共查询到19条相似文献，搜索用时 750 毫秒
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吴文江郑明军高占凤 《石家庄铁路职业技术学院学报》2015,(4):57-61
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
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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
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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
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为了研究钢纤维自密实混凝土的弯曲疲劳性能,采用威布尔函数对疲劳寿命进行了概率分析,建立了在不同失效概率下的P-S-N疲劳方程,对钢纤维自密实混凝土的疲劳性能进行了分析。结果表明,钢纤维自密实混凝土的疲劳寿命符合两参数威布尔分布,与普通混凝土相比,钢纤维自密实混凝土的疲劳性能明显增强。 相似文献
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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
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根据疲劳应力理论对振动横梁进行了疲劳应力分析,并利用有限元软件Workbench对振动横梁进行了疲劳应力仿真,得到它在正常工作状态下的应力及安全系数分布图。在满足疲劳寿命要求情况下对振动横梁进行了最大循环应力分析,结果表明,振动横梁的疲劳特性符合寿命要求。 相似文献
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《西安文理学院学报》2016,(2)
减振器座是车身结构重要部分之一,主要承受来自悬架系统的垂向载荷.对某车型在路试工况中后减振器座发生了轻微裂纹为研究对象,而后期提升整车综合性能需降低减振器阻尼系数,分析路试中减振器阻尼系数,车辆配重参数对减振器座疲劳寿命的影响.结合CAE将减振器座模型加载上跳工况获得载荷大小做静力学分析,计算应力载荷分布并确定应力敏感点.通过应变计获得不同减振器阻尼和车辆配重下的道路载荷谱,确定减振器座开裂原因,并提出在减振器座上增加加强筋改进方案.最后经过路试工况验证,使用效能可靠. 相似文献
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对高温合金材料GH4169加工成的拉扭薄壁管试样在650℃下进行了多轴变幅疲劳试验,利用有限元分析软件计算各种加载情况下薄壁管的应力应变场,并通过对加载特殊位置处应力、应变的计算结果进行分析和比较,确定出主导材料疲劳损伤的危险点,为以后薄壁管试件的寿命预测奠定基础。 相似文献
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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
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选择某企业选矿厂正在使用的湿式格子型球磨机 MQG2700×2100筒体进行结构分析,并对其进行模型简化,推导了其基本动力学方程,对设计极限状态和使用极限状态进行极限强度分析。并通过 PRO/Engineer 建立了 MQG2700×2100湿式格子型球磨机三维模型,利用有限元分析软件 ANSYS 对筒体部分进行固有振动特性分析和动力响应特性分析,通过应力、变形分析,得出危险工况下的应力及其变形。 相似文献
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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
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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
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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
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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
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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