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1.
研究了环氧沥青基有机涂层对16Mn钢腐蚀疲劳行为的影响。在恒幅疲劳载荷控制下比较了裸样与涂层试样在空气自然海水及不同阴极保护条件下的寿命变化规律,测量了试样在海水中CF过程自腐蚀电位随循环周次的变化,在不同阴极保护条件下记录阴极电流随循环周次的变化情况。  相似文献   

2.
研究了一种镍基高温合金在不同温度下的低周疲劳性能,分析了疲劳断口。结果表明,该合金循环应力响应行为表现出对温度和外加总应变幅很强的依赖关系,不同的循环应力响应行为可归因于位错、强化相和合金元素间复杂的交互作用。合金疲劳寿命与温度、外加总应变幅、氧化损伤程度有关。疲劳断裂行为受外加应变幅和氧化影响很大。  相似文献   

3.
对铸态高锰钢(120Mn13)进行了常温拉伸及低周疲劳试验,研究了试样在拉伸变形中的动态应变时效,在拉压疲劳变形过程中的循环应力应变行为、循环硬化软化行为及裂纹扩展行为等。结果表明:在拉伸曲线中发现了代表动态应变时效作用的峰状低频A型锯齿和波纹状高频B型锯齿。在不同应变幅下的低周疲劳实验中,试样均先循环硬化,后循环软化直至断裂。随着应变幅的增加,其最大循环拉应力逐渐增加,疲劳寿命却降低。高应变幅下的裂纹多沿晶界扩展,但裂纹偏转次数及二次裂纹数量增多,这是其寿命较低应变幅下相差较小的主要原因。  相似文献   

4.
应变幅与应变速率在形变加速腐蚀过程中的作用   总被引:1,自引:0,他引:1  
王政富  李劲  王俭秋  柯伟 《金属学报》1994,30(17):213-217
采用应变电极技术研究了应变幅、应变速率与外加电位对形变中金属电化学腐蚀过程的影响。选用的体系为工业纯Fe-3.5%NaCl水溶液和A537钢-3.5%NaCl+1%NaNO2水溶液结果表明,塑性变形对阳极过程的加速作用大于对阴极过程的加速作用,这种作用主要发生在自腐蚀电位附近。在强阳极与强阴极极化区,由于强的分反应驱动力,单个反应的电流增大,导致了形变电流的增加相对不重要。活化体系的金属溶解电流主要受应变幅控制,而钝化体系则主要由应变速率控制,取决于应变活化区域的再钝化动力学过程.  相似文献   

5.
在650℃以及拉压对称三角波(TR)、慢拉快压锯齿波(ST)和快拉慢压锯齿波(FT)3种应变波形下对Inconel625合金进行了低周疲劳实验,研究了合金在不同应变波形下的低周疲劳变形与断裂行为。结果表明:3种应变波形加载条件下,合金在0.3%~0.7%的外加总应变幅下均呈现循环硬化,其中在ST下的循环应力幅最高;采用锯齿波形时,由于拉伸蠕变分量和压缩蠕变分量的引入造成合金的疲劳寿命缩短;此外,合金的循环应力和应变之间呈现单斜率线性关系,且其塑性应变幅与弹性应变幅和疲劳寿命之间亦呈线性关系。利用扫描电子显微镜对Inconel625合金在3种加载波形下的低周疲劳断口形貌进行观察,结果表明,Inconel 625合金的疲劳裂纹萌生和扩展均是以穿晶方式进行的。  相似文献   

6.
通过外加总应变幅控制的拉-压对称疲劳试验,研究常温下挤压AZ31B镁合金在不同应变幅下的疲劳性能。结果表明,除了在低应变幅0.5%外,样品均呈现循环应变硬化;应变幅为0.5%时,样品在初始阶段呈现循环硬化,随后保持应力恒定;在压缩过程中孪晶的产生以及随后的卸载和反向拉伸过程中的去孪晶行为导致了高应变幅下的滞回环形状拉-压不对称现象,而低应变幅0.5%下的滞回环形状基本对称,说明低应变幅下孪生-去孪生现象不明显。在整个疲劳过程中,高应变和低应变下的应力—应变曲线呈现2种不同的滞回环形状,这是由不同疲劳阶段孪生和位错滑移2种不同的变形机制所导致。  相似文献   

7.
研究近α型TG6钛合金盘锻件双态组织在600 ℃不同应变幅条件下的低循环疲劳行为,总应变幅△εt/2控制在±0.6%~±1.5%,应变比R=-1,采用三角波方式加载.结果表明:600 ℃低循环疲劳条件下,随着总应变幅的增加,循环峰值应力smax提高,而疲劳寿命Nf下降;对于TG6钛合金盘锻件双态组织,存在一个循环软化/硬化的总应变幅临界值(△εt/2)c,约为±1.0%,当总应变幅高于此值,表现为循环硬化行为,而低于此值时,则表现为循环软化行为;在所有应变幅条件下,疲劳裂纹均为多源萌生模式,600 ℃低循环疲劳变形行为主要受α晶粒内位错的平面滑移所控制,位错平面滑移集中的结果是最早在α晶粒内萌生疲劳裂纹;随着疲劳测试温度的提高,不同滑移系上位错滑移的临界分切应力的差别缩小,促进位错交滑移的进行.  相似文献   

8.
应变幅与应变速率在形变加速腐蚀过程中的作用   总被引:1,自引:0,他引:1  
王政富  李劲 《金属学报》1994,30(5):B213-B217
采用应变电极技术研究了应变幅,应变速率与外加电位对形变中金属电化学腐蚀过程的影响,选用的体系为工业纯Fe-3.5%NaCl水溶液和A537钢-3.5%NaCl+1%NaNO2水溶液,结果表明,塑性变形对阳极过程的加速作用大于对阴极过程的加速作用,这种作用主要发生在自腐蚀电位附近,在强阳极与强阴极极化区,由于强的分反应驱动力,单个反应的电流增大,导致了形变电流的增加相对不重要,活化体系的金属溶解电流  相似文献   

9.
研究了锆-4合金在不同应变速率下的低周疲劳和带应变保持时间相关低周疲劳行为。结果表明:在不同加载方式下,锆-4合金均表现为循环硬化,应变保持和应变速率降低均进一步提高循环饱和应力。应变保持降低材料的疲劳寿命,特别是在高应变幅区域。随着应变速率降低,材料疲劳寿命降低。疲劳变形亚结构观察表明:锆-4合金时间相关疲劳过程中以柱面滑移和晶界滑移方式变形。  相似文献   

10.
研究了锆-4合金在不同应变速率下的低周疲劳和带应变保持时间相关低周疲劳行为。结果表明:在不同加载方式下,锆-4合金均表现为循环硬化,应变保持和应变速率降低均进一步提高环孢和应力。应变保持降低材料的疲劳寿命,特别是在高应变幅区域。随着应变速率降低、材料疲劳寿命降低。疲劳变形亚结构观察表明:锆-4合金时间相关疲劳过程中以{101↑-0}柱面滑移和晶界滑移方式变形。  相似文献   

11.
<正>一、引言 在腐蚀性水溶液中,金属的力学疲劳损伤因电化学作用(如溶解效应和氢还原反应等)而加剧,反之,在腐蚀疲劳过程中,力学疲劳引起的塑性形变局部化又会增加电化学腐蚀。  相似文献   

12.
I-Hsuang Lo 《Corrosion Science》2007,49(4):1847-1861
The effect of selective dissolution on fatigue crack initiation of 2205 duplex stainless steel (DSS) was investigated in this study. In mixed sulfuric and hydrochloric acid aqueous solution, there existed two distinctly separated anodic peaks in the active-to-passive transition region of the polarization curve. Either ferritic or austenitic phase was selectively dissolved at each characteristic anodic peak potential. Under sinusoidal cyclic loading condition, however, selective dissolution did not assist fatigue crack initiation instead resulting in the elimination of stress concentration site in the selectively dissolving phase. As a consequence, under selective dissolution condition, fatigue crack initiated in the phase while its dissolution rate was lower with respect to the other constituent phase in the duplex stainless steel. The microstructural evolution of the corrosion fatigue crack initiation in 2205 DSS in the mixed sulfuric and hydrochloric acid solution is highlighted in this investigation.  相似文献   

13.
Fatigue behaviour in the very high cycle regime (VHCF) of 1010 cycles were investigated with a cast iron (GS51) under ultrasonic fatigue test system (20 kHz) in ambient air at room temperature with a stress ratio R = −1.

The influence of frequency was examined by comparing similar data generated on conventional servo hydraulic test systems. An advanced, high-speed, and high-sensitivity infrared imaging system was used to measure the temperature changes during ultrasonic fatigue test at various load levels caused by internal damping due to a very high frequency cycling. The temperature field on the surface specimen was determined by using a non-destructive measurement technique called infrared pyrometer. An infrared camera made up of a matrix of 320 × 240 detectors was used.

The S-N curves obtained show that fatigue failure occurred beyond 109 cycles, fatigue limit does not exist for the cast iron and there is no evidence of frequency effect on the test results. A detailed study on fatigue specimens subjected to ultrasonic frequency shows that the temperature evolution of the cast iron specimen is very evident, the temperature increased just at the beginning of the test, the temperature increased depending on the maximum stress amplitude. Under the current test conditions, the high cycle fatigue (VHCF) behaviour of the cast iron exhibited a typical fatigue crack growth process, that is, fatigue initiation takes place always at the surface graphite or subsurface void; the distinctive stable fatigue crack growth zone can be found around the fatigue crack initiation site, the change of fatigue initiation site from surface to subsurface is associated with the complex effects of applied maximum stress level, surface condition.

Under lower stress amplitude and high cycle condition, surface graphite fatigue initiation is predominantly depended on cyclic stress amplitude; subsurface void fatigue initiation is determined by maximum cyclic stress.

In the process of small crack propagation, the temperature in local plastic zone increase very sharply. The temperature field of ultrasonic fatigue specimen can be changed with the cooling condition; internal heating can accelerate surface fatigue crack initiation and propagation.

Fatigue properties in VHCF regime were studied for cast iron (GS51) at 20 kHz frequency and for the first time, crack initiation and propagation stages were analyzed using a high-sensitivity infrared camera. The new Paris's model for fish eye formation in the gigacycle fatigue were also confirmed by this study.  相似文献   


14.
Electrochemical investigation of crack initiation during corrosion fatigue of stainless steels in the passive state The corrosion fatigue behaviour of three stainless steels - ferritic (12% Cr), austenitic (type 316 Ti) and austenitic-ferritic (type 31803; Duplex stainless steel) - was studied under rotating bending moments in aqueous sulphuric acid of 30°C. An instrumental set-up for recording the transient currents of specimens during potentiostatically controlled corrosion fatigue is described. Based on this transient current signal technique, three stages on the corrosion fatigue process can be discerned. In the incubation period, small stochastic current transients are caused by the response of the passive layer to alternating stresses and environmental conditions. The appearance of sinusoidal current signals indicates crack initiation whereas the phase angle between a fixed marker - i.e. a light barrier signal -, and the anodic amplitude represents the site of initiating cracks. Finally, the crack growth period is characterized by an increasing cell current and steadily growing sinusoidal current signals caused by the interplay of microplastic and repassivation processes at the crack tip.  相似文献   

15.
The corrosion fatigue propagation behaviour of high strength low alloy Cr-Ni and Si-Mnsteels has been investigated in 3.5 %NaCl solution spryly at the frequencies of 0.1 and 5.5 Hz.It was shown that the fatigue crack initiation resistances of the two steels are significantly re-duced in salt spray;the fatigue crack growth rates of steels increase with the decrease of fre-quency and are much higher in salt spray than in air within low ΔK range.A critical stress in-tensity factor was observed for each steel and the crack growth stoppage will occur if the ΔKvalues are lower than it.It was found that the active dissolution makes great contribution tothe fatigue crack growth within low ΔK range.  相似文献   

16.
The strain-controlled low cycle fatigue properties were evaluated on specimens of HT250 gray cast iron (GCI) at room temperature. The material exhibited cyclic stabilization at a low strain amplitude of 0.1% and cyclic softening characteristic at higher strain amplitudes (0.15-0.30%). At a representative total strain amplitude (0.30%), the hysteresis loops of HT250 GCI were asymmetric with a large amount of plastic deformation in the compressive phases. Furthermore, the hysteresis loop became larger in both width and height with increasing total strain amplitude (from 0.10 to 0.30%), and tended to exhibit a clockwise rotation. The fatigue crack propagation mechanisms were different at various total strain amplitudes, where high stress concentration due to dislocation pile-up favored fatigue crack initiation in the examined HT250. Finally, the roughness-induced crack closure was a key to determine the crack growth rate as well as fatigue life.  相似文献   

17.
45碳钢低周疲劳与应力循环棘轮失效的实验研究   总被引:4,自引:0,他引:4  
杨显杰 《金属学报》2004,40(8):0-857
对调质处理的45碳素结构钢进行了应变循环低周疲劳实验以及应力控制棘轮失效实验.对于前者进行了带平均应变和不带平均应变的实验,以研究平均应变对低周疲劳特性的影响;对于后者研究了平均应力和应力幅值对棘轮失效的影响.应变循环实验表明:平均应变对循环饱和行为以及低周疲劳循环失效圈数并没有明显的影响,但对材料的循环初期循环塑性行为有影响.棘轮失效实验结果表明:当应力幅值较大而平均应力较小时,材料的棘轮失效主要归于较大塑性应变幅值引起的低周疲劳破坏;当平均应力较大而应力幅值相对较小时,材料的棘轮失效主要归于较大的棘轮应变引起的材料韧性破坏,其失效准则可以用最大单调极限应变来表征.  相似文献   

18.
通过采用不同应变幅控制,对不同变形量冷拉银铜合金进行室温低周疲劳试验.结果表明,随着应变幅的增大,滞后环面积也随之增大;随着循环周次的增加,循环应力逐渐降低,从而产生疲劳软化;加工率为38%的银铜合金循环周期大于加工率为19%的银铜合金循环周期;试样断裂后存在三个明显疲劳特征区:裂纹源、裂纹扩展区、瞬断区;银铜合金的裂纹扩展具有穿晶和沿晶两种方式.  相似文献   

19.
A new methodology is described for in situ characterization of fatigue damage accumulation using nonlinear ultrasonic measurements via analysis of the feedback signal of a closed-loop ultrasonic fatigue system. In the very high-cycle fatigue regime, ultrasonic nonlinearity increases with initiation and growth of a dominant, life-limiting fatigue crack. Based on the increase in the ultrasonic nonlinearity with fatigue cycling, crack initiation, small fatigue crack growth and fast crack growth regimes have been distinguished during cycling in specimens with different pore sizes tested at various stress amplitudes. The fraction of fatigue life spent in initiation of a life-limiting fatigue crack decreases with increasing stress amplitude. For a constant stress amplitude, the initiation life also decreases with increasing pore size. The present study also demonstrates the applicability of the methodology for fatigue crack growth studies from natural defects located internally or at the surface in smooth specimens.  相似文献   

20.
The S–N curves of 7A85-T7452 aluminum alloy in laboratory air and in neutral 3.5 wt% NaCl solution were obtained by axial fatigue tests. Results show that the detrimental effect of the aggressive solution was not noticeable at high-cyclic-stress regions, but the effect was significant at low-stress region. Corrosion fatigue mechanism was discussed by corrosion morphology analysis, fracture surface analysis and microstructure characterization. It was found that the corrosion fatigue crack commonly initialed at the localized intergranular corrosion site. TEM analysis showed that the microstructures of 7A85-T7452 aluminum alloy were characterized by fine and homogeneously distributed matrix precipitates, as well as continually distributed anodic grain boundary precipitates. The types of microstructures are the reason for its intergranular corrosion susceptibility. The corrosion fatigue process of 7A85 aluminum alloy in 3.5 wt% NaCl solution can be divided into four stages: the crack initiation stage, the stable growth stage with low and high growth rate and the final rupture stage. The sodium chloride solution mainly affected the crack initiation stage and the stable growth stage with low growth rate, and when the crack growth rate reached a threshold, the effect was reduced.  相似文献   

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