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- W4387386179 abstract "A two-stage gas-coupled high-frequency pulse tube cryocooler (HFPTC) driven by a linear dual-opposed compressor has been designed. The coaxial structure is used for compactness in both stages. Inertance tubes and double-inlet values are adopted for each stage. A numerical simulation model was developed. The influence of inertance tube and double-inlet on the cooling performance of cryocooler was simulated. The influence of the phase distribution and the character of the gas distribution between two stages were analyzed. It indicates that the second stage’s inertance tube (IT 2) has less influence on the gas distribution in the first stage. However, the first stage’s inertance tube (IT 1) has a significant influence on the second stage. Meanwhile, the value of double-inlet has important influence on the performance of the cryocooler. The double-inlet value of the first stage (DI 1) has significant influence on the output characteristics of the compressor and the gas volume distribution between the two stages. However, the double-inlet value of the second stage (DI 2) has a smaller effect on the output PV characteristics and the phase distribution of the first stage. At the same time, it influences the gas volume distribution and the phase distribution of the second stage." @default.
- W4387386179 created "2023-10-06" @default.
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- W4387386179 date "2023-01-01" @default.
- W4387386179 modified "2023-10-07" @default.
- W4387386179 title "Numerical Simulation of Two-Stage Gas Coupled High Frequency Cryocooler" @default.
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- W4387386179 doi "https://doi.org/10.1007/978-981-99-6128-3_107" @default.
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