单裂隙砂岩破坏特征和破裂演化规律试验
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  • 英文篇名:Experimental Study on Failure Characteristics and Crack Evolution Laws of Sandstone Containing Pre-existing Single Crack
  • 作者:郭寿松
  • 英文作者:GUO Shousong;China Coal Technology and Engineering Group Chongqing Research Institute;State Key Laboratory of Gas Disaster Detecting,Preventing and Emergency Controlling;
  • 关键词:岩石力学 ; 裂隙倾角 ; 变形破坏特征 ; 声发射 ; 裂纹扩展
  • 英文关键词:rock mechanics;;crack dip angle;;deformation and failure characteristics;;acoustic emission;;crack propagation
  • 中文刊名:MKAQ
  • 英文刊名:Safety in Coal Mines
  • 机构:中煤科工集团重庆研究院有限公司;瓦斯灾害监控与应急技术国家重点实验室;
  • 出版日期:2019-07-20
  • 出版单位:煤矿安全
  • 年:2019
  • 期:v.50;No.541
  • 语种:中文;
  • 页:MKAQ201907013
  • 页数:5
  • CN:07
  • ISSN:21-1232/TD
  • 分类号:62-66
摘要
针对含不同倾角裂隙的板状砂岩试样开展单轴加载试验,从宏细观角度深入探索裂隙倾角对脆性岩石变形破坏特征、声发射及破裂演化规律的影响效应,揭示其破坏机制。结果表明:裂隙倾角α较小时(0°≤α≤30°),应力-应变曲线呈锯齿状;翼裂纹首先在初始裂隙中部萌生,次生拉伸裂纹扩展贯通导致试样破坏,声发射较为分散,以劈裂破坏为主;随裂隙倾角增加(30°<α<90°),应力跌落次数减少,峰值强度和弹性模量不断升高;翼裂纹起裂位置向初始裂隙尖端转移,起裂强度和起裂强度比逐渐增加,次生裂纹转为剪切裂纹,声发射趋于集中,破坏模式向剪切破坏过渡;裂隙倾角为90°时,应力-应变曲线光滑,初始裂隙起裂前试样瞬间破坏,声发射异常集中,以劈裂破坏为主,与完整试样基本一致。
        By the uniaxial compression test of slab sandstone specimen containing pre-existing single crack of different dip angles,the influence effect of crack dip angle on the deformation and failure characteristic, AE evolution law and crack propagation evolution law of brittle rock were deeply analyzed from macroscopic and mesoscopic perspectives, meanwhile, the failure mechanism was revealed. The results show that: when the crack angle was small(0°≤α≤30°), the stress-strain curve exhibited a "saw tooth"shape and failure mode was primarily splitting failure; the wing crack firstly sprouted in the middle of the initial crack, then the propagation and coalescence of secondary tensile crack caused the ultimate fail of the specimens, therefore, AE signal during the whole compression process was more dispersed; with the increasing of flaw angle(30°<α<90°), the number of stress dropping decreased, the peak strength and elastic modulus increased continuously, and the failure mode was primarily shear failure; the initiation position of wing crack firstly appeared in the initial crack tip, and the crack initiation strength and crack initiation strength ratio increased gradually, then, the secondary crack transferred to shear crack, which made the AE signal tended to concentrate; for the crack angle of 90°, the stress-strain curve was very smooth, the specimen failed instantaneously and caused AE signal concentrated abnormally before the crack initiation of the initial crack, and the fail mode was splitting damage, which was basically consistent with the complete sample.
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