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VIS-NIR multispectral synchronous imaging pyrometer for high-temperature measurements.
Fu, Tairan; Liu, Jiangfan; Tian, Jibin.
Afiliación
  • Fu T; Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Beijing Key Laboratory of CO Utilization and Reduction Technology, Department of Thermal Engineering, Tsinghua University, Beijing 100084, People's Republic of China.
  • Liu J; Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Beijing Key Laboratory of CO Utilization and Reduction Technology, Department of Thermal Engineering, Tsinghua University, Beijing 100084, People's Republic of China.
  • Tian J; Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Beijing Key Laboratory of CO Utilization and Reduction Technology, Department of Thermal Engineering, Tsinghua University, Beijing 100084, People's Republic of China.
Rev Sci Instrum ; 88(6): 064902, 2017 Jun.
Article en En | MEDLINE | ID: mdl-28667994
ABSTRACT
A visible-infrared multispectral synchronous imaging pyrometer was developed for simultaneous, multispectral, two-dimensional high temperature measurements. The multispectral image pyrometer uses prism separation construction in the spectrum range of 650-950 nm and multi-sensor fusion of three CCD sensors for high-temperature measurements. The pyrometer had 650-750 nm, 750-850 nm, and 850-950 nm channels all with the same optical path. The wavelength choice for each channel is flexible with three center wavelengths (700 nm, 810 nm, and 920 nm) with a full width at half maximum of the spectrum of 3 nm used here. The three image sensors were precisely aligned to avoid spectrum artifacts by micro-mechanical adjustments of the sensors relative to each other to position them within a quarter pixel of each other. The pyrometer was calibrated with the standard blackbody source, and the temperature measurement uncertainty was within 0.21 °C-0.99 °C in the temperatures of 600 °C-1800 °C for the blackbody measurements. The pyrometer was then used to measure the leading edge temperatures of a ceramics model exposed to high-enthalpy plasma aerodynamic heating environment to verify the system applicability. The measured temperature ranges are 701-991 °C, 701-1134 °C, and 701-834 °C at the heating transient, steady state, and cooling transient times. A significant temperature gradient (170 °C/mm) was observed away from the leading edge facing the plasma jet during the steady state heating time. The temperature non-uniformity on the surface occurs during the entire aerodynamic heating process. However, the temperature distribution becomes more uniform after the heater is shut down and the experimental model is naturally cooled. This result shows that the multispectral simultaneous image measurement mode provides a wider temperature range for one imaging measurement of high spatial temperature gradients in transient applications.

Texto completo: 1 Colección: 01-internacional Banco de datos: MEDLINE Idioma: En Revista: Rev Sci Instrum Año: 2017 Tipo del documento: Article

Texto completo: 1 Colección: 01-internacional Banco de datos: MEDLINE Idioma: En Revista: Rev Sci Instrum Año: 2017 Tipo del documento: Article