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    • 3. 发明授权
    • Hot gas temperature measurement in gas turbine using tunable diode laser
    • 燃气轮机采用可调二极管激光器进行热气体温度测量
    • US08702302B2
    • 2014-04-22
    • US12880681
    • 2010-09-13
    • Vivek Venugopal BadamiScott Mordin HoyteChayan MitraAyan Banerjee
    • Vivek Venugopal BadamiScott Mordin HoyteChayan MitraAyan Banerjee
    • G01K7/00
    • G01K13/02G01J3/108G01J3/427G01K11/12G01K2013/024
    • A combustion gas measurement apparatus mounted in a gas turbine including: a tunable laser generating a radiation beam passing through a combustion gas path; a controller tuning the laser to emit radiation having at least a first selected wavelength and a second selected wavelength which both correspond to temperature-dependent transitions of a combustion species of the gas, wherein the first selected wavelength and the second selected wavelength are not near absorption peaks of neighboring wavelengths; a detector sensing the radiation beam passing through the combustion gas and generating an absorption signal indicative of an absorption of the beam by the combustion gas at each of the first wavelength and the second wavelength, and a processor executing a program stored on a non-transitory storage medium determining a combustion gas temperature based on a ratio of the adoption signals for the first wavelength and the second wavelength.
    • 一种安装在燃气轮机中的燃烧气体测量装置,包括:可调谐激光器,其产生通过燃烧气体路径的辐射束; 调谐所述激光器以发射具有至少第一选定波长和第二选定波长的辐射的控制器,其对应于所述气体的燃烧物质的温度依赖性跃迁,其中所述第一选定波长和所述第二选定波长不接近吸收 相邻波长的峰; 检测器,其感测通过燃烧气体的辐射束,并且产生指示在第一波长和第二波长中的每一个处由燃烧气体吸收光束的吸收信号,以及处理器,其执行存储在非瞬时的程序 存储介质基于第一波长和第二波长的采用信号的比率来确定燃烧气体温度。
    • 4. 发明申请
    • HOT GAS TEMPERATURE MEASUREMENT IN GAS TURBINE USING TUNABLE DIODE LASER
    • 使用可旋转二极管激光器在气体涡轮机中进行热气温度测量
    • US20120060510A1
    • 2012-03-15
    • US12880681
    • 2010-09-13
    • Vivek Venugopal BadamiScott Mordin HoyteChayan MitraAyan Banerjee
    • Vivek Venugopal BadamiScott Mordin HoyteChayan MitraAyan Banerjee
    • F02C7/20H01S3/10
    • G01K13/02G01J3/108G01J3/427G01K11/12G01K2013/024
    • A combustion gas measurement apparatus mounted in a gas turbine including: a tunable laser generating a radiation beam passing through a combustion gas path; a controller tuning the laser to emit radiation having at least a first selected wavelength and a second selected wavelength which both correspond to temperature-dependent transitions of a combustion species of the gas, wherein the first selected wavelength and the second selected wavelength are not near absorption peaks of neighboring wavelengths; a detector sensing the radiation beam passing through the combustion gas and generating an absorption signal indicative of an absorption of the beam by the combustion gas at each of the first wavelength and the second wavelength, and a processor executing a program stored on a non-transitory storage medium determining a combustion gas temperature based on a ratio of the adoption signals for the first wavelength and the second wavelength.
    • 一种安装在燃气轮机中的燃烧气体测量装置,包括:可调谐激光器,其产生通过燃烧气体路径的辐射束; 调谐所述激光器以发射具有至少第一选定波长和第二选定波长的辐射的控制器,其对应于所述气体的燃烧物质的温度依赖性跃迁,其中所述第一选定波长和所述第二选定波长不接近吸收 相邻波长的峰; 检测器,其感测通过燃烧气体的辐射束,并且产生指示在第一波长和第二波长中的每一个处由燃烧气体吸收光束的吸收信号,以及处理器,其执行存储在非瞬时的程序 存储介质基于第一波长和第二波长的采用信号的比率来确定燃烧气体温度。