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dc.contributor.otherTurbomachinery Symposium (13th : 1984)
dc.creatorStephen R. Locke
dc.date.accessioned2017-10-05T14:47:09Z
dc.date.available2017-10-05T14:47:09Z
dc.date.issued1984
dc.identifier.urihttps://hdl.handle.net/1969.1/163664
dc.descriptionLectureen
dc.descriptionPg. 51-58en
dc.description.abstractSteps taken by a du Pont team to prevent surge in a 23,000 hp process air compressor are reviewed. The process has several reactors which must interlock down quickly for safety reasons. These interlocks can occur on one, several, or all reactors, simultaneously. During large upsets, the original control scheme could not prevent surge, which then caused shutdown of the entire system. Several constraints complicated the solution. To protect the axial compressor casing from excessive blade stresses, the compressor has to be interlocked on surge. The control margin between the surge control and actual surge line has to be small to conserve energy and improve turndown. A second control margin was required to feed any excess air to be fed to an energy recovery expander. The improved control scheme uses a dual-gain controller which shifts to high gain during upsets. High speed recording equipment was used to track process variables, control signals and actual valve position. This information was then used along with computer simulations to tune controllers and control valve boosters.en
dc.format.mediumElectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.publisherTexas A&M University. Turbomachinery Laboratories
dc.relation.ispartofProceedings of the 13th Turbomachinery Symposiumen
dc.subject.lcshTurbomachinesen
dc.titleAn Empirical Solution To An Anti-Surge Control Problem.en
dc.type.genrePresentationen
dc.type.materialTexten
dc.identifier.doihttps://doi.org/10.21423/R1TH4D


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