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1.
Contrast tests were carried out to study the fatigue performance of the butt joints treated by ultrasonic peening, aiming at the improvement of ultrasonic peening treatment(UPT) on welded joints of a new material. The material is a new generation of fine grain and high purity SS400 steel that has the same ingredients as the traditional low carbon steel. The specimens are in two different states:welded and ultrasonic peening conditions. The corresponding fatigue testing data were analyzed according to the regulation of the statistical method for fatigue life of the welded joints established by International Institute of Welding(IIW). Welding residual stress was considered in two different ways: the constant stress ratio R = 0.5 and the Ohta method. The nominalstress-number (σ-N) curves were corrected because of the different plate thickness compared to the standard and because there was no mismatch or angular deformation. The results indicated that: 1 ) Compared with the welded specimens, when the stress range was 200 MPa, the fatigue life of the SS400 steel specimens treated by ultrasonic peening is prolonged by over 58 times, and the fatigue strength FAT corresponding to 106 cycles is increased by about 66%; 2) As for the SS400 butt joint ( single side welding double sides molding) , after being treated by UPT, the nominal S-N curve (m = 10) of FAT 100 MPa(R =0.5) should be used for fatigue design. The standard S-N curves of FAT 100 MPa (R = 0.5, m = 10) could be used for fatigue design of the SS400 steel butt joints treated by ultrasonic peening.  相似文献   

2.
A method and procedure of high cycle fatigue life prediction for helicopter transmission system tail gearbox casing ispresented, including fatigue test load, three parameters S-N curve, reduction factor and cumulative damage law. According to thefatigue test results, the design load spectrum and the three parameters S-N curve, a fatigue life prediction of the tail gearboxcasing of a helicopter is performed as an example.  相似文献   

3.
该文用USF-2000超声疲劳实验机研究了50CrV4高强度弹簧钢的超高周疲劳性能,并用Quan-ta600扫描电子显微镜对疲劳断口形貌进行了观察。研究结果表明,所有的疲劳裂纹都是从内部或亚表面的夹杂物处萌生,能谱分析表明夹杂物的成分主要是钙铝的氧化物,并且测量的夹杂物的尺寸超过了临界夹杂的尺寸,因此在疲劳断口上并没有观察到夹杂物周围的光学暗区(ODA)。在109的循环周次内,50CrV4钢存在疲劳极限,其S-N曲线的形式为传统的疲劳极限型。  相似文献   

4.
针对机采油井油管经常发生疲劳断裂的问题,加工了J55油管疲劳试件,通过成组多级疲劳试验法,获得了J55油管高周疲劳分组试验数据。通过疲劳寿命的参数估计和疲劳寿命的分布类型检验,获得了J55油管在不同轴向应力水平下的疲劳寿命、分布规律和P-S-N曲线。结果显示,J55油管的疲劳寿命服从对数状态分布,其S-N曲线服从一般金属的疲劳S-N曲线形式。在疲劳寿命一定时,欲获得较高的可靠性,需大幅度降低油管的疲劳应力。  相似文献   

5.
本文对蜂窝纸板疲劳性能进行了尝试性的试验研究,得到了蜂窝纸板的S-N曲线,同时了解了频率对蜂窝纸板疲劳寿命的影响,从而对蜂窝纸板包装运输方案的设计提供一定的依据。  相似文献   

6.
在轴向承载十字焊接头疲劳试验的基础上,用一种新的有限元数值计算模型,并考虑多种影响因素的情况下拟合了两种裂纹类型的应力强度因子表达式,从而为焊接件的疲劳强度研究提供了有益的途径.  相似文献   

7.
Cold-stretched pressure vessels from austenitic stainless steels(ASS) are widely used for storage and transportation of liquefied gases,and have such advantages as thin wall and light weight.Fatigue is an important concern in these pressure vessels,which are subjected to alternative loads.Even though several codes and standards have guidelines on these pressure vessels,there are no relevant design methods on fatigue failure.To understand the fatigue properties of ASS 1.4301(equivalents include UNS S30400 and AISI 304) in solution-annealed(SA) and cold-stretched conditions(9% strain level) and the response of fatigue properties to cold stretching(CS),low-cycle fatigue(LCF) tests were performed at room temperature,with total strain amplitudes ranging from -.4% to -.8%.Martensite transformations were measured during the tests.Comparisons on cyclic stress response,cyclic stress-strain behavior,and fatigue life were carried out between SA and CS materials.Results show that CS reduces the initial hardening stage,but prolongs the softening period in the cyclic stress response.Martensite transformation helps form a stable regime and subsequent secondary hardening.The stresses of monotonic and cyclic stress-strain curves are improved by CS,which leads to a lower plastic strain and a much higher elastic strain.The fatigue resistance of the CS material is better than that of the SA material,which is approximately 1?03 to 2?04 cycles.The S-N curve of the ASME standard for ASS is compared with the fatigue data and is justified to be suitable for the fatigue design of cold-stretched pressure vessels.However,considering the CS material has a better fatigue resistance,the S-N curve will be more conservative.The present study would be helpful in making full use of the advantages of CS to develop a new S-N curve for fatigue design of cold-stretched pressure vessels.  相似文献   

8.
在零构件疲劳失效的分布规律的基础上,对多种零构件疲劳强度可靠性实验数据进行统计分析,充分利用疲劳S-N曲线的对数线性关系,通过引入静态机械性能参数断裂真应力和疲劳循环基数两个特征值点,较好地实现了零构件制造工艺性能参数与疲劳特性结合,获得一种零构件疲劳可靠性工程评价方法。本文还报告了在连杆、转向节、混凝土道路小样零构件的疲劳强度可靠性评估工作中的试验、统计、应用情况。本文方法具有简单、实用、易于推广的特点。  相似文献   

9.
Fatigue tests were conducted on tapered plain concrete prism specimens under triaxial constant-amplitude tension-compression cyclic loading. The low stress of the cyclic loading was taken as 0.2fc and the upper stress ranged from 0.20ft to 0.65ft. Three constant lateral pressures were 0.1fc, 0.2fc and 0.3fc respectively. Based on the results, the three-stage evolution nile of the fatigue stiffness, maximttm(minimum) longitudinal strain and damage were analyzed, and a unified S-N curve to calculate fatigue strength factors was worked out. The results show that the fatigue strength and fatigue life under triaxial constant-amplitude tension-compression cyclic loading are smaller than those under uniaxial fatigue condition. Moreover, the secondary strain creep rate is related to the fatigue life, a formula for describing their relation was derived. The investigation of this paper can provide information for the fatigue design of concrete structures.  相似文献   

10.
针对汽车疲劳驾驶提醒装置价格高、安装复杂的问题,提出了一种疲劳报警的新方法———开发一种软件实现智能手机疲劳驾驶提醒功能;提出对PERCLOS、眨眼频率、眼睛闭合速度等四种疲劳判断方法进行加权求和的判断法,提高了疲劳判断的精度和灵敏度;成功制作了软件图标、窗体和报警逻辑.  相似文献   

11.
LZ50车轴钢疲劳裂纹扩展试验研究   总被引:1,自引:0,他引:1  
完成了连铸和模铸LZ50车轴钢疲劳裂纹扩展试验,得到了两类LZ50车轴钢的疲劳裂纹扩展曲线。采用Paris公式和另一种全范围表达式研究了两种铸造工艺下LZ50车轴钢的疲劳裂纹扩展规律。研究结果表明:Paris公式仅能描述LZ50车轴钢疲劳裂纹稳定扩展阶段的规律;全范围表达式对LZ50车轴钢的全范围疲劳裂纹扩展规律描述较好,且得到的疲劳裂纹扩展门槛值与试验曲线得到的门槛值接近,相对误差小于3%;连铸LZ50车轴钢的疲劳裂纹扩展速率门槛值低于模铸LZ50车轴钢,其疲劳裂纹扩展性能不如模铸LZ50车轴钢。  相似文献   

12.
选取两种不同规格的玻璃纤维土工格栅,首先进行大量的静载强度试验,在此基础上,进行了不同应力水平下的恒幅疲劳试验,研究玻璃纤维土工格栅的P-S-N曲线、滞回曲线以及应变与循环次数的关系。结果表明:玻璃纤维土工格栅的应力-寿命关系可以用幂函数来拟合,其疲劳性能具有明显的脆性材料的特性,疲劳寿命较低;玻璃纤维土工格栅的应变-循环比特性曲线呈现出三阶段变化规律,第一阶段为循环的20%之前,应变增加较快,第二阶段为循环的20%~80%之间,应变变化平缓,第三阶段为循环的80%之后,应变剧增直至破坏。  相似文献   

13.
对单点与两点拉剪点焊试样分别进行了疲劳试验,观测了疲劳裂纹的形状和萌生位置,通过动态响应实验测量了疲劳破坏过程中固有频率的变化。对比两种试样的载荷幅寿命关系,认为两点试样的承载能力约为单点试样的两倍。有限分析了两种试样失效时的固有频率比,基于所测量的固有频率,确定了单点与两点试样疲劳失效时的频率比,对比了疲劳过程中的损伤。  相似文献   

14.
研究了LZ50车轴钢的循环相关特性,循环疲劳特性及循环应力-应变关系。试验结果表明:LZ50车轴钢的循环疲劳特性曲线及循环应力-应变曲线很好地符合双对数线性关系;其循环相关特性表现为先循环软化,稳定后又发生循环硬化,而且循环软化和循环硬化的程度随控制应变的不同而不同。  相似文献   

15.
复杂飞机结构裂纹萌生寿命确定的工程方法   总被引:1,自引:0,他引:1  
采用静拉伸应变测量试验的方法,确定了典型飞机复杂结构在载荷作用下的应变分布,并准确判断出其疲劳危险部位。对典型飞机复杂结构模拟件进行了等幅加载疲劳试验,并在疲劳试验过程中采用着色探伤方法测得了疲劳裂纹扩展数据。在此基础上,提出并建立了一种适用于确定复杂结构疲劳裂纹萌生寿命的工程方法,包括疲劳裂纹萌生寿命反推法和含有不确定寿命样本的统计推断方法。根据该方法对试验样本疲劳数据进行处理得出了裂纹萌生中值寿命及其在95%置信水平下的单侧置信下限。  相似文献   

16.
根据高炉炉壳生产实际,分别使用气电立焊和埋弧自动横焊两种焊接工艺对50 mm厚的BB503型炉壳用钢板进行焊接,对焊缝进行外观检查、无损探伤,对焊接接头进行拉伸、侧弯、冲击、硬度等性能测试,并对焊接热影响区的显微组织进行了观察和分析。结果表明,BB503炉壳用钢的气电立焊和埋弧自动横焊焊接接头抗拉强度和冲击吸收功均大于母材,具有优良的综合力学性能;焊缝区及热影响区的显微维氏硬度分布和热影响区的组织均匀性均显著优于传统的CO2气体保护焊和手工电弧焊接头。气电立焊和埋弧自动横焊工艺可以替代CO2气体保护焊和手工电弧焊工艺用于高炉炉壳焊接制造。  相似文献   

17.
焊接接头的疲劳强度是焊接结构能否承受动载荷的关键指标,它关系到焊接技术在工程中的应用.采用改善焊缝几何形状、减少消除应力、低相变点焊条、覆盖涂层等是提高焊接接头疲劳强度的有效方法.  相似文献   

18.
对针阀体使用中发生球头部位开裂的原因进行了硬度测定及金相检验等。结果表明,由于渗碳过程中,球头部位的尖角效应,使得该处碳势过高,导致球头部位出现网状碳化物,碳化物网状分布破坏了基体的连续性,从而降低了球头部位的疲劳强度,在交变高压油的作用下萌生微裂纹,并不断扩展导致球头出现开裂。  相似文献   

19.
Extensive research has shown that externally bonded carbon fiber reinforced polymer (CFRP) laminates are particularly suitable for improving the fatigue behavior of reinforced concrete (RC) beams. This paper presents the research on flexural rigidity evolvement laws by testing 14 simple-supported RC beams strengthened with carbon fiber laminates (CFL) under cyclic load, and 2 under monotone load as a reference. The cyclic load tests revealed the peak load applied onto the surface of a supported RC beam strengthened with CFL is linear to the logarithm of its fatigue life, and the flexural rigidity evolvement undergoes three distinct phases: a rapid decrease from the start to about 5% of the fatigue life; an even development from 5% to about 99% of the fatigue life; and a succedent rapid decrease to failure. When the ratio of fatigue cycles to the fatigue life is within 0.05 to 0.99, the flexural rigidity varies linearly with the ratio. The peak load does not affect the flexural rigidity evolvement if it is not high enough to make the main reinforcements yield. The dependences of the flexural rigidity of specimens formed in the same group upon their fatigue cycles normalized by fatigue life are almost coincident. This implies the flexural rigidity may be a material parameter independent of the stress level. These relationships of flexural rigidity to fatigue cycles, and fatigue life may be able to provide some hints for fatigue design and fatigue life evaluation of RC member strengthened with CFL; nevertheless the findings still need verifying by more experiments.  相似文献   

20.
一种新的可用于混凝土疲劳研究的非线性累积损伤模型   总被引:3,自引:0,他引:3  
研究混凝土疲劳问题的主要困难之一,就是混凝土疲劳损伤的累积速度与不同强度循环荷载的作用次序有关,且是非线性的。但通常 的一些非线性损伤模型却不能反映荷载作用次序的影响,为了解决此问题和混凝土结构在长期不稳定循环荷载作用下的疲劳问题,我们在Miner线性累积损伤模型的基础上提出了一个新的非线性累积损伤模型,通过两个 疲劳损伤实例的计算证明了该模型不仅能够反映出不同强度应力水平先后作用次序对疲劳损伤演变情况的影响,而且保留了Miner模型概念明确,使用方便的优点,当通过试验得到一组有关曲线之后,不稳定循环荷载作用的混凝土疲劳累积损伤计算将变得异常简单,极便于在工程设计中采用。  相似文献   

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