Method and system for in situ testing of metal combustion susceptibility characteristics
An in-situ testing and sensitive technology, applied in the field of spectral detection, can solve problems such as low resolution, inability to reflect changes in material structure, and poor accuracy of Raman spectral analysis, so as to improve accuracy and ensure accurate and reliable Raman spectral line information Effect
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Embodiment 1
[0067] The adopted system includes: sample stage, high-temperature plasma spray gun, dual colorimetric infrared thermometer, short-wavelength pulsed laser light source, Raman probe, Raman signal processing device, digital delay signal generator, and high-speed infrared photography device.
[0068] The method for in-situ testing of metal combustion susceptibility characteristics includes the following steps.
[0069] The metal sample pure titanium was fixed on the sample stage and placed in the air with a pressure of 0.10MPa. A short-wavelength pulsed laser light source is used to emit short-wavelength pulsed laser light and irradiate it on the surface of the metal sample, and the dual-colorimetric infrared thermometer and Raman probe are used to calibrate the pure titanium of the metal sample, so that the dual-colorimetric infrared thermometer can be used during the heating process. The position of temperature measurement, the position of short-wavelength pulsed laser irradiat...
Embodiment 2-15
[0075] Referring to the device and method of Example 1, the metal sample, gas type, pressure, heating method, maximum heating temperature, heating rate, pulse time and spectrum frequency test conditions in Table 1 were used to test the metal combustion sensitivity characteristics in situ. Among them, the metal samples of Examples 13-15 were placed in a closed chamber with an observation window, and after vacuuming, they were filled with pure oxygen of 0.09 MPa, 0.17 MPa, and 0.17 MPa, respectively, so that the metal samples were burned under the condition of pure oxygen; The metal samples of other examples were placed in air with a pressure of 0.10 MPa for combustion.
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