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MATERIALS SURFACE EMISSIVITY ANALYSES PERFORMED BY THE COMBINED USE OF DUAL AND SINGLE COLOR OPTICAL PYROMETERS

机译:通过组合使用双重和单色光学磁仪进行材料表面发射率分析

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The experimental determination of spectral emissivity of the surface of materials for thermal protection systems of re-entry vehicles in the Earth's atmosphere has always been a target during tests in the hypersonic plasma ground simulators. By this way, the application of non-intrusive optical devices, such as infrared pyrometers able to measure the surface temperature, makes possible the evaluation of emissivity of the surface of tested materials at different temperature values. The combined use of different types of pyrometers makes possible the emissivity evaluation by means of the comparison between the temperature values measured by dual color pyrometers and single color ones. By this way, some preliminary experiments were performed in air and at ambient pressure on metallic sample: optical pyrometers of dual color type and single color one, at different wavelengths, have been used to measure surface temperature and then to obtain values of spectral emissivity. In particular, a sample of OFHC Copper was installed on a quartz beam and then inserted inside the graphite spherical cavity of a black body in the temperature range from 400°C to 900°C. Moreover a K-type thermocouple installed in the sample through the quartz beam, was used during the tests in order to obtain an independent measurement of the sample temperature. In the copper-based sample the oxidation of the surface during the test has been observed with the formation of a grey surface scale. Thermogravimetric analysis (TGA) performed in air on a fraction of that corrosion scale has excluded the presence of graphite allowing to confirm that the cavity of black body is not able to contaminate the surface of tested samples by releasing of graphite gaseous during tests. By combining the temperatures measured by the pyrometers and the thermocouple the spectral emissivity of the samples as function of temperature at three different wavelengths has been determined. Moreover, the agreement between the experimental emissivity determined and the emissivity predicted by semi-empirical formulas has been verified.
机译:的用于在地球大气层再入飞行器的热保护系统的材料的表面的光谱辐射率的实验测定期间,在高超音速等离子体接地模拟器测试一直是一个目标。通过这种方式,非侵入式光学装置(例如红外高温计)能够测量表面温度的应用,可以在不同温度值下评估测试材料表面的发射率。不同类型的高温计的组合使用通过通过双色高温计和单个颜色的温度值之间的比较来实现发射率评估。通过这种方式,在空气中进行一些初步实验,在金属样品上进行环境压力:双色型和单色的光学蒸烟器,在不同的波长下,已经用于测量表面温度,然后获得光谱发射率的值。特别地,OFHC铜样品安装在石英梁上,然后在黑色体的石墨球形腔内插入400℃至900℃的温度范围内。此外,在测试期间使用在样品中安装在样品中的K型热电偶,以获得独立测量样品温度。在基于铜的样品中,通过形成灰色表面刻度,观察到测试期间表面的氧化。在空气中在空气中进行的热量标注分析(TGA)在腐蚀量的一部分中排除了石墨的存在,允许确认黑体的腔不能通过在测试期间通过释放石墨气体来污染测试样品的表面。通过将高温计测量的温度与热电偶相结合,确定了样品的光谱发射率作为温度在三种不同波长的函数中。此外,确定了实验发射率之间的协议,并验证了半经验公式预测的发射率。

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