This invention relates to the field of spectroscopic measurement technology, and particularly to a measurement
system and method for measuring the concentration of high-temperature
combustion gases in aero-engines. The measurement
system includes a
supercontinuum laser source, a first collimating mirror, a second collimating mirror, a
spectrometer, and a computer. The measurement method includes acquiring the actual
transmittance spectrum of the high-temperature
combustion gases; calculating the theoretical
transmittance spectrum of the high-temperature
combustion gases; constructing constraints; fitting the actual
transmittance spectrum and the theoretical transmittance spectrum into the constraints; and calculating the concentration of the high-temperature combustion gases. The measurement
system has a lightweight structure, requiring only holes for mounting the
laser emission and absorption devices on the inner wall of the aero-engine casing. The measurement method uses a
supercontinuum laser source, which, compared to ordinary lasers used in active gas detection, offers better
spatial coherence, a wider spectral adjustment range, and higher intensity, enabling the detection of more types of gases. The method uses a multi-band combustion gas absorption model to solve for the temperature of the high-temperature combustion gases, improving the accuracy of the concentration calculation.