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dc.contributor.otherTurbomachinery Symposium (17th : 1988)
dc.creatorAtkins, Kenneth E.
dc.creatorPerez, Robert X.
dc.date.accessioned2017-10-05T14:29:01Z
dc.date.available2017-10-05T14:29:01Z
dc.date.issued1988
dc.identifier.urihttps://hdl.handle.net/1969.1/163592
dc.descriptionLectureen
dc.descriptionPg. 9-18en
dc.description.abstractA gas seal retrofit project for a 2800 hp, 10200 rpm, five-stage hydrogen recycle compressor is described. This barrel-type compressor operates with a 1205 psia suction pressure and 1490 psia discharge pressure. The unit is directly driven by a steam turbine through a continuously lubricated gear-type coupling. The gas seal retrofit project was initiated as a solution to a rotordynamic instability problem experienced on the compressor. The rotordynamic analysis showed that the rotor system stability would be improved with the gas seals. The other advantages of gas seals were considered as secondary to the stability improvements.en
dc.format.mediumElectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.publisherTexas A&M University. Turbomachinery Laboratories
dc.relation.ispartofProceedings of the 17th Turbomachinery Symposiumen
dc.subject.lcshTurbomachinesen
dc.titleInfluence Of Gas Seals On Rotor Stability Of A High Speed Hydrogen Recycle Compressor.en
dc.type.genrePresentationen
dc.type.materialTexten
dc.identifier.doihttps://doi.org/10.21423/R1FW9P


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