Supersonic expansion cooling combined with swirl separation technology is a novel method for gas liquefaction separation that has been mainly employed to separate high freezing point components from multi-component gases in recent years. In this study

two typical structures of supersonic swirl separators are introduced. Thereafter

the theoretical development

numerical simulation

experimental research

and molecular simulation of the condensation phase transformation in the Laval nozzle are summarized. Subsequently

the shockwave problem and structural optimization are analyzed and recapitulated. Numerous experiments and field applications demonstrate the advantages of the device; for example

it saves energy and is environmentally friendly

it has no moving parts

and it eliminates the need to add chemical agents. It has thus been widely used in the field of natural gas purification treatment. Future research can focus on the condensation phase transformation mechanism of single-component and multi-component gases and on improving liquefaction efficiency to promote the application of supersonic swirl separation technology in liquefaction and refrigeration processes

particularly in the refrigeration temperature range and cryogenic temperature range of hydrogen and helium.