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航空发动机涡轮叶片温度测量综述
引用本文:王超,苟学科,段英,胡俊,张泽展,杨洋,姜晶,蒋洪川,丁杰雄,程玉华,李力,张江梅,陈洪敏,熊兵,刘先富,石小江. 航空发动机涡轮叶片温度测量综述[J]. 红外与毫米波学报, 2018, 37(4): 501-512
作者姓名:王超  苟学科  段英  胡俊  张泽展  杨洋  姜晶  蒋洪川  丁杰雄  程玉华  李力  张江梅  陈洪敏  熊兵  刘先富  石小江
作者单位:电子科技大学电子科学与工程学院;电子科技大学机械与电气工程学院;电子科技大学自动化工程学院;西南科技大学信息工程学院;中国航发四川燃气涡轮研究院
基金项目:装备预研教育部联合基金(14JL163502A);国家自然科学基金(No.61727818,51672037);四川省科技计划项目(2016JQ0022);国家重点研发计划(2017YFC0602102)
摘    要:简要介绍了航空发动机涡轮叶片表面温度的几种主要测量方法,总结了热电偶、晶体、示温漆、荧光、光纤、以及红外辐射、多光谱等测温方法的的测温原理、技术特点和国内外研究现状,并在此基础上对将来涡轮叶片温度测量发展方向进行了展望.

关 键 词:涡轮叶片  温度测量  辐射测温
收稿时间:2017-12-08
修稿时间:2018-05-24

A review of aero-engine turbine blade temperature measurement
WANG Chao,GOU Xue-Ke,DUAN Ying,HU Jun,ZhANG Ze-Zhan,YANG Yang,JIANG Jing,JIANG Hong-Chuan,DING Jie-Xiong,CHENG Yu-Hu,LI Li,ZHANG Jiang-Mei,CHEN Hong-Min,XIONG Bing,LIU Xian-Fu and SHI Xiao-Jiang. A review of aero-engine turbine blade temperature measurement[J]. Journal of Infrared and Millimeter Waves, 2018, 37(4): 501-512
Authors:WANG Chao  GOU Xue-Ke  DUAN Ying  HU Jun  ZhANG Ze-Zhan  YANG Yang  JIANG Jing  JIANG Hong-Chuan  DING Jie-Xiong  CHENG Yu-Hu  LI Li  ZHANG Jiang-Mei  CHEN Hong-Min  XIONG Bing  LIU Xian-Fu  SHI Xiao-Jiang
Affiliation:School of Electronic Science and Engineering, Univ.of Electronic Science and Technology of China,Coll of Microelectronics and Solid-state Electronics,Univ of Electronic Science and Technology of China,Coll of Microelectronics and Solid-state Electronics,Univ of Electronic Science and Technology of China,Coll of Microelectronics and Solid-state Electronics,Univ of Electronic Science and Technology of China,Coll of Microelectronics and Solid-state Electronics,Univ of Electronic Science and Technology of China,Coll of Microelectronics and Solid-state Electronics,Univ of Electronic Science and Technology of China,Coll of Microelectronics and Solid-state Electronics,Univ of Electronic Science and Technology of China,Coll of Mechatronics Engineer,Univ of Electronic Science and Technology of China,Coll of Automation Engineer,Univ of Electronic Science and Technology of China,AVIC Gas Turbine Establishment,AVIC Gas Turbine Establishment and AVIC Gas Turbine Establishment
Abstract:The paper briefly introduces several main temperature measurement methods of aero-engine turbine blades, and summarizes the temperature measurement principle, technical characteristics and current research status of thermocouple, crystal, temperature sensitive paint, fluorescence, optical fiber, infrared radiation and multispectral. Finally, the future development trend of turbine blade temperature measurement is prospected.
Keywords:turbine blade   temperature measurement   radiation temperature measurement
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