| Literature DB >> 35564124 |
Akhil Kishore1, Merbin John2, Alessandro M Ralls2, Subin Antony Jose2, Udaya Bhat Kuruveri3, Pradeep L Menezes2.
Abstract
Ultrasonic nanocrystal surface modification (UNSM) is a unique, mechanical, impact-based surface severe plastic deformation (S2PD) method. This newly developed technique finds diverse applications in the aerospace, automotive, nuclear, biomedical, and chemical industries. The severe plastic deformation (SPD) during UNSM can generate gradient nanostructured surface (GNS) layers with remarkable mechanical properties. This review paper elucidates the current state-of-the-art UNSM technique on a broad range of engineering materials. This review also summarizes the effect of UNSM on different mechanical properties, such as fatigue, wear, and corrosion resistance. Furthermore, the effect of USNM on microstructure development and grain refinement is discussed. Finally, this study explores the applications of the UNSM process.Entities:
Keywords: gradient nanostructured layers; mechanical properties; microstructure; severe plastic deformation; ultrasonic nanocrystal surface modification
Year: 2022 PMID: 35564124 PMCID: PMC9103050 DOI: 10.3390/nano12091415
Source DB: PubMed Journal: Nanomaterials (Basel) ISSN: 2079-4991 Impact factor: 5.719
Figure 1Schematic of UNSM process.
Figure 2Load cycles in UNSM.
Figure 3Schematic of generation of a UNSM-modified surface on the material’s surface. Reprinted with permission from ref. [45]. Copyright 2020, Elsevier.
Figure 4Schematic presentation of the grain refinement on the surface of a material subjected to UNSM. The numbers are only typical ones corresponding to a set of parameters in the selected material.
Figure 5TEM micrograph presenting (a) nanostructures on the surface of UNSM-treated Ti6Al4V, (b) magnified view of location b. Reprinted with permission from ref. [92]. Copyright 2019, Elsevier.
Figure 6TEM micrograph presenting nanostructured grains developed during UNSM on Inconel 690. Reprinted with permission from ref. [93]. Copyright 2018, Elsevier.
Figure 7UNSM-treated S500 MC steel substrate: (a,b) EBSD of the cross-sections at two different magnifications, (c) grain-size distribution at the top layer. Reprinted with permission from ref. [97]. Copyright 2021, Elsevier.
Figure 8The microstructure of 300 M steel after UNSM treatment: (a) the SPD layer, (b) the tempered martensite in the SPD layer. Reprinted with permission from ref. [77]. Copyright 2019, Elsevier.
Figure 9TEM of UNSM-treated AISI 304 steel: (a) at the top surface, (b) SAED pattern. Reprinted with permission from ref. [44]. Copyright 2013, Elsevier.
Figure 10Fatigue crack growth before UNSM treatment and after UNSM treatment. Reprinted with permission from ref. [43]. Copyright 2010, Elsevier.
Figure 11SN curves of AR, HT, and UNSM’ed substrate. Reprinted with permission from ref. [69]. Copyright 2018, Elsevier.
Figure 12Residual stress relaxation of USNM’ed specimen treated with three fatigue stresses. Reprinted with permission from ref. [69]. Copyright 2018, Elsevier.
Figure 13COF variation in untreated and UNSM’ed specimens. Reprinted with permission from ref. [56]. Copyright 2012, Elsevier.
Mechanical properties and microstructural features of USNM-treated substrate materials.
| Materials | Static Force | Roller Material, Hardness, and Diameter | Frequency and Amplitude | Observation |
|---|---|---|---|---|
| 304 ASS [ | 20 N | WC; Not Specified | 20 kHz; 10 µm |
SPD layer of 50 µm thickness. High hardness of 7 GPa. Increase in yield strength by 85.29%. Fatigue life improved by 7.67 times Maximum RCS of 1400 MPa |
| SUS 304 [ | 70 N, 90 N, 110 N and 130 N | WC; Not Specified, | ~20 kHz; 30 µm |
Surface roughness decreased from 1.05 µm to 0.32 µm. Maximum RCS of 43.1 MPa. Maximum fatigue strength of 510 MPa at 90 N, 82.14% increase. |
| AISI 304 [ | Not Specified | WC; Not Specified | 20000 or more per second; Not Specified |
Surface roughness improved from 1.7 µm to 1.3 µm. Maximum RCS of 1100 MPa. Surface hardness increased from 220 Hv to 390 Hv |
| 300 M [ | 50 N | WC; Not Specified | 20 kHz; 24 µm |
Surface roughness decreased by 40% compared to the nitrided specimen. Surface hardness increased by 40.64% compared to base material Surface hardness increased by 13.40% on the nitrided specimen. |
| A100 [ | 50 N | Cemented WC; Not Specified | 20 kHz; 24 µm |
Surface hardness increased from 574 Hv to 707 Hv (23.17% increase) Maximum RCS of 1706 MPa is induced, which is a 4.4 times increment. 14 times increase in plain fatigue life and 2 times increase in fretting fatigue life. |
| AISI 4340 [ | 40 N | WC; Not Specified; 2.38 mm | 20 kHz; 30 µm |
Ra and Rz decreased by 72.7% and 52.9%. Surface hardness increased by 38.59%. Maximum RCS of 717 MPa. Increase in fatigue strength by 45.45%. Increase in fatigue life of 214 times. |
| AA7075-T651 [ | 1 kg | WC; Not Specified | 20 kHz; 8 µm |
Fatigue life increased by 11 times when UNSM was applied on normal material. The fatigue life was 4 times higher in specimens subjected to corrosion for 2 h followed by UNSM than in specimens subjected to corrosion alone for 2 h Surface roughness increased from 2.3 µm to 2.4 µm for specimen subjected to corrosion for 2 h The maximum RCS was 600 MPa |
| AA7075-T6 [ | 30 N | WC; Not Specified; 2.38 mm | 20 kHz; 30 µm |
Surface roughness decreased by 15.75% Maximum RCS of 780 MPa. Microhardness increased by 26%. The wear rate improved by 2.75 times. COF was reduced by 6.4%. |
| CP Ti [ | 30 N | WC; Not Specified; 2.38 mm | 20 kHz; 30 µm |
Grain refined to 200 nm. Surface hardness increased by 32.19%. Maximum RCS of 1279.4 MPa |
| Ti64 [ | 60 N | WC; Not Specified; 2.38 mm | 20 kHz; 30 µm |
Grain refined to 1.2 µm and 0.8 µm for α and β. Surface hardness increased by 15.55%. Maximum RCS of 1142.7 MPa. |
| Ti-Nb-Ta-Zr [ | 25–40 N | WC; Not Specified | 20 kHz; 24 µm; 40 µm |
Decrease in surface roughness by 44.32% Surface hardness increased by 13.40%. Maximum RCS of 1094 MPa. Fatigue life increased by 100% in slow rotation and 160% in fast rotation during UNSM. |
| Inconel 718 [ | 40 N | WC; Not Specified; 2.38 mm | 20 kHz; 40 µm |
GNS layer formed up to a depth of 60 nm–200 nm. Increase in hardness of 102.63%. |
| ATI 718 plus [ | 10 N/50 N | WC; Not Specified; 2.5 mm | 25 kHz; 40 µm |
Grain refined up to 21.95 nm. Increase in surface hardness by 44%. Maximum RCS was higher than 1000 MPa. Fatigue life improved by 5.25 times |
| Inconel 690 [ | 20–40 N | WC; Not Specified; 2.5 mm | 25 kHz; 8–16 µm |
Surface hardness increased by 44.1%. Maximum RCS of 1376 MPa. Yield strength increased by 13%. Endurance strength increased by 13.5%. |
| CP Cu [ | 50 N | WC; Not Specified; 2.38 mm | 20 kHz; 50 µm |
Grain refinement up to 200 nm. Surface hardness increased by 142.65%. Maximum RCS of 1.5 GPa. Yield strength enhanced by 44.15%. Tensile strength increased by 6.75%. |
| AZ31B Mg Alloy [ | 5 N | WC; Not Specified; 4 mm | 20 kHz; 8 µm |
Surface roughness reduced by 21.19% Surface hardness increased by 63.98%. Yield strength increased by 43.48%. |
| AZ91D Mg Alloy [ | 10 N; 20 N; 30 N | WC; Si3N4; 2.38 mm | 20 kHz; 30 µm |
Grain refinement up to 39 nm. Surface hardness increased by 28.26%. The wear rate was reduced by 30%. COF was reduced by 23%. |
| Co-Cr-Mo Alloy [ | 50 N | WC; Not Specified; 2.38 mm | 20 kHz; 30 µm |
Surface roughness was reduced by 83.02% and 87.69% at room temperature (RT) and high temperature (HT) Surface hardness increased by 35.1% and 44.3% at RT and HT. Yield strength increased by 3.4% and 11.78% at RT and HT. Tensile strength increased by 5.5% and 10.8% at RT and HT. COF reduced at 23.36% and 48.07%. Specific wear rate (SWR) reduced by 43.1% at RT and 77.3% at HT. |
| CoCrFeMnNi High Entropy Alloy [ | 10 N; 20 N; 60 N | WC; Not Specified; 2.4 mm | 20 kHz; 30 µm |
Increase in surface hardness by 98.28%. Yield strength increased by 142.49%. |
| Nickel-Titanium Shape Memory Alloy [ | 3 kg | WC; Not Specified; 2.4 mm | 20 kHz; 20 µm |
Surface roughness decreased from 12.1 µm to 9.0 µm. Surface hardness increased from 304 Hv to 408 Hv (34.2% increase). Corrosion current decreased from 157 nA to 53.1 nA. |
| Nickel-Titanium Shape Memory Alloy [ | 20 N | WC; Not Specified | 20 kHz; 12 µm |
Corrosion resistance improved Surface hardness increased by 21.81%. Cell adhesion increased |
Figure 14The wear track profiles of the (a) bulk and (b) UNSM 300 M martensitic ultra-high-strength steel, (c) wear depths, and (d) wear rates. Reprinted with permission from ref. [73]. Copyright 2020, Elsevier.
Figure 15The surface morphology of the (a) base and (b) USNM’ed HVOF SAE 52100 bearing steel. Reprinted with permission from ref. [111]. Copyright 2021, Elsevier.
Figure 16The cyclic potentiodynamic polarization curves obtained from USNM Ni 690 alloy subjected to 10 N, 30 N, and 50 N static loads. Reprinted with permission from ref. [112]. Copyright 2019, MDPI.
Figure 17The pitting corrosion characteristics of (a) SLM 316L SS, (b) SLM 316L SS + UNSM, and (c) SLM 316L SS + UNSM + HT. Reprinted with permission from ref. [116]. Copyright 2020, Elsevier.
Figure 18Schematic of EP-UNSM.
Figure 19SEM of (a) 300 M steel, (b) UNSM’ed substrate, (c) CC-UNSM’ed substrate, and (d) EP-UNSME’ed substrate. Reprinted with permission from ref. [121]. Copyright 2020, Elsevier.