| Literature DB >> 34105292 |
Wenzheng Zhai1, Lichun Bai2, Runhua Zhou3, Xueling Fan4, Guozheng Kang5, Yong Liu3, Kun Zhou6,7.
Abstract
There has been tremendous interest in the development of different innovative wear-resistant materials, which can help to reduce energy losses resulted from friction and wear by ≈40% over the next 10-15 years. This paper provides a comprehensive review of the recent progress on designs, properties, and applications of wear-resistant materials, starting with an introduction of various advanced technologies for the fabrication of wear-resistant materials and anti-wear structures with their wear mechanisms. Typical strategies of surface engineering and matrix strengthening for the development of wear-resistant materials are then analyzed, focusing on the development of coatings, surface texturing, surface hardening, architecture, and the exploration of matrix compositions, microstructures, and reinforcements. Afterward, the relationship between the wear resistance of a material and its intrinsic properties including hardness, stiffness, strength, and cyclic plasticity is discussed with underlying mechanisms, such as the lattice distortion effect, bonding strength effect, grain size effect, precipitation effect, grain boundary effect, dislocation or twinning effect. A wide range of fundamental applications, specifically in aerospace components, automobile parts, wind turbines, micro-/nano-electromechanical systems, atomic force microscopes, and biomedical devices are highlighted. This review is concluded with prospects on challenges and future directions in this critical field.Entities:
Keywords: anti-wear applications; mechanical properties; tribology; wear-resistant materials
Year: 2021 PMID: 34105292 PMCID: PMC8188226 DOI: 10.1002/advs.202003739
Source DB: PubMed Journal: Adv Sci (Weinh) ISSN: 2198-3844 Impact factor: 16.806
Figure 1Nearly ubiquitous impact of wear in various advanced technologies from nanoscale to macroscale applications.(NEMS) Reproduced with permission.[ ] Copyright 2016, American Chemical Society; (Biomimetic) Reproduced withpermission.[ ] Copyright 2001, Elsevier; (Biomimetic) Reproduced with permission.[ ] Copyright 2016, Elsevier; (Wind energy, Biomedical, MEMS, and Aerospace) Reproduced with permission.[ ] Copyright 2015, Elsevier; (Water transport) Reproduced with permission.[ ] Copyright 2017, Elsevier; (AFM) Reproduced with permission.[ ] Copyright 2016, Elsevier; (Cosmetic) Reproduced with permission.[ ] Copyright 2007, Elsevier.
Microstructural parameters of dimples and test conditions and the corresponding observations for various surface textures
| Material | Microstructural parameter of dimples | Test parameter | Typical observation | Ref. |
|---|---|---|---|---|
| Hardened steel | Diameters of 40–120 µm, depth of 5 µm, area density of 7.5–30% | Sliding speeds of 0.012–1.2 m s−1, contact stress of 780 MPa | Textures remained effective at severe sliding conditions |
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| Diameters of 35 and 50 µm, depths of 20–30 and 10–13 µm | Sliding speeds of 0.004–0.16 m s−1 | Deeper and denser textures led to obvious decreases in friction and wear |
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| Bearing steel | Diameters of 58 and 78 µm, depths of 5 and 5.5 µm, area density of 15% and 12% | Sliding speeds of 0.03–0.76 m s−1, contact stresses of 0.16–700 MPa | Regime transited from boundary to hydrodynamic lubrication at higher speeds |
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| Diameter of 60 µm and depths of 1–2 µm, grooves with pitch of 150 µm and width of 50 µm | Rolling speed of 30 m s−1, contact stresses of 700–2000 MPa | Friction reduced in the transverse direction |
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| Diameter of 221 µm, depth of 9.5 µm, area density of 6.7% and 26.8% | Sliding speeds of 0.01–0.12 m s−1, contact stress of 870 MPa | Dimples led to increases in friction at high speeds |
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| Diameter of 64 µm, depth of 16.5 µm, area density of 3.6% | Sliding speed of 0.015 m s−1, contact stress of 870 MPa | Textures led to a 10% increase in friction |
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| Diameter of 80 µm, depth of 5.5 µm, area density of 12% | Sliding speeds of 0.08–0.16 m s−1, contact stresses of 500–700 MPa | Friction reduced at high‐load and low‐sliding conditions |
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| Diameter of 200 µm, depth of 5.5 µm, area density of 7–20% | Sliding speeds of 0.09–0.55 m s−1, contact stresses of 260–640 MPa | Friction decreased with increasing sliding speeds and contact stresses |
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| Diameters of 20–60 µm and depths of 0.6–1.8 µm, area density of 7% | Sliding speeds of 0.09–0.55 m s−1, contact stresses of 390–960 MPa | Dimples with the diameter of 20 µm gave rise to decreases in friction |
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| Stainless steel | Diameter of 100 µm, depth of 50 µm, area density of 40% | Sliding speed of 0.4 m s−1, contact stress of 1000 MPa | Friction was reduced by 50% |
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Figure 2a) Wear rates of the initial and plasma diffusion modified surfaces. Plasma diffusion modified surfaces with b) craters shown by scanning electron microscopy (SEM), c) ultra‐fine grains, d) dislocations, and e,f) deformed twins shown by transmission electron microscopy (TEM) images, where the inset in (e) shows the average grain size. g) Element mapping results of plasma diffusion modified surfaces. Reproduced with permission.[ ] Copyright 2020, Elsevier.
Figure 3Biological hierarchical surfaces and their functionality. Reproduced with permission.[ ] Copyright 2018, Elsevier.
Figure 4SEM images of a) initial AZ91 and b) AZ91 with 3 wt% rare earth (RE) elements. c) Wear rates of AZ91 and alloys with 1, 2, and 3 wt% RE elements after sliding 1000 m. Reproduced with permission.[ ] Copyright 2013, Elsevier.
Figure 5a) Friction coefficients and wear rates at a normal load of 2 N, b) Raman spectra of B1− C films, where the intensity between 1000 and 1600 cm−1 wavenumber was enhanced by the increase in the amorphous carbon content. Reproduced with permission.[ ] Copyright 2015, Elsevier.
Figure 6a) Wear rates of WC‐Co with various grain sizes. SEM images showing the surface morphology of WC‐Co with different grain sizes of b,c) 2.2 µm, d) 1.6 µm, e) 0.8 µm, and f) 0.4 µm after micro‐abrasion tests at a contact load of 0.2 N. Reproduced with permission.[ ] Copyright 2019, Elsevier.
Figure 7a) Hardness of specimens with different grain sizes before and after wear with the inset showing the hardness difference and dotted line representing the values obtained from the Hall–Petch relation. Wear volumes plotted against b) grain sizes and c) the corresponding hardness, where the dotted line represents values calculated on the basis of Archard theories. Reproduced with permission.[ ] Copyright 2010, Elsevier.
Hardness, mass loss, and wear resistance of different materials,[ ] where the relation between wear resistance R and H′/E follows R = 2.539(1000H′/E) − 1.02.
| Material | Original hardness [HB] | Wear‐related hardness [HB] | Mass loss [mg] | Wear resistance [×103 kg mm−1] |
|---|---|---|---|---|
| Al6061 | 53.9 | 59.9 | 5.8 | 0.42 |
| Q235 | 127 | 204.5 | 3.4 | 2.06 |
| 1Cr13 | 162.5 | 260.5 | 2.3 | 3.08 |
| 0Cr19Ni9 | 171.3 | 305.7 | 2.6 | 2.75 |
| ZGMn13 | 238.3 | 404.3 | 1.6 | 4.46 |
| TC11 | 241.5 | 267.5 | 0.9 | 4.48 |
| 30CrMo | 246.5 | 281.5 | 3.3 | 2.15 |
| TC4 | 317 | 329 | 0.7 | 5.71 |
| AlCrFeCoNiCu | 335.5 | 441.5 | 2.1 | 3.42 |
Summary of the yield strength, strain hardening coefficient, and roughness of the thermal‐treated steel
| Steel | Yield strength [MPa] | Strain hardening coefficient | Roughness [µm] | Ref. |
|---|---|---|---|---|
| AISI 5160 | 633.96 ± 5.05 | 0.15 ± 0.01 | 0.3115 ± 0.007 |
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| AISI O1 | 386.53 ± 39.02 | 0.22 ± 0.01 | 0.2947 ± 0.005 | |
| AISI 1045 | 488.80 ± 16.09 | 0.28 ± 0.01 | 0.2781 ± 0.009 | |
| AISI 1045 | 530 ± 12 | 0.04 ± 0.01 | — |
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| Welded AISI 1045 | 415 ± 20 | 0.22 ± 0.02 | — | |
| Welded AISI 1045 | 242 ± 11 | 0.39 ± 0.03 | — | |
| Welded AISI 1045 | 324 ± 13 | 0.31 ± 0.02 | — |
Figure 8Relationship between the wear rate and H/E ratio of metals, cermets, ceramics, and amorphous materials (color‐coded).[ ]
Typical stress‐related wear damages of ceramics
| Contact stress | Wear damage |
|---|---|
| Low (below the elasticity limit) | Elastic deformation, no obvious wear |
| Medium (below the plasticity limit) | Plastic deformation‐induced wear |
| High (close to the critical failure stress) | Cracks‐induced wear |
| Very high (above the critical stress) | Fracture |
Figure 9Snapshots of wear of a) single‐crystalline and b) nanocrystalline SiC sliding against a tip (blue color), where the pulling‐out of a nanocrystalline SiC grain was observed. c) Plot of the shear stress on the grain boundary against the sliding distance, where the lower panels indicate the plastic deformation in nanocrystalline SiC caused by grain boundary sliding. d) Formation of voids at grain boundaries caused by grain boundary sliding. Reproduced with permission.[ ] Copyright 2014, Wiley‐VCH.
Figure 10Relation between the coefficients of friction and coating thickness, where CoT denotes the ratio of the average thickness during wear to the initial thickness. Reproduced with permission.[ ] Copyright 2008, Elsevier.
Figure 11a) Diagrammatic sketch of the AM 316L stainless steel at various length scales. b) Electron‐backscatter diffraction (EBSD) inverse‐pole figure (IPF) and c) SEM images of AM specimens, showing grain orientations and unique cellular structures. d) TEM image of the unique cells. e) High‐angle annular dark‐field scanning TEM image of the cells. f) EBSD IPF image obtained at a 1 µm step size. g) EBSD image quality map showing low‐angle grain boundaries. h) Kernel average misorientation image showing the misorientation. i) TEM images of the cells with the energy dispersive spectrum mapping. Reproduced with permission.[ ] Copyright 2018, Springer Nature.
Figure 12Overview of the AM process presented by the central diagrammatic sketch. a) Conventional Al powder. b) Nanoparticle‐modified Al powder. c) Typical columnar growth of dendrites during AM. d) Nanoparticle‐induced uniform nucleation. e) Typical large grains and cracks by traditional AM methods. f) Fine‐equiaxed grains in the nanoparticle‐modified powder. g) Typical AM Al piston. h) AM‐manufactured Al HRL logo. Reproduced with permission.[ ] Copyright 2017, Springer Nature.
Figure 13Structures with the indicated hardness of a) Ni superalloy + hard alloy composite and b) Ni3Al‐based alloy coatings, where ZhS26 was the substrate; HAZ denotes the heat‐affected zone; Hh20N80, SM64, and VKNA‐2M are Ni superalloy, hard alloy, and Ni3Al‐based alloy, respectively. Reproduced with permission.[ ] Copyright 2019, Springer Nature.
Summary of materials, wear data, and testing conditions for different types of AFM probes
| Material (probe‐specimen) | Testing condition | Wear behavior | Ref. |
|---|---|---|---|
| SiN | 10 nN, 10 m s−1, 25.6 mm | Fatigue wear |
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| 100 nN, 20 m s−1, 72 mm | Adhesive, abrasive, and fatigue wear with a wear rate of 5 × 10–2 mm3 (Nm)−1 |
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| Si‐SiO2 | 1–6 µN, 20 µm s−1, KOH solution | Tribochemical wear with wear rates of 10–4–10–2 mm3 (Nm)−1, depending on the pH of the KOH solution |
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| SiN | 1–6 N, 16 m s−1, 67.5 mm sliding distance, water, NH4OH, and HCl solutions | Tribochemical wear independent of pH |
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| Si/SiN | 10–300 nN, 5 m s−1, 2.56–25.6 mm, 20–60% RH | Wear rates of 10–4–10–2 and 10–6–10–5 mm3 (Nm)−1 for Si and SiN |
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| Si‐Si/DLC | 10–100 nN, 1 m s−1, 0.032–70 mm, air and N2 | Wear rates of 10–5–10–3 mm3 (Nm)−1 depending on the environmental conditions |
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| Si‐piezoelectric ceramic materials | 10–50 N, 2 m s−1, 1.6–18 mm | Wear rates of 10–5–10–3 mm3 (Nm)−1 depending on the probe shapes |
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| Si‐polymers | 5–100 nN, 1.5 mm s−1, 750 m, vacuum | Exponential wear rate dependent on the contact stresses |
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| Si/SiN | 0 N, 3.97 m s−1, 102.4 mm, ambient conditions | Failure of Si probes and SiN |
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| SiC/Si‐polymers/ SiO2 | 2.5–10 nN, 1.5 mm s−1, 40–100 m, vacuum and ambient conditions | Higher wear resistance of SiC probes |
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| Si‐diamonds | 0 N, 4, 21 nm s−1, 0.2–4.5 m, vacuum conditions | Wear volume of 25 nm3 |
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| Carbon‐coated probes‐Si/SiO2 | — | Higher wear resistance of carbon coated probes |
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| Diamonds‐Si | 60 N, 2 m s−1, 7.68 mm | Wear rate of 1.9 × 10–9 mm3 (Nm)−1 |
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| CNT‐polycrystalline Si | 2 m | Higher wear resistance of CNT probes (20 times more than that of Si probes) |
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| Polycrystalline diamond coated probes‐Cu/Si/SiN | 1–5 N, 1 m s−1, 0.3–1.5 mm | Wear rate of 10–7–10–6 mm3 (Nm)−1 |
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| Ultrananocrystalline diamonds‐ultrananocrystalline diamonds | 0–100 nN, 3.75–20.3 m s−1, 1.024–204.8 mm, 15% and 70% RH | Ultrahigh wear resistance of ultrananocrystalline diamond probes |
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| Si‐doped DLC‐SiO2 | 1–17.5 nN, 10–250 m s−1, 2 m, ambient conditions | Wear rates of 10–7–10–5 mm3 (Nm)−1 |
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| Ti/Pt/Au coated probes‐SiO2 and highly oriented pyrolytic graphite | Electric contact at ambient conditions | Rapid wear |
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| Au/Pt/Ir coated probes‐Cu and highly oriented pyrolytic graphite | Electric contact at ultra‐high vacuum conditions | Weakness of metal‐coated probes to the lateral force and melting of the coating layer |
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| Pt‐coated probes‐DLC | 50–100 nN, 0.1–100 mm s−1, 2 m | Adhesive, abrasive, and tribochemical wear at a logarithmic wear rate, depending on the sliding speeds |
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| Pt/AuNi/PtIr/PtNi coated probes‐piezoelectric ceramic materials | 1–80 nN, 10–100 mm s−1, 100–300 m | Wear rate of 10–7 mm3 (Nm)−1 |
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Figure 14a) Anatomies of the hip joint. b) Examples of artificial joints illustrating total hip replacement components with corresponding materials. Left: ceramic‐on‐polyethylene structure; right: examples of metal‐on‐metal, ceramic‐on‐polyethylene, and metal‐on‐polyethylene systems. Reproduced with permission.[ ] Copyright 1995, Elsevier. Reproduced with permission.[ ] Copyright 2010, Elsevier.
Figure 15Experimental and numerical simulation results of the wear volume, where dotted lines 1 and 2 represent the expected wear volume obtained based on the numerical model and the Archard relation, respectively; solid line 3 denotes the fitted curve for the experimental wear volume. Reproduced with permission.[ ] Copyright 2015, Elsevier.