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1.
为了获得火车轮钢材的疲劳设计数据,对K型和B型火车轮钢材分别进行了疲劳性能试验,用升降法试验测定了2种钢材的疲劳极限,使用成组法试验对2种车轮钢材在三级应力水平下测试了其疲劳寿命,运用可靠性原理比较了2种不同材质、不同结构对车轮疲劳性能的影响。结果表明,K型车轮的疲劳寿命分布集中,可靠性高;B型车轮的疲劳寿命分布相对分散。结合升降法所得的疲劳极限值和成组法试验数据,计算了2种车轮钢材的S—N曲线方程;运用概率方法计算了2种车轮钢材的P—S—N方程,为2种车轮制定设计标准和安全寿命评估提供理论依据。  相似文献   

2.
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   

3.
使用通用斜率法建立16Mn R的S-N曲线,借助ANSYS软件,计算出危险点的应力幅,分别根据钢制压力容器—分析设计标准公式和ANSYS后处理,求得球罐的疲劳寿命,为工业上计算寿命提供了高效的计算模式.  相似文献   

4.
动态径向疲劳试验是评测铝合金车轮安全性的三大性能试验之一,采用有限元方法实现试验的仿真分析和疲劳寿命预测,能够减少物理试验次数,提高车轮设计研发效率.基于ANSYS Workbench平台,考虑轮胎充气压力对仿真结果的影响,建立了试验仿真有限元模型,实现了15×6JJ铝合金车轮动态径向疲劳试验的仿真分析,运用S-N疲劳分析方法得到了径向试验载荷下车轮的疲劳寿命及损伤分布情况.研究结果表明,轮缘、胎圈座和辐条根部后侧是疲劳损伤的主要集中部位,需要进行设计改进.  相似文献   

5.
结构细节疲劳额定值DFR及其试验方法的研究   总被引:1,自引:0,他引:1  
该文介绍了使用细节疲劳额定值(DFR)对结构进行疲劳分析和对疲劳品质进行评估的基本原理,讨论了细节疲劳额定值与标准S-N曲线的关系.通过试验探索,给出了有关细节疲劳额定值试验方法的一些实用建议,并推导了疲劳损伤的折算公式,通过铝合金螺接试件试验验证了所提出的试验方法和疲劳损伤的折算公式.  相似文献   

6.
采用超声疲劳试验技术对一种高强汽车弹簧用钢进行了超高周疲劳试验。采用扫描电镜对失效试样进行断口分析,并对断口特征区域尺寸进行了测量。结果表明:在0~10~6循环周次内失效的试样断口起源萌生于试样表面;而在10~6~10~9循环周次内失效的试样断口萌生于试样次表面或内部,且断口呈现鱼眼状特征,随着夹杂物处应力强度因子幅的减小,疲劳寿命增加;而粒状亮面处的应力强度因子幅并不随寿命变化而明显变化,基本为一常数。弹簧钢的超高周疲劳S-N曲线呈现二次下降型特性,其S-N曲线的形态特征跟试样夹杂物尺寸密切相关。  相似文献   

7.
气门弹簧是内燃机配气机构中气门组件的重要组成部分,它能确保气门组件的正常工作。为对某柴油机气门弹簧工作过程中的应力分布和疲劳寿命进行研究,利用MSC.Patran有限元软件对气门弹簧进行有限元分析,得出气门弹簧在各种工况下的应力分布情况,然后对其进行模态分析以检验共振情况,校核分析结果和设计要求。运用ADAMS对配气机构进行动力学仿真,导出了疲劳分析所需要的载荷谱。然后运用疲劳分析软件Fatigue对气门弹簧进行疲劳寿命分析,评估进、排气门弹簧的疲劳寿命。最后搭建气门弹簧试验台架,进行试验研究,验证疲劳寿命理论分析结果。  相似文献   

8.
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   

9.
单点与双点拉剪点焊试样的疲劳特性比较   总被引:1,自引:0,他引:1  
对单点与两点焊拉剪点焊疲劳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,分析了两种试样的疲劳性能。通过有限元模型分析了同等载荷作用下两种试样的变形,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。基于此,使用单点试样的载荷幅寿命曲线,预测了两点试样的疲劳寿命,寿命预测结果与实验寿命结果一致。  相似文献   

10.
采用数理统计的方法,分析了整体铸造铝合金材料的疲劳特性,求出其在一定可靠度和一定置信度下的疲劳强度极限及其标准偏差.以2A12铝合金标准试件为研究对象,首先开展了预腐蚀疲劳试验,计算得到了地面腐蚀影响系数曲线,即C(t)曲线,通过模拟腐蚀疲劳交替过程,结合Miner理论,计算得到了其理论寿命.同腐蚀疲劳交替试验结果进行对比,发现二者寿命差别较为明显,在交替周期为4天时,二者之差能达到25%以上.进一步通过扫描电镜观察,发现试件在预腐蚀疲劳试验条件下存在明显的小孔形核,同疲劳试验的断裂过程类似;在腐蚀疲劳交替作用下的腐蚀形貌呈不规则的纹理.最后分析了产生上述差异的原因.  相似文献   

11.
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   

12.
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   

13.
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   

14.
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   

15.
16.
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   

17.
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   

18.
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   

19.
A newly developed pure rolling fatigue test rig with three contact points for bearing balls was used to perform rolling contact fatigue (RCF) tests. The fatigue properties of GCr15 steel balls and two kinds of Si3N4 ceramic balls (GSN-200 and NBD-200) produced with different technologies were compared. Ball surfaces were examined after failure with optical microscope and scanning electron microscope (SEM). It was identified by tests that the failure mode of ceramic balls was surface spall. The main factor of ceramic ball failure was principal tensile stress. Life tests data, summarized in accordance with the Weibull theory, showed that the life of GSN-200 balls was close to that of GCr15 balls, whereas the life of NBD-200balls was much longer than those of GSN-200 and GCr15. Under the same working condition, the temperature rise of all ceramic balls was lower than that of steel balls, and their crack propagation rates were slower than that of steel balls.  相似文献   

20.
在役管道材料的低周疲劳性能测试   总被引:1,自引:0,他引:1  
对在役输油管道的X60材料进行了低周疲劳性能测试。拟合得到管道材料的应变-寿命曲线公式,依据管道材料的低周疲劳性能,预测该输油管道的疲劳寿命,为管道的安全维护提供了依据。  相似文献   

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