共查询到20条相似文献，搜索用时 15 毫秒
1.
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
2.
Improving the Fatigue Performance of the Welded Joints of Ultra-Fine Grain Steel by Ultrasonic Peening 总被引：2，自引：0，他引：2
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
3.
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
4.
Cun-jian MIAO Jin-yang ZHENG Xiao-zhe GAO Ze HUANG A-bin GUO Du-yi YE Li MA 《浙江大学学报(A卷英文版)》2013,14(1):31-37
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
5.
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
6.
A combined cycle fatigue （CCF） testing system with ultrasonic frequency component was developed toevaluate the CCF properties of S350 steel welded joints in this study. The fatigue testing results indicated that the S-Ncurves of CCF did not have fatigue limit, which agreed with those of pure high frequency fatigue of welded joints. TheS-N curves showed that the CCF strength of welded joints dropped greatly with the increasing interaction between highand low frequency fatigue loading. An approximation design method of CCF was presented using amplitude envelopeas the stress range. 相似文献
7.
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
8.
为获得路用水泥混凝土在高应力比作用下其疲劳可靠度的变化规律,首先推导了包括混凝土疲劳寿命在内的单调随机变量的概率密度,然后推导了 Miner 与 Chaboche-Zhao 疲劳损伤模型的概率密度. 借助室内疲劳试验结果,获得这 2 种模型的疲劳损伤概率密度函数. 最后,将荷载作用次数代入上述函数,从而获得水泥混凝土疲劳可靠度随荷载作用次数的变化规律. 结果表明: 随着荷载作用次数的增加,相同应力比下,疲劳可靠度从 100%逐渐衰减为 0%; 无论何种应力比,在荷载作用初期,疲劳可靠度均有一个较为稳定的阶段; 随着应力比的增加,该稳定阶段逐渐缩短,且可靠度为 0%时对应的荷载作用次数也减小; 在可靠度衰减阶段,对于相同荷载作用次数,应力比越高,则混凝土可靠度越低; 此外,Miner 疲劳损伤模型比Chaboche-Zhao 疲劳损伤模型偏安全. 相似文献
9.
一种腐蚀疲劳损伤的非线性累加演化模型 总被引：1，自引：0，他引：1
研究目的：提出一种新的腐蚀疲劳损伤演化模型,建立基于损伤演化的腐蚀疲劳寿命预测模型。创新要点：将应力腐蚀损伤与疲劳损伤非线性耦合,建立腐蚀疲劳损伤演化律,依托实验确定腐蚀疲劳损伤演化参数,形成基于损伤演化律的腐蚀疲劳寿命预测模型。研究方法：采用理论研究与实验验证相结合的研究方法。选取特定材料设计应力腐蚀实验,回归应力腐蚀门槛值应力和损伤参数（图2）;查阅疲劳实验数据建：立变幅疲劳损伤模型,将应力腐蚀损伤与变幅疲劳损伤非线性累加形成腐蚀疲劳损伤非线性演化模型。根据腐蚀疲劳实验结果,验证腐蚀疲劳损伤演化模型并确定非线性损伤累加参数（图5和6）,形成基于损伤演化律的腐蚀疲劳寿命预测模型。重要结论：从损伤力学角度,将材料的腐蚀疲劳损伤处理成应力腐蚀损伤与疲劳损伤的非线性累加,形成腐蚀疲劳损伤演化模型。结合LY12CZ铝合金的试验结果,验证了损伤演化模型的可行性。该方法可以为材料腐蚀疲劳的寿命评价研究提供新的思路。 相似文献
10.
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
11.
LI Yong-de LIU Yang-bo YANG Zhen-guo LI Guang-yi LI Shou-xin HUI Wei-jun WENG Yu-qing 《实验室研究与探索》2007,(10)
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
12.
为了提高高速货运列车转向架弹簧的耐疲劳性能,对两个炉号的棒状60Si2CrVAT弹簧钢用相同工艺热处理后,在MTS880材料试验机上进行了三点弯曲疲劳寿命对比试验,实验载荷采用阶梯式增加法;用扫描电镜对弹簧钢的疲劳断口和基体组织进行观察。疲劳实验结果表明,不同炉号的弹簧钢疲劳寿命相差很大。组织分析表明,疲劳寿命较低的弹簧钢中,淬火加热前存在颗粒状碳化物,奥氏体化时未溶入奥氏体而残留在淬火组织中,并在局部聚集,导致疲劳寿命降低。 相似文献
13.
薄片漏斗试样的应变等效换算与Zr-4合金疲劳寿命估算 总被引：1，自引：0，他引：1
完成了Zr-4合金薄片漏斗小试样的横向等幅应变疲劳试验;提出了薄片漏斗试样细腰部与薄片等直试样疲劳损伤等效的局部损伤等效假设;基于弹塑性有限元分析,建立了Zr-4合金薄片漏斗小试样横向测试应变向轴向应变转换的应变等效转换模型,该模型考虑了几何效应和泊松效应;结合实验结果,提出了用于Zr-4合金应变疲劳寿命估算的Manson-Coffin(M-C)模型。研究表明:薄片漏斗小试样及其应变等效转换模型可以有效应用于薄片金属材料的低周疲劳试验和寿命估算;国标推荐的应变换算公式应用于薄片漏斗小试样的Zr-4合金疲劳寿命估算会带来很大安全余量。 相似文献
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15.
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
16.
低周疲劳寿命预测模型分析 总被引：3，自引：0，他引：3
综合分析了几种低周疲劳寿命预测模型,特别是对能量法则的寿命预测模型进行了讨论。评述了各种不同预测方法的基本假设、特点和应用范围。叙述了各种低周疲劳寿命预测模型的计算步骤,并提出实际应用中应考虑的问题。该文对低周疲劳寿命预测,尤其是对航空高温合金具有较大的工程参考价值。文中所论述的三参数能量预测模型具有易懂、简捷的工程应用前景。 相似文献
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18.
Thermal fatigue (TF) is one of the most important factors that influence turbine’s life. This paper establishes a 3D solid-fluid
coupling model for a steady temperature analysis of a high-pressure turbine nozzle at different turbine inlet gas total temperatures
(TIGTTs). The temperature analysis supplies the temperature load for subsequent 3D finite element analysis to obtain the strain
values. Following this, the prediction of the TF life is made on the basis of equivalent strain range. The results show that
the strain increases with TIGTT, and the predicted TF life decreases correspondingly. This life prediction was confirmed by
one TF test. 相似文献
19.
采用周期浸润加速腐蚀试验的方法,对某型飞机42框横梁模拟件分组进行了不同时间的加速预腐蚀试验,并通过随机载荷谱下的疲劳试验获得了预腐蚀后模拟件的疲劳寿命。结果表明,在加速腐蚀时间不大于300小时的情况下,预腐蚀对42框横梁结构模拟件疲劳寿命的影响不明显。 相似文献
20.
发动机气缸盖是较易发生疲劳破坏的发动机零件之一,其机械疲劳强度与螺栓预紧力之间存在关系。利用Solidworks建立气缸的简化模型,导入Workbench中进行静力学分析：在Workbench中建立两个不同的载荷环境,利用组合求解功能对螺栓预紧力和气缸盖受到气缸内气体的最高爆发压力进行线性组合,完成非比例载荷的疲劳寿命计算,得到不同螺栓预紧力下的气缸盖疲劳寿命曲线,由此获知螺栓预紧力和气缸盖疲劳寿命之间的关系,这为合理选择螺栓预紧力提供了依据。 相似文献