Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning
Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyz...
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| Autor*in: |
Wang, Menghan [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2023 |
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| Anmerkung: |
© The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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| Übergeordnetes Werk: |
Enthalten in: The international journal of advanced manufacturing technology - London : Springer, 1985, 127(2023), 5-6 vom: 07. Juni, Seite 2723-2735 |
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| Übergeordnetes Werk: |
volume:127 ; year:2023 ; number:5-6 ; day:07 ; month:06 ; pages:2723-2735 |
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| DOI / URN: |
10.1007/s00170-023-11634-4 |
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| Katalog-ID: |
SPR052078949 |
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| 520 | |a Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. | ||
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| 700 | 1 | |a Li, Songlin |4 aut | |
| 700 | 1 | |a Wang, ZhouTian |4 aut | |
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10.1007/s00170-023-11634-4 doi (DE-627)SPR052078949 (SPR)s00170-023-11634-4-e DE-627 ger DE-627 rakwb eng Wang, Menghan verfasserin aut Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. Large stepped shaft (dpeaa)DE-He213 Extrusion (dpeaa)DE-He213 Prediction of shrinkage cavity defects (dpeaa)DE-He213 Machine learning (dpeaa)DE-He213 Du, Menglong aut Li, Songlin aut Wang, ZhouTian aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 127(2023), 5-6 vom: 07. Juni, Seite 2723-2735 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:127 year:2023 number:5-6 day:07 month:06 pages:2723-2735 https://dx.doi.org/10.1007/s00170-023-11634-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 127 2023 5-6 07 06 2723-2735 |
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10.1007/s00170-023-11634-4 doi (DE-627)SPR052078949 (SPR)s00170-023-11634-4-e DE-627 ger DE-627 rakwb eng Wang, Menghan verfasserin aut Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. Large stepped shaft (dpeaa)DE-He213 Extrusion (dpeaa)DE-He213 Prediction of shrinkage cavity defects (dpeaa)DE-He213 Machine learning (dpeaa)DE-He213 Du, Menglong aut Li, Songlin aut Wang, ZhouTian aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 127(2023), 5-6 vom: 07. Juni, Seite 2723-2735 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:127 year:2023 number:5-6 day:07 month:06 pages:2723-2735 https://dx.doi.org/10.1007/s00170-023-11634-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 127 2023 5-6 07 06 2723-2735 |
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10.1007/s00170-023-11634-4 doi (DE-627)SPR052078949 (SPR)s00170-023-11634-4-e DE-627 ger DE-627 rakwb eng Wang, Menghan verfasserin aut Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. Large stepped shaft (dpeaa)DE-He213 Extrusion (dpeaa)DE-He213 Prediction of shrinkage cavity defects (dpeaa)DE-He213 Machine learning (dpeaa)DE-He213 Du, Menglong aut Li, Songlin aut Wang, ZhouTian aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 127(2023), 5-6 vom: 07. Juni, Seite 2723-2735 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:127 year:2023 number:5-6 day:07 month:06 pages:2723-2735 https://dx.doi.org/10.1007/s00170-023-11634-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 127 2023 5-6 07 06 2723-2735 |
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10.1007/s00170-023-11634-4 doi (DE-627)SPR052078949 (SPR)s00170-023-11634-4-e DE-627 ger DE-627 rakwb eng Wang, Menghan verfasserin aut Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. Large stepped shaft (dpeaa)DE-He213 Extrusion (dpeaa)DE-He213 Prediction of shrinkage cavity defects (dpeaa)DE-He213 Machine learning (dpeaa)DE-He213 Du, Menglong aut Li, Songlin aut Wang, ZhouTian aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 127(2023), 5-6 vom: 07. Juni, Seite 2723-2735 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:127 year:2023 number:5-6 day:07 month:06 pages:2723-2735 https://dx.doi.org/10.1007/s00170-023-11634-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 127 2023 5-6 07 06 2723-2735 |
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10.1007/s00170-023-11634-4 doi (DE-627)SPR052078949 (SPR)s00170-023-11634-4-e DE-627 ger DE-627 rakwb eng Wang, Menghan verfasserin aut Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. Large stepped shaft (dpeaa)DE-He213 Extrusion (dpeaa)DE-He213 Prediction of shrinkage cavity defects (dpeaa)DE-He213 Machine learning (dpeaa)DE-He213 Du, Menglong aut Li, Songlin aut Wang, ZhouTian aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 127(2023), 5-6 vom: 07. Juni, Seite 2723-2735 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:127 year:2023 number:5-6 day:07 month:06 pages:2723-2735 https://dx.doi.org/10.1007/s00170-023-11634-4 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 127 2023 5-6 07 06 2723-2735 |
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| author |
Wang, Menghan |
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Wang, Menghan misc Large stepped shaft misc Extrusion misc Prediction of shrinkage cavity defects misc Machine learning Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning |
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Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning Large stepped shaft (dpeaa)DE-He213 Extrusion (dpeaa)DE-He213 Prediction of shrinkage cavity defects (dpeaa)DE-He213 Machine learning (dpeaa)DE-He213 |
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Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning |
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10.1007/s00170-023-11634-4 |
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analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning |
| title_auth |
Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning |
| abstract |
Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
| abstractGer |
Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
| abstract_unstemmed |
Abstract A stepped shaft, as an integral part of an aeroengine system, is prone to shrinkage cavity defects during open-die composite extrusion, which affects the service performance and life of the fan shaft. First, the deformation process of the fan shaft in open-die composite extrusion was analyzed using finite element simulation. The shrinkage primarily occurred in the forward extrusion stage. Subsequently, the mathematical conditions of the shrinkage cavity in the forward extrusion were obtained using the differential element method. The die parameters affecting the shrinkage cavity were mainly the die inclination and extrusion ratio. A finite element simulation of a simplified forward extrusion model and a machine learning classification algorithm were used to create a shrinkage cavity prediction diagram with solid performance and good generalization. Stepped-shaft forging with satisfactory performance and no shrinkage was obtained by selecting appropriate die parameters according to the shrinkage prediction diagram. © The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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5-6 |
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Analysis and prediction of shrinkage cavity defects of a large stepped shaft in open-die composite extrusion based on machine learning |
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https://dx.doi.org/10.1007/s00170-023-11634-4 |
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Du, Menglong Li, Songlin Wang, ZhouTian |
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Du, Menglong Li, Songlin Wang, ZhouTian |
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270127712 |
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| doi_str |
10.1007/s00170-023-11634-4 |
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2024-07-04T01:09:48.327Z |
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| score |
7.401846 |