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Frontiers of Structural and Civil Engineering

ISSN 2095-2430

ISSN 2095-2449(Online)

CN 10-1023/X

Postal Subscription Code 80-968

2018 Impact Factor: 1.272

Front. Struct. Civ. Eng.    2021, Vol. 15 Issue (6) : 1372-1389    https://doi.org/10.1007/s11709-021-0772-2
RESEARCH ARTICLE
Crack evolution of soft–hard composite layered rock-like specimens with two fissures under uniaxial compression
Dong ZHOU1, Yicheng YE1,2, Nanyan HU1,2(), Weiqi WANG1, Xianhua WANG3
1. School of Resources and Environmental Engineering, Wuhan University of Science and Technology, Wuhan 430081, China
2. Hubei Key Laboratory for Efficient Utilization and Agglomeration of Metallurgic Mineral Resources, Wuhan 430081, China
3. Sinosteel Wuhan Safety and Environmental Protection Research Institute Co., Ltd., Wuhan 430081, China
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Abstract

Acoustic emission and digital image correlation were used to study the spatiotemporal evolution characteristics of crack extension of soft and hard composite laminated rock masses (SHCLRM) containing double fissures under uniaxial compression. The effects of different rock combination methods and prefabricated fissures with different orientations on mechanical properties and crack coalescence patterns were analyzed. The characteristics of the acoustic emission source location distribution, and frequency changes of the crack evolution process were also investigated. The test results show that the damage mode of SHCLRM is related to the combination mode of rock layers and the orientation of fractures. Hard layers predominantly produce tensile cracks; soft layers produce shear cracks. The first crack always sprouts at the tip or middle of prefabricated fractures in hard layers. The acoustic emission signal of SHCLRM with double fractures has clear stage characteristics, and the state of crack development can be inferred from this signal to provide early warning for rock fracture instability. This study can provide a reference for the assessment of the fracture development status between adjacent roadways in SHCLRM in underground mines, as well as in roadway layout and support.

Keywords soft−hard composite layered rock mass      double cracks      crack evolution      acoustic emission      digital image correlation     
Corresponding Author(s): Nanyan HU   
Just Accepted Date: 09 November 2021   Online First Date: 06 December 2021    Issue Date: 21 January 2022
 Cite this article:   
Dong ZHOU,Yicheng YE,Nanyan HU, et al. Crack evolution of soft–hard composite layered rock-like specimens with two fissures under uniaxial compression[J]. Front. Struct. Civ. Eng., 2021, 15(6): 1372-1389.
 URL:  
https://academic.hep.com.cn/fsce/EN/10.1007/s11709-021-0772-2
https://academic.hep.com.cn/fsce/EN/Y2021/V15/I6/1372
Fig.1  Schematic diagram of an underground mine roadway layout.
sample αa) βb) 2ac) (mm) 2bd) (mm)
HSH-60 45° 60° 10 46.19
HSH-75 45° 75° 10 41.41
HSH-90 45° 90° 10 40.00
HSH-105 45° 105° 10 41.41
HSH-120 45° 120° 10 46.19
SHS-60 45° 60° 10 46.19
SHS-75 45° 75° 10 41.41
SHS-90 45° 90° 10 40.00
SHS-105 45° 105° 10 41.41
SHS-120 45° 120° 10 46.19
Tab.1  Experimental design scheme
Fig.2  Schematic diagram of the combination of soft and hard composite rock formations. The fissure length is 2a, the rock bridge length is 2b, the fissure inclination is α, and the rock bridge inclination is β.
specimens cement:gypsum:quartz sand water–cement ratio σca)(MPa) Eb)(GPa) νc)
hard rock 1.0:0:0.4 0.32 36.19 7.51 0.20
soft rock 1.0:0.3:0.4 0.46 19.36 5.29 0.23
Tab.2  Basic physical and mechanical parameters of rock samples
Fig.3  Test mold and sample: (a) combination mold; (b) rock-like specimen; (c) speckled specimen.
Fig.4  Test system diagram. DIC: digital image correlation; AE: acoustic emission; CCD: charge-coupled device.
sample σca) (MPa) εcb) (10?3) σccc) (MPa) σcid) (MPa) σci/σce) (%) σcdf) (MPa)
HSH-60 12.77 13.25 1.83 7.41 58.03 10.35
HSH-75 12.14 15.92 2.5 6.1 50.24 11.2
HSH-90 11.70 15.83 1.2 7.6 64.96 10.6
HSH-105 9.26 18.00 2.0 5.8 62.63 8.6
HSH-120 9.87 16.25 2.9 6.2 62.82 8.3
SHS-60 8.36 9.75 2.0 6.2 74.16 7.3
SHS-75 8.31 13.83 1.7 5.5 66.19 7.4
SHS-90 6.98 15.08 0.6 2.7 38.68 5.0
SHS-105 6.53 11.67 1.35 4.62 70.75 5.83
SHS-120 7.52 13.58 2.0 4.4 58.51 6.6
Tab.3  Mechanical test results of soft and hard composite laminated rock specimens with double fissures
Fig.5  Stress?strain curve of the cracked specimens in different orientations. (a) HSH; (b) SHS.
Fig.6  The final failure mode of soft and hard composite rock mass with double fissures.
types shear coalescence tensile coalescence mixed coalescence no coalescence
form
specimens HSH-60,75 SHS-75,90,105 HSH-120SHS-60,120 HSH-90,105
Tab.4  Four coalescence modes of double fractures in rock samples
Fig.7  Evolution diagram of principal strain and displacement of the HSH-60 specimen. ε1 is the principal strain, U is the displacement in the X-direction (perpendicular to the load direction), and V is the displacement in the Y-direction (parallel to the load direction).
Fig.8  Evolution diagram of principal strain and displacement of the SHS-105 specimen. ε1 is the principal strain, U is the displacement in the X-direction (perpendicular to the load direction), and V is the displacement in the Y-direction (parallel to the load direction).
Fig.9  Evolution diagram of principal strain and displacement of the SHS-60 specimen. ε1 is the principal strain, U is the displacement in the X-direction (perpendicular to the load direction), and V is the displacement in the Y-direction (parallel to the load direction).
Fig.10  Evolution diagram of principal strain and displacement of the HSH-105 specimen. ε1 is the principal strain, U is the displacement in the X-direction (perpendicular to the load direction), and V is the displacement in the Y-direction (parallel to the load direction).
Fig.11  The change law of axial stress and acoustic emission (AE) counts of HSH-60 specimen.
Fig.12  Spatiotemporal evolution distribution and principal strain cloud diagram of seismic source acoustic emission at key points of HSH-60 specimen failure: (a)σcc point; (b)σci point; (c)σcd point; (d)σc point; (e)σce point.
Fig.13  Spatiotemporal evolution distribution and principal strain cloud diagram of seismic source acoustic emission at the critical point of SHS-105 specimen failure: (a) σcc point; (b) σci point; (c) σcd point; (d) σc point; (e) σce point.
Fig.14  The change law of axial stress and acoustic emission counts of SHS-105 specimen.
Fig.15  Acoustic emission signal waveform and frequency spectrum: (a) time domain signal and (b) frequency domain signal.
Fig.16  Crack extension acoustic emission frequency and amplitude variation: (a) HSH-60 and (b) SHS-105.
specimens frequence stage Ⅰ stage Ⅱ stage Ⅲ stage Ⅳ
num. ratio num. ratio num. ratio num. ratio
HSH-60 low freq. 46 23.12% 28 14.14% 177 20.39% 242 16.81%
medium freq. 50 25.13% 37 18.69% 176 20.28% 399 27.71%
high freq. 103 51.75% 133 67.17% 515 59.33% 799 55.48%
SHS-105 low freq. 6 40.00% 11 9.82% 130 36.52% 191 47.75%
medium freq. 4 26.67% 2 1.79% 30 8.43% 58 14.50%
high freq. 5 33.33% 99 88.39% 196 55.05% 151 37.75%
Tab.5  Statistics of acoustic emission frequency change during crack extension
type coalescence patterns description of crack coalescence type mode of coalescence specimens
coalescence of two type 2 S cracks shear coalescence HSH-60
coalescence of two type 1 S cracks shear coalescence HSH-75
coalescence of two type 2 S cracks and type 2 T crack mixed coalescence SHS-60
coalescence of two type 1 T cracks tensile coalescence SHS-90
coalescence of type 3 T crack and type 1 T crack tensile coalescence SHS-105
coalescence of type 3 T crack, short type 1 S crack and type 1 T crack mixed coalescence SHS-120
coalescence of two type 3 T cracks and short type 1 S crack mixed coalescence HSH-120
Ⅷ (new) coalescence of type 2 T crack, type 1 T crack and interface crack tensile coalescence SHS-75
Ⅸ (new) no coalescence no coalescence HSH-90HSH-105
Tab.6  Types of crack coalescence in the present experimental results
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