基于气体温度阶跃法的热电偶时间常数校准装置设计
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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


Design of a thermocouple time constant calibration device 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:

    针对快响应热电偶响应时间常数校准缺乏有效手段的问题,研制了基于气体温度阶跃法的热电偶时间常数校准装置。通过理论计算,并利用Ansys fluent进行仿真,对校准装置的整体结构、气源及加热器、阶跃温度发生模块和校准工作流程进行了设计,介绍了热电偶响应时间常数的校准方法。对校准装置进行试验,结果表明:气体温度阶跃幅值达到200℃以上,温度阶跃激励时间约为2.2ms,可实现快响应热电偶响应时间常数的校准。

    Abstract:

    Aiming at the lack of effective methods for calibrating the response time constant of fast-response thermocouples, a thermocouple time constant calibration device based on the gas temperature step method was developed. Through theoretical calculations and simulations using Ansys Fluent, the overall structure of the calibration device, gas source and heater, step temperature generation module, and calibration workflow were designed, and the calibration method for the thermocouple response time constant was introduced. Tests were conducted on the calibration device, and the results show that the gas temperature step amplitude reaches more than 200°C, and the temperature step excitation time is approximately 2.2 ms, which can realize the calibration of the response time constant of fast-response thermocouples.

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  • 收稿日期:2025-10-14
  • 最后修改日期:2025-11-15
  • 录用日期:2025-11-20
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