Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V
Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and an...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Zhang, Kun [verfasserIn] Zhang, Kai [verfasserIn] Zhu, Yuman [verfasserIn] Wu, Xinhua [verfasserIn] Williams, Jim [verfasserIn] Liang, Enquan [verfasserIn] Ma, Jisheng [verfasserIn] Zhang, Ren [verfasserIn] Lim, Chao Voon Samuel [verfasserIn] Huang, Aijun [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2021 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Journal of materials engineering and performance - New York, NY : Springer, 1992, 30(2021), 2 vom: 05. Jan., Seite 1147-1156 |
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| Übergeordnetes Werk: |
volume:30 ; year:2021 ; number:2 ; day:05 ; month:01 ; pages:1147-1156 |
| Links: |
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| DOI / URN: |
10.1007/s11665-020-05396-3 |
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| Katalog-ID: |
SPR043147208 |
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| 520 | |a Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. | ||
| 650 | 4 | |a anneal |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a globular primary α |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a microstructure |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a mechanical properties |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a texture |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Ti-6Al-4V |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Zhang, Kai |e verfasserin |4 aut | |
| 700 | 1 | |a Zhu, Yuman |e verfasserin |4 aut | |
| 700 | 1 | |a Wu, Xinhua |e verfasserin |4 aut | |
| 700 | 1 | |a Williams, Jim |e verfasserin |4 aut | |
| 700 | 1 | |a Liang, Enquan |e verfasserin |4 aut | |
| 700 | 1 | |a Ma, Jisheng |e verfasserin |4 aut | |
| 700 | 1 | |a Zhang, Ren |e verfasserin |4 aut | |
| 700 | 1 | |a Lim, Chao Voon Samuel |e verfasserin |4 aut | |
| 700 | 1 | |a Huang, Aijun |e verfasserin |4 aut | |
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10.1007/s11665-020-05396-3 doi (DE-627)SPR043147208 (DE-599)SPRs11665-020-05396-3-e (SPR)s11665-020-05396-3-e DE-627 ger DE-627 rakwb eng 620 660 670 ASE Zhang, Kun verfasserin aut Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. anneal (dpeaa)DE-He213 globular primary α (dpeaa)DE-He213 microstructure (dpeaa)DE-He213 mechanical properties (dpeaa)DE-He213 texture (dpeaa)DE-He213 Ti-6Al-4V (dpeaa)DE-He213 Zhang, Kai verfasserin aut Zhu, Yuman verfasserin aut Wu, Xinhua verfasserin aut Williams, Jim verfasserin aut Liang, Enquan verfasserin aut Ma, Jisheng verfasserin aut Zhang, Ren verfasserin aut Lim, Chao Voon Samuel verfasserin aut Huang, Aijun verfasserin aut Enthalten in Journal of materials engineering and performance New York, NY : Springer, 1992 30(2021), 2 vom: 05. Jan., Seite 1147-1156 (DE-627)329975447 (DE-600)2048384-3 1544-1024 nnns volume:30 year:2021 number:2 day:05 month:01 pages:1147-1156 https://dx.doi.org/10.1007/s11665-020-05396-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA 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_65 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_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_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 30 2021 2 05 01 1147-1156 |
| spelling |
10.1007/s11665-020-05396-3 doi (DE-627)SPR043147208 (DE-599)SPRs11665-020-05396-3-e (SPR)s11665-020-05396-3-e DE-627 ger DE-627 rakwb eng 620 660 670 ASE Zhang, Kun verfasserin aut Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. anneal (dpeaa)DE-He213 globular primary α (dpeaa)DE-He213 microstructure (dpeaa)DE-He213 mechanical properties (dpeaa)DE-He213 texture (dpeaa)DE-He213 Ti-6Al-4V (dpeaa)DE-He213 Zhang, Kai verfasserin aut Zhu, Yuman verfasserin aut Wu, Xinhua verfasserin aut Williams, Jim verfasserin aut Liang, Enquan verfasserin aut Ma, Jisheng verfasserin aut Zhang, Ren verfasserin aut Lim, Chao Voon Samuel verfasserin aut Huang, Aijun verfasserin aut Enthalten in Journal of materials engineering and performance New York, NY : Springer, 1992 30(2021), 2 vom: 05. Jan., Seite 1147-1156 (DE-627)329975447 (DE-600)2048384-3 1544-1024 nnns volume:30 year:2021 number:2 day:05 month:01 pages:1147-1156 https://dx.doi.org/10.1007/s11665-020-05396-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA 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_65 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_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_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 30 2021 2 05 01 1147-1156 |
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10.1007/s11665-020-05396-3 doi (DE-627)SPR043147208 (DE-599)SPRs11665-020-05396-3-e (SPR)s11665-020-05396-3-e DE-627 ger DE-627 rakwb eng 620 660 670 ASE Zhang, Kun verfasserin aut Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. anneal (dpeaa)DE-He213 globular primary α (dpeaa)DE-He213 microstructure (dpeaa)DE-He213 mechanical properties (dpeaa)DE-He213 texture (dpeaa)DE-He213 Ti-6Al-4V (dpeaa)DE-He213 Zhang, Kai verfasserin aut Zhu, Yuman verfasserin aut Wu, Xinhua verfasserin aut Williams, Jim verfasserin aut Liang, Enquan verfasserin aut Ma, Jisheng verfasserin aut Zhang, Ren verfasserin aut Lim, Chao Voon Samuel verfasserin aut Huang, Aijun verfasserin aut Enthalten in Journal of materials engineering and performance New York, NY : Springer, 1992 30(2021), 2 vom: 05. Jan., Seite 1147-1156 (DE-627)329975447 (DE-600)2048384-3 1544-1024 nnns volume:30 year:2021 number:2 day:05 month:01 pages:1147-1156 https://dx.doi.org/10.1007/s11665-020-05396-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA 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_65 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_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_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 30 2021 2 05 01 1147-1156 |
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10.1007/s11665-020-05396-3 doi (DE-627)SPR043147208 (DE-599)SPRs11665-020-05396-3-e (SPR)s11665-020-05396-3-e DE-627 ger DE-627 rakwb eng 620 660 670 ASE Zhang, Kun verfasserin aut Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. anneal (dpeaa)DE-He213 globular primary α (dpeaa)DE-He213 microstructure (dpeaa)DE-He213 mechanical properties (dpeaa)DE-He213 texture (dpeaa)DE-He213 Ti-6Al-4V (dpeaa)DE-He213 Zhang, Kai verfasserin aut Zhu, Yuman verfasserin aut Wu, Xinhua verfasserin aut Williams, Jim verfasserin aut Liang, Enquan verfasserin aut Ma, Jisheng verfasserin aut Zhang, Ren verfasserin aut Lim, Chao Voon Samuel verfasserin aut Huang, Aijun verfasserin aut Enthalten in Journal of materials engineering and performance New York, NY : Springer, 1992 30(2021), 2 vom: 05. Jan., Seite 1147-1156 (DE-627)329975447 (DE-600)2048384-3 1544-1024 nnns volume:30 year:2021 number:2 day:05 month:01 pages:1147-1156 https://dx.doi.org/10.1007/s11665-020-05396-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA 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_65 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_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_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 30 2021 2 05 01 1147-1156 |
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10.1007/s11665-020-05396-3 doi (DE-627)SPR043147208 (DE-599)SPRs11665-020-05396-3-e (SPR)s11665-020-05396-3-e DE-627 ger DE-627 rakwb eng 620 660 670 ASE Zhang, Kun verfasserin aut Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. anneal (dpeaa)DE-He213 globular primary α (dpeaa)DE-He213 microstructure (dpeaa)DE-He213 mechanical properties (dpeaa)DE-He213 texture (dpeaa)DE-He213 Ti-6Al-4V (dpeaa)DE-He213 Zhang, Kai verfasserin aut Zhu, Yuman verfasserin aut Wu, Xinhua verfasserin aut Williams, Jim verfasserin aut Liang, Enquan verfasserin aut Ma, Jisheng verfasserin aut Zhang, Ren verfasserin aut Lim, Chao Voon Samuel verfasserin aut Huang, Aijun verfasserin aut Enthalten in Journal of materials engineering and performance New York, NY : Springer, 1992 30(2021), 2 vom: 05. Jan., Seite 1147-1156 (DE-627)329975447 (DE-600)2048384-3 1544-1024 nnns volume:30 year:2021 number:2 day:05 month:01 pages:1147-1156 https://dx.doi.org/10.1007/s11665-020-05396-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA 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_65 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_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_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 30 2021 2 05 01 1147-1156 |
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Zhang, Kun @@aut@@ Zhang, Kai @@aut@@ Zhu, Yuman @@aut@@ Wu, Xinhua @@aut@@ Williams, Jim @@aut@@ Liang, Enquan @@aut@@ Ma, Jisheng @@aut@@ Zhang, Ren @@aut@@ Lim, Chao Voon Samuel @@aut@@ Huang, Aijun @@aut@@ |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR043147208</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230519085509.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">210215s2021 xx |||||o 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s11665-020-05396-3</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR043147208</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)SPRs11665-020-05396-3-e</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s11665-020-05396-3-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">620</subfield><subfield code="a">660</subfield><subfield code="a">670</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Zhang, Kun</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2021</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. 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Zhang, Kun |
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Zhang, Kun ddc 620 misc anneal misc globular primary α misc microstructure misc mechanical properties misc texture misc Ti-6Al-4V Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V |
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620 660 670 ASE Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V anneal (dpeaa)DE-He213 globular primary α (dpeaa)DE-He213 microstructure (dpeaa)DE-He213 mechanical properties (dpeaa)DE-He213 texture (dpeaa)DE-He213 Ti-6Al-4V (dpeaa)DE-He213 |
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effect of deformation reduction on microstructure, texture, and mechanical properties of forged ti-6al-4v |
| title_auth |
Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V |
| abstract |
Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. |
| abstractGer |
Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. |
| abstract_unstemmed |
Abstract In this work, the effects of nominal reductions during forging experiments on microstructures, tensile and fatigue properties of Ti-6Al-4V have been investigated. The microstructure of the starting material was a combination of equiaxed and lamellar α phases. With further deformation and annealing heat treatment, the volume fraction of globular primary α increased by about 20% as the nominal reduction increased from 10 to 50%. More notably, the ultimate tensile stress and yield stress were increased by approximately 50 MPa, and the ductility remained constant, with the nominal reduction from 10 up to 50%. Further detailed characterization revealed that the improvement in tensile and fatigue properties could be attributed to the reduction in the effective slip length, increase in the interface density, and realignment of the (0002) planes with the tensile axis. |
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2 |
| title_short |
Effect of Deformation Reduction on Microstructure, Texture, and Mechanical Properties of Forged Ti-6Al-4V |
| url |
https://dx.doi.org/10.1007/s11665-020-05396-3 |
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true |
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Zhang, Kai Zhu, Yuman Wu, Xinhua Williams, Jim Liang, Enquan Ma, Jisheng Zhang, Ren Lim, Chao Voon Samuel Huang, Aijun |
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Zhang, Kai Zhu, Yuman Wu, Xinhua Williams, Jim Liang, Enquan Ma, Jisheng Zhang, Ren Lim, Chao Voon Samuel Huang, Aijun |
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| doi_str |
10.1007/s11665-020-05396-3 |
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2024-07-03T16:53:08.571Z |
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| score |
7.399453 |