| 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 | |