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Experimental and numerical investigation of 2 K heat exchanger for superfluid helium cryogenic systems at KEK
Author(s) -
Ashish Kumar,
H. Nakai,
Koichi Nakanishi,
Hirotaka Shimizu,
Yukio Kojima,
K. Hara,
T. Honma
Publication year - 2020
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/755/1/012061
Subject(s) - superfluid helium 4 , helium , liquid helium , superfluidity , lambda point refrigerator , superconducting radio frequency , heat exchanger , materials science , heat transfer , cryogenics , physics , atomic physics , thermodynamics , nuclear physics , nuclear engineering , condensed matter physics , particle accelerator , beam (structure) , optics , engineering
Superfluid helium cryogenic systems at KEK are constructed for research and development of cryomodules of the compact Energy Recovery Linac (cERL) and the International Linear Collider (ILC). The niobium superconducting radio frequency (SRF) cavities in cERL and ILC operate at temperatures of 2.0 K or below. The SRF cavities are cooled with saturated superfluid helium, which is another phase of the liquid helium (LHe), when it is cooled below 2.17 K under saturation condition. To produce superfluid helium continuously, a Joule-Thomson (JT) valve is employed in the cryogenic system. Also, a 2 K heat exchanger (2K HX) is introduced in series with the JT valve to recover the coldness from 2.0 K gaseous helium (GHe) evaporating from the helium tanks of the SRF cavities. This increases the production rate of superfluid helium by reducing the incoming LHe temperature from 4.4 K to 2.2 K or above before the JT valve. At KEK, we have a 2K HX consisting of a helical coil and laminated fins for thermal loads up to 100 W. Its performance needs to be determined and is characterized by a factor known as effectiveness, which is the ratio of actual heat transfer to the maximum possible heat transfer between the fluids. The performance of the 2K HX has been determined experimentally using the heat exchanger test stand and numerically by computational fluid dynamics (ANSYS CFX®), respectively. In the heat exchanger test stand, the mass flow rate of incoming LHe is kept identical to the outgoing GHe through the 2K HX, using the level and pressure control of superfluid helium. An electric cartridge heater is immersed in the superfluid helium to vary the mass flow rate of evaporating superfluid helium. In the future, the optimization of the 2K HX design will be performed to improve its performance.

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