期刊文献+
共找到8篇文章
< 1 >
每页显示 20 50 100
时效析出对2E12铝合金疲劳断裂行为的影响 被引量:18
1
作者 李海 郑子樵 +1 位作者 魏修宇 王芝秀 《中国有色金属学报》 EI CAS CSCD 北大核心 2008年第4期589-594,共6页
测试等屈服强度条件下190℃,1 h欠时效和190℃,46 h过时效状态Al-Cu-Mg系2E12铝合金的疲劳寿命,并分别采用扫描电镜和透射电镜观察了疲劳断口形貌及时效析出特征,并在此基础上解释时效析出对2E12铝合金疲劳断裂行为的影响。结果表明:疲... 测试等屈服强度条件下190℃,1 h欠时效和190℃,46 h过时效状态Al-Cu-Mg系2E12铝合金的疲劳寿命,并分别采用扫描电镜和透射电镜观察了疲劳断口形貌及时效析出特征,并在此基础上解释时效析出对2E12铝合金疲劳断裂行为的影响。结果表明:疲劳裂纹主要萌生于试样表面的粗大残留相位置;由于过时效试样晶内析出大量的S平衡相降低疲劳变形时的位错滑移可逆性,加剧晶界处位错塞积程度;同时晶界上较宽的无析出带和沿晶界析出的粗大针状S相进一步促进晶界集中变形和开裂,从而降低过时效试样的疲劳寿命。 展开更多
关键词 铝合金 疲劳断裂行为 时效析出
下载PDF
热作模具钢在高温热机械应力循环下的疲劳断裂行为 被引量:10
2
作者 方健儒 姜启川 +1 位作者 韩增祥 王海清 《材料工程》 EI CAS CSCD 北大核心 2002年第10期11-14,共4页
研究了热作模具钢在应力控制下的等温疲劳和同相热机械疲劳寿命 ,发现在相同的应力幅下 ,同相热机械疲劳寿命低于上限温度的等温疲劳寿命。通过研究疲劳过程中的循环应变响应和疲劳断口特征时发现 ,等温疲劳条件下 ,滞后环朝压缩方向发... 研究了热作模具钢在应力控制下的等温疲劳和同相热机械疲劳寿命 ,发现在相同的应力幅下 ,同相热机械疲劳寿命低于上限温度的等温疲劳寿命。通过研究疲劳过程中的循环应变响应和疲劳断口特征时发现 ,等温疲劳条件下 ,滞后环朝压缩方向发展 ,疲劳裂纹主要为穿晶萌生与扩展 ;在热机械疲劳条件下 ,滞后环朝拉伸方向发展 ,疲劳裂纹主要沿晶萌生与扩展。 展开更多
关键词 热机械应力 疲劳断裂行为 热作模具钢 热机械疲劳 等温疲劳 温度循环 应力控制
下载PDF
应力控制下7075-T651铝合金的疲劳断裂行为 被引量:3
3
作者 陈涛 赵路远 +2 位作者 李慧 黄俊 吴玉程 《机械工程材料》 CSCD 北大核心 2017年第7期1-5,12,共6页
在不同应力幅下(60%σ_s,70%σ_s,80%σ_s,90%σ_s,σ_s为试验合金屈服强度)对7075-T651铝合金进行了应力控制下的疲劳试验,研究了其循环应变响应,观察了疲劳断口形貌、表面损伤形貌以及显微组织,分析了疲劳裂纹的萌生及扩展机制。结果... 在不同应力幅下(60%σ_s,70%σ_s,80%σ_s,90%σ_s,σ_s为试验合金屈服强度)对7075-T651铝合金进行了应力控制下的疲劳试验,研究了其循环应变响应,观察了疲劳断口形貌、表面损伤形貌以及显微组织,分析了疲劳裂纹的萌生及扩展机制。结果表明:试验合金中析出了微米级的Al7Cu2Fe颗粒、纳米级的η′(MgZn2)相和尺寸较大的η(MgZn2)相,此外,还存在尺寸为3~10nm的细小球状GP区;在较高应力幅(80%σ_s,90%σ_s)控制下,试验合金表现出先软化后硬化直至断裂的疲劳行为,而在较低应力幅(60%σ_s,70%σ_s)下则先软化后明显硬化并趋于稳定;试验合金主要发生微孔聚集韧窝型断裂,在较高应力幅下,裂纹源位于粗大夹杂物Al7Cu2Fe和第二相MgZn2处,位错大量缠结,而在低应力幅下,裂纹源位于基体轻微撕裂处,位错形态为分散的短或长直位错线。 展开更多
关键词 7075-T651铝合金 显微组织 疲劳断裂行为
下载PDF
2195铝锂合金的温热低周疲劳行为和疲劳寿命预测
4
作者 孟子杰 张存生 +4 位作者 吴承格 张豪 陈良 赵国群 闫海 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2023年第9期2574-2587,共14页
为研究2195铝锂合金在温热条件下(100和200℃)的低周疲劳行为,首先进行应变控制的低周疲劳试验。结果表明,合金的起始和中值寿命滞回环均呈现中心对称特征。在100℃、应变幅值为0.6%条件下的循环应力响应曲线表现出完全循环硬化特征,而... 为研究2195铝锂合金在温热条件下(100和200℃)的低周疲劳行为,首先进行应变控制的低周疲劳试验。结果表明,合金的起始和中值寿命滞回环均呈现中心对称特征。在100℃、应变幅值为0.6%条件下的循环应力响应曲线表现出完全循环硬化特征,而其他条件下的循环应力响应曲线均呈先循环硬化、然后循环软化的循环特征。随后,采用多种低周疲劳寿命预测模型对2195铝锂合金疲劳寿命进行评价。结果表明,基于总应变能密度的寿命预测模型具有最佳的预测精度。最后,为揭示2195铝锂合金的疲劳断裂机理,对不同试验条件下合金的疲劳断口进行观察。结果表明,在100℃、应变幅值为0.6%的条件下,合金断面上的疲劳条纹十分明显,但随着试验温度和应变幅值的升高,合金断面上的疲劳条纹逐渐弱化。在温度为200℃、应变幅值为1.0%条件下的疲劳断口呈明显沿晶断裂特征。 展开更多
关键词 2195铝锂合金 低周疲劳行为 疲劳寿命预测 疲劳断裂行为
下载PDF
Strength and fatigue fracture behavior of Al-Zn-Mg-Cu-Zr(-Sn) alloys 被引量:2
5
作者 陈璐 严安 +1 位作者 刘华山 李晓谦 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2013年第10期2817-2825,共9页
The strength and fatigue fracture behavior of A1-Zn-Mg-Cu-Zr(-Sn) alloys were studied by performing tensile tests and fatigue crack propagation (FCP) tests. The microstructures of the experimental alloys were furt... The strength and fatigue fracture behavior of A1-Zn-Mg-Cu-Zr(-Sn) alloys were studied by performing tensile tests and fatigue crack propagation (FCP) tests. The microstructures of the experimental alloys were further analyzed using optical microscopy (OM), scanning electron microscopy (SEM), and transmission electron microscopy (TEM); phase analysis of these alloys was conducted with an X-ray diffraction (XRD). The results show that when Sn is included, growth of the recrystallization grains in the solution-treated A1-Zn-Mg-Cu-Zr alloy is obstructed, the precipitation-free zone (PFZ) of the overaged A1-Zn-Mg-Cu-Zr-Sn alloy becomes narrow, and the grain boundary precipitates are smaller. Consequently, the FCP resistance is higher. In addition, the overaged Sn-containing alloy has considerably higher tensile strength than the alloy without Sn. 展开更多
关键词 AL-ZN-MG-CU-ZR SN STRENGTH fatigue fracture behavior MICROSTRUCTURE
下载PDF
High-cycle fatigue and fracture behaviours of SLM AlSi10Mg alloy 被引量:11
6
作者 S.GLODEŽ J.KLEMENC +1 位作者 F.ZUPANIČ M.VESENJAK 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2020年第10期2577-2589,共13页
The high-cycle fatigue and fracture behaviours of the selective laser melting(SLM)AlSi10Mg alloy were investigated.Flat specimens were designed directly in the shape required for the fatigue tests under pulsating load... The high-cycle fatigue and fracture behaviours of the selective laser melting(SLM)AlSi10Mg alloy were investigated.Flat specimens were designed directly in the shape required for the fatigue tests under pulsating loading in tension(R=0,R is the dynamic factor).The fatigue−life(S−N)curves were modelled with a conditional Weibull’s probability density function,where the real-valued genetic algorithm(GA)and the differential ant-stigmergy algorithm(DASA)were applied to estimating the needed Weibull’s parameters.The fractography of the fatigue specimens showed that the fatigue cracks initiated around the surface defects produced by SLM and then propagated in an unstable manner.However,the presence of large SLM defects mainly influenced the crack initiation period and did not have a strong influence on the crack propagation.The obtained experimental results present a basis for further investigation of the fatigue behaviour of advanced materials and structures(e.g.cellular metamaterials)fabricated by additive manufacturing(AM).Especially,in the case of two-dimensional cellular structures,the cross-section of cellular struts is usually rectangular which corresponds to the specimen shape considered in this work. 展开更多
关键词 selective laser melting AlSi10Mg alloy high-cycle fatigue fracture behaviour
下载PDF
应力比对单晶高温合金高周疲劳行为的影响 被引量:7
7
作者 谢洪吉 李嘉荣 韩梅 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2018年第11期3381-3386,共6页
为了研究应力比对DD6单晶高温合金高周疲劳行为的影响,在轴向疲劳试验机上分别测试了DD6合金1070℃条件下应力比为-1、-0.33、0.1、0.5、0.8的疲劳性能,采用扫描电镜(SEM)和能谱(EDS)仪观察分析了不同应力比合金的断口形貌和显微组织。... 为了研究应力比对DD6单晶高温合金高周疲劳行为的影响,在轴向疲劳试验机上分别测试了DD6合金1070℃条件下应力比为-1、-0.33、0.1、0.5、0.8的疲劳性能,采用扫描电镜(SEM)和能谱(EDS)仪观察分析了不同应力比合金的断口形貌和显微组织。结果表明:DD6合金在不同应力比条件下的疲劳寿命均随应力幅值和平均应力的增加而降低;当应力幅值恒定时,DD6合金疲劳寿命随着应力比的增大而降低;当平均应力恒定时,应力比R<0.5条件下的疲劳寿命随着应力比的增大而增加,同时,当平均应力增大到一定程度时,应力比对合金的疲劳寿命无明显影响。DD6合金低应力比条件下的疲劳断裂模式为类解理断裂,该条件下高温氧化有助于疲劳裂纹的萌生和扩展;高应力比条件下的疲劳断裂模式为韧窝断裂;中等应力比条件下疲劳断裂模式具有类解理断裂和韧窝断裂同时存在的特征。 展开更多
关键词 单晶高温合金 应力比 高周疲劳行为:断裂模式
原文传递
Fatigue and fracture behavior of nickel-based superalloy Inconel 718 up to the very high cycle regime 被引量:11
8
作者 Xian-feng MA Zheng DUAN +2 位作者 Hui-ji SHI Ryosuke MURAI Eiichi YANAGISAWA 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2010年第10期727-737,共11页
The fatigue and fracture behavior of nickel-based superalloy Inconel 718 was investigated up to the very high cycle regime under rotary bending tests at room temperature. It was found that this superalloy can still fr... The fatigue and fracture behavior of nickel-based superalloy Inconel 718 was investigated up to the very high cycle regime under rotary bending tests at room temperature. It was found that this superalloy can still fracture after exceeding 107 cycles. Fractographic analysis revealed that there was a transition from fatigue crack initiation at multi-sites to single initiation with decreasing stress levels. The fracture surface can be divided into four areas according to the appearance, associated with fracture mechanics analysis of the corresponding stress intensity factors. The fracture mechanism dominant in each area was disclosed by scanning electron microscope examination and analyzed in comparison with those obtained from the crack growth tests. Subsequently, life prediction modeling was proposed by estimating the crack initiation and propagation stage respectively. It was found that Chan (2003)'s model for initiation life and the Paris law for growth life can provide comparable predictions against the experimental life. 展开更多
关键词 Nickel-based superalloy High cycle fatigue (HCF) Fatigue crack initiation Crack growth Life prediction
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部