基于气体温度阶跃法的热电偶响应时间常数校准装置
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1.贵州航天计量测试技术研究所;2.贵州师范大学

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TB9

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多物理量耦合的复杂环境下气体传感系统校准技术研究


Calibration Device for Thermocouple Response Time Constant Based on the Gas Temperature Step Method
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1.Guizhou AerospaceInstitute of Measuring and Testing Technology,Guiyang;2.Guizhou Normal University,Guiyang

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    摘要:

    为满足气体介质条件下快响应K型热电偶响应时间常数的校准需求,研制基于气体温度阶跃法的热电偶响应时间常数校准装置。通过理论计算确定加热器功率、节流孔面积、喷嘴流量等关键参数,利用Ansys Fluent软件进行仿真以优化阶跃温度发生模块结构。提出基于动态压力同步监测的校准方法,以压力阶跃时刻为基准,规避非理想激励干扰,确保响应时间常数计算精准。利用基于气体温度阶跃法的热电偶响应时间常数校准装置进行试验,结果表明:该装置产生的气体温度阶跃幅值达到200 ℃以上,温度阶跃激励时间约为2.2 ms,能够有效实现不同偶丝直径的K型热电偶响应时间常数校准,具有重要工程应用价值。

    Abstract:

    To address the calibration demand for the response time constant of fast-response K-type thermocouples under gas medium conditions, a calibration device based on the gas temperature step method was developed. Key parameters including heater power, orifice area, and nozzle flow rate were determined via theoretical calculations, and Ansys Fluent software was utilized for simulation to optimize the structure of the step temperature generation module. A calibration method based on synchronous dynamic pressure monitoring was proposed, which takes the pressure step moment as the reference to eliminate non-ideal excitation interference and ensure the calculation accuracy of the response time constant. Experimental tests were conducted using the developed device, and the results indicate that the gas temperature step amplitude generated by the device exceeds 200 ℃ with a temperature step excitation time of approximately 2.2 ms. The device can effectively calibrate the response time constant of K-type thermocouples with different wire diameters, demonstrating significant engineering application value.

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  • 收稿日期:2025-10-14
  • 最后修改日期:2025-11-30
  • 录用日期:2025-12-01
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