缺陷介质切槽爆破断裂行为的动焦散线实验

杨仁树; 许鹏; 杨立云; 陈程

doi:10.11883/1001-1455(2016)02-0145-08

缺陷介质切槽爆破断裂行为的动焦散线实验

doi: 10.11883/1001-1455(2016)02-0145-08

杨仁树^{1, 2},
许鹏^1, ,,
杨立云¹,
陈程²

1.
中国矿业大学(北京)力学与建筑工程学院，北京 100083
2.
中国矿业大学深部岩土力学与地下工程国家重点实验室，北京 100083

基金项目:

国家自然科学基金项目 51134025

高等学校学科创新引智计划项目 B14006

高等学校博士学科点专项科研基金项目 20120023120020

详细信息

作者简介:
杨仁树(1963—)，男，博士，教授，博士生导师

通讯作者:
许鹏，pxcumtb@163.com

中图分类号: O381;O346.1
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- 被引次数: 0
出版历程
- 收稿日期: 2014-08-13
- 修回日期: 2014-10-08
- 刊出日期: 2016-03-25

Dynamic caustic experiment on fracture behaviors of flawed material induced by pre-notched blasting

Yang Renshu^{1, 2},
Xu Peng^{1
, ,},
Yang Liyun¹,
Chen Cheng²

1.
School of Mechanics & Civil Engineering, China University of Mining & Technology, Beijing 100083, China
2.
State Key Laboratory for Geomechanics and Deep Underground Engineering, China University of Mining & Technology, Beijing 100083, China

摘要

摘要: 利用数字激光动态焦散线实验系统，对含缺陷介质在切槽爆破和普通炮孔爆破中爆生裂纹的断裂行为进行对比研究。结果表明，切槽爆破中沿切槽方向起裂的主裂纹比非切槽方向早10 μs，有利于能量优先沿切槽方向释放；切槽方向主裂纹的起裂韧度为0.58 MN/m^3/2，其裂纹扩展的平均速度为277 m/s，分别是普通爆破时主裂纹相应值的54%和86%；当切槽方向主裂纹与缺陷介质贯通后，为爆生气体提供了足够的膨胀空间，诱导爆生气体向预制裂纹两端释放，翼裂纹起裂以Ⅰ型拉伸破坏为主，并在裂纹扩展的60~250 μs内，Ⅰ型动态应力强度因子保持在0.6~0.8 MN/m^3/2，形成了明显的平台，延缓了翼裂纹扩展速度的衰减，最终较普通炮孔翼裂纹扩展时间和扩展长度分别增加了22.7%和17.8%。
- 爆炸力学 /
- 动态断裂行为 /
- 动焦散线实验 /
- 缺陷介质 /
- 切槽爆破 /
- 裂纹扩展
Abstract: Using a digital laser dynamic caustics experimental system, the fracture behavior of blast-induced cracks in flawed materials under both ordinary borehole and pre-notched borehole were studied. The results show that the main crack propagating along the pre-notched direction is 10 μs earlier than that along the non-notched direction, which attributes the blast energy release along with the pre-notched direction. The initiation toughness and average speed of the main crack in the pre-notched direction is 0.58 MN/m^3/2 and 277 m/s, respectively, corresponding to 54% and 86% of the ordinary blasting. For the pre-notched blasting, The space is large enough for the detonation gas expansion, when the main crack goes through with the pre-crack, and the detonation gas energy moving to the both ends of the pre-crack, leading mainly mode Ⅰ type initiation fracture of the wing crack, with which its mode Ⅰ dynamic stress intensity factor stays between 0.6 MN/m^3/2 and 0.8 MN/m^3/2 during 60-250 μs, which forms an obvious platform in the histories of mode Ⅰ dynamic stress intensity factor, and the decrease rate of wing crack velocity are also delayed. Eventually, the duration time of the crack propagation and the crack length are increased by 22.7% and 17.8%, respectively, compared with the ordinary borehole blasting.
- mechanics of explosion /
- dynamic fracture behavior /
- dynamic caustics experiment /
- flawed material /
- pre-notched blasting /
- crack propagation

HTML全文

图 1 焦散线成像示意图

Figure 1. Schematic diagram of caustics formation

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图 2 实验系统光路图

Figure 2. Optical system for new-type dynamic caustics system

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图 3 试件模型示意图

Figure 3. Schematic diagrams of specimen models

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图 4 普通炮孔动态焦散线系列图片

Figure 4. Series photos of dynamic caustics for ordinary blast hole

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图 5 切槽炮孔动态焦散线系列图片

Figure 5. Series photos of dynamic caustics for pre-notched blast hole

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图 6 试件破坏图样

Figure 6. Sketch of specimen after blasting

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图 7 主裂纹尖端动态应力强度因子时程曲线

Figure 7. Histories of dynamic stress intensity factor of blast-induced main crack

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图 8 主裂纹扩展速度时程曲线

Figure 8. Histories of crack propagation velocity of blast-induced main crack

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图 9 翼裂纹O-w₁尖端动态应力强度因子时程曲线

Figure 9. Histories of dynamic stress intensity factor of blast-induced wing crack O-w₁

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图 10 翼裂纹S-w₁尖端动态应力强度因子时程曲线

Figure 10. Histories of dynamic stress intensity factor of blast-induced wing crack S-w₁

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图 11 翼裂纹扩展速度、加速度时程曲线

Figure 11. Histories of crack propagation velocity and accelertation of blast-induced wing crack

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