contributor author | W. Shapiro | |
contributor author | C. Lee | |
contributor author | H. Jones | |
date accessioned | 2017-05-08T23:28:20Z | |
date available | 2017-05-08T23:28:20Z | |
date copyright | July, 1988 | |
date issued | 1988 | |
identifier issn | 0742-4787 | |
identifier other | JOTRE9-28471#525_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/104521 | |
description abstract | Helium 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Analysis and Design of a Gas-Lubricated, Sectored, Floating Ring Seal | |
type | Journal Paper | |
journal volume | 110 | |
journal issue | 3 | |
journal title | Journal of Tribology | |
identifier doi | 10.1115/1.3261666 | |
journal fristpage | 525 | |
journal lastpage | 531 | |
identifier eissn | 1528-8897 | |
keywords | Hydrostatics | |
keywords | Friction | |
keywords | Temperature | |
keywords | Clearances (Engineering) | |
keywords | Design | |
keywords | Helium | |
keywords | Space vehicles | |
keywords | Storage AND Leakage | |
tree | Journal of Tribology:;1988:;volume( 110 ):;issue: 003 | |
contenttype | Fulltext | |