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Titlebook: Cryocoolers 13; Ronald G. Ross Conference proceedings 2005 Springer-Verlag US 2005 X-ray.development.modeling

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发表于 2025-3-21 18:05:41 | 显示全部楼层 |阅读模式
书目名称Cryocoolers 13
编辑Ronald G. Ross
视频video
概述Presents the latest developments and performance measurements for both users and developers of cryocoolers.Discusses pulse tube, Gifford-McMahon, and tactical Stirling cryocoolers, as well as progress
图书封面Titlebook: Cryocoolers 13;  Ronald G. Ross Conference proceedings 2005 Springer-Verlag US 2005 X-ray.development.modeling
描述The last two years have witnessed a continuation in the breakthrough shift toward pulse tube cryocoolers for long-life, high-reliability cryocooler applications. New this year are papers de­ scribing the development of very large pulse tube cryocoolers to provide up to 1500 watts of cooling for industrial applications such as cooling the superconducting magnets of Mag-lev trains, coolmg superconducting cables for the power mdustry, and liquefymg natural gas. Pulse tube coolers can be driven by several competing compressor technologies. One class of pulse tube coolers is referred to as "Stirling type" because they are based on the linear Oxford Stirling-cooler type compressor; these generally provide coolmg m the 30 to 100 K temperature range and operate ^t frequencies from 30 to 60 Hz. A second type of pulse tube cooler is the so-called "Gifford-McMahon type. " Pulse tube coolers of this type use a G-M type compressor and lower frequency operation (~1 Hz) to achieve temperatures in the 2 to 10 K temperature range. The third type of pulse tube cooler is driven by a thermoacoustic oscillator, a heat engine that functions well in remote environments where electricity is not readily av
出版日期Conference proceedings 2005
关键词X-ray; development; modeling
版次1
doihttps://doi.org/10.1007/0-387-27533-9
isbn_softcover978-1-4419-3670-7
isbn_ebook978-0-387-27533-8
copyrightSpringer-Verlag US 2005
The information of publication is updating

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发表于 2025-3-21 22:10:44 | 显示全部楼层
Folkert Graafsma,Siddhartha Rajagopaling input power to the electronics. The total mass of the cooler and electronics system is less than 40 kg. The software driven control electronics provide the cooler control functions that are fully re-configurable and based on the NGST flight-qualified Advanced Cooler Electronics (ACE) with minor
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Conclusion and Further Research,lessons learned and performance achieved in the MIRI cryocooler application. In the final proposed configuration, all of the MIRI/JWST design considerations were successfully met. Although the cryocooler option was eventually deselected in favor of a solid-hydrogen stored cryogen system, the cryocoo
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The RTP Literature: Mind the Gap! View based control algorithm. In parallel to this effort, a manufacturing method was developed to enable production of very long continuous lengths of small bore finned tubing. This tubing is used in the highly effective recuperative heat exchanger associated with each stage of the cryocooler. A th
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The RTP Literature: Mind the Gap!ation problems due to outgassing has been diminished because the coils are not part of the helium circuit. Furthermore, all connections in the LSF95xx are laser-welded, which means that there is no additional locking required inside the cooler. By using a different magnet design, no magnet segments
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