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Fatigue deformation and damage characteristics of bolting system under stress-controlled cyclic pullout  ( SCI-EXPANDED收录 EI收录)   被引量:7

文献类型:期刊文献

英文题名:Fatigue deformation and damage characteristics of bolting system under stress-controlled cyclic pullout

作者:Xue, Fei[1,2,3];Zhao, Tongyang[1,2];Feng, Xiaowei[3];Wang, Tianzuo[1,2]

机构:[1]Shaoxing Univ, Coll Civil Engn, Key Lab Rock Mech & Geohazards Zhejiang Prov, Shaoxing 312000, Peoples R China;[2]Shaoxing Univ, Zhejiang Collaborat Innovat Ctr Prevent & Control, Shaoxing 312000, Peoples R China;[3]China Univ Min & Technol, Key Lab Deep Coal Resource Min, Minist Educ, Xuzhou 221116, Jiangsu, Peoples R China

年份:2021

卷号:285

外文期刊名:CONSTRUCTION AND BUILDING MATERIALS

收录:SCI-EXPANDED(收录号:WOS:000647563100008)、、EI(收录号:20211110084600)、Scopus(收录号:2-s2.0-85102382529)、WOS

基金:The authors would like to acknowledge the financial support for this study provided by the Natural Science Foundation of Zhejiang Province (LQ20E080006) and thank the reviewers' valuable comments and suggestions for improvement of the manuscript.

语种:英文

外文关键词:Bolt; Fatigue; Short encapsulated cyclic pullout test; Acoustic emission; Fatigue damage model

外文摘要:This study explored the fatigue mechanical properties and acoustic emission (AE) characteristics of bolting system under cyclic pullout tests controlled by different upper stress levels. A novel compression-pull load conversion device was designed to precisely apply cyclic pullout load on bolting system. Strain gauges and AE sensors were employed to capture the surface strain variations of rock bolts and microfracture development during static and cyclic testing. The fatigue strength, deformation, axial/shear stress distributions and AE characteristics of the bolting system were comprehensively investigated. Fatigue threshold, an important value determining the service life of a bolting system, was supposed to be lower than 85% of the static strength in this study. The bolt residual slip strain curve was S-shaped and comprised three stages: the initial stage, constant-velocity stage and acceleration stage. The constant-velocity stage accounted for most of the fatigue life and was the main stage of fatigue development. The fatigue failure of the anchorage system was presumably controlled by the entire static stress-strain process, and the residual strain at fatigue failure corresponded to the peak strain at the peak stress under static loading. The anchorage fatigue damage development completely coincided with the residual strain evolution, and the turning points were identical between the different deformation stages. Based on the residual slip strain development, nonlinear inverted S-shaped cumulative fatigue damage models were proposed for different upper stress levels. A comparison of the results from different samples revealed that the damage evolution was highly dependent on the upper stress level. The fatigue life of the bolting system decreased as the upper stress level increased due to the increased steepness of the second stage and the decreased proportion of the second stage to the entire fatigue process. (C) 2021 Elsevier Ltd. All rights reserved.

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