Performance of all-metal demountable cryogenic seals at superfluid helium temperatures
Two all-metal demountable cryogenic seals with an outside diameter of 36.6 mm, inside diameter of 27.2 mm and thickness of 0.51 mm were leak tested at room temperature (300 K), liquid nitrogen temperature (21 cycles at 77 K), liquid helium temperature (nine cycles at 4.2 K) and superfluid helium tem...
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Veröffentlicht in: | Cryogenics (Guildford) 1991-11, Vol.31 (11), p.993-995 |
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creator | Salerno, L.J. Spivak, A.L. Kittel, P. |
description | Two all-metal demountable cryogenic seals with an outside diameter of 36.6 mm, inside diameter of 27.2 mm and thickness of 0.51 mm were leak tested at room temperature (300 K), liquid nitrogen temperature (21 cycles at 77 K), liquid helium temperature (nine cycles at 4.2 K) and superfluid helium temperature (four cycles at 1.6 K). Each seal was mounted and demounted for 13 cycles. Thickness measurements at 90° intervals along the circumference showed a maximum seal compression of 0.038 mm. Leak rate measurements at all temperatures showed no detectable leak above the helium background level, typically 0.1 × 10
−9 std cm
3 s
−1, during testing. |
doi_str_mv | 10.1016/0011-2275(91)90226-M |
format | Article |
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−9 std cm
3 s
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−9 std cm
3 s
−1, during testing.</description><subject>Applied sciences</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Exact sciences and technology</subject><subject>helium</subject><subject>leaks</subject><subject>Mechanical Engineering</subject><subject>Rational use of energy: conservation and recovery of energy</subject><subject>seals</subject><issn>0011-2275</issn><issn>1879-2235</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1991</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNqNkU1LXTEQhoO04K31H7jIQoouTptJzlc2gogfBaVdVLchd86kjeScc5vkFPz35nrFpXSTwMzzDsMzjB2B-AoC2m9CAFRSds2JhlMtpGyruz22gr7TpayaD2z1huyzTyk9CiFq2coVe_hJ0c1xtBMSnx23IVQjZRv4QOO8TNmuA3GMT_NvmjzyRDYkbjNPy6Ykw-IH_oeCX0aeaSwlm5dI6TP76ApIh6__Abu_uvx1cVPd_rj-fnF-W2ENkKtBS-WUbNYkNLgOQFkE1WsrW6oBNWJL2HWo3RrXzg0KNWjse7DCIVCvDtiX3dxNnP8ulLIZfUIKwU40L8nIRnVNU97_AWvVqwLWOxDjnFIkZzbRjzY-GRBma9tsVZqtSqPBvNg2dyV2_DrfJrTBxSLUp7ds0-i61tt9j3bYZJM1U47JgNZSCCVaAaV9tmtTcfbPUzQJPZXTDD4SZjPM_v01ngE0Y50K</recordid><startdate>19911101</startdate><enddate>19911101</enddate><creator>Salerno, L.J.</creator><creator>Spivak, A.L.</creator><creator>Kittel, P.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>CYE</scope><scope>CYI</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>8BQ</scope><scope>JG9</scope></search><sort><creationdate>19911101</creationdate><title>Performance of all-metal demountable cryogenic seals at superfluid helium temperatures</title><author>Salerno, L.J. ; Spivak, A.L. ; Kittel, P.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c411t-d923f325be091f7113ac1389a26e41c9cc6ec77c9fbcbffd3c919c881a0fc1e83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1991</creationdate><topic>Applied sciences</topic><topic>Energy</topic><topic>Energy. Thermal use of fuels</topic><topic>Exact sciences and technology</topic><topic>helium</topic><topic>leaks</topic><topic>Mechanical Engineering</topic><topic>Rational use of energy: conservation and recovery of energy</topic><topic>seals</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Salerno, L.J.</creatorcontrib><creatorcontrib>Spivak, A.L.</creatorcontrib><creatorcontrib>Kittel, P.</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>METADEX</collection><collection>Materials Research Database</collection><jtitle>Cryogenics (Guildford)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Salerno, L.J.</au><au>Spivak, A.L.</au><au>Kittel, P.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Performance of all-metal demountable cryogenic seals at superfluid helium temperatures</atitle><jtitle>Cryogenics (Guildford)</jtitle><date>1991-11-01</date><risdate>1991</risdate><volume>31</volume><issue>11</issue><spage>993</spage><epage>995</epage><pages>993-995</pages><issn>0011-2275</issn><eissn>1879-2235</eissn><coden>CRYOAX</coden><abstract>Two all-metal demountable cryogenic seals with an outside diameter of 36.6 mm, inside diameter of 27.2 mm and thickness of 0.51 mm were leak tested at room temperature (300 K), liquid nitrogen temperature (21 cycles at 77 K), liquid helium temperature (nine cycles at 4.2 K) and superfluid helium temperature (four cycles at 1.6 K). Each seal was mounted and demounted for 13 cycles. Thickness measurements at 90° intervals along the circumference showed a maximum seal compression of 0.038 mm. Leak rate measurements at all temperatures showed no detectable leak above the helium background level, typically 0.1 × 10
−9 std cm
3 s
−1, during testing.</abstract><cop>Legacy CDMS</cop><pub>Elsevier Ltd</pub><doi>10.1016/0011-2275(91)90226-M</doi><tpages>3</tpages><oa>free_for_read</oa></addata></record> |
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source | Elsevier ScienceDirect Journals; NASA Technical Reports Server |
subjects | Applied sciences Energy Energy. Thermal use of fuels Exact sciences and technology helium leaks Mechanical Engineering Rational use of energy: conservation and recovery of energy seals |
title | Performance of all-metal demountable cryogenic seals at superfluid helium temperatures |
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