Vis enkel innførsel

dc.contributor.advisorBakken, Lars Eirik
dc.contributor.advisorBjørge, Tor
dc.contributor.advisorBakken, Martin
dc.contributor.advisorLangørgen, Erik
dc.contributor.authorMyklestad, Håkon
dc.date.accessioned2017-09-15T14:00:51Z
dc.date.available2017-09-15T14:00:51Z
dc.date.created2017-06-11
dc.date.issued2017
dc.identifierntnudaim:17496
dc.identifier.urihttp://hdl.handle.net/11250/2454916
dc.description.abstractToday, most of the large and easily accessible oil and gas fields on the Norwegian continental shelf has been developed. Future production potential is found in development of fields at large depths and cost-efficient methods of improving the recovery of existing fields at the tail production stage. Development of wet gas compression technology for subsea boosting is one pathway to achieving this. Introducing multiphase flow into the already complex flow pattern inside compressors makes it challenging to develop accurate analytical models. Current research is therefore highly dependent on test data from real scale compressor rigs. One such compressor rig is built at the Department of Energy and Process Engineering. This thesis focus on transients aerodynamics phenomenons in centrifugal compressors. These primarily occur at low flow rate where the compressors performance is limited by stall and surge. Encountering stall or surge is highly unwanted during operation and it is therefore of interest to investigate how wet gas affect them. A compressor that is exposed directly to the wellstream also needs to handle inlet instabilities in the form of liquid content fluctuations, especially if the downstream pipelines are prone to slug formation. This is a unique challenge for wet gas compressors. A vibration approach is taken, and the author has focused on analysis of frequency spectra, primarily based on dynamic pressure readings in the diffuser. The results show a mild increase of noise during wet conditions due to the dispersed liquid droplets causing reflection of pressure waves. Left limit tests suggest that the compressor encounters impeller rotating stall that is severe enough to cause flow instabilities, but no signs of surge oscillations are seen. The same is observed for wet gas, but this occurs at a lower flow rate. Slug tests performed in the surge area gives no indication of instability, as the stall cells are immediately re-energized and no excitations are observed around the rotors natural frequency.
dc.languageeng
dc.publisherNTNU
dc.subjectNatural Gas Technology
dc.titleWet Gas Compression - Transients
dc.typeMaster thesis


Tilhørende fil(er)

Thumbnail
Thumbnail

Denne innførselen finnes i følgende samling(er)

Vis enkel innførsel