| Literature DB >> 29364844 |
Yinying Sheng1, Youlu Hua2,3, Xiaojian Wang4, Xueyang Zhao5, Lianxi Chen6, Hanyu Zhou7, James Wang8, Christopher C Berndt9, Wei Li10,11.
Abstract
The technology of high-density electropulEntities:
Keywords: crack healing; dislocation behaviour; high-density electropulsing; mechanical properties; oriented microstructure or texture; recrystallization; resistivity of materials; solid phase transition
Year: 2018 PMID: 29364844 PMCID: PMC5848882 DOI: 10.3390/ma11020185
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Figure 1The microstructure of different alloys before treatment (a1–a7) and after electropulsing treatment (EPT) treatment (b1–b7).
Figure 2Electron back-scattered diffraction (EBSD) maps and the corresponding distributions of the misorientation angle of static recrystallization (SRX) for the magnesium alloy under EPT: (a) Cold-rolled AZ91 alloy with different frequencies: (a1) no-EPT; (a2) 100 Hz; and (a3) 110 Hz [66]. (b) Rolled ZK60 alloy with different pulse widths: (b1) 20 μs; (b2) 22 μs; and (b3) 30 μs [67].
Figure 3Schematic diagram of phase transition and ultra-fine grains: (a) low-carbon steel [77]; (b) Cu-Zn alloy [79]: (1) nucleation of γ or β phase, (2) grain growth of γ and β phase, (3) formation of α phase nucleation and (4) formation of ultra-fine grains and twin structure of α phase and β′ phase.
Figure 4The formation of orientation microstructures in pearlite: (a,b) various configurations of pearlite microstructure [91]; (c,d) SEM images of samples after EPT [93].
Figure 5The {0001} and {10} pole figures of the AZ91 alloy after EPT: (a) cold-rolled sample; (b) 100 Hz-EPT; (c) 110 Hz-EPT; (d) 133 Hz-EPT [68].
Mechanical properties of pure titanium and titanium alloys before and after EPT.
| Sample State | Ultimate Tensile Strength (MPa) | Yield Strength (MPa) | Tensile Elongation (%) | Ref. | |
|---|---|---|---|---|---|
| TA15 sheet | cold-rolled | 1175 | - | 7.2 | [ |
| electropulsed | 1100 | - | 13.9 | ||
| increase by (%) | −6 | - | +93 | ||
| TC4 sheet | annealed | 1033 | 936 | 15.6 | [ |
| electropulsed | 947 | 750 | 23.18 | ||
| increase by (%) | −8.3 | −19.8 | +48.6 | ||
| TA1-A CP-Ti sheet | annealed | 300 | 210 | 40 | [ |
| electropulsed | 400 | 300 | 31.5 | ||
| increase by (%) | +33 | +43 | −21 | ||
Figure 6Stress-strain curves of TA15 alloys and ZA22 alloys at different pulse current densities: (a) TA15 [62]; and (b) ZA22 [86].
Mechanical properties of zinc alloys before and after EPT.
| Sample State | Peak Current Density (A/mm2) | Ultimate Tensile Strength (MPa) | Tensile Elongation (%) | Ref. | |
|---|---|---|---|---|---|
| ZA22 sheet | non-EPT | - | 298 | 4.5 | [ |
| EPT | 8.13 | 272 | 6.4 | ||
| 12.32 | 300 | 8.5 | |||
| 15.75 | 260 * | 5.5 | |||
| 21.21 | 275 | 6.4 | |||
* The mechanical properties are estimated from Figure 1 in [86].
Mechanical properties of magnesium alloys before and after EPT.
| Sample State | Hardness (HV) | Ultimate Tensile Strength (MPa) | Yield Strength (MPa) | Tensile Elongation (%) | Refs. | |
|---|---|---|---|---|---|---|
| ZK60 sheet | cold rolled | 848 | 210 | — | 15.7 | [ |
| Electropulsed | 728 | 320 | — | 30 | ||
| increase by% | −14.15 | +52.4 | — | +91 | ||
| AZ91 strip | cold rolled | — | 330 | 245 | 16.2 | [ |
| Electropulsed | — | 362~370 | 270 | 27.6~28.4 | ||
| increase by% | — | +11~12 | +10 | +70~75 | ||
| AZ31 strip | cold rolled | — | 315 * | 280 * | 10 | [ |
| Electropulsed | — | 295~262 * | 265~185 * | 29~43 | ||
| increase by% | — | −6~18 | −5~34 * | +190~330 | ||
* The mechanical properties are estimated from Figure 4 in [112].
Figure 7Stress-strain curves for magnesium alloys: (a) pulse width [67]; (b) temperature [89]; (c) pulse frequency [13]; and (d) voltage [114].
Mechanical properties of steels before and after EPT. TRIP, transformation-induced plasticity.
| Sample State | Ultimate Tensile Strength (MPa) | Yield Strength (MPa) | Tensile Elongation (%) | Vickers Hardness (HV) | Ref. | |
|---|---|---|---|---|---|---|
| TRIP sheet | hot rolled | 700 * | 570 * | 23 * | 230 * | [ |
| electropulsed | 630 * | 480 * | 26 * | 180 * | ||
| increase by (%) | −0 | −15.79 | +13.04 | −21.74 | ||
| Low-carbon steel sheet | annealed | 580 | — | 40 | 179 | [ |
| electropulsed | 1040 | — | 45 | 325 | ||
| increase by (%) | +79 | — | +13 | +82 | ||
| DP600 sheet | cold rolled | 1034.25 | 773.26 | 3.31 | 301 ± 8 | [ |
| electropulsed | 1126.33 | 1074.66 | 3.12 | 364 ± 12 | ||
| increase by (%) | +8.90 | +38.98 | −5.74 | +20.9 | ||
* The mechanical properties are estimated rom Figure 8, Figure 9, Figure 10 and Figure 11 in [58].
Figure 8S-N curves of stainless steel (SUS316) before and after EPT [116].
Figure 9Schematic diagram of defect healing and recrystallization: (a) plastic deformation to form defects and defective areas of the current bypass; (b) the formation of pressure around the metal defects; (c) healing defects, recrystallization and high energy EPT cladding (EPTC) [55,124].
Figure 10Morphology of healed cracks and healing areas: (a) pre-crack; (b) healed area; (c) healing areas; (d,e) partially enlarged view [125].
Figure 11Closure of an entire fatigue crack by multiple applications of high-density electropulsing [128].
Figure 12The average maximum temperature of different metals and alloys with different peak current densities [24,30,52,53,59,63,67,78,82,85,98,101,112,114,123,125,131].
Figure 13Schematic diagram of dislocation behaviour during recovery and recrystallization and (a–f) corresponding TEM images of the Ti-6Al-4V alloy during the process [124].