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Frontiers in Energy

ISSN 2095-1701

ISSN 2095-1698(Online)

CN 11-6017/TK

邮发代号 80-972

2019 Impact Factor: 2.657

Frontiers in Energy  2021, Vol. 15 Issue (2): 345-357   https://doi.org/10.1007/s11708-020-0708-x
  本期目录
Performance improvement of a pulse tube cryocooler with a single compressor through cascade utilization of cold energy
Xuming LIU1, Xiafan XU1, Biao YANG1, Xiaotong XI1, Liubiao CHEN2(), Junjie WANG1, Yuan ZHOU1()
1. Key Laboratory of Cryogenics, Technical Institute of Physics and Chemistry, Chinese Academy of Sciences, Beijing 100190, China; University of the Chinese Academy of Sciences, Beijing 100049, China
2. Key Laboratory of Cryogenics, Technical Institute of Physics and Chemistry, Chinese Academy of Sciences, Beijing 100190, China
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Abstract

The high-frequency pulse tube cryocooler (HPTC) has been attracting increasing and widespread attention in the field of cryogenic technology because of its compact structure, low vibration, and reliable operation. The gas-coupled HPTC, driven by a single compressor, is currently the simplest and most compact structure. For HPTCs operating below 20 K, in order to obtain the mW cooling capacity, hundreds or even thousands of watts of electrical power are consumed, where radiation heat leakage accounts for a large proportion of their cooling capacity. In this paper, based on SAGE10, a HPTC heat radiation calculation model was first established to study the effects of radiation heat leakage on apparent performance parameters (such as temperature and cooling capacity), and internal parameters (such as enthalpy flow and gas distribution) of the gas-coupled HPTC. An active thermal insulation method of cascade utilization of the cold energy of the system was proposed for the gas-coupled HPTC. Numerical simulations indicate that the reduction of external radiation heat leakage cannot only directly increase the net cooling power, but also decrease the internal gross losses and increase the mass and acoustic power in the lower-temperature section, which further enhances the refrigeration performance. The numerical calculation results were verified by experiments, and the test results showed that the no-load temperature of the developed cryocooler prototype decreased from 15.1 K to 6.4 K, and the relative Carnot efficiency at 15.5 K increased from 0.029% to 0.996% when substituting the proposed active method for the traditional passive method with multi-layer thermal insulation materials.

Key wordsradiation heat leakage    active thermal insulation    cascade utilization    cold energy    performance improvement    cryocooler
收稿日期: 2020-05-01      出版日期: 2021-06-18
Corresponding Author(s): Liubiao CHEN,Yuan ZHOU   
 引用本文:   
. [J]. Frontiers in Energy, 2021, 15(2): 345-357.
Xuming LIU, Xiafan XU, Biao YANG, Xiaotong XI, Liubiao CHEN, Junjie WANG, Yuan ZHOU. Performance improvement of a pulse tube cryocooler with a single compressor through cascade utilization of cold energy. Front. Energy, 2021, 15(2): 345-357.
 链接本文:  
https://academic.hep.com.cn/fie/CN/10.1007/s11708-020-0708-x
https://academic.hep.com.cn/fie/CN/Y2021/V15/I2/345
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Fig.13  
A Area/m2
e Mass-specific total gas energy/J
F Pressure gradient/(Pa·m–1)
H Enthalpy flow/J
k Thermal conductivity/(W·m–1·K–1)
L Length/m
m Mass/kg
P Pressure/Pa
q Heat flux vector/J
Q Heat/J
Qc Cooling power/J
Qcond Conduction leakage/J
Qrad Radiation heat leakage/J
R Ideal gas constant/(J·Kg–1·K–1)
S Entropy/(J·K–1)
Sirr Entropy production/(J·K–1)
T Temperature/K
u Velocity/(m·s–1)
W Power/J
Wa Acoustic power/J
We Electric power/J
Wlost Loss/J
x Longitude coordinate/m
Δx Control volume length/m
Z Compressibility factor
γ Adiabatic index
ε Empirical factor
τ Time/s
φ Porosity
ρ Density/ (kg·m–3)
ν Specific volume/(m3·kg–1)
Δ Gradient
Laplace operator
ac Aftercooler
c Cold end
ch Cold-end heat exchanger
co Compressor
du Duct
g Gas
h Hot end
i Node number
m Mean value
pt Pulse tube
r Regenerator matrix
reg Regenerator
w Wall
·(dot) Time derivative
HPTC High-frequency pulse tube cryocooler
PTC Pulse tube cryocooler
MB Multi-bypass
PT Pulse tube
IT Inertance tube
Res Reservoir
RS Radiation shield
〈〉 Time-average values
  
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