A compact spring-loading design has been proposed to increase the reliability of seals in the joints of vacuum cryogenic systems. Heretofore, such joints have been, variously, compact or reliable, but not both, for the following reasons: In all such joints, sealing is effected by compression of soft metal (typically, indium or alloys of indium) O rings between flanges. Over time, the soft O-ring metal flows, with consequent reduction of preload, sometimes leading to loss of seal. To ensure reliable seals, it is necessary to spring-load the flanges to maintain compression of the O rings. However, spring-loaded joints of traditional design are not compact.
This work was done by Bob Bamford, Talso Chui, and Warren Holmes of Caltech for NASA’s Jet Propulsion Laboratory.
This Brief includes a Technical Support Package (TSP).
Unfortunately the TSP Improved Flange Design for Cryogenic Vaccum O-Ring Seals (reference NPO-21006) appears to be missing from our system.
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NASA Tech Briefs Magazine
This article first appeared in the June, 2002 issue of NASA Tech Briefs Magazine.
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