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Comparative regasification thermal-hydraulics performance analyses of supercritical methane in tubes with different structures 超临界甲烷在不同结构管道中再气化热工性能对比分析
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-31 DOI: 10.1016/j.cryogenics.2025.104226
Zhipeng Chen , Haokang Deng , Yizhong Wu , Kang Wang , Changliang Han
Liquefied natural gas vaporizers serve as prominent regasification equipment in engineering receiving terminals. Nevertheless, the lack of comparative data and dimensionless correlations hinders the optimization of heat exchanger tubes for vaporizers. In this paper, the comprehensive regasification thermal-hydraulics performance of supercritical methane (S-CH4) in tubes with different structures—straight tube (ST), helical tube (HT) and coil tube (CT) is analyzed using computational fluid dynamics simulation methods. The variations of regasification thermodynamic parameters of S-CH4 in ST, HT and CT are revealed. The effects of the ratio of heat flux to mass flux, pressure, buoyancy and gravity on the regasification heat transfer of S-CH4 are also studied. Notably, the progressive supercritical boundary layer theory is adopted to explain performance differences. The key findings show that the curvature-induced centrifugal forces in HT and CT disrupt the symmetry of regasification kinetic parameters, enhancing the heat transfer coefficient by 28.5 % and 30.4 % compared to ST. As pressure increases, geometry-induced turbulence gradually diminishes relative to specific heat-driven thermal transport. ST exhibits the largest hydrodynamic boundary layer thickness with the upper part of 2.72 mm and the lower part of 1.74 mm due to buoyancy-driven stratification. ST demonstrates higher quantitative vorticity magnitudes in the boundary layer compared to HT and CT. Finally, three new dimensionless correlations incorporating a pseudo-boiling K number are respectively developed for S-CH4 in ST, HT and CT, yielding the expression of Nub = CRebn1Prbn2Kn3. The negative exponents (−0.0714, −0.0729 and −0.0549) for K number can effectively clarify enhanced regasification heat transfer of S-CH4 at elevated pressures. These findings can provide valuable insights for designing heat exchange tubes of vaporizers.
液化天然气汽化器是工程接收站中重要的再气化设备。然而,缺乏比较数据和无量纲相关性阻碍了汽化器热交换器管的优化。本文采用计算流体力学模拟方法,对超临界甲烷(S-CH4)在直管(ST)、螺旋管(HT)和盘管(CT)三种不同结构的管道中综合再气化热水力性能进行了分析。揭示了S-CH4在ST、HT和CT中再气化热力学参数的变化规律。研究了热通量比、压力、浮力和重力对S-CH4再气化换热的影响。值得注意的是,采用了渐进超临界边界层理论来解释性能差异。研究结果表明,高温和连续油管中曲率离心力破坏了再气化动力学参数的对称性,使换热系数比高温分别提高了28.5%和30.4%。随着压力的增加,几何诱导的湍流相对于比热驱动的热输运逐渐减小。由于浮力驱动的分层作用,ST区水动力边界层厚度最大,上部为2.72 mm,下部为1.74 mm。与高温和CT相比,ST在边界层中显示出更高的定量涡量。最后,对S-CH4在ST、HT和CT中分别建立了包含伪沸腾K数的三个新的无量纲相关性,得到了Nub = CRebn1Prbn2Kn3的表达。K值的负指数(- 0.0714,- 0.0729和- 0.0549)可以有效地解释S-CH4在高压下的强化再气化换热。这些发现可以为蒸发器换热管的设计提供有价值的见解。
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引用次数: 0
A novel off-design operation optimization method for a reverse Brayton refrigerator for boil-off gas reliquefaction 一种用于蒸发气体再液化的逆布雷顿制冷机非设计运行优化新方法
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-30 DOI: 10.1016/j.cryogenics.2025.104225
Baohua Chao , Jinzhen Wang , Huaiyu Chen , Jin Shang , Cui Lv , Lei Yi , Yicheng Li , Jihao Wu
This study proposes two optimization strategies that employ the genetic algorithm and corrected turbomachinery performance curves to enhance the off-design operation of a reverse Brayton refrigerator. Experimental validation was conducted to confirm the accuracy and reliability of the computational fluid dynamics (CFD) models in predicting dynamic parameters. The proposed optimization strategies modify the operating points of both compressors and the expander by adjusting their rotational speeds, enabling efficient operation across various off-design scenarios. The optimization results show that the two strategies achieve average coefficient of performance (COP) improvements of 5.06 % and 9.40 %, respectively, in the cooling down scenario. The analyses indicate that the fundamental mechanism of the optimization algorithm involves enhancing the expander efficiency and reducing the system’s mass flow rate. This study establishes a framework for off-design operation optimization for turbomachinery-based refrigeration systems.
本研究提出了两种优化策略,采用遗传算法和修正涡轮机械性能曲线来提高逆布雷顿制冷机的非设计运行。通过实验验证,验证了计算流体动力学(CFD)模型预测动力参数的准确性和可靠性。所提出的优化策略通过调整压缩机和膨胀机的转速来改变它们的工作点,从而在各种非设计场景下实现高效运行。优化结果表明,在冷却场景下,两种策略的平均性能系数(COP)分别提高了5.06%和9.40%。分析表明,优化算法的根本机理在于提高膨胀机效率和降低系统质量流量。本研究建立了基于涡轮机械的制冷系统非设计运行优化的框架。
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引用次数: 0
Development and characterization of a low-speed cryogenic pellet injector using a pneumatic-driven mechanical launcher 使用气动驱动的机械发射器的低速低温颗粒喷射器的开发和特性
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-29 DOI: 10.1016/j.cryogenics.2025.104227
J. Mishra , P. Panchal , H. Agravat , M. Banaudha , S. Mukherjee , V. Gupta , P. Nayak , R. Gangradey
A pneumatic-driven mechanical actuator-based low-speed cryogenic pellet injector has been developed and presented in this study. The objective of this technology development is to investigate the freezing and launching of large-sized pellets of gas species pertinent to disruption mitigation studies (DMS) in a tokamak plasma. For pellet freezing, a cryocooler-based refrigeration system has been used. The pellets are frozen in-situ in the gun barrel, connected to the cryocooler’s cold head. To facilitate pellet launching, a mechanical pneumatic launcher (MPL) has been designed and integrated into the gun barrel, enabling the launch of high-strength cryogenic pellets. Key MPL parameters influencing cryogenic pellet launching were characterized using a dedicated test bench and subsequently applied in experimental trials. Experiments are performed on cylindrical-shaped solid hydrogen pellets having dp ∼ 4.2 mm and lp/dp = 1.5, where lp and dp are the length and diameter of the pellet, respectively. Compared to conventional gas gun injection methods, the MPL demonstrated a substantial reduction in required propellant pressure. The experiment was conducted for a propellant pressure range of 0.4 to 1.6 MPa, achieving corresponding pellet speeds of 80 to 140 m/s. Over 200 pellets were successfully launched, with the system achieving an injection reliability exceeding 90 %. Additionally, preliminary investigations into the pellet-shattering study have been initiated.
本文研制了一种基于气动机械执行器的低温颗粒喷射器。这项技术开发的目的是研究托卡马克等离子体中与干扰缓解研究(DMS)相关的大尺寸气体颗粒的冻结和发射。对于颗粒冷冻,使用了基于制冷机的制冷系统。弹丸在枪管中就地冷冻,连接到制冷机的冷头。为了方便弹丸发射,设计了一个机械气动发射器(MPL),并将其集成到炮管中,可以发射高强度的低温弹丸。利用专用实验台架对影响低温球团发射的MPL关键参数进行了表征,并将其应用于实验试验。实验是在dp ~ 4.2 mm和lp/dp = 1.5的圆柱形固体氢球团上进行的,其中lp和dp分别是球团的长度和直径。与传统的气枪喷射方法相比,MPL显示了所需推进剂压力的大幅降低。实验在推进剂压力0.4 ~ 1.6 MPa范围内进行,相应的球团速度为80 ~ 140 m/s。超过200个颗粒成功发射,系统的注入可靠性超过90%。此外,对颗粒粉碎研究的初步调查已经启动。
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引用次数: 0
Performance optimization of active temperature control for mechanical cryocoolers based on automated multiphysics co-simulation 基于自动化多物理场联合仿真的机械制冷机主动温度控制性能优化
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-29 DOI: 10.1016/j.cryogenics.2025.104223
Jie Zhang , Baoyu Yang , Yuhan Li , Xiao Tang , Shangju Li , Jinghao Zhu
The increasing demand for cryogenic technology applications is driving mechanical cryocoolers toward high-precision temperature control. In the meantime, the shortcomings of conventional control strategies in terms of adaptability and interference resistance are becoming progressively apparent, necessitating urgent improvements. However, current designs of cryocooler electronics and control systems still lack a comprehensive, efficient, and easily implementable simulation platform for active temperature control. Consequently, newly developed intelligent control strategies face significant challenges in verifying their effectiveness and performing multi-parameter tuning before implementation. In response to the millikelvin-level temperature stability requirements of the thermal control layer in the quantum satellite, this study proposes an integrated approach based on multiphysics co-simulation (named MPCS) and multidisciplinary optimization. By incorporating intelligent technologies such as automated workflows and efficient optimization algorithms, the proposed method accelerates the simulation process of active cryocooler temperature control systems and enables adaptive optimization of key controller parameters. The results show that the approach improves single-simulation efficiency by approximately 71.46%. Furthermore, by comparing the temperature control performance under various single-objective global optimization algorithms, the respective advantages of Fuzzy-PID and LADRC strategies in terms of response speed and disturbance rejection are validated, while strictly maintaining the required stability. This approach provides effective support for the engineering design optimization and tuning of cryocooler temperature control systems.
对低温技术应用日益增长的需求正在推动机械制冷机向高精度温度控制方向发展。与此同时,传统控制策略在适应性和抗干扰性方面的不足也日益显现,亟需改进。然而,目前的冷冻机电子和控制系统设计仍然缺乏一个全面、高效、易于实现的主动温度控制仿真平台。因此,新开发的智能控制策略面临着验证其有效性和在实施前进行多参数调谐的重大挑战。针对量子卫星热控层对毫开尔文级温度稳定性的要求,本研究提出了一种基于多物理场联合仿真(MPCS)和多学科优化的集成方法。该方法结合自动化工作流程和高效优化算法等智能技术,加速了主动制冷机温度控制系统的仿真过程,并实现了关键控制器参数的自适应优化。结果表明,该方法将单次仿真效率提高了约71.46%。此外,通过比较各种单目标全局优化算法下的温度控制性能,验证了Fuzzy-PID和LADRC策略在严格保持所需稳定性的同时,在响应速度和抗扰性方面各自的优势。该方法为制冷机温度控制系统的工程设计优化和整定提供了有效的支持。
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引用次数: 0
Development of adsorption storage systems for boil-off gas from LNG-powered ships based on typical adsorbents 基于典型吸附剂的lng船舶蒸发气吸附储存系统的开发
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-28 DOI: 10.1016/j.cryogenics.2025.104222
Baifeng Yang , Qingrong Zheng , Shenhua Yang
Efficient and safe utilizations of the boil-off gas (BOG) from LNG is crucial to its onboard applications. In this paper, the technique of adsorbed natural gas (ANG) was employed to adsorb the BOG released from a typical ship powered by LNG. Researches were conducted by designing the fuel supplying system consisting of the natural gas evaporated from the LNG vessel and that from the ANG. Aspen HYSYS was utilized to calculate the temperature and pressure of the BOG inside the vessel, and performances of adsorption equilibrium of methane were compared on four typical kinds of adsorbent which include HKUST-1, MIL-101(Cr), AX-21, and ZIF-8. Charging characteristics of the BOG-ANG system packed with the selected adsorbents were further evaluated by performing numerical simulations on a 1L storage vessel, which was typically designed to conduct the tests under the flow rate of methane corresponding to those required by the propulsion unit under typical working loads. The results indicated that, within the temperature–pressure range respectively 150 K-162 K and 1.0 MPa-1.6 MPa, HKUST-1 and MIL-101(Cr) were adsorbents having larger usable capacities (UC) for methane storage. At the BOG inlet flow rates associated with engine loads between 25 % and 100 %, HKUST-1 had a larger adsorption amount with the final pressure of the adsorbent bed being approximately a quarter of that of MIL-101(Cr). Meanwhile, using MIL-101(Cr) in the storage system increased temperature fluctuations in the adsorbent bed, leading to a more pronounced thermal impact on the system. It suggests that the ANG storage system packed with HKUST-1 can be more preferable for meeting the requirement of managing the BOG released from onboard LNG.
高效、安全地利用液化天然气(LNG)的蒸发气(BOG)对其在船上的应用至关重要。本文采用吸附天然气(ANG)技术对典型LNG动力船舶排放的BOG进行了吸附。设计了由LNG船蒸发天然气和ANG蒸发天然气组成的燃料供应系统,进行了研究。利用Aspen HYSYS计算了BOG容器内的温度和压力,并比较了四种典型吸附剂(HKUST-1、MIL-101(Cr)、AX-21和ZIF-8)对甲烷的吸附平衡性能。通过在1L存储容器上进行数值模拟,进一步评估了装载所选吸附剂的BOG-ANG系统的充注特性,该容器通常设计用于在与推进装置在典型工作负载下所需的甲烷流量相对应的情况下进行测试。结果表明,在150 K ~ 162 K和1.0 MPa ~ 1.6 MPa的温度-压力范围内,HKUST-1和MIL-101(Cr)具有较大的甲烷储存能力。在与发动机负荷相关的BOG进口流量在25%至100%之间时,HKUST-1的吸附量较大,吸附床的最终压力约为MIL-101(Cr)的四分之一。同时,MIL-101(Cr)在存储系统中的使用增加了吸附床的温度波动,对系统的热影响更加明显。结果显示,HKUST-1装载的ANG储存系统更适合管理船上液化天然气释放的BOG。
{"title":"Development of adsorption storage systems for boil-off gas from LNG-powered ships based on typical adsorbents","authors":"Baifeng Yang ,&nbsp;Qingrong Zheng ,&nbsp;Shenhua Yang","doi":"10.1016/j.cryogenics.2025.104222","DOIUrl":"10.1016/j.cryogenics.2025.104222","url":null,"abstract":"<div><div>Efficient and safe utilizations of the boil-off gas (BOG) from LNG is crucial to its onboard applications. In this paper, the technique of adsorbed natural gas (ANG) was employed to adsorb the BOG released from a typical ship powered by LNG. Researches were conducted by designing the fuel supplying system consisting of the natural gas evaporated from the LNG vessel and that from the ANG. Aspen HYSYS was utilized to calculate the temperature and pressure of the BOG inside the vessel, and performances of adsorption equilibrium of methane were compared on four typical kinds of adsorbent which include HKUST-1, MIL-101(Cr), AX-21, and ZIF-8. Charging characteristics of the BOG-ANG system packed with the selected adsorbents were further evaluated by performing numerical simulations on a 1L storage vessel, which was typically designed to conduct the tests under the flow rate of methane corresponding to those required by the propulsion unit under typical working loads. The results indicated that, within the temperature–pressure range respectively 150 K-162 K and 1.0 MPa-1.6 MPa, HKUST-1 and MIL-101(Cr) were adsorbents having larger usable capacities (UC) for methane storage. At the BOG inlet flow rates associated with engine loads between 25 % and 100 %, HKUST-1 had a larger adsorption amount with the final pressure of the adsorbent bed being approximately a quarter of that of MIL-101(Cr). Meanwhile, using MIL-101(Cr) in the storage system increased temperature fluctuations in the adsorbent bed, leading to a more pronounced thermal impact on the system. It suggests that the ANG storage system packed with HKUST-1 can be more preferable for meeting the requirement of managing the BOG released from onboard LNG.</div></div>","PeriodicalId":10812,"journal":{"name":"Cryogenics","volume":"152 ","pages":"Article 104222"},"PeriodicalIF":2.1,"publicationDate":"2025-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145412663","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Feasibility Study of the Mechanical Cooler System for LiteBIRD LiteBIRD机械冷却系统的可行性研究
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-28 DOI: 10.1016/j.cryogenics.2025.104216
Keisuke Shinozaki , Kimihide Odagiri , Keisuke Yoshihara , Yutaro Sekimoto , Tadayasu Dotani , Ryuichi Fujimoto , Katsuhiro Narasaki , Seiji Yoshida , Shoji Tsunematsu , Masahito Isshiki , Kenichi Kanao , LiteBIRD Collaboration
LiteBIRD is the second strategic large-class mission of JAXA aiming to test inflation models. In this mission, cryogenic telescopes and low-temperature scientific instruments are needed to provide high-sensitivity. A mechanical cooler system will cool these telescopes to 5 K or lower, using the 4K-class Joule Thomson cooler (4K-JT) that provides 4.5 K and the 2K Joule Thomson cooler (2K-JT) that provides 1.7 K, which serve as the precoolers of the multistage adiabatic demagnetization refrigerator (ADR). The 20K-class double-stage Stirling coolers (2ST) are also used as precoolers for the JT coolers and shield coolers. This paper presents a feasibility study of the mechanical cooler system and the status of these cooler developments.
LiteBIRD是JAXA的第二个战略大型任务,旨在测试膨胀模型。在这项任务中,需要低温望远镜和低温科学仪器来提供高灵敏度。机械冷却系统将这些望远镜冷却到5 K或更低,使用提供4.5 K的4k级焦耳汤姆逊冷却器(4K-JT)和提供1.7 K的2K焦耳汤姆逊冷却器(2K- jt),它们作为多级绝热消磁冰箱(ADR)的预冷器。20k级双级斯特林冷却器(2ST)也用作JT冷却器和屏蔽冷却器的预冷却器。本文对机械冷却器系统的可行性进行了研究,并介绍了这些冷却器的发展现状。
{"title":"Feasibility Study of the Mechanical Cooler System for LiteBIRD","authors":"Keisuke Shinozaki ,&nbsp;Kimihide Odagiri ,&nbsp;Keisuke Yoshihara ,&nbsp;Yutaro Sekimoto ,&nbsp;Tadayasu Dotani ,&nbsp;Ryuichi Fujimoto ,&nbsp;Katsuhiro Narasaki ,&nbsp;Seiji Yoshida ,&nbsp;Shoji Tsunematsu ,&nbsp;Masahito Isshiki ,&nbsp;Kenichi Kanao ,&nbsp;LiteBIRD Collaboration","doi":"10.1016/j.cryogenics.2025.104216","DOIUrl":"10.1016/j.cryogenics.2025.104216","url":null,"abstract":"<div><div><em>LiteBIRD</em> is the second strategic large-class mission of JAXA aiming to test inflation models. In this mission, cryogenic telescopes and low-temperature scientific instruments are needed to provide high-sensitivity. A mechanical cooler system will cool these telescopes to 5 K or lower, using the 4K-class Joule Thomson cooler (4K-JT) that provides 4.5 K and the 2K Joule Thomson cooler (2K-JT) that provides 1.7 K, which serve as the precoolers of the multistage adiabatic demagnetization refrigerator (ADR). The 20K-class double-stage Stirling coolers (2ST) are also used as precoolers for the JT coolers and shield coolers. This paper presents a feasibility study of the mechanical cooler system and the status of these cooler developments.</div></div>","PeriodicalId":10812,"journal":{"name":"Cryogenics","volume":"152 ","pages":"Article 104216"},"PeriodicalIF":2.1,"publicationDate":"2025-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145412658","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Investigation of interior seed effects on levitation force in Melt-Grown YBCO superconductors by experimental and numerical methods 用实验和数值方法研究熔体生长YBCO超导体内部种子效应对悬浮力的影响
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-28 DOI: 10.1016/j.cryogenics.2025.104224
Ufuk Kemal Öztürk , Babe Cheikh Abderrahmane , Oğuzhan Uzun , Murat Abdioğlu , Sait Barış Güner , Loïc Quéval
This study introduces a novel Top‐Interior Multi-Seeding Melt Growth (TI-MSMG) technique for fabricating high-performance YBCO bulk superconductors and explanations some physical background based on FEM modelling. The depth of the interior seed was gradually changed as 0, 2 and 4 mm (samples S0, S2 and S4, respectively) from the upper surface of the samples. By incorporating an interior seed into the precursor pellet, the TI-MSMG method enables systematic control over grain morphology and critical current density distribution. Magnetic levitation and guidance forces were measured using a three-axis force measurement system, and a two-dimensional finite element method (FEM) model based on the H-formulation of Maxwell’s equations was developed to simulate the electromagnetic behaviour of the superconductors with different seed positions.
Experimental and modelling results reveal that samples incorporating an interior seed (S2) exhibit significantly enhanced levitation and guidance forces compared to S0 and S4, attributable to improved inter-domain interactions and morphological consistency, so a better current coupling. The numerical simulations accurately reproduced the experimental findings, confirming the validity of the modelling approach. These findings indicate that the TI-MSMG process not only addresses some limitations of conventional top-seeding methods but also enhances levitation force performance through optimization of interior seed depth, thereby enabling more efficient and tailored designs for high-temperature superconducting systems such as magnetic levitation, energy storage, and superconducting motors.
本文介绍了一种新型的顶部-内部多种子熔体生长(TI-MSMG)技术,用于制造高性能的YBCO块体超导体,并基于有限元模型解释了一些物理背景。内部种子的深度从样品上表面逐渐变化,分别为0、2和4 mm(样品S0、S2和S4)。TI-MSMG方法通过在前体颗粒中加入内部种子,可以系统地控制颗粒形态和临界电流密度分布。利用三轴力测量系统测量了悬浮力和导向力,建立了基于麦克斯韦方程组h型的二维有限元模型,模拟了不同种子位置下超导体的电磁行为。实验和建模结果表明,与S0和S4相比,含有内部种子(S2)的样品表现出显著增强的悬浮力和引导力,这是由于结构域间相互作用和形态一致性的改善,因此具有更好的电流耦合。数值模拟准确地再现了实验结果,证实了模型方法的有效性。这些发现表明,TI-MSMG工艺不仅解决了传统顶部播种方法的一些局限性,而且通过优化内部播种深度来提高悬浮力性能,从而实现更高效和定制的高温超导系统设计,如磁悬浮、储能和超导电机。
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引用次数: 0
Superconducting properties of commercially available solders for low-field applications 市售低场焊料的超导性能
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-27 DOI: 10.1016/j.cryogenics.2025.104219
C. Hickman , K.K.H. Leung , A.H. Al-Tawhid , B.W. Filippone , P.R. Huffman , E. Korobkina , D.P. Kumah , C.M. Swank
Solders with superconducting transitions around 4K are useful in low magnetic field environments for AC current leads or in electrical and mechanical bonds. Accurate knowledge of these solders’ superconducting properties is essential for improving high precision experiments. We have measured the electrical resistance of five commercially-available eutectic or near-eutectic solders: 50%Sn-50%Pb, 60%Sn-40%Pb, 60%Sn-40%Pb-0.3%Sb, 52%In-48%Sn, and 96.5%Sn-3.5%Ag, down to 2.3K and in applied magnetic fields from 0 to 0.1T. We report critical temperatures Tc(B), 90%–10% transition widths ΔTc, and zero-temperature critical fields Bc,0. Our best candidate for low-loss AC current wiring in low fields is 50%Sn-50%Pb, which has a zero-field Tc,0=7.1K (with ΔTc=0.6K), and remained high at Tc(0.1T)=6.9K (ΔTc=0.6K). We also report, for the first time, Tc and Bc of 60%Sn-40%Pb-0.3%Sb and Bc,0 of 96.5%Sn-3.5%Ag. Our Tc,0=3.31K (ΔTc=0.08K) for 96.5%Sn-3.5%Ag disagrees with a widely adopted value.
具有4K左右超导跃迁的焊料在交流电流引线或电气和机械键的低磁场环境中非常有用。准确地了解这些焊料的超导特性是提高高精度实验的必要条件。我们测量了五种市售共晶或近共晶焊料的电阻:50%Sn-50%Pb, 60%Sn-40%Pb, 60%Sn-40%Pb-0.3% sb, 52%In-48%Sn和96.5%Sn-3.5%Ag,在0到0.1T的外加磁场下,电阻降至2.3K。我们报告了临界温度Tc(B), 90%-10%转变宽度ΔTc和零温度临界场Bc,0。我们的低场低损耗交流电流接线的最佳候选是50%Sn-50%Pb,它具有零场Tc,0=7.1K (ΔTc=0.6K),并在Tc(0.1T)=6.9K (ΔTc=0.6K)时保持高位。我们还首次报道了60%Sn-40%Pb-0.3%Sb和Bc的Tc和Bc, 96.5%Sn-3.5%Ag的0。我们的Tc,0=3.31K (ΔTc=0.08K)为96.5%Sn-3.5%Ag,与广泛采用的值不一致。
{"title":"Superconducting properties of commercially available solders for low-field applications","authors":"C. Hickman ,&nbsp;K.K.H. Leung ,&nbsp;A.H. Al-Tawhid ,&nbsp;B.W. Filippone ,&nbsp;P.R. Huffman ,&nbsp;E. Korobkina ,&nbsp;D.P. Kumah ,&nbsp;C.M. Swank","doi":"10.1016/j.cryogenics.2025.104219","DOIUrl":"10.1016/j.cryogenics.2025.104219","url":null,"abstract":"<div><div>Solders with superconducting transitions around <span><math><mn>4</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span> are useful in low magnetic field environments for AC current leads or in electrical and mechanical bonds. Accurate knowledge of these solders’ superconducting properties is essential for improving high precision experiments. We have measured the electrical resistance of five commercially-available eutectic or near-eutectic solders: 50%Sn-50%Pb, 60%Sn-40%Pb, 60%Sn-40%Pb-0.3%Sb, 52%In-48%Sn, and 96.5%Sn-3.5%Ag, down to <span><math><mn>2.3</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span> and in applied magnetic fields from 0 to 0.1<span><math><mstyle><mspace></mspace></mstyle><mrow><mtext>T</mtext></mrow></math></span>. We report critical temperatures <span><math><msub><mi>T</mi><mi>c</mi></msub><mo>(</mo><mi>B</mi><mo>)</mo></math></span>, 90%–10% transition widths <span><math><mi>Δ</mi><msub><mi>T</mi><mi>c</mi></msub></math></span>, and zero-temperature critical fields <span><math><msub><mi>B</mi><mrow><mi>c</mi><mo>,</mo><mn>0</mn></mrow></msub></math></span>. Our best candidate for low-loss AC current wiring in low fields is 50%Sn-50%Pb, which has a zero-field <span><math><msub><mi>T</mi><mrow><mi>c</mi><mo>,</mo><mn>0</mn></mrow></msub><mo>=</mo><mn>7.1</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span> (with <span><math><mi>Δ</mi><msub><mi>T</mi><mi>c</mi></msub><mo>=</mo><mn>0.6</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span>), and remained high at <span><math><msub><mi>T</mi><mi>c</mi></msub><mo>(</mo><mn>0.1</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>T</mtext></mrow><mo>)</mo><mo>=</mo><mn>6.9</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span> (<span><math><mi>Δ</mi><msub><mi>T</mi><mi>c</mi></msub><mo>=</mo><mn>0.6</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span>). We also report, for the first time, <span><math><msub><mi>T</mi><mi>c</mi></msub></math></span> and <span><math><msub><mi>B</mi><mi>c</mi></msub></math></span> of 60%Sn-40%Pb-0.3%Sb and <span><math><msub><mi>B</mi><mrow><mi>c</mi><mo>,</mo><mn>0</mn></mrow></msub></math></span> of 96.5%Sn-3.5%Ag. Our <span><math><msub><mi>T</mi><mrow><mi>c</mi><mo>,</mo><mn>0</mn></mrow></msub><mo>=</mo><mn>3.31</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span> (<span><math><mi>Δ</mi><msub><mi>T</mi><mi>c</mi></msub><mo>=</mo><mn>0.08</mn><mstyle><mspace></mspace></mstyle><mrow><mtext>K</mtext></mrow></math></span>) for 96.5%Sn-3.5%Ag disagrees with a widely adopted value.</div></div>","PeriodicalId":10812,"journal":{"name":"Cryogenics","volume":"153 ","pages":"Article 104219"},"PeriodicalIF":2.1,"publicationDate":"2025-10-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145555392","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Veritrek-based thermal design and validation of spaceborne cooler micro-vibration isolation system combined with graphite sheets and vibration isolators 基于veritrec的石墨片与隔振器相结合的星载冷却器微振隔离系统的热设计与验证
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-25 DOI: 10.1016/j.cryogenics.2025.104221
Hye-In Kim , Bong-Geon Chae , Hyun-Ung Oh
Spaceborne cryogenic coolers generate undesirable micro-vibrations and excessive heat during on-orbit operations. Therefore, appropriate vibration isolators and thermal designs are required to ensure optimal cooling performance, mission lifetime, and vibration stability. In this study, we propose a thermal design strategy using graphite sheets with low stiffness and high thermal conductivity to enhance both the thermal control and vibration isolation performance of cryogenic coolers. The cooler assembly was optimized using Veritrek software, an advanced design optimization software based on a reduced-order model (ROM), to determine the optimal number of graphite sheet layers, radiator area, and thickness that meet the allowable temperature requirements of the cooler. In addition, free-vibration test was performed to verify the basic characteristics of the cooler assembly. The micro-vibration isolation performance of the applied graphite sheets was validated through micro-vibration test under a gravity offloading conditions.
星载低温冷却器在在轨运行过程中会产生不良的微振动和过热。因此,需要适当的隔振器和热设计来确保最佳的冷却性能,任务寿命和振动稳定性。在这项研究中,我们提出了一种热设计策略,使用低刚度和高导热系数的石墨片来提高低温冷却器的热控制和隔振性能。使用Veritrek软件对冷却器组件进行了优化,Veritrek软件是一种基于降阶模型(ROM)的先进设计优化软件,以确定满足冷却器允许温度要求的最佳石墨片层数、散热器面积和厚度。此外,还进行了自由振动试验,验证了冷却器总成的基本特性。通过重力卸载条件下的微振动试验,验证了所加石墨片的微振动隔振性能。
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引用次数: 0
A HTS-MI magnet cooled by neon pulsating heat pipes system 氖气脉动热管冷却高温超导磁体
IF 2.1 3区 工程技术 Q3 PHYSICS, APPLIED Pub Date : 2025-10-25 DOI: 10.1016/j.cryogenics.2025.104214
Tisha Dixit, Thibault Lecrevisse, Gilles Authelet, Matthias Durochat, Vadim Stepanov, Emeric Benoist, Antomne Caunes, Théophile Benoit, Bruno Maloeuvre, Edouard Pepinter, Philippe Fazilleau, Bertrand Baudouy
This paper reports the development and the successful testing of the first operational high-temperature superconductor (HTS) magnet cooled with a single two-stage cryocooler using two cryogenic pulsating heat pipes (PHP) as thermal links. The superconducting magnet is a metal-as-insulation (MI) REBCO double-pancake “10 T class magnet” built in-house and was operated at neon temperature (around 30 K). The superconducting magnet, the current leads, the cryogenic cooling system and scheme, the pulsating heat pipes and the overall experimental facility are detailed in length. The operational working limit, quench, alternating current (AC) losses and heat dissipation evaluations as well as constant current stability tests were performed and are methodically discussed. A maximum magnetic field of 4.24 T was reached during ramp-up, while a field of 1.72 T was maintained in direct current (DC) conditions for more than six hours with the neon PHPs evidently active. Numerous tests have verified that the cryogenic system, which includes the cryocooler, PHPs, thermal links and power regulation system, is sufficiently dynamic to cope with the transient heat generated by the superconducting magnet. The AC tests demonstrated that this test setup, with the aid of cryogenic PHPs and its power regulation system, can serve as an evaluation tool for power dissipation due to AC losses.
本文报道了用两个低温脉动热管(PHP)作为热链路,研制并成功测试了第一台用单级制冷机冷却的高温超导体(HTS)磁体。超导磁体是内部建造的金属绝缘(MI) REBCO双层煎饼“10 T级磁体”,并在氖温度(约30 K)下运行。详细介绍了超导磁体、电流引线、低温冷却系统和方案、脉动热管以及整个实验装置。进行了运行极限、猝灭、交流损耗和散热评估以及恒流稳定性测试,并进行了系统的讨论。在加速过程中达到了4.24 T的最大磁场,而在直流条件下保持了1.72 T的磁场超过6小时,氖PHPs明显活跃。大量的试验已经证实,低温系统,包括低温冷却器、PHPs、热链路和功率调节系统,具有足够的动态能力来应对超导磁体产生的瞬态热量。交流试验表明,该试验装置在低温PHPs及其功率调节系统的帮助下,可以作为交流损耗功耗的评估工具。
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Cryogenics
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