郭奇峰, 武旭, 蔡美峰, 任奋华, 潘继良. 预制裂隙花岗岩的裂纹起裂机理试验研究[J]. 煤炭学报, 2019, 44(S2): 476-483. DOI: 10.13225/j.cnki.jccs.2019.1212
引用本文: 郭奇峰, 武旭, 蔡美峰, 任奋华, 潘继良. 预制裂隙花岗岩的裂纹起裂机理试验研究[J]. 煤炭学报, 2019, 44(S2): 476-483. DOI: 10.13225/j.cnki.jccs.2019.1212
GUO Qifeng, WU Xu, CAI Meifeng, REN Fenhua, PAN Jiliang. Crack initiation mechanism of pre-existing cracked granite[J]. Journal of China Coal Society, 2019, 44(S2): 476-483. DOI: 10.13225/j.cnki.jccs.2019.1212
Citation: GUO Qifeng, WU Xu, CAI Meifeng, REN Fenhua, PAN Jiliang. Crack initiation mechanism of pre-existing cracked granite[J]. Journal of China Coal Society, 2019, 44(S2): 476-483. DOI: 10.13225/j.cnki.jccs.2019.1212

预制裂隙花岗岩的裂纹起裂机理试验研究

Crack initiation mechanism of pre-existing cracked granite

  • 摘要: 为了探究含裂隙花岗岩材料的裂纹起裂机理,以取自三山岛金矿的花岗岩为研究对象,利用金刚石砂线切割机对试件预制不同倾角的裂隙。采用声发射与表面应变监测等手段,并基于最大畸变能理论对单轴压缩条件下裂隙花岗岩的裂纹起裂强度、起裂角以及裂纹扩展路径进行试验与计算。试验结果表明,岩石强度随裂隙倾角的增加呈非线性变化规律,裂隙倾角与加载方向一致时,试件峰值强度最大。裂纹起裂均位于预制裂隙尖端,裂纹起裂角随预制裂隙倾角的增加而单调增加; 裂纹起裂强度的变化特征与岩石峰值强度相似,均呈现先降低后增加的规律。当0°< β< 90°时,裂隙尖端产生翼型裂纹,随着外荷载增加,反翼型裂纹产生并导致试件失稳破坏; β=0°时,起裂裂纹与裂隙近似平行但未持续扩展,试件呈显著地压剪破坏; β=90°时,裂隙端部受张拉应力作用生成与裂隙近似垂直的张拉裂纹。通过声发射振铃计数突变特征与应力-时间曲线判断,当裂隙倾角β为45°时,起裂强度最小,仅为峰值应力的40%,此类岩石在较低荷载作用下发生破裂,岩石破裂为渐进式,裂纹扩展速度相对较慢; 相比之下,裂隙倾角β为0°和90°时,起裂强度较高,岩石的破裂过程较为迅速,裂纹在较高应力作用下起裂并快速扩展导致岩石破坏,呈现出明显的脆性破坏特征,岩石破裂的预判难度较大。以最大畸变能理论为依据的计算结果表明,复合型裂隙的起裂角与裂隙倾角呈单调增加的关系,与最大周向拉应力准则相比,理论计算与试验值吻合程度更高。最大畸变能理论可用于判断单轴加载条件下单裂隙岩石的起裂特征。

     

    Abstract: In order to explore the crack initiation mechanism of pre-existing cracked granite under uniaxial com-pression, the crack initiation angle, crack initiation stress and failure mode of cracked granite specimens with dif-ferent dip angles were analyzed by mechanical test and numerical calculation based on acoustic emission and surface strain field variation characteristics.The results show that the crack initiation is located at the tip of pre-existing crack, and the crack initiation angle increases monotonically with the increase of pre-existing crack angle.When the dip angle is 45°, the minimum crack initiation stress is 24.65 MPa.When 0°< β< 90°, the airfoil crack appears at the crack tip, and before loading to the peak strength, the anti-airfoil crack appears and leads to the instability failure of the specimen.When β=0°, the initiation crack is approximately parallel to the crack but does not continue to expand, and the specimen shows a compression shear failure mode.When β=90°, the initiation crack is approximately perpendicular to the crack and extends to the specimen.

     

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