Show simple item record

contributor authorW. Shapiro
contributor authorC. Lee
contributor authorH. Jones
date accessioned2017-05-08T23:28:20Z
date available2017-05-08T23:28:20Z
date copyrightJuly, 1988
date issued1988
identifier issn0742-4787
identifier otherJOTRE9-28471#525_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104521
description abstractHelium buffered floating-ring seals used in cryogenic turbopumps are sujbect to large temperature variations, shaft centrifugal growth, and dynamic shaft excursions. To prevent dangerous contact friction over a wide range of operating conditions generally requires liberal clearances with consequent high leakage. Reduction of helium consumption translates into lower space vehicle helium storage requirements and thus increased payload. A hydrostatic sectored floating-ring seal is described with self-adjusting clearance capabilities that enables the seal to operate with small clearances over the operating range to minimize leakage.
publisherThe American Society of Mechanical Engineers (ASME)
titleAnalysis and Design of a Gas-Lubricated, Sectored, Floating Ring Seal
typeJournal Paper
journal volume110
journal issue3
journal titleJournal of Tribology
identifier doi10.1115/1.3261666
journal fristpage525
journal lastpage531
identifier eissn1528-8897
keywordsHydrostatics
keywordsFriction
keywordsTemperature
keywordsClearances (Engineering)
keywordsDesign
keywordsHelium
keywordsSpace vehicles
keywordsStorage AND Leakage
treeJournal of Tribology:;1988:;volume( 110 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record