform and non-contact eddy current displacement sensor. Through the research of sensor calibration and vibration stress calibration methods in this paper, the non-contact-measuring vibration fatigue test method of titanium alloy blades based on eddy current displacement sensor was developed. Then, the fatigue stress experiment and crack propagation experiment were accomplished, where the variation laws of crack length and natural frequency with respect to accumulated fatigue cycles was studied. Experimental results demonstrated that the titanium alloy blades possessed good fatigue resistance with relatively long fatigue crack initiation life. However, their fatigue crack propagation life was relatively short.
Keywords:Titanium blades  Vibration fatigue  Calibration method  Vibration stress  Crack propagation
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