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Cost-effective use of liquid nitrogen in cryogenic wind tunnels, phase 2Cryogenic seal tests were performed and Rulon A was selected for the subject nutating positive displacement expander. A four-chamber expander was designed and fabricated. A nitrogen reliquefier flow system was also designed and constructed for testing the cold expander. Initial tests were unsatisfactory because of high internal friction attributed to nutating Rulon inlet and outlet valve plates. Replacement of the nutating valves with cam-actuated poppet valves improved performance. However, no net nitrogen reliquefaction was achieved due to high internal friction. Computer software was developed for accurate calculation of nitrogen reliquefaction from a system such as that proposed. These calculations indicated that practical reliquefaction rates of 15 to 19 percent could be obtained. Due to mechanical problems, the nutating expander did not demonstrate its feasibility nor that of the system. It was concluded that redesign and testing of a smaller nutating expander was required to prove concept feasibility.
Document ID
19910005875
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcintosh, Glen E.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Lombard, David S.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Leonard, Kenneth R.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Morhorst, Gerald D.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1990
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-182088
NAS 1.26:182088
D6-44238-5
Report Number: NASA-CR-182088
Report Number: NAS 1.26:182088
Report Number: D6-44238-5
Accession Number
91N15188
Funding Number(s)
PROJECT: RTOP 324-02-00
CONTRACT_GRANT: SBIR-02.02-2796A
CONTRACT_GRANT: NAS1-18481
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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