Show simple item record

dc.creatorOnari, Maki M.
dc.date.accessioned2022-08-31T16:21:42Z
dc.date.available2022-08-31T16:21:42Z
dc.date.issued2021
dc.identifier.urihttps://hdl.handle.net/1969.1/196716
dc.descriptionCase Study
dc.description.abstractA large aero-derivative gas turbine in electrical generation service was exhibiting high vibration at the LP compressor section (1.5 in/s peak) at low load operation. Thorough testing, using Experimental Modal Analysis (EMA) and Operating Deflection Shape (ODS) indicated that the vibration was due to a structural resonance (4-day testing). This excessive flexibility of the baseplate could have been detected immediately (one day) using Motion Magnification Video (MMV) testing technology. This involves a high speed video camera and related software, to magnify the motion of the engine and baseplate in slow motion. Unfortunately, MMV was not yet developed.
dc.format.mediumElectronicen
dc.format.mediumElectronic
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.language.isoen
dc.publisherTurbomachinery Laboratory, Texas A&M Engineering Experiment Station
dc.relation.ispartofProceedings of the 50th Turbomachinery Symposium
dc.titleAero-Derivat ive Gas Turbine Vibration Troubleshooting Comparing Traditional ODS and
dc.type.genreconference publication
dc.type.materialtexten
dc.type.materialText
dc.format.digitalOriginborn digitalen
dc.format.digitalOriginborn digital
dc.publisher.digitalTexas A & M University. Libraries
dc.publisher.digitalTexas A & M University. Libraries


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record