A mixed-refrigerant J - T cooler using gas mixture (N2+CH4+C2H6+C3H8) is experimentally investigated in this paper. In the experiment, the influence of different discharging pressure, different sucking pressure and ...A mixed-refrigerant J - T cooler using gas mixture (N2+CH4+C2H6+C3H8) is experimentally investigated in this paper. In the experiment, the influence of different discharging pressure, different sucking pressure and different hotinend temperature of heat exchanger on thermodynamic performance of the J - T cooler have been done experimentally. When working at condition of discharging pressure from 3.0MPa to 6.0MPa and sucking pressure from 0.1MPa to 0.12MPa, the mixed-refrigerant cooler can achieve the temperature of 80K to 82K and thermal efficiency of 10%, 3 to 5 times of pure nitrogen cooler. Consequently,using mixed refrigerant is effective way to improve the thermodynamic performance of J -T cooler.展开更多
经过多次调整,计划将于2018年发射的詹姆斯·韦伯太空望远镜(James Webb Space Telescope,简称JWST)中的中红外仪(Mid-Infrared Instrument,简称MIRI)低温制冷系统最终选用三级脉管制冷机预冷J-T(Joule-Thomson)循环的复合型低温制...经过多次调整,计划将于2018年发射的詹姆斯·韦伯太空望远镜(James Webb Space Telescope,简称JWST)中的中红外仪(Mid-Infrared Instrument,简称MIRI)低温制冷系统最终选用三级脉管制冷机预冷J-T(Joule-Thomson)循环的复合型低温制冷技术。详细介绍了该技术的发展历程,表明该复合型低温制冷技术已在空间任务中逐渐替代固氢或液氦杜瓦技术,以期为国家未来空间计划的实施提供借鉴。展开更多
在介绍已发射和在研液氦温区低温探测器的任务目标和对低温系统性能要求的基础上,分析了空间用液氦温区机械式制冷技术的设计方法和工作性能,并对其发展趋势进行了展望.当前空间液氦温区机械式制冷技术主要采用线性压缩机驱动的预冷型4...在介绍已发射和在研液氦温区低温探测器的任务目标和对低温系统性能要求的基础上,分析了空间用液氦温区机械式制冷技术的设计方法和工作性能,并对其发展趋势进行了展望.当前空间液氦温区机械式制冷技术主要采用线性压缩机驱动的预冷型4 He和3 He J-T节流制冷技术,而对于提供预冷的斯特林制冷机、吸附制冷机和高频脉管制冷机而言,进一步提高制冷效率是实现整机高效运行的关键.展开更多
文摘A mixed-refrigerant J - T cooler using gas mixture (N2+CH4+C2H6+C3H8) is experimentally investigated in this paper. In the experiment, the influence of different discharging pressure, different sucking pressure and different hotinend temperature of heat exchanger on thermodynamic performance of the J - T cooler have been done experimentally. When working at condition of discharging pressure from 3.0MPa to 6.0MPa and sucking pressure from 0.1MPa to 0.12MPa, the mixed-refrigerant cooler can achieve the temperature of 80K to 82K and thermal efficiency of 10%, 3 to 5 times of pure nitrogen cooler. Consequently,using mixed refrigerant is effective way to improve the thermodynamic performance of J -T cooler.
文摘经过多次调整,计划将于2018年发射的詹姆斯·韦伯太空望远镜(James Webb Space Telescope,简称JWST)中的中红外仪(Mid-Infrared Instrument,简称MIRI)低温制冷系统最终选用三级脉管制冷机预冷J-T(Joule-Thomson)循环的复合型低温制冷技术。详细介绍了该技术的发展历程,表明该复合型低温制冷技术已在空间任务中逐渐替代固氢或液氦杜瓦技术,以期为国家未来空间计划的实施提供借鉴。
文摘在介绍已发射和在研液氦温区低温探测器的任务目标和对低温系统性能要求的基础上,分析了空间用液氦温区机械式制冷技术的设计方法和工作性能,并对其发展趋势进行了展望.当前空间液氦温区机械式制冷技术主要采用线性压缩机驱动的预冷型4 He和3 He J-T节流制冷技术,而对于提供预冷的斯特林制冷机、吸附制冷机和高频脉管制冷机而言,进一步提高制冷效率是实现整机高效运行的关键.