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《中国造船》2020,(1)
船舶纵骨节点往往存在焊接缺陷,焊接缺陷将引发裂纹,大大降低构件的疲劳性能。本文基于断裂力学理论,将焊接缺陷等效成半椭圆型表面裂纹,采用FRANC3D和ABAQUS联合仿真的方法,研究带初始裂纹的船舶舭部纵骨与横舱壁连接节点裂纹的扩展寿命评估方法。分析了初始裂纹位置、形状、裂纹面角度对裂纹扩展寿命的影响规律。并根据纵骨节点试验中的初始缺陷的位置,采用此联合仿真方法模拟了裂纹扩展过程。结果表明初始裂纹位置、形状对扩展寿命影响较大,随着初始裂纹向腹板靠近,寿命变短,裂纹扩展寿命随着初始裂纹形状比的增大而增大。初始裂纹角度对疲劳寿命影响不明显,随着角度增大,寿命变长。通过对试验中初始缺陷的等效简化,在裂纹稳定扩展阶段,仿真得到的裂纹扩展寿命与试验结果吻合较好。 相似文献
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采用试验形式研究矩形扶强材和削斜扶强材结构形式的某铝合金船体纵骨贯穿舱壁结构疲劳性能。首先建立舱段结构的有限元模型(目标船纵骨采用6082铝合金,其他部分采用5083铝合金材料),确定载荷工况并计算分析2种扶强材结构在相应载荷水平下的应力分布状态。在此基础上,设计并开展实际板厚4点弯曲疲劳模型试验,获得试验模型在不同载荷水平下的疲劳失效循环次数,根据试验测得数据得到2种扶强结构形式的S-N曲线。试验结果表明,矩形扶强材形式的纵骨贯穿舱壁结构疲劳性能优于削斜扶强材形式,该结论可为舰船上纵骨贯穿舱壁结构处节点形式的设计以及5083、6082铝合金焊接结构形式(T型焊接和趾端焊接)的疲劳强度评估提供依据。 相似文献
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《船海工程》2019,(6)
综合考虑散货船设计面临的结构轻量化需求和纵向舱口围板趾端和舱口角隅容易产生裂纹的问题,以21万t散货船为例,提出一种连续的纵向舱口围板结构设计方案。结合HCSR规范,采用有限元分析方法,研究连续纵向舱口围板对整个主甲板区域重量以及对舱口角隅应力和疲劳的影响,结果表明,连续纵向舱口围板方案在散货船上是可行的,该方案可使整个甲板区减重41.54 t,而且舱口角隅处的应力水平和疲劳强度比传统方案有所改善,应力水平下降4.69%,疲劳寿命提高37.64%。与传统的不连续纵向舱口围板相比,连续纵向舱口围板设计方案可实现散货船结构轻量化,消除了舱口围板趾端疲劳裂纹隐患,降低了舱口角隅应力水平。 相似文献
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为了研究矩形扶强材和削斜扶强材结构形式的某铝合金船体纵骨贯穿舱壁结构疲劳性能,对此进行了试验研究。首先建立舱段结构的有限元模型(该目标船纵骨采用6082铝合金,其他部分采用5083铝合金材料),确定载荷工况并计算分析两种扶强材结构在相应载荷水平下的应力分布状态。在此基础上,设计并开展了实际板厚四点弯曲疲劳模型试验,获得了试验模型在不同载荷水平下的疲劳失效循环次数,并且根据试验测得数据得到了两种扶强结构形式的S-N曲线。试验结果表明矩形扶强材形式的纵骨贯穿舱壁结构疲劳性能优于削斜扶强材形式,该结论可为舰船上纵骨贯穿舱壁结构处节点形式的设计以及5083与6082铝合金焊接结构形式(T型焊接和趾端焊接)的疲劳强度评估提供依据。 相似文献
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复杂载荷作用下潜艇结构疲劳裂纹扩展预报方法 总被引:4,自引:0,他引:4
统一疲劳裂纹扩展模型是课题组在McEvily模型基础上提出来的,它将疲劳裂纹扩展的3个扩展区域统一起来,并能解释更多的疲劳试验现象.本文介绍了统一疲劳裂纹扩展模型的基本表达式.将此模型与焊缝焊趾表面裂纹应力强度因子的计算方法结合起来,探讨复杂载荷作用下潜艇结构疲劳裂纹扩展预报方法.将服从Weibull分布的随机载荷系列编排为升序、降序载荷谱及随机载荷谱,预报潜艇锥柱结合壳焊缝焊趾处表面裂纹在3种载荷谱下的疲劳裂纹扩展情况,并分析随机载荷谱下载荷次序效应及初始裂纹尺寸对疲劳裂纹扩展行为的影响.结果表明,载荷次序效应对潜艇结构疲劳寿命的影响很明显,且合理的确定初始裂纹尺寸对潜艇结构的疲劳寿命预报是非常重要的. 相似文献
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Fatigue crack propagation under the biaxial tensile loading, which loading directions are normal and parallel to the initial crack position, is highlighted in this study. Most of in-service structures and vessels are subjected to many types of loading. Generally, these loadings have different axial components with different phases. However, the structural integrities of structures and vessels are evaluated according to design codes based on theoretical and experimental investigations under a uniaxial loading condition. Most of these codes are based on the S–N curves approach. An approach that does not use S–N curves has been favored by researchers, with the fracture mechanics approach preferred for evaluating the fatigue life of structures. An advanced fracture mechanics approach was developed based on the Re-tensile Plastic zone Generating (RPG) stress criterion for fatigue crack propagation. In this study, fatigue crack propagation tests under biaxial loading with six different phase and loading conditions are performed and the effect of the phase difference under biaxial loading is evaluated. A numerical simulation method of fatigue crack propagation based on the RPG stress criterion under different biaxial loading phase conditions is presented and compared to measured data. 相似文献
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根据应力幅长期分布的Weibull分布假设及结构材料疲劳的S-N曲线和线性累积损伤Miner准则,使用数值分析与解析相结合的混合法对34000DWT大潮型散货船结构进行了分析计算,结果令人满意,证实本文介绍的方法解决船体结构在疲劳载荷作用下疲劳寿命估算的实用方法。 相似文献
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Creep and fatigue are involved in the loading of deep manned submersible, which is a rather complex variable amplitude pattern. Dwell effects resulting in lower life than pure fatigue are observed in the prior experimental research while no proper prediction methods are available to explain the phenomenon. Recently, the authors proposed a modified crack growth rate model to explain the creep effect under the cyclic loading which is validated for the crack growth of some titanium alloys under cyclic creep loading, however, its application is restricted to the condition where lots of parameters have to be determined based on many experiments and it is not very convenient in the material selection and primary design stage of a component. In this paper, a simplified prediction model for the load pattern of constant amplitude cyclic loading is proposed aiming at one of the most applicable materials for the pressure hull of submersibles, Ti–6Al–4V ELI. The method can be easily used to estimate the life of the pressure hull based on two series of basic mechanical properties of the material and validated by the modified crack growth rate model with parameters determined by large amounts of experimental data. 相似文献
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具初始裂纹钢桥梁焊接构件疲劳裂纹扩展和疲劳寿命计算 总被引:1,自引:1,他引:0
钢桥梁构件因焊接缺陷或者在疲劳应力交互作用下萌生裂纹,钢桥梁构件因存在初始裂纹大大地降低焊接构件的疲劳性能.文中考虑到焊接构件往往会存在初始缺陷,研究了含初始缺陷的桥梁焊接构件的疲劳分析方法.在已有的大量含裂纹构件的疲劳实验工作基础上,结合课题组所做的焊接构件疲劳实验资料,假设初始裂纹焊接构件在疲劳裂纹扩展过程中裂纹形状保持为半椭圆形状;针对桥梁构件实际受力特征,由钢桥梁构件的高周疲劳损伤演化方程入手,考虑初始裂纹条件下裂纹前缘的损伤区的存在及其对裂纹扩展的影响,采用虚拟裂纹扩张方法推导了适用于钢桥梁构件的疲劳裂纹扩展分析的疲劳裂纹扩展率公式,建议了裂纹扩展和疲劳寿命数值计算方法.采用文中的计算方法,研究了已有的钢桥梁结构焊接构件疲劳实验的裂纹扩展过程和疲劳寿命的计算.计算结果表明:裂纹的扩展过程中裂纹的深度和表面半长度之比a/c是一个变化的数值,且在一定的a0/t0条件下,随着a0/c0的增加,循环次数逐渐增大. 相似文献
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疲劳是船体损坏的主要因素之一,在设计建造阶段提高结构物疲劳寿命具有重要意义。结合船舶在建造和营运中的经验与反馈,以船级社共同规范为指导,对散货船船体结构的疲劳分析进行了探讨。分析了二维情况下的纵骨疲劳,同时利用三维有限元方法对船体主要支撑构件的疲劳强度进行了分析和总结,对影响疲劳强度的一些关键因素进行了讨论。 相似文献
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金属疲劳裂纹扩展率曲线与S-N曲线之间的关系 总被引:3,自引:0,他引:3
目前有两种不同的理论用于预报金属结构的疲劳寿命。一种是基于S-N曲线的累积疲劳损伤理论,另一种是基于裂纹扩展率曲线的疲劳裂纹扩展理论,如果都把一个构件的最终断裂作为疲劳破坏的定义,则S-N曲线和裂纹扩展率曲线均是反映金属在疲劳载荷作用下的基本材料特性。尽管在过去这两种曲线是分别测试的,但它们之间应该存在一些相互关系。本文的主要目的就是讨论它们之间的关系。基于S-N曲线的一个一般表达式和裂纹扩展率曲线的一个有代表性的表达式,本文建立了两种曲线之间的一个正式关系,这表明只需要测试一种曲线,而另一种曲线就可以根据已有的试验结果导出。文章以一个中央裂纹平板作为例子,演示了如何根据一种曲线推导另一种曲线。 相似文献
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基于散货船共同结构规范(CSRBC)的热点应力法,对一艘30000t级散货船内底板与底凳的斜板相交处进行了疲劳强度分析。通过对疲劳热点位置建立精细网格模型,采用中国船级社开发的软件CCS-Tools及英国劳氏船级社开发的SHIPRIGHT进行了热点应力分析及疲劳寿命计算。另外,还介绍了采用电子表格计算疲劳寿命的方法。 相似文献
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Beom-Seon Jang Hisashi Ito Kyung-Su Kim Yong-Suk Suh Hyun-Tae Jeon Young-Soo Ha 《Journal of Marine Science and Technology》2010,15(2):176-189
Predicting fatigue crack growth after its detection during in-service inspection is necessary to prevent a loss of serviceability,
such as the oil and/or water tightness of critical compartments. This paper focuses on the most typical fatigue cracks that
start at the weld joint between a flat bar stiffener on a transverse web frame and the flange of a longitudinal stiffener
on a bottom plate or inner bottom plate. An experiment is carried out to observe the fatigue crack propagation for two kinds
of flat bars at the abovementioned connection. The experimental results, especially the surface crack growth on the flange
(which dominates during the total fatigue life of the longitudinal stiffener), are compared with crack growth curves predicted
using a few existing formulas. Based on the comparative study, a formula that shows the best agreement with the experiment
results is selected. Weld toe magnification factors for the web stiffener are computed from the crack propagation rates measured
in the experiment, and two equations for the magnification factors versus crack depth are developed for two types of web stiffeners.
The selected existing formula and the proposed equations are applied to two connections at the inner bottom and side longitudinal
bulkhead of an LNG carrier. The equivalent stress approach based on a long-term distribution is employed to avoid the complexity
involved in dealing with the actual stress history. Using this prediction, the remaining service life until an oil or water
leakage occurs at a tank boundary can be estimated when a fatigue crack at the connection is detected. 相似文献