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dc.contributor.otherTurbomachinery Symposium (30th : 2001)
dc.creatorFulton, John W.
dc.creatorKlein, John M.
dc.creatorMarriott, Andrew
dc.creatorGraham, A. David
dc.date.accessioned2017-10-05T00:19:37Z
dc.date.available2017-10-05T00:19:37Z
dc.date.issued2001
dc.identifier.urihttps://hdl.handle.net/1969.1/163325
dc.descriptionLectureen
dc.descriptionPg. 79-88en
dc.description.abstractA two casing high-pressure injection compressor train driven by a directly coupled high-speed induction motor was tested to demonstrate satisfactory electrical, aerothermal, and rotordynamic performance. Some key test aspects are discussed and illustrated with typical results. These include the influence of misalignment and thrust reaction forces on magnetic bearing loading, compressor rotor stability in magnetic bearings, rotor behavior in the landing bearings during simulated magnetic bearing failure, performance of the active thrust control system under transient and simulated failure conditions, and controls tuning of the variable frequency drive. Observations and difficulties encountered during commissioning and plant startup in the field are also discussed.en
dc.format.mediumElectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.publisherTexas A&M University. Turbomachinery Laboratories
dc.relation.ispartofProceedings of the 30th Turbomachinery Symposiumen
dc.subject.lcshTurbomachinesen
dc.titleFull-Load Testing Of An All-Electric Centrifugal Compressor For Miscible Gas Injection.en
dc.type.genrePresentationen
dc.type.materialTexten
dc.identifier.doihttps://doi.org/10.21423/R1ZD2V


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