会议论文详细信息
Cryogenic Engineering Conference 2015 | |
Development of a J-T Micro Compressor | |
材料科学;物理学 | |
Champagne, P.^1 ; Olson, J.R.^1 ; Nast, T.^1 ; Roth, E.^1 ; Collaco, A.^1 ; Kaldas, G.^1 ; Saito, E.^2 ; Loung, V.^2 | |
Advanced Technology Center, Lockheed Martin Space Systems Company, Palo Alto | |
CA | |
94304, United States^1 | |
Santa Barbara Focalplane, Lockheed Martin Missiles and Fire Control, Goleta | |
CA | |
93117, United States^2 | |
关键词: Flexure-bearing; High pressure ratio; High reliability; Joule-Thomson; Linear drives; Lockheed Martin; Piston compressor; Pressure waves; | |
Others : https://iopscience.iop.org/article/10.1088/1757-899X/101/1/012009/pdf DOI : 10.1088/1757-899X/101/1/012009 |
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学科分类:材料科学(综合) | |
来源: IOP | |
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【 摘 要 】
Lockheed Martin has developed and tested a space-quality compressor capable of delivering closed-loop gas flow with a high pressure ratio, suitable for driving a Joule-Thomson cold head. The compressor is based on a traditional "Oxford style" dual-opposed piston compressor with linear drive motors and flexure-bearing clearance-seal technology for high reliability and long life. This J-T compressor retains the approximate size, weight, and cost of the ultra-compact, 200 gram Lockheed Martin Pulse Tube Micro Compressor, despite the addition of a flow-rectifying system to convert the AC pressure wave into a steady flow.
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