| Literature DB >> 28772491 |
Baobing Zheng1, Meiguang Zhang2, Canjun Wang3.
Abstract
First-principles calculations were employed to study the mechanical properties for the recently proposed tetragonal B₄CO₄ (t-B₄CO₄). The calculated structural parameters and elastic constants of t-B₄CO₄ are in excellent agreement with the previous results, indicating the reliability of the present calculations. The directional dependences of the Young's modulus and shear modulus for t-B₄CO₄ are deduced in detail, and the corresponding results suggest that the t-B₄CO₄ possesses a high degree of anisotropy. Based on the strain-stress method, the ideal tensile and shear strengths along the principal crystal directions are calculated, and the obtained results indicate that the shear mode along (001)[100] slip system dominates the plastic deformation of t-B₄CO₄, which can be ascribed to the breaking of the ionic B-O bonds. The weakest ideal shear strength of 27.5 GPa demonstrates that the t-B₄CO₄ compound is not a superhard material, but is indeed a hard material. Based on the atomic explanation that the ternary B-C-O compounds cannot acquire high ideal strength, we propose two possible routes to design superhard B-C-O compounds.Entities:
Keywords: B-C-O compound; anisotropic properties; ideal strengths; superhard
Year: 2017 PMID: 28772491 PMCID: PMC5459106 DOI: 10.3390/ma10020128
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Figure 1Crystal structures of t-B4CO4 as viewed along the [001] direction (a) and the [010] direction (b), the red, blue, and black spheres represent O, B, and C atoms, respectively.
Calculated Elastic Constants C, Bulk Modulus B, Shear Modulus G, Young’s Modulus E, and ideal strength (minimum tensile strength and shear strength ) of t-B4CO4 together with other ternary B-C-O compounds (in units of GPa).
| Compounds | Source | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| This work | 481 | 452 | 269 | 260 | 150 | 129 | −52 | 248 | 218 | 505 | |||
| Theory 1 | 480 | 449 | 268 | 259 | 152 | 131 | 248 | 220 | 509 | ||||
| tI16-B2CO | Theory 2 | 600 | 646 | 304 | 283 | 182 | 144 | 310 | 265 | ||||
| tP4-B2CO | Theory 3 | 736 | 591 | 240 | 254 | 53 | 157 | 311 | 254 | ||||
| oP8-B2CO | Theory 4 | 732 | 675 | 238 | 260 | 112 | 69 | 298 | 270 | ||||
| B2C2O | Theory 5 | 763 | 590 | 229 | 174 | 15 | 135 | 299 | 264 | 611 | |||
| B2C3O | Theory 5 | 808 | 664 | 283 | 299 | 32 | 183 | 322 | 302 | 690 | |||
| B2C5O | Theory 5 | 889 | 740 | 346 | 335 | 30 | 135 | 345 | 351 | 787 | |||
| B2O | Theory 2 | 327 | 497 | 232 | 207 | 230 | 144 | 242 | 124 | ||||
| Theory 6 | 786 | 445 | 172 | 376 | 390 | ||||||||
| Diamond | Theory 7 | 1052 | 555 | 122 | 432 | 517 | 1109 |
1 Ref. [27]; 2 Ref. [24]; 3 Ref. [24,26]; 4 Ref. [25]; 5 Ref. [26]; 6 Ref. [35]; 7 Ref. [36,37].
Formulas of Young’s moduli for the tensile axis within specific planes.
| Tensile Plane |
| Orientation Angle |
|---|---|---|
| (001) |
| between [ |
| (100) |
| between [0 |
|
|
| between [hkl] and [001] |
Figure 2Orientation dependence of Young’s Modulus E (a,c) and the corresponding projection in the ab, ac, and bc planes (b) for the t-B4CO4, orientation dependence of the shear modulus of t-B4CO4 (d).
Formulas of shear moduli for the shear stress direction within specific planes.
| Shear Plane |
| Orientation Angle |
|---|---|---|
| (001) |
| between [ |
| (100) |
| between [ |
|
|
| between [ |
Figure 3Calculated stress-strain relations for t-B4CO4 in various tensile (a) and shear (b) directions.
Figure 4Structural and ELF transformation before (a) and after (b) the lattice instability for t-B4CO4.
Figure 5Calculated phonon dispersion curves for t-B4CO4 before (a) and after (b) shear deformation.