作者：徐锐¹, 徐红琴², 沈献绍¹, 曹昆华², 张宗林¹

作者单位：1. 解放军驻黎阳机械公司军事代表室, 贵州 平坝 561102;
2. 中航工业贵州航空发动机研究所, 贵州 平坝 561102

关键词：红外测温; 航空发动机; 测量准确度; 发射率; 热电偶; 确定

摘要：

该文论述了红外测温基本理论和红外测温仪工作原理,设计开发了适用于航空发动机轮盘试验的非接触红外测温系统,分析影响红外测温系统测量准确度的主要因素,研究发射率的确定方法,在轮盘静止和旋转状态下进行了试验验证。其结果表明:影响红外测温系统测量准确度最重要的因素是发射率;用热电偶对发射率进行确定的方法是可行的;轮盘在静止和旋转状态下的发射率相同,静止状态下确定的发射率可用于旋转状态下的温度测量。

Application of infrared temperature measurement system in aeroengine turbine disk test

XU Rui¹, XU Hong-qin², SHEN Xian-shao¹, CAO Kun-hua², ZHANG Zong-Lin¹

1. The PLA Representation Office at Liyang Machinery Company, Pingba 561102, China;
2. AVIC Guizhou AeroEngine Institute, Pingba 561102, China

Abstract: This paper discussed the basic theory of infrared temperature measurement and the working principle of infrared radiation thermometers. The authors designed and developed the non-contract infrared temperature measurement system suitable for aeroengine turbine disk test, analyzed the main factors which influence the measuring accuracy of the infrared temperature measurement system and researched the calibration method of emissivity. Test verification was carried out under the conditions of the turbine disk in static and in rotation respectively. The results showed that the most important factor which influences measuring accuracy of the infrared temperature measurement system was emissivity and the method of calibrating the emissivity with thermocouple is feasible and the emissivity of stationary state was same with its rotation station. The emissivity calibrated at stationary state can be used to measure the temperature of the aeroengine turbine disk at rotation station.

Keywords: infrared temperature measurement; aeroengine; measuring accuracy; emissivity; thermocouple; calibration

2012, 38(4): 32-35  收稿日期: 2011-8-7;收到修改稿日期: 2011-11-13

基金项目: 

作者简介: 徐锐(1981-),男,陕西礼泉县人,工程师,硕士,主要从事航空发动机试验测试质量监督工作。

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