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首页> 外文期刊>International Journal of Thermophysics >Processing Method of Multi-Wavelength Pyrometer Data for Continuous Temperature Measurements
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Processing Method of Multi-Wavelength Pyrometer Data for Continuous Temperature Measurements

机译:用于连续温度测量的多波长高温计数据的处理方法

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摘要

The processing of multi-wavelength pyrometer data is a problem that needs further improvements. The solutions developed in earlier decades generally assumed one particular mathematical relation for emissivity versus wavelength in the wavelength range of the measurements. Sometimes this assumption worked and produced acceptable results, but in many other cases this approach provided erroneous results. Individual results were strongly dependent on the assumed mathematical relation that often needed some prior knowledge of the emissivity behavior in the wavelength range. A new data processing method for a multi-wavelength pyrometer for continuous temperature measurements is presented. A linear relation between emissivity and true temperature at different wavelengths is assumed. Based on this assumption, the true temperatures and spectral emissivities at the two continuous temperature measurement points can be simultaneously calculated. Some experimental results for the practical data processing of measurements performed on a solid propellant rocket engine show that the difference between the calculated true temperature and the theoretical true temperature indicated by the rocket engine designer is within ±20 K.
机译:多波长高温计数据的处理是一个需要进一步改进的问题。几十年前开发的解决方案通常假设发射率与测量波长范围内的波长之间存在一种特殊的数学关系。有时,这种假设起作用并产生可接受的结果,但是在许多其他情况下,此方法提供了错误的结果。各个结果在很大程度上取决于假定的数学关系,该数学关系通常需要对波长范围内的辐射率行为有一些先验知识。提出了一种用于多波长高温计连续温度测量的新数据处理方法。假设在不同波长下发射率与真实温度之间存在线性关系。基于此假设,可以同时计算两个连续温度测量点的真实温度和光谱发射率。对固体推进剂火箭发动机进行的测量的实际数据处理的一些实验结果表明,计算出的真实温度与火箭发动机设计者指示的理论真实温度之间的差在±20 K之内。

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