Publication:
Gas Turbine Casing Vibrations under Blade Pressure Excitation
Gas Turbine Casing Vibrations under Blade Pressure Excitation
dc.contributor.author | Forbes, Gareth Llewellyn | en_US |
dc.contributor.author | Randall, Robert Bond | en_US |
dc.date.accessioned | 2021-11-25T13:33:56Z | |
dc.date.available | 2021-11-25T13:33:56Z | |
dc.date.issued | 2009 | en_US |
dc.description.abstract | The non-intrusive measurement of the condition of blades within a gas turbine would be a significant aid in the maintenance and continued operation of these engines. Online condition monitoring of the blade health by non-contact measurement methods is the ambition of most techniques. The current dominant method uses proximity probes to measure blade arrival time for subsequent monitoring. It has recently been proposed however, that measurement of the turbine casing vibration response could provide a means of blade condition monitoring, and even give the prospect of providing an estimation of the blade modal parameters. The casing vibration is believed to be excited pre-dominantly by (i) the moving pressure waveform around each blade throughout its motion and (ii) the moments applied by the stationary stator blades. Any changes to the pressure profile around the rotating blades, due to their vibration, will in turn affect these two dominant excitation forces, such that there will be some correlation between the casing response and blade vibrations. Previous work has introduced an analytical model of a gas turbine casing, and simulated pressure signal, associated with the rotating blades. The effect of individual rotor blade vibrations has been developed in order to understand the complex relationship between these excitation forces. A simplified turbine test rig has been constructed. Various aspects of the previous analytical modelling are presented, and then investigated and verified using results from the experimental program with this simplified test rig. | en_US |
dc.description.uri | http://www.mfpt.org/ | en_US |
dc.identifier.uri | http://hdl.handle.net/1959.4/39965 | |
dc.language | English | |
dc.language.iso | EN | en_US |
dc.publisher | Society for Machinery Failure Prevention Technology | en_US |
dc.rights | CC BY-NC-ND 3.0 | en_US |
dc.rights.uri | https://creativecommons.org/licenses/by-nc-nd/3.0/au/ | en_US |
dc.source | Legacy MARC | en_US |
dc.subject.other | casing vibrations | en_US |
dc.subject.other | gas turbines | en_US |
dc.subject.other | forced response | en_US |
dc.subject.other | rotor blade vibrations | en_US |
dc.title | Gas Turbine Casing Vibrations under Blade Pressure Excitation | en_US |
dc.type | Conference Paper | en |
dcterms.accessRights | open access | |
dspace.entity.type | Publication | en_US |
unsw.accessRights.uri | https://purl.org/coar/access_right/c_abf2 | |
unsw.description.publisherStatement | Proceedings published by the British Institute of Non-destructive Testing: http://www.bindt.org/ | en_US |
unsw.identifier.doi | https://doi.org/10.26190/unsworks/543 | |
unsw.publisher.place | Dayton | en_US |
unsw.relation.faculty | Engineering | |
unsw.relation.ispartofconferenceLocation | Dayton, USA | en_US |
unsw.relation.ispartofconferenceName | MFPT 2009 Failure Prevention: Implementation, Success Stories and Lessons Learned | en_US |
unsw.relation.ispartofconferenceProceedingsTitle | Proceedings of The 2009 Conference of the Society for Machinery Failure Prevention Technology | en_US |
unsw.relation.ispartofconferenceYear | 2009 | en_US |
unsw.relation.ispartofpagefrompageto | 723-733 | en_US |
unsw.relation.originalPublicationAffiliation | Forbes, Gareth Llewellyn, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW | en_US |
unsw.relation.originalPublicationAffiliation | Randall, Robert Bond, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW | en_US |
unsw.relation.school | School of Mechanical and Manufacturing Engineering | * |
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