Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression
To reveal the effect of high-temperature creep on the blade-tip radial running clearance of aeroengine high-pressure turbines, a distributed collaborative generalized regression extremum neural network is proposed by absorbing the heuristic thoughts of distributed collaborative response surface meth...
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description | To reveal the effect of high-temperature creep on the blade-tip radial running clearance of aeroengine high-pressure turbines, a distributed collaborative generalized regression extremum neural network is proposed by absorbing the heuristic thoughts of distributed collaborative response surface method and the generalized extremum neural network, in order to improve the reliability analysis of blade-tip clearance with creep behavior in terms of modeling precision and simulation efficiency. In this method, the generalized extremum neural network was used to handle the transients by simplifying the response process as one extremum and to address the strong nonlinearity by means of its nonlinear mapping ability. The distributed collaborative response surface method was applied to handle multi-object multi-discipline analysis, by decomposing one “big” model with hyperparameters and high nonlinearity into a series of “small” sub-models with few parameters and low nonlinearity. Based on the developed method, the blade-tip clearance reliability analysis of an aeroengine high-pressure turbine was performed subject to the creep behaviors of structural materials, by considering the randomness of influencing parameters such as gas temperature, rotational speed, material parameters, convective heat transfer coefficient, and so forth. It was found that the reliability degree of the clearance is 0.9909 when the allowable value is 2.2 mm, and the creep deformation of the clearance presents a normal distribution with a mean of 1.9829 mm and a standard deviation of 0.07539 mm. Based on a comparison of the methods, it is demonstrated that the proposed method requires a computing time of 1.201 s and has a computational accuracy of 99.929% over 104 simulations, which are improvements of 70.5% and 1.23%, respectively, relative to the distributed collaborative response surface method. Meanwhile, the high efficiency and high precision of the presented approach become more obvious with the increasing simulations. The efforts of this study provide a promising approach to improve the dynamic reliability analysis of complex structures. |
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In this method, the generalized extremum neural network was used to handle the transients by simplifying the response process as one extremum and to address the strong nonlinearity by means of its nonlinear mapping ability. The distributed collaborative response surface method was applied to handle multi-object multi-discipline analysis, by decomposing one “big” model with hyperparameters and high nonlinearity into a series of “small” sub-models with few parameters and low nonlinearity. Based on the developed method, the blade-tip clearance reliability analysis of an aeroengine high-pressure turbine was performed subject to the creep behaviors of structural materials, by considering the randomness of influencing parameters such as gas temperature, rotational speed, material parameters, convective heat transfer coefficient, and so forth. It was found that the reliability degree of the clearance is 0.9909 when the allowable value is 2.2 mm, and the creep deformation of the clearance presents a normal distribution with a mean of 1.9829 mm and a standard deviation of 0.07539 mm. Based on a comparison of the methods, it is demonstrated that the proposed method requires a computing time of 1.201 s and has a computational accuracy of 99.929% over 104 simulations, which are improvements of 70.5% and 1.23%, respectively, relative to the distributed collaborative response surface method. Meanwhile, the high efficiency and high precision of the presented approach become more obvious with the increasing simulations. The efforts of this study provide a promising approach to improve the dynamic reliability analysis of complex structures.</description><identifier>ISSN: 1996-1944</identifier><identifier>EISSN: 1996-1944</identifier><identifier>DOI: 10.3390/ma12213552</identifier><identifier>PMID: 31671898</identifier><language>eng</language><publisher>Basel: MDPI AG</publisher><subject>Accuracy ; Aerospace engines ; Blade tips ; Collaboration ; Computing time ; Convective heat transfer ; Creep strength ; Efficiency ; Gas temperature ; Heat transfer coefficients ; High temperature ; Mathematical models ; Methods ; Network reliability ; Neural networks ; Nonlinearity ; Normal distribution ; Parameters ; Precipitation hardening ; Reliability analysis ; Reliability engineering ; Response surface methodology ; Simulation ; Statistical analysis ; Stress concentration ; Structural reliability ; Tip clearance ; Turbine blades ; Turbines ; Wavelet transforms</subject><ispartof>Materials, 2019-10, Vol.12 (21), p.3552</ispartof><rights>2019 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><rights>2019 by the authors. 2019</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c383t-3d270c7fb1568782cfb2539f1f251df60372bec2b79c36c93a220e8d416156973</citedby><cites>FETCH-LOGICAL-c383t-3d270c7fb1568782cfb2539f1f251df60372bec2b79c36c93a220e8d416156973</cites><orcidid>0000-0002-5939-1048 ; 0000-0001-5333-1055</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.ncbi.nlm.nih.gov/pmc/articles/PMC6861887/pdf/$$EPDF$$P50$$Gpubmedcentral$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.ncbi.nlm.nih.gov/pmc/articles/PMC6861887/$$EHTML$$P50$$Gpubmedcentral$$Hfree_for_read</linktohtml><link.rule.ids>230,314,723,776,780,881,27901,27902,53766,53768</link.rule.ids></links><search><creatorcontrib>Zhang, Chun-Yi</creatorcontrib><creatorcontrib>Wei, Jing-Shan</creatorcontrib><creatorcontrib>Wang, Ze</creatorcontrib><creatorcontrib>Yuan, Zhe-Shan</creatorcontrib><creatorcontrib>Fei, Cheng-Wei</creatorcontrib><creatorcontrib>Lu, Cheng</creatorcontrib><title>Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression</title><title>Materials</title><description>To reveal the effect of high-temperature creep on the blade-tip radial running clearance of aeroengine high-pressure turbines, a distributed collaborative generalized regression extremum neural network is proposed by absorbing the heuristic thoughts of distributed collaborative response surface method and the generalized extremum neural network, in order to improve the reliability analysis of blade-tip clearance with creep behavior in terms of modeling precision and simulation efficiency. In this method, the generalized extremum neural network was used to handle the transients by simplifying the response process as one extremum and to address the strong nonlinearity by means of its nonlinear mapping ability. The distributed collaborative response surface method was applied to handle multi-object multi-discipline analysis, by decomposing one “big” model with hyperparameters and high nonlinearity into a series of “small” sub-models with few parameters and low nonlinearity. Based on the developed method, the blade-tip clearance reliability analysis of an aeroengine high-pressure turbine was performed subject to the creep behaviors of structural materials, by considering the randomness of influencing parameters such as gas temperature, rotational speed, material parameters, convective heat transfer coefficient, and so forth. It was found that the reliability degree of the clearance is 0.9909 when the allowable value is 2.2 mm, and the creep deformation of the clearance presents a normal distribution with a mean of 1.9829 mm and a standard deviation of 0.07539 mm. Based on a comparison of the methods, it is demonstrated that the proposed method requires a computing time of 1.201 s and has a computational accuracy of 99.929% over 104 simulations, which are improvements of 70.5% and 1.23%, respectively, relative to the distributed collaborative response surface method. Meanwhile, the high efficiency and high precision of the presented approach become more obvious with the increasing simulations. The efforts of this study provide a promising approach to improve the dynamic reliability analysis of complex structures.</description><subject>Accuracy</subject><subject>Aerospace engines</subject><subject>Blade tips</subject><subject>Collaboration</subject><subject>Computing time</subject><subject>Convective heat transfer</subject><subject>Creep strength</subject><subject>Efficiency</subject><subject>Gas temperature</subject><subject>Heat transfer coefficients</subject><subject>High temperature</subject><subject>Mathematical models</subject><subject>Methods</subject><subject>Network reliability</subject><subject>Neural networks</subject><subject>Nonlinearity</subject><subject>Normal distribution</subject><subject>Parameters</subject><subject>Precipitation hardening</subject><subject>Reliability analysis</subject><subject>Reliability engineering</subject><subject>Response surface methodology</subject><subject>Simulation</subject><subject>Statistical analysis</subject><subject>Stress concentration</subject><subject>Structural reliability</subject><subject>Tip clearance</subject><subject>Turbine blades</subject><subject>Turbines</subject><subject>Wavelet transforms</subject><issn>1996-1944</issn><issn>1996-1944</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNpdkU1LAzEQhoMoVrQXf0HAiwirm6SbTS6CFr-gKEg9h2x2UqPppia7Ff-9W1v8mssMzDvPvMMgdEjyU8ZkfjbXhFLCioJuoT0iJc-IHI22f9UDNEzpJe-DMSKo3EUDRnhJhBR7yI4jwCK71Alq_Aje6cp5137gq6X2nW5daHCweNrFyjWAL72uIZu6BR570FE3BvC7a5_xfViCx_fQRb1K7XuIrz1vFiGlnnGAdqz2CYabvI-erq-m49ts8nBzN76YZIYJ1maspmVuSluRgotSUGMrWjBpiaUFqS3PWUkrMLQqpWHcSKYpzUHUI8L7CVmyfXS-5i66ag61gabtDalFdHMdP1TQTv3tNO5ZzcJSccGJECvA8QYQw1sHqVVzlwx4rxsIXVKUEcJ7H1-7jv5JX0IXm_48RYuRKCnnUvSqk7XKxJBSBPtthuRq9UH180H2CUtHjBc</recordid><startdate>20191029</startdate><enddate>20191029</enddate><creator>Zhang, Chun-Yi</creator><creator>Wei, Jing-Shan</creator><creator>Wang, Ze</creator><creator>Yuan, Zhe-Shan</creator><creator>Fei, Cheng-Wei</creator><creator>Lu, Cheng</creator><general>MDPI AG</general><general>MDPI</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>PDBOC</scope><scope>PHGZM</scope><scope>PHGZT</scope><scope>PIMPY</scope><scope>PKEHL</scope><scope>PQEST</scope><scope>PQGLB</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>7X8</scope><scope>5PM</scope><orcidid>https://orcid.org/0000-0002-5939-1048</orcidid><orcidid>https://orcid.org/0000-0001-5333-1055</orcidid></search><sort><creationdate>20191029</creationdate><title>Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression</title><author>Zhang, Chun-Yi ; Wei, Jing-Shan ; Wang, Ze ; Yuan, Zhe-Shan ; Fei, Cheng-Wei ; Lu, Cheng</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c383t-3d270c7fb1568782cfb2539f1f251df60372bec2b79c36c93a220e8d416156973</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Accuracy</topic><topic>Aerospace engines</topic><topic>Blade tips</topic><topic>Collaboration</topic><topic>Computing time</topic><topic>Convective heat transfer</topic><topic>Creep strength</topic><topic>Efficiency</topic><topic>Gas temperature</topic><topic>Heat transfer coefficients</topic><topic>High temperature</topic><topic>Mathematical models</topic><topic>Methods</topic><topic>Network reliability</topic><topic>Neural networks</topic><topic>Nonlinearity</topic><topic>Normal distribution</topic><topic>Parameters</topic><topic>Precipitation hardening</topic><topic>Reliability analysis</topic><topic>Reliability engineering</topic><topic>Response surface methodology</topic><topic>Simulation</topic><topic>Statistical analysis</topic><topic>Stress concentration</topic><topic>Structural reliability</topic><topic>Tip clearance</topic><topic>Turbine blades</topic><topic>Turbines</topic><topic>Wavelet transforms</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhang, Chun-Yi</creatorcontrib><creatorcontrib>Wei, Jing-Shan</creatorcontrib><creatorcontrib>Wang, Ze</creatorcontrib><creatorcontrib>Yuan, Zhe-Shan</creatorcontrib><creatorcontrib>Fei, Cheng-Wei</creatorcontrib><creatorcontrib>Lu, Cheng</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>Materials Science Database</collection><collection>Materials Science Collection</collection><collection>ProQuest Central (New)</collection><collection>ProQuest One Academic (New)</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Middle East (New)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Applied & Life Sciences</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>MEDLINE - Academic</collection><collection>PubMed Central (Full Participant titles)</collection><jtitle>Materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhang, Chun-Yi</au><au>Wei, Jing-Shan</au><au>Wang, Ze</au><au>Yuan, Zhe-Shan</au><au>Fei, Cheng-Wei</au><au>Lu, Cheng</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression</atitle><jtitle>Materials</jtitle><date>2019-10-29</date><risdate>2019</risdate><volume>12</volume><issue>21</issue><spage>3552</spage><pages>3552-</pages><issn>1996-1944</issn><eissn>1996-1944</eissn><abstract>To reveal the effect of high-temperature creep on the blade-tip radial running clearance of aeroengine high-pressure turbines, a distributed collaborative generalized regression extremum neural network is proposed by absorbing the heuristic thoughts of distributed collaborative response surface method and the generalized extremum neural network, in order to improve the reliability analysis of blade-tip clearance with creep behavior in terms of modeling precision and simulation efficiency. In this method, the generalized extremum neural network was used to handle the transients by simplifying the response process as one extremum and to address the strong nonlinearity by means of its nonlinear mapping ability. The distributed collaborative response surface method was applied to handle multi-object multi-discipline analysis, by decomposing one “big” model with hyperparameters and high nonlinearity into a series of “small” sub-models with few parameters and low nonlinearity. Based on the developed method, the blade-tip clearance reliability analysis of an aeroengine high-pressure turbine was performed subject to the creep behaviors of structural materials, by considering the randomness of influencing parameters such as gas temperature, rotational speed, material parameters, convective heat transfer coefficient, and so forth. It was found that the reliability degree of the clearance is 0.9909 when the allowable value is 2.2 mm, and the creep deformation of the clearance presents a normal distribution with a mean of 1.9829 mm and a standard deviation of 0.07539 mm. Based on a comparison of the methods, it is demonstrated that the proposed method requires a computing time of 1.201 s and has a computational accuracy of 99.929% over 104 simulations, which are improvements of 70.5% and 1.23%, respectively, relative to the distributed collaborative response surface method. Meanwhile, the high efficiency and high precision of the presented approach become more obvious with the increasing simulations. The efforts of this study provide a promising approach to improve the dynamic reliability analysis of complex structures.</abstract><cop>Basel</cop><pub>MDPI AG</pub><pmid>31671898</pmid><doi>10.3390/ma12213552</doi><orcidid>https://orcid.org/0000-0002-5939-1048</orcidid><orcidid>https://orcid.org/0000-0001-5333-1055</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Accuracy Aerospace engines Blade tips Collaboration Computing time Convective heat transfer Creep strength Efficiency Gas temperature Heat transfer coefficients High temperature Mathematical models Methods Network reliability Neural networks Nonlinearity Normal distribution Parameters Precipitation hardening Reliability analysis Reliability engineering Response surface methodology Simulation Statistical analysis Stress concentration Structural reliability Tip clearance Turbine blades Turbines Wavelet transforms |
title | Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression |
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