期刊文献+

铋层状与铌酸锂复合压电陶瓷传感器的温度特性 被引量:5

Temperature Characteristics of a Bi_4Ti_3O_(12)-LiNbO_3 Compound Piezoelectric Ceramic Sensor
下载PDF
导出
摘要 铋层状结构铁电体具有良好的机械性能和较高的居里温度Tc,因而被广泛用作高温传感器的敏感器件.高温压电传感器在核能、燃气轮机、航空、舰船发动机以及需要测量高温振动和压力的场合有着极大需求,但目前国内外用于这些领域的基于铋层状压电传感器在高温时的灵敏度与常温时比较,漂移率达到10%~20%,无法满足满温度范围内(-50~450℃)传感器的灵敏度温漂的要求(≤±5%).因此,本文研究了一种铋层状与铌酸锂复合的压电陶瓷传感器,进行了传感器温度特性理论分析,建立了相应数学模型,并进行实验验证.测试结果表明,这种新型复合式压电陶瓷传感器满温度量程灵敏度漂移小于±3%,具有优异的温度特性,无需采用软件修正测量偏差,能满足美国航空无线电技术委员会(RTCA)制定的DO160要求,可直接用于高温环境的温度精密测量. Bi4 Ti3 O12 has been wildly used on high temperature sensor due to its excellent mechanical performance and high curie temperature.There is a lot of the demand for high temperature sensors in the industries, such as nuclear energy, turbo engine of avia- tion and ship as well as other high temperature testing applications. However, comparison with working at room temperature, the sensor based on Bi4 Tia O12 material has a sensitivity shift of 10 %-20 % when in the high temperature, and fails to meet the require- ment of ≤± 5 % in the temperature range from -50 ℃ to 450 ℃ .In order to address this problem, a new type of structural composite piezoelectric sensor that based on Bi4 Ti3 O12-LiNbOa is studied and developed.In this paper, the main research work are presented, which the temperature characteristic is analyzed theoretically, and the mathematical model is established and the experimental study is carried out for the sensor.h has shown from the testing results, this new type of structural composite piezoelectric sensor has an extraordinarily good temperature characteristic and has a sensitivity shift of full temperature range less than ± 30% .Moreover,it does not require software to correct measurement deviation.It can be directly used in high temperature environment and is able to meet DO160 regulatory requirement of Radio Technical Commission for Aeronautics (RTCA).Therefore,this new type of sensor has the broad application prospects.
出处 《厦门大学学报(自然科学版)》 CAS CSCD 北大核心 2016年第3期441-444,共4页 Journal of Xiamen University:Natural Science
基金 福建省自然科学基金(2013J01251)
关键词 高温压电传感器 温度漂移 温度补偿 BI4TI3O12 LINBO3 high temperature piezoelectric sensor temperature shift temperature compensation Bi4 Ti3 O12 LiNbOs
  • 相关文献

参考文献6

  • 1JENNIONS I K.Integrated vehicle health management:perspective on an emerging field[M]. New York,USA:SAE International,2011 : 124-135.
  • 2何必海,马向东,郎振.民用航空发动机振动监测方法研究[J].燃气涡轮试验与研究,2012,25(2):59-62. 被引量:4
  • 3DOANE P M, KINLEY W R. Inflight engine conditionmonitoring system,F/A-l8[R].Washington DC: AIAA,2001:3069-3082.
  • 4蔚瑄楷,杨立,战立光,等.航空发动机预测与健康管理[M].北京:国防工业出版社,2014 :198-221.
  • 5SHULMAN H S,TESTORF M D, SETTER N. Micro-structure? electronic conductivity,and piezoelectric prop-erties of bismuth titanate[J].Journal of the American Ce-ramic Society,1996,79(12) :3124-3128.
  • 6胡天林,谢海鹤,颜黄苹,黄元庆.电涡流位移传感器测量模型及其在叶尖间隙测量中的空间滤波效应[J].厦门大学学报(自然科学版),2014,53(1):66-70. 被引量:4

二级参考文献10

  • 1CCAR-25-R3.运输类飞机适航标准[S].中国:中国民用航空局,2001.
  • 2Doane P M, Kinley W R. F/A-18 Inflight Engine Condi- tion Monitoring System[R]. AIAA 83-1237,1983.
  • 3Jang C M, Gukano T, Furukawa M. Effects of the tip clearanceon vertical flow and its relation to noise in an ax- ial flow fan [J] JSME International Journal, 2003, 46: 356-365.
  • 4Wiseman,M W,Guo T.An investigation of life extending control techniques for gas turbine engines [C] // Proceedings of the American Control Conference. Arling- ton, VA : IEEE, 2001,5:3706-3707.
  • 5E1-Batsh H M, Hanna M B.An investigation on the effect of endwall movement on the tip clearance loss using an- nular turbine cascade[J].International Journal of Rotating Machinery,2011(2011) :489150.
  • 6Tappert P, von Flotow A, Mercadal M. Autonomous PHM with blade-tip sensors:algorithms and seeded fault experience[C] // Aerospace Conference Proceedings. Big Sky, MT: IEEE, 2001,7 : 3287-3295.
  • 7Woike M R,Abdul-Aziz A,Bencic T J.A microwave blade tip clearance sensor for propulsion health monitoring[R]. Washington D C : NASA, 2010.
  • 8Lawson C P, Ivey P C. Tubomachinery blade vibration amplitude measurement through tip timing with capaci- tance tip clearance probes[J].Sensors and Actuators A, 2005,118:14-24.
  • 9Holst T A.Analysis of spatial filtering in phase-based mi- crowave measurements of turbine blade tips [D].Atlanta: Georgia Institute of Technology, 2005.
  • 10Beauseroy P, Lengelle R.Nonintrusive turbomachine blade vibration measurement system[J]. Mechanical Systems and Signal Processing,2007,21(4):1717-1738.

共引文献6

同被引文献22

引证文献5

二级引证文献15

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部