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dc.contributor.authorDing, H
dc.contributor.authorChen, Z
dc.contributor.authorSun, H
dc.contributor.authorYang, Y
dc.contributor.authorLiang, Z
dc.contributor.authorZhang, Y
dc.date.accessioned2023-05-09T11:18:25Z
dc.date.issued2023-05-08
dc.date.updated2023-05-09T09:31:23Z
dc.description.abstractGas-liquid two-phase flow widely exists in the natural gas transportation industry. Accurate measurement of the liquid film is conducive to enhancing the efficiency and economy of supersonic separators. Therefore, a flexible printed circuit (FPC) liquid film conductance sensor based on array arrangement is designed. Firstly, the geometric parameters of sensors are optimized by the finite element method. The modules of electrical signal excitation and collection system based on FPGA are designed. A liquid film calibration device is built to calibrate the FPC sensor, the liquid film thickness is fitted through calibration experiments, and the fitting curve error is within ±5.0 %. Secondly, to analyze the liquid film thickness and velocity at the wet-gas outlet section of the supersonic separator, serval experiments are carried out in different working conditions, and the signals of liquid film thickness are processed by time and frequency domain analysis. The results reveal that the liquid film thickness has a bimodal characteristic, where the thickness of the thin base layer is about 70 μm, and fluctuating layer thickness is related to working conditions. The normalized energy ratio and fluctuation characteristics significantly changed under different frequency bands. At the same time, the existence of shock waves seriously influences the generation of liquid film, resulting in a decrease in the liquid film thickness seriously. Last, the cross-correlation algorithm is used to analyze the liquid film velocity. The different signal transmitter and receiver electrode orders can realize the velocity measurement in different directions. The experimental results show that the liquid film velocity at the outlet of the supersonic separator maintains at 54.8 mm/s ~ 339.0 mm/s when the back pressure ranges from 0.350-0.717, the maximum RMSE of flow direction velocity is 4.51 mm/s and the maximum RMSE of circumferential direction velocity is 3.38 mm/s.en_GB
dc.description.sponsorshipNational Natural Science Foundation of Chinaen_GB
dc.description.sponsorshipEngineering and Physical Sciences Research Council (EPSRC)en_GB
dc.format.extent1-1
dc.identifier.citationPublished online 8 May 2023en_GB
dc.identifier.doihttps://doi.org/10.1109/tim.2023.3273670
dc.identifier.grantnumber52276159en_GB
dc.identifier.grantnumber51876143en_GB
dc.identifier.grantnumber61873184en_GB
dc.identifier.grantnumberEP/X027147/1en_GB
dc.identifier.urihttp://hdl.handle.net/10871/133107
dc.language.isoenen_GB
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE)en_GB
dc.rights© 2023 IEEE. This version is made available under the CC-BY 4.0 license: https://creativecommons.org/licenses/by/4.0/en_GB
dc.subjectNatural gas dehydrationen_GB
dc.subjectsupersonic separatoren_GB
dc.subjectFPC sensoren_GB
dc.subjectliquid film thicknessen_GB
dc.subjecttime and frequency domain analysisen_GB
dc.subjectcross-correlation velocityen_GB
dc.titleMeasurement of the thin liquid film at the wet-gas outlet of the supersonic separator by FPC conductance sensoren_GB
dc.typeArticleen_GB
dc.date.available2023-05-09T11:18:25Z
dc.identifier.issn0018-9456
dc.descriptionThis is the author accepted manuscript. The final version is available from IEEE via the DOI in this recorden_GB
dc.identifier.eissn1557-9662
dc.identifier.journalIEEE Transactions on Instrumentation and Measurementen_GB
dc.relation.ispartofIEEE Transactions on Instrumentation and Measurement
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/en_GB
rioxxterms.versionAMen_GB
rioxxterms.licenseref.startdate2023-05-08
rioxxterms.typeJournal Article/Reviewen_GB
refterms.dateFCD2023-05-09T11:15:42Z
refterms.versionFCDAM
refterms.dateFOA2023-05-09T11:18:39Z
refterms.panelBen_GB


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© 2023 IEEE. This version is made available under the CC-BY 4.0 license: https://creativecommons.org/licenses/by/4.0/
Except where otherwise noted, this item's licence is described as © 2023 IEEE. This version is made available under the CC-BY 4.0 license: https://creativecommons.org/licenses/by/4.0/