微型晶体测温技术发展
摘要
将微型晶体测温技术应用于航空发动机的温度测量试验一直是前沿性的热点研究方向。微型晶体测温技术能够在航空发动机复杂的试验环境中取得高试验成活率,是解决航空发动机表面、气流温度测量的理想方法。
引文
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[7]Ruan Y F, Wang P F, Huang L, et al. HighTemperature Sensor Based on Neutron-Irradiated6H-SiC[J]. Key Engineering Materials, 2011,495:335-338.
[8]王鹏飞.中子辐照6H-SiC的缺陷分析与应用[D].天津:天津大学,2013.
[9]张兴,张志学,薛秀生,等.航空发动机测温晶体的退火特性研究[J].航空发动机,2013,39(4):72-77.
[2]Volinsky A A,Ginzbursky L. Irradiated Cubic Single Crystal SiC as a High Temperature Sen-sor[J]. Mrs Proceedings,2003,792.
[3]Malak M, Jong L, Khosro M. Further Investigation into Hot Gas Ingestion into Turbine Shroud Cavity Using Uniform Crystal Temperature Sensors Measurement for Baseline Configuration[R].ISABE2015-20142, 2015.
[4]Brown J, Devoe J, Ginzbursky L.The Challenges of Uniform Crystal Temperature Sensor(UCTS)Application in Turbomachinery[C]//ASME Turbo Expo2013:Turbine Technical Conference and Exposition,2013:V03CT14A030.
[5]李杨,李志敏,李华臣,等.航空发动机微型晶体测温技术[J].航空动力,2018(2).
[6]Shukin S, Annerfeldt M, Bjorkman M. Siemens SCGT-800 Industrial Gas Turbine Enhanced to 47MW.Design Modifications and Operation Experience:ASME Turbo Expo:SE-612 83[R]. Fin-Spong:Sweden, 2008.
[7]Ruan Y F, Wang P F, Huang L, et al. HighTemperature Sensor Based on Neutron-Irradiated6H-SiC[J]. Key Engineering Materials, 2011,495:335-338.
[8]王鹏飞.中子辐照6H-SiC的缺陷分析与应用[D].天津:天津大学,2013.
[9]张兴,张志学,薛秀生,等.航空发动机测温晶体的退火特性研究[J].航空发动机,2013,39(4):72-77.