Show simple item record

contributor authorS. Yoshimoto
contributor authorY. Yoshida
contributor authorK. Yagi
contributor authorResearch Assistant
date accessioned2017-05-09T00:14:34Z
date available2017-05-09T00:14:34Z
date copyrightApril, 2004
date issued2004
identifier issn0742-4787
identifier otherJOTRE9-28722#310_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130898
description abstractThis paper investigates the performance of a seal system for an aerostatic journal bearing used in a high vacuum chamber. The seal system consists of axially spaced viscous seals and annular exhaust grooves that are located between the viscous seals. Each exhaust groove is coupled to a separate vacuum pump in order to achieve a vacuum chamber pressure of less than 10−3 Pa. The vacuum chamber pressure is affected by design parameters such as the number of viscous seal stages, seal length, seal gap, and exhaust tube conductance. The influence of these design parameters on the pressure distribution across seal regions and the vacuum chamber pressure are discussed theoretically. It is subsequently shown that an aerostatic journal bearing with three-stage seal system installed can obtain a reduction in the vacuum chamber pressure almost to the ultimate pressure of a vacuum pump, providing there is no leak or outgassing from materials.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Seal System in Aerostatic Journal Bearings for High Vacuum Chambers
typeJournal Paper
journal volume126
journal issue2
journal titleJournal of Tribology
identifier doi10.1115/1.1611498
journal fristpage310
journal lastpage315
identifier eissn1528-8897
keywordsPressure
keywordsVacuum
keywordsExhaust systems
keywordsVacuum pumps
keywordsJournal bearings
keywordsLeakage
keywordsElectrical conductance AND Flow (Dynamics)
treeJournal of Tribology:;2004:;volume( 126 ):;issue: 002
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record