XU W W, YE W, LI Z Y, et al. Progress and application of large-flux high-pressure gas reducing valve[J]. Acta Aerodynamica Sinica, 2023, 41(1): 49−56. DOI: 10.7638/kqdlxxb-2022.0173
Citation: XU W W, YE W, LI Z Y, et al. Progress and application of large-flux high-pressure gas reducing valve[J]. Acta Aerodynamica Sinica, 2023, 41(1): 49−56. DOI: 10.7638/kqdlxxb-2022.0173

Progress and application of large-flux high-pressure gas reducing valve

  • Gaseous large-flux high-pressure reducing valve is the core equipment of the large continuous hypersonic test system. Its gas pressure reducing supply capacity, working stability and reliability have a significant impact on the test capacity of the hypersonic test system. This paper first introduces the principle, technical routine, evaluation index and technical difficulties of pressure-reducing valves for large-flow-rate and high-pressure gas. Second, the development and application of such pressure-reducing valves in the National University of Defense Technology (NUDT) in the past 15 years are summarized, with particular attention paid to the 35 MPa, 100 kg/s pressure-reducing valve developed by NUDT. At last, the application of these valves in complex working conditions, such as large decompression ratios and a wide range of inlet pressure-ratio variation, as well as the future development trend of pressure-reducing valves in hypersonic test systems, are prospected.
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