| Literature DB >> 35564097 |
Yanfei Liu1, Shengtao Yu1, Qiuyu Shi2, Xiangyu Ge1, Wenzhong Wang1.
Abstract
Friction and wear usually lead to huge energy loss and failure of machine pairs, which usually causes great economic losses. Researchers have made great efforts to reduce energy dissipation and enhance durability through advanced lubrication technologies. Single-layer coatings have been applied in many sectors of engineering, but the performance of single-layer coatings still has many limitations. One solution to overcome these limitations is to use a multilayer coating that combines different components with varied physical and chemical properties. In addition, multilayer coating with alternating layers only containing two components can lead to improved performance compared to a coating with only two different layers. This paper systematically reviews the design concept and properties of different types of multilayer coatings, including transition-metal nitride coatings, diamond-like carbon-based coatings, and other multilayer coatings. The inherent functional mechanisms of the multilayer structures are also detailed and discussed.Entities:
Keywords: diamond-like carbon; friction; multilayer coating; transition-metal nitride; tribology; wear
Year: 2022 PMID: 35564097 PMCID: PMC9102559 DOI: 10.3390/nano12091388
Source DB: PubMed Journal: Nanomaterials (Basel) ISSN: 2079-4991 Impact factor: 5.719
Figure 1The fracture pattern on the Ti-TiN-(Ti,Al,Cr)N multilayer coatings with nanolayer thickness of (a) 302 nm and (b) 10 nm after the cutting tests with different cutting speeds (vc). (a) With nanolayer thickness of 302 nm, the formation of longitudinal cracks and internanolayer delaminations is typical. (b) With nanolayer thickness of 10 nm, rarer internanolayer delaminations can be observed. Reprinted with permission from [59].
Figure 2(a) SEM and (b,c) TEM image of multilayer CrN/TiN coating with bilayer period of 6.4 nm; (d) COF of different multilayer coatings under ambient condition; (e) COF of CrN/TiN/TiN coating under different environment conditions. Reprinted with permission from [78].
Figure 3Multilayer designing of CrN/MoN coatings. (a) XRD results and (b) cross-section images of CrN/MoN coatings with different layer thicknesses; (c) EBSD results of a CrN/MoN coating; (d) mechanical behavior of CrN/MoN coatings with different layer thicknesses. Reprinted with permission from [83].
Figure 4(a) Relationships between underlayers and the properties in a DLC-based multilayer coating; (b) the cross-sectional morphology of multilayer coating; (c) structure of multilayer coatings with different underlayers; (d) hardness of different multilayer coatings; (e) COF of different multilayer coatings. Reprinted with permission from [93].
Figure 5(a) Schematic diagram of the MoS2/Ti–MoS2/Si multilayer coating; (b,c) cross-sectional morphology of a MoS2/Ti–MoS2/Si multilayer coating; (d,e) COFs of different MoS2/Ti–MoS2/Si multilayer coatings under normal loads of 2 N and 8 N. Reprinted with permission from [103].
Figure 6(a) Schematic diagram of the designing of coating samples; (b) cross-sectional images of the coatings; (c) TRIM simulations of the selected coating samples, showing the extent of atomic mixing. In this figure, AlTiC represents Al2O3 + TiC composite material; CP represents sputter-deposited carbon overcoat; CF represents FCVA-deposited carbon overcoat; T represents high-energy carbon treatment. Reprinted with permission from [106].
Figure 7(a) Schematic diagram of the conventional multilayer coating and Cr20 coating; (b) relation between the wear rate and the proposed Ƙ parameter; (c) characteristics of the parameters affecting the tribological performance of the textured coating samples. Reprinted with permission from [107].
Figure 8Multilayer design of PEI/GO coatings. (a) Photograph of the steel substrate and that deposited with multilayer PEI/GO coatings; (b) cross-sectional morphology of a PEI/GO coating with 15 bilayer periods; (c) COFs of the multilayer coatings under different test environments; (d) HRTEM image of the wear debris containing GO in N2 environment. Reprinted with permission from [124].
Figure 9Schematic diagram of the mechanisms of the multilayer designing of coating. (a) Crack deflection and stress relaxation in multilayer coating. Reprinted with permission from [39]. (b) Theoretical constitution of supporting interlayers of DLC coating. Reprinted with permission from [45].
Friction and wear-reduction mechanisms of multilayer coatings.
| Types of Multilayer Coatings | Preparing Methods | Lubrication Properties | Friction-Reduction Mechanisms | Wear-Reduction Mechanisms |
|---|---|---|---|---|
| TiN/Ti [ | Large area filtered cathodic arc deposition | COF reduced from 0.82 (TiN) to 0.6 (with Ti layers thickness of 25 nm) | Lower shear strength of soft Ti layers | — |
| Ti/TiN [ | High-vacuum magnetron sputtering | COF reduced from 0.54 (TiN) to 0.48 | Formation of TiAlNxOy and TiNxOy tribolayers | — |
| TiN/CrN [ | Reactive magnetron cathodic sputtering | COF reduced from 0.9 (TiN) and 0.6–0.7 (CrN) to 0.3–0.5 | Enhanced hardness and formation of the dense Cr2O3, and CrO3 oxide layer | |
| CrNHIPIMS/TiNDCMS [ | High-power impulse magnetron sputtering (HIPIMS) and DC unbalanced magnetron sputtering (DCMS) | COF reduced to 0.05 | Formation of humidity-triggered layers during dry-sliding tests under humid conditions | — |
| (Ti–Cr)N [ | Cathodic arc deposition | COF reduced from 0.7 (TiN) and 0.75 (CrN) to 0.4 | Formation of mixed-phase films with plastic deformed wear debris | |
| CrTiN/TiCN and CrTiN/CrCN [ | Cathodic arc PVD | COF reduced from 0.8–1.0 (bare substrates) to 0.2 | Graphitization of the amorphous carbon phase | Improved adhesion between individual layers; increased coating hardness; graphitization |
| CrN/DLC/Cr-DLC [ | PECVD | COF reduced to 0.087 | Lubrication of DLC; supporting of CrN layers; enhancement of crack-propagation inhibition; increased elastic recovery capability | |
| Multilayer DLC with hard and soft layers [ | Unbalanced closed-field magnetron sputtering | Lower COF during running-in process with soft top layer | Formation of transfer layer with soft top layer to provide low friction and wear | |
| MoS2/Ti–MoS2/Si [ | Unbalanced magnetron sputtering | COF reduced to 0.0432 | Improved compactness and orientation of MoS2; improved oxidation and moisture resistance of MoS2; higher hardness; hindered dislocations motion and crack propagation | |
| C/SiNx overcoats [ | Magnetron sputtering in situ with carbon deposition; high-energy carbon treatment | COF reduced from 0.4 (bare substrates) to lower than 0.2 | Extremely high adhesion governed by atomic intermixing, sufficient carbon thickness; high sp3 bonding | |
| Polyethylenimine/graphene oxide [ | Layer-by-layer deposition | COF reduced from 0.60 (substrate) to lower than 0.01 | Reduction in the contact area due to the formation of carbon nanoparticles in dry conditions | — |
* The influence of environment humidity on the lubrication behaviors was investigated.