Double-working medium refrigeration experiment system used for turbine blade of gas turbine
A technology of turbine blades and gas turbines, which is applied in the direction of gas turbine engine testing, jet engine testing, machine/structural component testing, etc., and can solve problems such as data reliability and accuracy cannot be guaranteed, steam cooling cannot be realized, and duration is short, etc.
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[0026] The working principle and operation method of the experimental system of the present invention will be described in detail below in conjunction with the accompanying drawings.
[0027] Referring to Figure 1, the experimental system mainly includes the following parts: ① Mainstream air source unit; ② Experimental section unit; ③ Cooling air unit; ④ Cooling steam unit; ⑤ Data acquisition unit; ⑥ Control unit; ⑦ Exhaust unit.
[0028] The experimental section unit mainly includes an air intake rectifying device 302 and an experimental section 304 . The air intake rectifying device 302 is equipped with a honeycomb 301 and a damping net. The air intake rectification device is equipped with a honeycomb 301 and a damping net, so that the quality of the mainstream air flow passing through the rectification device is better, and a turbulent grid is also installed at the entrance of the test section 304 to adjust the gas turbulence entering the test section degree is within the ...
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