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dc.contributor.otherTurbomachinery Symposium (45th : 2016)
dc.creatorHayes, Jeremy
dc.creatorMankowski, Vincent E.
dc.creatorBueno, Pablo
dc.date.accessioned2017-03-14T21:29:07Z
dc.date.available2017-03-14T21:29:07Z
dc.date.issued2016
dc.identifier.urihttps://hdl.handle.net/1969.1/159776
dc.descriptionCase Studyen
dc.description.abstractObjective: • Design an inlet piping system for a double flow centrifugal compressor that effectively utilizes existing site spacing constraints: • Distributes flow to each inlet evenly with minimal pressure loss and without gas swirl or other flow disturbances that may cause long term compressor performance and mechanical reliability issues. • Utilizes standard piping components for construction and minimizing piping support structure to minimize capital investment. • Offers simple control methodology eliminating the need for flow control valves and a complicated control system. • Provide most effective design solution with minimal engineering hours and reviews.en
dc.format.mediumElectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.publisherTurbomachinery Laboratories, Texas A&M Engineering Experiment Station
dc.relation.ispartofProceedings of the 45th Turbomachinery Symposiumen
dc.subject.lcshTurbomachinesen
dc.titleDouble Flow Refrigeration Compressor Inlet Piping Design and Analysisen
dc.type.genrePresentationen
dc.type.materialTexten
dc.format.digitalOriginborn digitalen
dc.identifier.doihttps://doi.org/10.21423/R1001N


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