A novel method for predicting the response variability of friction-damped gas turbine blades
Predicting the response of gas turbine blades with underplatform friction dampers is challenging due to the combination of frictional nonlinearity and system uncertainty: a traditional Monte Carlo approach to predicting response distributions requires a large number of nonlinear simulations which is...
Gespeichert in:
Veröffentlicht in: | Journal of sound and vibration 2019-02, Vol.440, p.372-398 |
---|---|
Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 398 |
---|---|
container_issue | |
container_start_page | 372 |
container_title | Journal of sound and vibration |
container_volume | 440 |
creator | Butlin, T. Ghaderi, P. Spelman, G. Midgley, W.J.B. Umehara, R. |
description | Predicting the response of gas turbine blades with underplatform friction dampers is challenging due to the combination of frictional nonlinearity and system uncertainty: a traditional Monte Carlo approach to predicting response distributions requires a large number of nonlinear simulations which is computationally expensive. This paper presents a new approach based on the principle of Maximum Entropy that provides an estimate of the response distribution that is approximately two orders of magnitude faster than Monte Carlo Harmonic Balance Method simulations. The premise is to include the concept of ‘computational uncertainty’: incorporating lack of knowledge of the solution as part of the uncertainty, on the basis that there are diminishing returns in computing precise solutions to an uncertain system. To achieve this, the method uses a describing function approximation of the friction-damped part of the system; chooses an ignorance prior probability density function for the complex value of the describing function based on Coulombs friction law; updates the distribution using an estimate of the mean solution, the admissible domain of solutions, and the principle of Maximum Entropy; then carries out a linear Monte Carlo simulation to estimate the response distribution. The approach is validated by comparison with HBM simulations and experimental tests, using an idealised academic system consisting of a periodic array of beams (with controllable uncertainty) coupled by single-point friction dampers. Comparisons with two- and eight-blade systems show generally good agreement. Predicting the response statistics of the maximum blade amplitude reveals specific well-understood circumstances when the method is less effective. Predictions of the overall blade response statistics agree with Monte Carlo HBM extremely well across a wide range of excitation amplitudes and uncertainty levels. Critically, experimental comparisons reveal the care that is needed in accurately characterising uncertainty in order to obtain agreement of response percentiles. The new method allowed fast iteration of uncertainty parameters and correlations to achieve good agreement, which would not have been possible using traditional methods.
•A new approach to predict variability of friction-damped turbine blades is presented.•The method uses Maximum Entropy to estimate a PDF of the friction describing function.•Computationally expensive Monte Carlo simulations of the nonlinear system are |
doi_str_mv | 10.1016/j.jsv.2018.10.013 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2155910261</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0022460X18306801</els_id><sourcerecordid>2155910261</sourcerecordid><originalsourceid>FETCH-LOGICAL-c368t-8af74c2cb6043ba90369ad7d739a6d6c9b6e661c5bf4dd02b07592da24434ccc3</originalsourceid><addsrcrecordid>eNp9kMtqwzAQRUVpoenjA7oTdO10JNuyTVch9AWBblrooiBkaZzIOJYrOYb8fWXSdVfDDPfO3DmE3DFYMmDioV22YVpyYGXsl8DSM7JgUOVJmYvynCwAOE8yAV-X5CqEFgCqLM0W5HtFezdhR_c47pyhjfN08GisHm2_peMOqccwuD4gnZS3qradHY_UNbTxs8j1iVH7AQ3dqkDHg69tj7TulMFwQy4a1QW8_avX5PP56WP9mmzeX97Wq02iU1GOSamaItNc1wKytFYVpKJSpjBFWilhhK5qgUIwnddNZgzwGoq84kbxLL6gtU6vyf1p7-DdzwHDKFt38H08KTnL84oBFyyq2EmlvQvBYyMHb_fKHyUDOUOUrYwQ5QxxHkWI0fN48mCMP1n0MmiLvY6APOpRGmf_cf8Cd1l7JA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2155910261</pqid></control><display><type>article</type><title>A novel method for predicting the response variability of friction-damped gas turbine blades</title><source>Elsevier ScienceDirect Journals</source><creator>Butlin, T. ; Ghaderi, P. ; Spelman, G. ; Midgley, W.J.B. ; Umehara, R.</creator><creatorcontrib>Butlin, T. ; Ghaderi, P. ; Spelman, G. ; Midgley, W.J.B. ; Umehara, R.</creatorcontrib><description>Predicting the response of gas turbine blades with underplatform friction dampers is challenging due to the combination of frictional nonlinearity and system uncertainty: a traditional Monte Carlo approach to predicting response distributions requires a large number of nonlinear simulations which is computationally expensive. This paper presents a new approach based on the principle of Maximum Entropy that provides an estimate of the response distribution that is approximately two orders of magnitude faster than Monte Carlo Harmonic Balance Method simulations. The premise is to include the concept of ‘computational uncertainty’: incorporating lack of knowledge of the solution as part of the uncertainty, on the basis that there are diminishing returns in computing precise solutions to an uncertain system. To achieve this, the method uses a describing function approximation of the friction-damped part of the system; chooses an ignorance prior probability density function for the complex value of the describing function based on Coulombs friction law; updates the distribution using an estimate of the mean solution, the admissible domain of solutions, and the principle of Maximum Entropy; then carries out a linear Monte Carlo simulation to estimate the response distribution. The approach is validated by comparison with HBM simulations and experimental tests, using an idealised academic system consisting of a periodic array of beams (with controllable uncertainty) coupled by single-point friction dampers. Comparisons with two- and eight-blade systems show generally good agreement. Predicting the response statistics of the maximum blade amplitude reveals specific well-understood circumstances when the method is less effective. Predictions of the overall blade response statistics agree with Monte Carlo HBM extremely well across a wide range of excitation amplitudes and uncertainty levels. Critically, experimental comparisons reveal the care that is needed in accurately characterising uncertainty in order to obtain agreement of response percentiles. The new method allowed fast iteration of uncertainty parameters and correlations to achieve good agreement, which would not have been possible using traditional methods.
•A new approach to predict variability of friction-damped turbine blades is presented.•The method uses Maximum Entropy to estimate a PDF of the friction describing function.•Computationally expensive Monte Carlo simulations of the nonlinear system are avoided.•Comparisons with numerical and experimental tests show generally good agreement.•The method enables rapid estimates of the response distribution.</description><identifier>ISSN: 0022-460X</identifier><identifier>EISSN: 1095-8568</identifier><identifier>DOI: 10.1016/j.jsv.2018.10.013</identifier><language>eng</language><publisher>Amsterdam: Elsevier Ltd</publisher><subject>Accuracy ; Amplitudes ; Computer simulation ; Conditional probability ; Dampers ; Damping ; Friction ; Friction damping ; Gas turbine engines ; Gas turbines ; Harmonic balance method ; Iterative methods ; Localisation ; Localised nonlinearities ; Maximum entropy ; Mistuning ; Nonlinear vibration ; Nonlinearity ; Parameter uncertainty ; Predictions ; Probability density functions ; Turbine blades ; Uncertainty ; Underplatform dampers ; Vibration</subject><ispartof>Journal of sound and vibration, 2019-02, Vol.440, p.372-398</ispartof><rights>2018</rights><rights>Copyright Elsevier Science Ltd. Feb 3, 2019</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c368t-8af74c2cb6043ba90369ad7d739a6d6c9b6e661c5bf4dd02b07592da24434ccc3</citedby><cites>FETCH-LOGICAL-c368t-8af74c2cb6043ba90369ad7d739a6d6c9b6e661c5bf4dd02b07592da24434ccc3</cites><orcidid>0000-0003-3786-1691</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0022460X18306801$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27903,27904,65309</link.rule.ids></links><search><creatorcontrib>Butlin, T.</creatorcontrib><creatorcontrib>Ghaderi, P.</creatorcontrib><creatorcontrib>Spelman, G.</creatorcontrib><creatorcontrib>Midgley, W.J.B.</creatorcontrib><creatorcontrib>Umehara, R.</creatorcontrib><title>A novel method for predicting the response variability of friction-damped gas turbine blades</title><title>Journal of sound and vibration</title><description>Predicting the response of gas turbine blades with underplatform friction dampers is challenging due to the combination of frictional nonlinearity and system uncertainty: a traditional Monte Carlo approach to predicting response distributions requires a large number of nonlinear simulations which is computationally expensive. This paper presents a new approach based on the principle of Maximum Entropy that provides an estimate of the response distribution that is approximately two orders of magnitude faster than Monte Carlo Harmonic Balance Method simulations. The premise is to include the concept of ‘computational uncertainty’: incorporating lack of knowledge of the solution as part of the uncertainty, on the basis that there are diminishing returns in computing precise solutions to an uncertain system. To achieve this, the method uses a describing function approximation of the friction-damped part of the system; chooses an ignorance prior probability density function for the complex value of the describing function based on Coulombs friction law; updates the distribution using an estimate of the mean solution, the admissible domain of solutions, and the principle of Maximum Entropy; then carries out a linear Monte Carlo simulation to estimate the response distribution. The approach is validated by comparison with HBM simulations and experimental tests, using an idealised academic system consisting of a periodic array of beams (with controllable uncertainty) coupled by single-point friction dampers. Comparisons with two- and eight-blade systems show generally good agreement. Predicting the response statistics of the maximum blade amplitude reveals specific well-understood circumstances when the method is less effective. Predictions of the overall blade response statistics agree with Monte Carlo HBM extremely well across a wide range of excitation amplitudes and uncertainty levels. Critically, experimental comparisons reveal the care that is needed in accurately characterising uncertainty in order to obtain agreement of response percentiles. The new method allowed fast iteration of uncertainty parameters and correlations to achieve good agreement, which would not have been possible using traditional methods.
•A new approach to predict variability of friction-damped turbine blades is presented.•The method uses Maximum Entropy to estimate a PDF of the friction describing function.•Computationally expensive Monte Carlo simulations of the nonlinear system are avoided.•Comparisons with numerical and experimental tests show generally good agreement.•The method enables rapid estimates of the response distribution.</description><subject>Accuracy</subject><subject>Amplitudes</subject><subject>Computer simulation</subject><subject>Conditional probability</subject><subject>Dampers</subject><subject>Damping</subject><subject>Friction</subject><subject>Friction damping</subject><subject>Gas turbine engines</subject><subject>Gas turbines</subject><subject>Harmonic balance method</subject><subject>Iterative methods</subject><subject>Localisation</subject><subject>Localised nonlinearities</subject><subject>Maximum entropy</subject><subject>Mistuning</subject><subject>Nonlinear vibration</subject><subject>Nonlinearity</subject><subject>Parameter uncertainty</subject><subject>Predictions</subject><subject>Probability density functions</subject><subject>Turbine blades</subject><subject>Uncertainty</subject><subject>Underplatform dampers</subject><subject>Vibration</subject><issn>0022-460X</issn><issn>1095-8568</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNp9kMtqwzAQRUVpoenjA7oTdO10JNuyTVch9AWBblrooiBkaZzIOJYrOYb8fWXSdVfDDPfO3DmE3DFYMmDioV22YVpyYGXsl8DSM7JgUOVJmYvynCwAOE8yAV-X5CqEFgCqLM0W5HtFezdhR_c47pyhjfN08GisHm2_peMOqccwuD4gnZS3qradHY_UNbTxs8j1iVH7AQ3dqkDHg69tj7TulMFwQy4a1QW8_avX5PP56WP9mmzeX97Wq02iU1GOSamaItNc1wKytFYVpKJSpjBFWilhhK5qgUIwnddNZgzwGoq84kbxLL6gtU6vyf1p7-DdzwHDKFt38H08KTnL84oBFyyq2EmlvQvBYyMHb_fKHyUDOUOUrYwQ5QxxHkWI0fN48mCMP1n0MmiLvY6APOpRGmf_cf8Cd1l7JA</recordid><startdate>20190203</startdate><enddate>20190203</enddate><creator>Butlin, T.</creator><creator>Ghaderi, P.</creator><creator>Spelman, G.</creator><creator>Midgley, W.J.B.</creator><creator>Umehara, R.</creator><general>Elsevier Ltd</general><general>Elsevier Science Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope><orcidid>https://orcid.org/0000-0003-3786-1691</orcidid></search><sort><creationdate>20190203</creationdate><title>A novel method for predicting the response variability of friction-damped gas turbine blades</title><author>Butlin, T. ; Ghaderi, P. ; Spelman, G. ; Midgley, W.J.B. ; Umehara, R.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c368t-8af74c2cb6043ba90369ad7d739a6d6c9b6e661c5bf4dd02b07592da24434ccc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Accuracy</topic><topic>Amplitudes</topic><topic>Computer simulation</topic><topic>Conditional probability</topic><topic>Dampers</topic><topic>Damping</topic><topic>Friction</topic><topic>Friction damping</topic><topic>Gas turbine engines</topic><topic>Gas turbines</topic><topic>Harmonic balance method</topic><topic>Iterative methods</topic><topic>Localisation</topic><topic>Localised nonlinearities</topic><topic>Maximum entropy</topic><topic>Mistuning</topic><topic>Nonlinear vibration</topic><topic>Nonlinearity</topic><topic>Parameter uncertainty</topic><topic>Predictions</topic><topic>Probability density functions</topic><topic>Turbine blades</topic><topic>Uncertainty</topic><topic>Underplatform dampers</topic><topic>Vibration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Butlin, T.</creatorcontrib><creatorcontrib>Ghaderi, P.</creatorcontrib><creatorcontrib>Spelman, G.</creatorcontrib><creatorcontrib>Midgley, W.J.B.</creatorcontrib><creatorcontrib>Umehara, R.</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of sound and vibration</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Butlin, T.</au><au>Ghaderi, P.</au><au>Spelman, G.</au><au>Midgley, W.J.B.</au><au>Umehara, R.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A novel method for predicting the response variability of friction-damped gas turbine blades</atitle><jtitle>Journal of sound and vibration</jtitle><date>2019-02-03</date><risdate>2019</risdate><volume>440</volume><spage>372</spage><epage>398</epage><pages>372-398</pages><issn>0022-460X</issn><eissn>1095-8568</eissn><abstract>Predicting the response of gas turbine blades with underplatform friction dampers is challenging due to the combination of frictional nonlinearity and system uncertainty: a traditional Monte Carlo approach to predicting response distributions requires a large number of nonlinear simulations which is computationally expensive. This paper presents a new approach based on the principle of Maximum Entropy that provides an estimate of the response distribution that is approximately two orders of magnitude faster than Monte Carlo Harmonic Balance Method simulations. The premise is to include the concept of ‘computational uncertainty’: incorporating lack of knowledge of the solution as part of the uncertainty, on the basis that there are diminishing returns in computing precise solutions to an uncertain system. To achieve this, the method uses a describing function approximation of the friction-damped part of the system; chooses an ignorance prior probability density function for the complex value of the describing function based on Coulombs friction law; updates the distribution using an estimate of the mean solution, the admissible domain of solutions, and the principle of Maximum Entropy; then carries out a linear Monte Carlo simulation to estimate the response distribution. The approach is validated by comparison with HBM simulations and experimental tests, using an idealised academic system consisting of a periodic array of beams (with controllable uncertainty) coupled by single-point friction dampers. Comparisons with two- and eight-blade systems show generally good agreement. Predicting the response statistics of the maximum blade amplitude reveals specific well-understood circumstances when the method is less effective. Predictions of the overall blade response statistics agree with Monte Carlo HBM extremely well across a wide range of excitation amplitudes and uncertainty levels. Critically, experimental comparisons reveal the care that is needed in accurately characterising uncertainty in order to obtain agreement of response percentiles. The new method allowed fast iteration of uncertainty parameters and correlations to achieve good agreement, which would not have been possible using traditional methods.
•A new approach to predict variability of friction-damped turbine blades is presented.•The method uses Maximum Entropy to estimate a PDF of the friction describing function.•Computationally expensive Monte Carlo simulations of the nonlinear system are avoided.•Comparisons with numerical and experimental tests show generally good agreement.•The method enables rapid estimates of the response distribution.</abstract><cop>Amsterdam</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.jsv.2018.10.013</doi><tpages>27</tpages><orcidid>https://orcid.org/0000-0003-3786-1691</orcidid><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0022-460X |
ispartof | Journal of sound and vibration, 2019-02, Vol.440, p.372-398 |
issn | 0022-460X 1095-8568 |
language | eng |
recordid | cdi_proquest_journals_2155910261 |
source | Elsevier ScienceDirect Journals |
subjects | Accuracy Amplitudes Computer simulation Conditional probability Dampers Damping Friction Friction damping Gas turbine engines Gas turbines Harmonic balance method Iterative methods Localisation Localised nonlinearities Maximum entropy Mistuning Nonlinear vibration Nonlinearity Parameter uncertainty Predictions Probability density functions Turbine blades Uncertainty Underplatform dampers Vibration |
title | A novel method for predicting the response variability of friction-damped gas turbine blades |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T14%3A32%3A20IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20novel%20method%20for%20predicting%20the%20response%20variability%20of%20friction-damped%20gas%20turbine%20blades&rft.jtitle=Journal%20of%20sound%20and%20vibration&rft.au=Butlin,%20T.&rft.date=2019-02-03&rft.volume=440&rft.spage=372&rft.epage=398&rft.pages=372-398&rft.issn=0022-460X&rft.eissn=1095-8568&rft_id=info:doi/10.1016/j.jsv.2018.10.013&rft_dat=%3Cproquest_cross%3E2155910261%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2155910261&rft_id=info:pmid/&rft_els_id=S0022460X18306801&rfr_iscdi=true |