| Literature DB >> 34151071 |
Yanchun Li1, Shuaiwei Wang1, Baocheng Yang1.
Abstract
Auxetic structure and tunable phase transitions are fascinating properties for future application. Herein, we propose two three-dimensional (3D) carbon honeycombs (CHC), known as Cmcm -CHC and Cmmm-CHC. Based on first-principles calculations, these novel 3D materials exhibit auxeticity with a fascinating negative Poisson's ratio, which stems from (i) the puckered structure of Cmcm -CHC along the tube axis and (ii) significant change of angle-dominant deformation for Cmmm-CHC in the armchair direction. In addition, the moderate strain drives semimetal to semiconductor phase transition in CHCs, which thoroughly establishes its C-C bond formation. In the meantime, two new phases, namely P63/mmc-CHC and P6/mmm-CHC, form and exhibit semiconductor characteristics. Our results also show that Cmcm -CHC and P63/mmc-CHC are superhard materials. The outstanding negative Poisson's ratio and phase transition properties make CHCs highly versatile for innovative applications in microelectromechanical and nanoelectronic devices.Entities:
Year: 2021 PMID: 34151071 PMCID: PMC8209820 DOI: 10.1021/acsomega.1c00718
Source DB: PubMed Journal: ACS Omega ISSN: 2470-1343
Figure 1Optimized atomic structures of (a) -CHC and (b) Cmmm-CHC from top, side, and perspective views along x (zigzag), y (armchair), and z (tube) directions. The blue/red box represents the basic unit cell/calculation model of the CHC structure. The pink and blue carbon atoms are sp3-hybridized and sp2-hybridized, respectively.
Figure 2Poisson’s ratio as a function of the uniaxial deformation of -CHC and Cmmm-CHC structures. (a) Strain ε versus ε and ε for the -CHC structure subjected to uniaxial tensile loading in the zigzag direction. (b) Poisson’s ratio of the -CHC structure along the tube axis. (c) Strain ε versus ε and ε for Cmmm-CHC structure subject to uniaxial tensile loading along the tube axis. (d) Poisson’s ratio of the Cmmm-CHC structure in the armchair direction.
Comparison of the Poisson’s Ratio of CHCs with Those of Some Previously Reported Materials
| structures | υ | υ | υ | ||
|---|---|---|---|---|---|
| 3D carbon-based materials | 0.038∼−0.042 | strain-induced | |||
| 0.14∼−0.63 | |||||
| bco-C20[ | ∼−0.13 | ||||
| carbon honeycomb[ | –0.32 | ||||
| 2D carbon-based materials | Penta-graphene[ | –0.068 | –0.068 | intrinsic | |
| Xgraphene[ | 0.18∼−0.053 | strain-induced | |||
| tetrahex C[ | 0.04∼−0.081 | 0.036∼−0.127 | |||
| graphene[ | 0.3∼−0.04 | ||||
| other materials | B4N[ | –0.018 | –0.032 | intrinsic | |
| Ag2S[ | –0.12 | –0.54 | |||
| gallium thiophosphate[ | –0.033 | –0.62 | |||
Figure 3Deformation mechanism for NPR. The blue arrows indicate the movement direction of the atoms by stretching along the zigzag direction of (a) -CHC and tube axis of (d) Cmmm-CHC structure. The atomic positions along the y and z axis for (b, c) -CHC and x and y axis for (e, f) Cmmm-CHC are shown. The red arrows display the movement direction after tensile loading. (g, h) Distances d1 and d2 as a function of strain.
Figure 4Strain–stress curve of (a) -CHC and (b) Cmmm-CHC.
Figure 5Structure evolution under uniaxial tensile loading for (a) -CHC and (b) Cmmm-CHC structures at different strains. The bond length and bond angle as a function of strain for (c) -CHC and (d) Cmmm-CHC structures. The upper inset picture in (c) and (d) shows the unit cell of a new structure under tensile loading.
Figure 6Band structures of (a) P63/mmc-CHC and (b) P6/mmm -CHC structures at different strains.
Bulk Modulus (B), Shear Modulus (G), Young’s Modulus (E), and Vickers Hardness (Hv) of -CHC, Cmmm-CHC, Graphene, Diamond, and Other Carbon Materialsa
| graphene | diamond | other carbon materials | |||||
|---|---|---|---|---|---|---|---|
| 313 | 190 | 324 | 195 | 432 | |||
| 289 | 164 | 302 | 126 | 519 | |||
| 663 | 383 | 691 | 312 | 1024 | 1220 | ||
| 47 | 30 | 49 | 17 | 93 | 84–96 |
The units of B, E, G, and Hv are GPa.
Density functional theory (DFT) calculations in ref (44).
DFT calculations in ref (5).
Ref (45).
Ref (43).