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8.8级M24高强螺栓的常幅疲劳性能试验研究 被引量:2

EXPERIMENTAL RESEARCH ON CONSTANT-AMPLITUDE FATIGUE CHARACTERISTICS OF 8.8 GRADE M24 HIGH-STRENGTH BOLTS
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摘要 为研究8.8级高强螺栓“轴心拉-拉”常幅疲劳性能,对材质为35K的M24高强螺栓进行了3个试件静力拉伸试验和15个试件(应力比为0.3)的常幅疲劳试验,拟合了S-N曲线,对代表性试件疲劳断口进行宏观和微观分析,并与基于GB 50017—2017《钢结构设计标准》相关公式的计算结果进行了对比。结果表明:疲劳试验数据总体较为离散,但均在95%置信区间内,拟合的S-N曲线基本反映不同应力幅下试件的疲劳寿命;试件缺口效应明显,尤其在螺栓螺纹齿根处,应力集中程度严重,点状疲劳源易扩展形成线状疲劳源,断口韧窝特征明显;相比标准建议值,试验所得2×106次对应疲劳强度为其1.61倍。 In order to study the constant-amplitude fatigue performance of 8.8 grade high-strength bolts under axial tension-tension condition,3 static tensile tests and 15 M24 bolts with 35K material were carried out.S-N curves were fitted and the fatigue fracture surfaces of representative specimens were analyzed macroscopically and microscopically.In addition,all the test results were compared with those calculated based on the relevant formula of Standard for Classification of Steel Structures(GB 50017—2017).The conclusions are as follows:The fatigue test data were generally discrete,but all within 95%confidence interval;The S-N curves could basically reflect the fatigue life of specimens under different stress amplitudes;At the root of the screw thread,the stress concentration was especially serious,punctiform fatigue source was easy to expand to form linear fatigue source,the notch effect of the specimen was evident;Comparing the test results with the recommended values of allowable fatigue strength stipulated in the national standards,the corresponding fatigue strength of 2×106 times was 1.61 times of the recommended value.
作者 翟彬 刘勇 商文念 张继亮 焦晋峰 ZHAI Bin;LIU Yong;SHANG Wennian;ZHANG Jiliang;JIAO Jinfeng(Shandong Electric Power Engineering Consulting Institute Co.,Ltd.,Jinan 250013,China;College of Civil Engineering,Taiyuan University of Technology,Taiyuan 030024,China)
出处 《工业建筑》 CSCD 北大核心 2020年第9期122-127,共6页 Industrial Construction
基金 国家自然科学基金项目(51578357) 山西省留学人员科技活动择优资助项目(DC1900000602) 山西省研究生联合培养基地人才培养项目(2016JD11)。
关键词 8.8级 高强螺栓 常幅疲劳 疲劳断口 S-N曲线 8.8 grade high-strength bolts constant-amplitude fatigue fatigue surface S-N curve
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