Integrated resonant self-pumped loop and pulse tube cryocooler for cryogenic cooling distribution.
Author(s) : NGUYEN C. T.
Summary
Cooling distribution is a vital technology concerning cryogenic thermal management systems for many future space applications, such as in-space, zero boil-off, long-term propellant storage, cooling infrared sensors at multiple locations or at a distance from the cryocooler, and focal-plane arrays in telescopes. These applications require a cooling distribution technology that is able to efficiently and reliably deliver cooling power (generated by a cryocooler) to remote locations and uniformly distribute it over a large-surface area. On-going efforts by others under this technology development area have not shown any promising results. This paper introduces the concept of using a resonant self-pumped loop (RSPL) integrated with the proven, highly efficient pulse tube cryocooler. The RSPL and pulse tube cryocooler combination generates cooling power and provides a distributive cooling loop that can be extended long distances, has no moving parts, and is driven by a single linear compressor. The RSPL is fully coupled with the oscillating flow of the pulse tube working fluid and utilizes gas diodes to convert the oscillating flow to one-directional steady flow that circulates through the cooling loop. The proposed RSPL is extremely simple, lightweight, reliable, and flexible for packaging. There are several requirements for the RSPL to operate efficiently. These requirements will be presented in this paper. Compared to other distributive cooling technologies currently under development, the RSPL technology is unique. [Reprinted with permission from Elsevier. Copyright, 2010].
Details
- Original title: Integrated resonant self-pumped loop and pulse tube cryocooler for cryogenic cooling distribution.
- Record ID : 2010-1719
- Languages: English
- Source: 2009 Space Cryogenics Workshop, Arcadia, USA, June 23-25.
- Publication date: 2010/09
- DOI: http://dx.doi.org/10.1016/j.cryogenics.2010.02.023
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Indexing
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Design and preliminary testing of a large heat ...
- Author(s) : TROLLIER T., TANCHON J., BUQUET J., et al.
- Date : 2006/07/17
- Languages : English
- Source: Multiconference CryoPrague 2006 (9th Cryogenics 2006, ICEC 21, ICMC'06)
- Formats : PDF
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- Author(s) : FUJINAMI F.
- Date : 1995
- Languages : Japanese
- Source: Cryogenics/ Cryog. Eng. - vol. 30 - n. 2
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An overview of Air Force Phillips Laboratory cr...
- Author(s) : CRAWFORD L. D., KALIVODA C. M., GLAISTER D. S.
- Date : 1996/06/25
- Languages : English
- Source: Cryocoolers 9. Proceedings of the International Cryocooler Conference.
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Northrop Grumman aerospace systems cryocooler o...
- Author(s) : RAAB J., TWARD E.
- Date : 2010/09
- Languages : English
- Source: 2009 Space Cryogenics Workshop, Arcadia, USA, June 23-25.
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Advanced pulse tube cold head development.
- Author(s) : CHAN C. K., JACO C., NGUYEN T.
- Date : 1996/06/25
- Languages : English
- Source: Cryocoolers 9. Proceedings of the International Cryocooler Conference.
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