共查询到19条相似文献,搜索用时 421 毫秒
1.
在老龄化引起的船舶结构安全性问题中,裂纹损伤是结构强度衰减的一个重要因素。文章采用逐步加载法对含裂纹损伤的加筋板压缩剩余极限强度进行试验研究。设计六种典型的穿透裂纹损伤加筋板,对损伤试件进行轴向压缩试验。通过改变裂纹尺寸、位置及倾角参数并根据试验观测结果,探讨了不同裂纹参数下加筋板的屈曲破坏特点和对剩余极限强度影响。试验结果表明,不同的裂纹长度以及裂纹位置改变加筋板结构承载力的分布,影响结构应力应变场,进而改变其失效崩溃模式;倾角为45°的裂纹相对于垂直于加筋的裂纹对加筋板结构的剩余极限强度影响较小,此外初始缺陷对结构的剩余极限强度的影响也不容忽视。 相似文献
2.
运用非线性有限元软件ANSYS,研究铝质船舶加筋板在单轴拉—压循环载荷下的极限强度特性,重点讨论铝质加筋板热影响区的分布方式、热影响区的范围大小、不同循环载荷历程对铝质加筋板极限强度的影响,所获结果对铝质加筋板的设计与制造具有一定的参考价值。 相似文献
3.
为了快速评估含船冰碰撞凹陷损伤下加筋板在轴向压缩载荷作用下的极限强度,本文采用非线性有限元法对低温凹陷损伤加筋板的极限强度进行研究。根据EH36钢在低温下的材料力学性能试验,通过折减因子评估法,基于完整加筋板在轴向压缩下极限强度的经验公式,提出以加筋板柔度和加筋板壳板柔度为变化参数,采用最小二乘法拟合折减系数,得到低温含凹陷损伤加筋板剩余极限强度的经验公式。结果表明,相比于凹陷长度和凹陷深度,凹陷宽度对加筋板极限强度的影响较大;对比分析凹陷损伤加筋板极限强度的经验公式和有限元法的计算结果,误差较小,验证了船冰碰撞凹陷损伤下加筋板的极限强度快速评估方法的准确性。 相似文献
4.
极区船舶与浮冰发生碰撞时,冰载荷压力并不均匀,主要分布于结构与浮冰接触的中心区域,这与冰区加强区域结构设计和强度校核采用均布压力作为设计载荷并不一致.参考真实压力分布,以实测压力分布形式离散模拟冰载荷,形成考虑空间分布的冰载荷加载方法.建立舷侧结构有限元模型,分别以均布和考虑空间分布的离散方式将基于能量法计算所得冰载荷作用于舷侧,同时考虑不同浮冰形状和作用位置对空间分布的影响.结果 表明,冰载荷的空间分布对结构响应结果的影响较大,其中浮冰形状为楔形,且作用位置为板格中心的加载工况最为显著.研究过程与结论可为极区船舶设计考虑船冰相互作用时的冰载荷加载方式提供参考. 相似文献
5.
[目的]为研究碳纤维增强复合材料(CFRP)粘贴修复含裂纹加筋板的极限强度,[方法]采用非线性有限元法对在轴向压缩载荷作用下的CFRP修复含裂纹加筋板的极限强度进行分析,基于CFRP修复含裂纹加筋板模型,对仿真结果与文献的试验结果进行比较,验证所提方法的准确性。以CFRP双面修复含裂纹加筋板为例,研究CFRP加筋板的极限强度,并对胶层剥离机理和胶层应力进行分析。[结果]结果表明,使用CFRP修复含裂纹加筋板后其极限强度得到了明显提高,且接近于含几何初始缺陷加筋板的极限强度;CFRP修复含裂纹加筋板的脱胶行为发生在极限强度之后。[结论]使用CFRP修复含裂纹损伤的加筋板可有效提高其极限承载能力,研究结果可为船舶与海洋工程结构修复提供参考。 相似文献
6.
7.
为研究基于船冰碰撞的含凹陷损伤加筋板的极限强度,结合Derradji-Aouat各向同性三维失效准则和弹脆性破坏模式,提出基于线弹性的多表面失效海冰本构模型。利用Ls-dyna二次开发技术,编译生成相应的求解器。通过与球形冰撞击刚性板和柱形冰撞击船体舷侧板架仿真对比分析,验证了基于线弹性多表面失效海冰动力本构模型更加适用于船冰碰撞问题的研究。利用Ls-dyna模拟海冰与船体加筋板碰撞,并将含凹陷损伤加筋板模型导入Ansys中进行加筋板剩余极限强度的计算,得到考虑凹陷影响的加筋板极限强度。结果表明,凹陷对加筋板极限强度的衰减主要体现在凹陷面积,并且凹陷面积和深度对加筋板极限强度的衰减作用随着面积和深度的增加而逐步减弱。 相似文献
8.
9.
10.
[目的]长期服役于恶劣海洋环境中的船舶与海洋工程结构,不可避免地会产生裂纹和点蚀,这些损伤会对结构的极限承载能力产生较大影响。为探讨裂纹、点蚀同时存在时对结构承载能力的影响,[方法]采用非线性有限元法开展含裂纹、点蚀损伤的加筋板在轴向压载作用下的极限强度研究。在讨论网格尺寸对含裂纹、点蚀损伤加筋板极限强度影响的基础上,开展裂纹点蚀坑相对位置、点蚀数目、裂纹长度对含裂纹、点蚀损伤加筋板剩余极限强度的影响。[结果]计算结果表明,裂纹长度、点蚀的增加会使加筋板的剩余极限强度下降明显。[结论]这些结果可用于指导全寿期船舶与海洋工程结构的设计与维护。 相似文献
11.
12.
为研究含裂纹加筋板的极限拉伸强度,本文建立一系列不同长细比、不同裂纹长度、不同裂纹位置的含裂纹加筋板有限元模型,并基于J积分理论对其在单轴拉伸载荷下的极限强度进行了计算。结果发现含裂纹加筋板极限拉伸强度随加筋板长细比的增大略有减小,但减小的程度并不明显;含裂纹加筋板极限拉伸强度随裂纹长度的增大而减小,且减小的幅度逐渐增大;加强筋上的裂纹对含裂纹加筋板极限强度的影响小于底板上的裂纹,而裂纹同时出现在底板和加强筋上时对含裂纹加筋板极限拉伸强度的影响最大。表明含贯穿型裂纹的加筋板在单轴拉伸载荷下的剩余强度对加筋板长细比不敏感,而对裂纹长度较为敏感。 相似文献
13.
Existing rule scantling formulae of plate members are based on conventional plastic design theory, and do not necessarily reflect complicated plate bending phenomena under axial loads. In this study, we first formulated the effect of axial load on the fully plastic moment based on the von Mises yield criterion for longitudinally stiffened plate in addition to the well-known formula for transversely stiffened plate. In addition, we derived a theoretical formulation of the lateral pressure corresponding to 2-point hinge and 3-point hinge formation taking account of the effect of the additional lateral force due to the axial loads on the deflected plating, using a simple plate strip bending model assuming a long plate with a large aspect ratio.Then, a series of elastic-plastic FE analyses was carried out to verify the structural behavior and the effect of axial load on the plate plastic bending strength. The plate strength was evaluated based on the residual deflection criteria of two cases (0.26 mm and 4.0 mm), and the results were compared with the theoretical derivation. As a result, it was found that assumption of linear strength reduction to the axial stress can cover the transversely stiffened plate under compressive axial stress conservatively. As to the transversely stiffened plate under tensile axial stress and the longitudinally stiffened plate, the strength reduction was in accordance with the reduction in the fully plastic moment based on the von Mises yield criterion in the conservative side. Finally, based on the findings, the required plate thickness coefficients were proposed on an empirical basis both for transversely and longitudinally stiffened plate under compressive and tensile axial loads. 相似文献
14.
15.
The present work investigates the compressive axial ultimate strength of fillet-welded steel-plated ship structures subjected to uniaxial compression, in which the residual stresses in the welded plates are calculated by a thermo-elasto-plastic finite element analysis that is used to fit an idealized model of residual stress distribution. The numerical results of ultimate strength based on the simplified model of residual stress show good agreement with those of various methods including the International Association of Classification Societies (IACS) Common Structural Rules (CSR), leading to the conclusion that the simplified model can be effectively used to represent the distribution of residual stresses in steel-plated structures in a wide range of engineering applications. It is concluded that the widths of the tension zones in the welded plates have a quasi-linear behavior with respect to the plate slenderness. The effect of residual stress on the axial strength of the stiffened plate is analyzed and discussed. 相似文献
16.
为了快速方便地求取船舶加筋板塑性性能的两个重要参数—裂纹尖端塑性区半径(Ry)和裂纹尖端张开位移(CTOD),文章提出了一种基于裂纹最大张口位移(MCOD)来确定加筋板的裂纹尖端塑性区半径和裂纹尖端张开位移的简便方法。该法基于理想弹塑性材料,以提出的裂纹最大张口位移与裂纹尖端塑性区半径及裂纹尖端张开位移的拟合函数关系为基础,考虑了模型尺寸效应、材料特性参数及外载荷的影响。文中还对不同裂纹长度、不同屈服极限条件、不同板/筋刚度比时方法的适用性进行了分析,研究表明:该方法能够消除裂纹长度、屈服极限和外载荷等因素的影响,适用于有限宽船舶加筋板的弹塑性分析。 相似文献
17.
18.
The present work investigates the compressive axial ultimate strength of fillet-welded steel-plated ship structures subjected to uniaxial compression, in which the residual stresses in the welded plates are calculated by a thermo-elasto-plastic finite element analysis that is used to fit an idealized model of residual stress distribution. The numerical results of ultimate strength based on the simplified model of residual stress show good agreement with those of various methods including the International Association of Classification Societies(IACS) Common Structural Rules(CSR), leading to the conclusion that the simplified model can be effectively used to represent the distribution of residual stresses in steel-plated structures in a wide range of engineering applications. It is concluded that the widths of the tension zones in the welded plates have a quasi-linear behavior with respect to the plate slenderness. The effect of residual stress on the axial strength of the stiffened plate is analyzed and discussed. 相似文献
19.
现代舰船的直升机起降时会通过轮胎将载荷作用于飞行甲板的板架上,这种载荷通常被称为轮印载荷。除此之外,相对于传统加筋板结构形式,I型夹层结构具有轻质、高比强度等优点,是一种可以应用于船舶飞行甲板的新型结构形式。本文针对轮印载荷局部重载和位置不确定的特点,设计了合理的试验贴片方案及加载程序,并将试验数据与理论值对比,分析误差原因,研究I型夹层板架结构的板格在四种典型位置轮印载荷作用下的静强度力学性能。试验结果表明,夹层板架结构在载荷附近测点的应力水平较大,同时其上面板沿船宽方向的弯曲应力大于沿船长方向的弯曲应力,而下面板2个方向的弯曲应力特性与上面板相反。这些结论对于I型夹层板架结构在轮印载荷下的力学性能研究具有重要意义。 相似文献