| Literature DB >> 32437359 |
Hongtu Zhang1,2, Dengke Wang1,2, Chong Yu1,2, Jianping Wei1,2, Shumin Liu3, Jianhua Fu1,2.
Abstract
To understand the effects of thermal shock on microcrack propagation and permeability in coal, thermal shock tests were conducted on coal specimens by using a constant temperature drying oven (105 °C) and a SLX program controlled cryogenic tank. The growth and propagation of microcracks were measured with computer tomography (CT) scanning and scanning electron microscope (SEM) tests. Results showed that thermal shocks improved the permeability of coal significantly. Notably, the permeability of coal after thermal shocks increased from 211.31% to 368.99% and was positively correlated with temperature difference. CT scanning images revealed that thermal shocks increased the crack number, crack volume and crack width as well as smoothened and widened the gas flow paths, thereby enhancing coal permeability. Moreover, SEM images showed that heating-cooling shocks created more new microcracks, forming more complex crack propagation paths and better connectivity among microcracks in coal compared to cooling shocks. We proposed a crack propagation criterion for coal to explain the mechanism of crack failure and propagation during thermal shocks. Our experiment results and theoretical analysis indicate that the heating-cooling shock is more effective in damaging and breaking coal than the cooling shock. Thus, it can be used as an alternative approach to enhance coal permeability in the production of coalbed methane (CBM).Entities:
Year: 2020 PMID: 32437359 PMCID: PMC7241728 DOI: 10.1371/journal.pone.0232182
Source DB: PubMed Journal: PLoS One ISSN: 1932-6203 Impact factor: 3.240
Specimen parameters and numbers.
| Group No. | Specimen | Volume (cm3) | Mass (g) | Apparent density (g/cm3) | Temperature range |
|---|---|---|---|---|---|
| A | A1 | 98.196 | 142.513 | 1.451 | From 90 °C to -90 °C |
| A2 | 97.055 | 141.434 | 1.457 | ||
| A3 | 95.663 | 141.650 | 1.481 | ||
| B | B1 | 97.000 | 144.341 | 1.488 | From 120 °C to -`120 °C |
| B2 | 96.417 | 142.275 | 1.476 | ||
| B3 | 95.662 | 139.863 | 1.462 | ||
| C | C1 | 95.836 | 140.741 | 1.468 | From 150 °C to -150 °C |
| C2 | 98.428 | 142.442 | 1.447 | ||
| C3 | 97.616 | 142.489 | 1.459 | ||
| D | D1 | 95.296 | 141.708 | 1.487 | From 180 °C to -180 °C |
| D2 | 97.616 | 144.490 | 1.480 | ||
| D3 | 98.002 | 142.346 | 1.452 |
Proximate analysis and density.
| Group No. | Coal rank | Proximate analysis | True density | |||
|---|---|---|---|---|---|---|
| (g/cm3) | ||||||
| A, B, C, D, E and G | anthracite | 0.92 | 16.7 | 6.43 | 1.59 | |
| F and H | bituminous coal | 1.10 | 16.62 | 19.00 | 1.45 | |
Mad is moisture; Aad denotes ash yield; Vdaf means volatile matter.
Fig 1The sampling locations of coal specimens in China.
Fig 2The test process of permeability changes and internal crack evolution under thermal shocks.
The main technical parameters of X-ray sources.
| Parameters | Micro-focus X-ray source | Nano-focus X-ray source |
|---|---|---|
| Voltage | From 10 kV to 240 kV | From 10 kV to 180 kV |
| The minimum size of focus | Less than 3 μm | Less than 1 μm |
| The maximum power | Larger than 320 W | Larger than 15 W |
| The minimum distance between the focus and the specimen | Less than 4.5 mm | Less than 0.35 mm |
| Resolution | Less than 2 μm | Less than 0.5 μm |
| Electric current | From 0.01 Am to 3.0 Am | From 0.01 Am to 0.88 Am |
Fig 3The SEM test process of coal particles under thermal shocks.
Fig 4Effect of thermal shocks on coal permeability (TD of 180 °C means the temperature difference of 180 °C).
Fig 5The reconstructed 3D crack structures in the examined coal specimens before and after thermal shocks.
Fig 6SEM images of anthracite coal particles before and after cooling shock.
Fig 7SEM images of bituminous coal particles before and after cooling shock.
Fig 8SEM images of anthracite coal particles before and after the heating-cooling shock.
Fig 9SEM images of bituminous coal particles before and after heating-cooling shock.
Fig 10Stress model of central oblique crack [66].
Fig 11Crack-tip stress field in a polar coordinate.