共查询到20条相似文献,搜索用时 46 毫秒
1.
HRB500高强钢筋拉压疲劳性能研究及断口分析 总被引:1,自引:0,他引:1
通过轴向拉压疲劳试验得到HRB500钢筋在应力比R=0.1时107周次的疲劳强度σ0.1=587.5 MPa,远高于一般碳素结构钢的疲劳强度;再利用三参数幂函数法非线性回归得到S-N曲线方程为lg(Nf)=7.092-1.144 7lg(σmax-586.3);并研究发现直径大小对钢筋的疲劳强度基本没影响,疲劳强度主要与材料的成分、组织及夹杂物有关。还利用扫描电镜与能谱仪分析试样的疲劳断口,得到HRB500钢筋的疲劳破坏均属于表面基体起裂,与钢中脆性夹杂物有关;疲劳裂纹呈放射状在基体中扩展,呈现比较明显的片层状结构,以准解理裂纹扩展为主;瞬断区呈韧性断裂,出现大量韧窝状组织,主要由于夹杂物引起微孔聚集断裂。 相似文献
2.
应用压电超声疲劳试验技术,开发20 kHz频率下的三点弯曲疲劳试验系统,完成室温下TiAl合金超高周弯曲疲劳试验.结果表明,在疲劳循环大于107周时,试样仍会发生疲劳断裂.S-N曲线显示,当应力比R=0.7时,在107周后会出现疲劳极限,表面粗糙度对疲劳性能没有明显影响.当R=0.1 及R=0.5时,在105~1010周之间疲劳强度随循环次数的增加连续下降,S-N曲线未出现水平.光学显微观察发现,TiAl合金由α2-Ti3Al 和γ-TiAl组成(γ α2钛铝合金),具有全片层状显微结构.疲劳破坏主要起源于试件表面承受应力最大处,层状晶体内层间裂纹萌生是 TiAl合金主要的裂纹萌生方式,疲劳裂纹主要以穿晶方式扩展.在超高周循环条件下, 疲劳裂纹也会从试样近表层处的铸造缩孔萌生. 相似文献
3.
4.
对2.0 mm厚汽车用SPHC热轧薄钢板进行低周循环应变疲劳试验,获得了应力-应变曲线、应变-寿命曲线、应变滞回环曲线以及相关疲劳常数指标,并对疲劳断口形貌进行观察.结果表明:SPHC钢在试验范围内具有非Masing效应;拟合得到SPHC钢的循环强度系数为284,循环应变硬化指数为0.128;通过Manson-Coffin方程拟合得到SPHC钢的疲劳强度系数为467 MPa,疲劳强度指数为-0.078,疲劳延性系数为0.323,疲劳延性指数为-0.609;疲劳断口由裂纹源区、裂纹扩展区、瞬断区组成,裂纹扩展区由大量疲劳辉纹组成,瞬断区存在大量韧窝,SPHC钢具有良好的塑韧性. 相似文献
5.
6.
Q235材料的Paris常数C、m及△Kth值测试 总被引:4,自引:1,他引:3
以大型机械结构最常用的Q235板材(等同于ASTM A36)为研究对象,在实验室条件下测取裂纹扩展速率的Paris常数C、m,并验证与轧制方向垂直的裂纹受平行于轧制方向应力作用时最易扩展的结论.同时以应力比R=0.1加载试验数据外延计算获得其门槛值△Kth(da/d/N=0.5×10-6mm/cycle时). 相似文献
7.
分别采用钨极氩弧焊(GTAW)和搅拌摩擦焊(FSW)对10mm厚5754铝合金进行双面同步焊接,对比研究了应力幅为162,135,117,108,99MPa时焊接接头的疲劳性能,并对其疲劳断裂机理进行了分析。结果表明:在指定应力幅下,5754铝合金GTAW接头的疲劳强度明显高于FSW接头的,在50%和95%存活率下,GTAW接头的疲劳强度特征值比FSW接头的分别提高了27%和30%,GTAW接头的疲劳性能优于FSW接头的;GTAW接头与FSW接头的疲劳断裂机理基本相同,疲劳裂纹均起源于接头熔合区的外表面,随着应力幅的降低,疲劳裂纹扩展区在断口中的占比增加,且同等应力幅下GTAW接头疲劳裂纹扩展区的占比高于FSW接头的;同等应力幅下GTAW接头的疲劳辉纹间距比FSW接头的小,GTAW接头的疲劳寿命长于FSW接头的。 相似文献
8.
对TLVW1114Ti材料进行了疲劳试验,得到了应力 寿命曲线,当σ>σ0.1=402MPa时,N=4.102×1044σ-14.501;得到了应变疲劳特性Δσ/2=1006(2Nf)-0.0998,Δεp/2=1.1758(2Nf)-0.7487,Δσ/2=977.7(Δεp/2)0.1321;当da/dN≥5×10-5mm/周,其裂纹扩展速率为da/dN=2.2364×10-9(ΔK)3.1541,当da/dN<5×10-5mm/周,da/dN=1.54147×10-14(ΔK)8.644。 相似文献
9.
室温下,对覆板TA2、基板Q345、爆炸复合板TA2/Q345的光滑试样进行静态拉伸和高周疲劳试验;线性拟合出最大应力幅σ_(max)和疲劳寿命N的关系曲线,并对其疲劳断口进行扫描分析。结果表明,复合板TA2/Q345的抗拉强度优于基板和覆板,疲劳强度介于基板与覆板之间,σ_(-1p)=0. 31σ_b,复合板的疲劳比较小,抵抗疲劳作用的能力较差。复合板TA2/Q345疲劳断口呈现多源性,裂纹萌生于基板Q345表面,终断于覆板TA2;多源裂纹扩展交汇时形成台阶,基板Q345向覆板TA2扩展时出现了"爬坡"现象,且覆板TA2侧出现了"剥离撕裂"。由于覆板和基板弹性模量、晶体结构、金相组织的差异,造成复合板结合界面开裂。 相似文献
10.
航空发动机涡轮盘用GH4133B合金疲劳裂纹扩展行为研究 总被引:3,自引:1,他引:3
材料的疲劳寿命由裂纹形成寿命和扩展寿命两部分组成。针对航空发动机涡轮盘用GH4133B合金,进行室温下不同应力比的疲劳裂纹扩展试验,测试疲劳裂纹扩展门槛值。Paris公式回归分析结果表明,裂纹扩展速率随应力强度因子和应力比的增大而增大,含门槛值的修正Paris公式能精确描述疲劳裂纹扩展行为。利用光学显微镜在线观测裂纹扩展路径,并利用扫描电镜考察试样断口微观形貌。结果发现,随应力强度因子增大,裂纹扩展路径由平直变得曲折。在疲劳裂纹萌生区、稳定扩展区和快速扩展区,断裂表面依次呈现为解理断裂、疲劳条带和沿晶韧窝混合断裂模式。基于断口反推理论反推载荷和裂纹扩展方程,结果表明,利用反推方程预测疲劳裂纹的扩展,可有效防范疲劳断裂的发生。 相似文献
11.
介绍了疲劳设计准则的基本类型,说明了疲劳门槛的意义及其在疲劳设计中的作用,指出疲劳设计准则、疲劳载荷谱及无损检测技术是决定疲劳门槛能否作为疲劳设计参数的三个主要因素。 相似文献
12.
13.
14.
加速疲劳试验的疲劳编辑技术 总被引:8,自引:0,他引:8
疲劳编辑技术可用来预估零部件疲劳测试周期,浓缩载荷信号以加速在实验室里用单通道、、多通道等技术进行的疲劳耐久性试验。结合一个实例介绍了多种工程上常用的疲劳编辑技术的思路及特点。 相似文献
15.
主要论述了使用高频疲劳试验机测定材料的疲劳寿命曲线的方法和实现过程;用最小二乘法进行曲线拟合的原理和处理方法。对于测试材料的疲劳寿命具有一定的实际意义。 相似文献
16.
AbstractEvaluating new materials for rolling element bearings (REBs) is an expensive, time-consuming, and difficult process. This work presents a continuum damage mechanics (CDM)-based finite element model (FEM) that incorporates gradual material degradation under cyclic loading and discrete material representation to predict rolling contact fatigue (RCF) failure. The fully reversed orthogonal shear stress was considered the critical stress for the CDM RCF modeling. Torsional fatigue results available from the open literature were used to determine the critical parameters for CDM FEM. In contrast to previous modeling approaches, in this investigation the CDM material parameters were considered probabilistic in nature to represent variations in material strength or resistance to fatigue. This modification to the modeling procedure resulted in RCF life predictions that capture life scatter characteristic of the RCF phenomena for REBs. Based on the model results, a fatigue life equation was developed to corroborate the Lundberg and Palmgren (LP) theory. The results obtained from the predictive life equation generated from the CDM-based FEM using material parameters obtained from torsional fatigue results are in good agreement with the LP model. 相似文献
17.
18.
Generally, the fatigue crack is initiated and then it is propagated toward the welding direction and the thickness direction. Finally, the joints lose the resistance to the external force. At present, as there is no deciding method of the fatigue strength (fatigue life), this paper proposed it from the result obtained by bending test for fillet welded joints. Judging initiation of the fatigue crack from the measured value of strain gages, there was a possibility that the fatigue crack occurred at both sides of fillet welded joints. However, this was a different result from that of macrograph of cross section. On the other hand, the results obtained by FSM (field signature method) coincided with the result of macrograph of cross section. For the initial state, potential difference obtained by the electrostatic analysis based on FEM (finite element method) and that by FSM was accurately coincided. After confirming validity of the crack model for analysis, the crack model was specified by reproducing the propagating process of crack accurately through trial and error. It was concluded that the state which could not resist to the external force was regarded as fatigue strength based on equivalent stress obtained by elastic stress analysis for specified crack model. From the experimental result, it was proposed that 90% of repetition number corresponding to the state which could not resist to the external force (at the finish of the test) was regarded as fatigue strength (fatigue life) in consideration of safety and as the first approximation. 相似文献
19.
超声疲劳试验方法在40Cr钢疲劳性能研究中的应用 总被引:4,自引:2,他引:4
用超声疲劳试验方法(频率为20kHz)测定40Cr钢在10^5~10^10周次范围内的疲劳寿命(S-N)曲线。结果表明,40Cr钢的疲劳寿命(SN)曲线在10^5~10^10周次范围内始终保持下降趋势,在l0^5周次以上没有水平段。超高频疲劳载荷下的S-N曲线同样能用Basquin关系式描述。与常规频率下的疲劳性能相比,高频载荷下的疲劳强度增加。20kHz循环载荷下,40Cr钢10^7周次的疲劳强度为443MPa,10^10周次时为235MPa。 相似文献