Nanomechanical characterization of the fracture toughness of Al/SiC nanolaminates
Introduction
Nanolaminates made up of alternating metallic and ceramic nanoscale thick layers are promising materials in numerous engineering applications, due to their outstanding mechanical properties including high strength and wear resistance [1], [2], [3], [4], [5], [6], as well as unique electrical and optical properties [7], [8]. It has been argued that the fracture toughness of metal–ceramics nanolaminates can be higher than that of conventional metal–ceramic composites due to several reasons. Firstly, cracking of the brittle ceramic layers can be delayed due their nanoscale dimensions, which limit the size of the pre-existing flaws that initiate fracture. Secondly, the energy dissipated by the plastic deformation of metallic layers can arrest cracks at the metal–ceramic interfaces. And finally, the large number of interfaces associated with the nanoscale dimensions of the layers can introduce substantial energy dissipation through crack deflection mechanisms [9].
Nevertheless, there is very little reliable information on the fracture toughness of nanolaminates because most of them are fabricated in the form of thin-films or coatings, and appropriate techniques to measure the fracture toughness of coatings are still lacking [10], [11], [12]. Several strategies have been proposed to measure fracture toughness at the microscale, most of them based on bending of cantilevers of different geometries, such as Chevron notch cantilevers [13], [14], clamped beams [15] or double cantilever beams [16], [17], [18]. These strategies are very time consuming because they require the fabrication of the beams by focused ion beam milling and ion-induced damage at the root of the pre-notch may introduce additional artifacts [19]. Another approach is based on the micropillar splitting method, developed by Sebastiani et al. [20], [21], which does not require the introduction of pre-notches. Instead, the cracks are introduced directly by a sharp pyramidal indenter and propagate in mode I.
In this investigation, both micropillar splitting and bending of notched cantilevers were used to determine the fracture toughness of Al/SiC nanolaminates with different layer thicknesses (in the range 10 nm to 100 nm).
Section snippets
Materials and experimental techniques
The Al/SiC nanolaminates were fabricated by magnetron sputtering physical vapor deposition on a Si wafer in Los Alamos National Laboratory. The sputter unit is made up of dual sputter guns for the deposition of Al and SiC in a high vacuum chamber, using high purity Al and SiC targets (99.5%, Kurt J. Lesker, Clairton, PA). The designed multilayer structure of Al/SiC was built up by means of a computer controlled shutter system. The deposition rates were 7.5 nm/min for Al and 3.9 nm/min for
Micropillar splitting
The force–displacement curves of Al/SiC nanolaminates obtained in the micropillar splitting tests are shown in Fig. 2. Up to 5 tests were carried out for each layer thickness and the curves show good reproducibility. They are characterized by a monotonous increase of the load up to a critical load () that indicates the micropillar splitting. It is clear that the critical load increased considerably as the layer thickness decreased from 100 nm to 25 nm, and dropped again for a layer thickness
Conclusions
The fracture toughness of Al/SiC nanolaminates with different layer thicknesses (in the range 10 to 100 nm) was measured by means of two different micromechanical testing techniques, micropillar splitting and bending of a notched beam. The crack path was perpendicular to the layers in the former and parallel and perpendicular to the crack plane in the latter. Overall, the toughness of the nanolaminates in the parallel orientation was higher than that in the perpendicular orientation. In the
Declaration of Competing Interest
The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
Acknowledgments
This investigation was supported by the European Research Council (ERC) under the European Union’s Horizon 2020 research and innovation programme (Advanced Grant VIRMETAL, grant agreement No. 669141). Additional support is gratefully acknowledged from the U.S. National Science Foundation and the Spanish Ministry of Economy and Competitiveness under the Materials World Network Program through the project “High temperature mechanical behavior of metal/ceramic nanolaminate composites” (Dr.
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