PRIMARILY EXPERIMENTAL STUDY OF AN IMPROVED TRAVELLING WAVE THERMO-ACOUSTIC PRIME ENGINE

SUN Li-yong; LUO Er-cang; LIANG Jing-tao; ZHOU Yuan

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VACUUM AND CRYOGENICS > 2001 > 7(2): 97-101.

SUN Li-yong, LUO Er-cang, LIANG Jing-tao, et al. PRIMARILY EXPERIMENTAL STUDY OF AN IMPROVED TRAVELLING WAVE THERMO-ACOUSTIC PRIME ENGINE[J]. VACUUM AND CRYOGENICS, 2001, 7(2): 97-101.

Citation:

SUN Li-yong, LUO Er-cang, LIANG Jing-tao, et al. PRIMARILY EXPERIMENTAL STUDY OF AN IMPROVED TRAVELLING WAVE THERMO-ACOUSTIC PRIME ENGINE[J]. VACUUM AND CRYOGENICS, 2001, 7(2): 97-101.

Citation:

SUN Li-yong, LUO Er-cang, LIANG Jing-tao, et al. PRIMARILY EXPERIMENTAL STUDY OF AN IMPROVED TRAVELLING WAVE THERMO-ACOUSTIC PRIME ENGINE[J]. VACUUM AND CRYOGENICS, 2001, 7(2): 97-101.

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PRIMARILY EXPERIMENTAL STUDY OF AN IMPROVED TRAVELLING WAVE THERMO-ACOUSTIC PRIME ENGINE

1. Cryogenic Lab, Chinese Academy of Sciences, Beijing 100080, China

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Received Date: November 12, 2000

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The experiment bench of the improved travelling wave thermoacoutic prime engine is introduced and compared with the original one,the experimental data are analyzed.Nitrogen is used in the experiment.The pressure ratio of 1.083 is accomplished when the temperature of the gas at the hot end is 615 ℃with the charge pressure of 1.56 MPa.
- thermoacoustic prime engine,
- onset temperature,
- pressure oscillation,
- jump of temperature

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PRIMARILY EXPERIMENTAL STUDY OF AN IMPROVED TRAVELLING WAVE THERMO-ACOUSTIC PRIME ENGINE

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