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加筋板抗撞击性能的比较研究 总被引:1,自引:0,他引:1
研究加筋板的抗撞击性能对于深入理解船舶碰撞的力学机理和开展耐撞性船舶结构设计都具有重要的指导意义。本文用数值仿真法研究了普通的船舶加筋板结构的抗撞击性能,并与三种改进型加筋板作了比较。研究表明,三种改进型加筋板的抗撞击性能均比原结构有所提高,这可为新式船舶结构形式研究提供一定的依据。 相似文献
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在研究水下爆炸作用下加筋板架的稳态响应方面,以往的研究主要利用瞬态显式算法,得到的稳态响应结果存在一定的精度缺陷。提出一种改进的水下爆炸数值模拟方法。该方法利用ABAQUS/Explicit Standard算法,针对瞬态显式与稳态隐式静力分析,建立联合数值模拟方法。利用该方法分析某船体加筋板架的“瞬态稳态”响应。结果表明:联合“瞬态显式稳态隐式”算法的仿真结果与试验结果相差在10%以内,说明该方法可用于水下爆炸作用下加筋板架结构的响应分析,且采用联合“显式隐式”算法得到的结果更接近试验值,误差降低了39.8%。 相似文献
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开展夹层板单元防护性能研究可为舰船防护结构设计提供指导。以某船底加筋板架为应用对象,设计出U型折叠式夹层板结构;利用MSC.Dytran对船底板架及夹层板结构在水下爆炸冲击载荷下的动态响应进行数值仿真分析,通过分析流-固耦合压力、损伤变形、速度、加速度、结构塑性吸能等性能参数,对比研究两结构的防护性能;分析夹层板在不同冲击强度下的损伤特性,面板厚度、夹芯板厚、夹芯与面板夹角、夹芯单元宽度、夹芯高度等结构参数对夹层板损伤变形、结构吸能等特性的影响。通过研究得到了U型夹层板在水下爆炸冲击载荷下的损伤特性、变形模式等,U型夹层板的防护性能明显优于传统加筋板架,夹芯层在夹层板抵抗水下冲击载荷中起到关键作用,结构参数对防护性能产生不同程度的影响。 相似文献
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加筋板穿透数值仿真中网格尺寸对失效应变的影响分析研究 总被引:1,自引:0,他引:1
运用数值仿真分析碰撞过程时,基于最大等效塑性应变失效准则确定的材料失效应变取值与网格尺寸具有明显的依赖关系,因此,研究碰撞载荷下加筋板网格尺寸对失效应变取值的影响对于评估加筋板架的耐撞性及开展耐撞性结构设计具有重要意义。文中基于LS-DYNA非线性有限元分析软件对光板及加筋板穿透过程分别进行仿真分析,以国外学者相应准静态穿透试验的结果为参照,探讨了加筋板与光板的有限元网格尺寸和失效应变之间的关系,同时对是否有必要考虑骨材与板壳之间的焊缝进行了探究。研究表明:加筋板与光板的失效应变取值存在明显的差异,确定加筋板材料失效应变取值时,应优先参考适用于加筋板网格尺寸与失效应变取值的关系曲线;在决定是否考虑加筋板结构中的焊缝时需要结合网格尺寸与焊缝等效单元的相对大小进行判断。 相似文献
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《舰船科学技术》2017,(15)
随着船舶向大型化发展势头迅猛,船舶碰撞所带来的灾难性后果也显著增大。为评估船舶结构的耐撞能力,国内外研究人员分别从试验和数值模拟2个方面开展研究工作。针对船舶碰撞场景的仿真模拟中,经常采用常应变失效准则来定义单元是否失效。然而失效应变取值强烈依赖于单元尺寸大小,因此,开展失效应变与单元网格尺寸关系研究对船舶结构的耐撞性能准确评估意义重大。本文通过对光板及加筋板的耐撞性能的试验研究,并应用非线性有限元软件LS-DYNA对试验结果进行仿真模拟,探讨了光板及加筋板的单元尺寸和失效应变之间的关系。结果表明:光板和加筋板的单元尺寸与失效应变关系曲线明显不同,因此采用常应变失效准则时应区别对待,不能混用。研究结论对船舶结构碰撞有限元仿真具有一定的指导意义。 相似文献
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针对船舶舷侧结构抗碰撞问题,开展有无聚脲涂层舷侧板架落锤试验研究。以某型舰船结构为依据建立舷侧板架有限元模型,利用瞬态动力学软件MSC/Dytran对模型进行数值仿真并确定落锤高度及试验工况。在此基础上,制作模型板架进行有无聚脲涂层舷侧板架落锤冲击试验,分别获得有涂层和无涂层舷侧板架在碰撞冲击载荷作用下的损伤变形、破口大小及碰撞力,对比研究聚脲材料的抗撞防护性能。结果表明,聚脲涂层的存在能够加强舷侧板架的耐撞防护性能。 相似文献
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A series of collapse analyses is performed applying nonlinear FEM on stiffened panels subjected to longitudinal thrust. MSC.Marc is used. Numbers, types and sizes of stiffeners are varied and so slenderness ratio as well as aspect ratio of local panels partitioned by stiffeners keeping the spacing between adjacent longitudinal stiffeners the same. Initial deflection of a thin-horse mode is imposed on local panels and that of flexural buckling and tripping modes on stiffeners to represent actual initial deflection in stiffened panels in ship structures. On the basis of the calculated results, buckling/plastic collapse behaviour of stiffened panels under longitudinal thrust is investigated. The calculated ultimate strength are compared with those obtained by applying several existing methods such as CSR for bulk carriers and PULS. Simple formulas for stiffened panels, of which collapse is dominated fundamentally by the collapse of local panels between longitudinal stiffeners, are also examined if they accurately estimate the ultimate strength. Through comparison of the estimated results with the FEM results, it has been concluded that PULS and modified FYH formulas fundamentally give good estimation of the ultimate strength of stiffened panels under longitudinal thrust. 相似文献
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Rational structural design of ships or offshore platforms against collisions requires prediction of the extent of damage to stiffened plates generated by lateral impact. In predicting the extent of collision damage, most researchers employ numerical analysis methods using commercial software packages. Like other structural problems, any nonlinear dynamic analysis methods should be substantiated with relevant test data prior to being employed for design. Unfortunately, full-scale collision tests on marine structures are very rare. Still, results from collision tests on marine structural elements can help to substantiate theoretical methods for collision analyses. Lateral collision test data for unstiffened plates are available, but it is difficult to find results from tests on stiffened plates in the open literature. In this paper, the results of lateral collision tests on 33 stiffened plates are reported. A simplified analytical method is developed for the prediction of the extent of damage to stiffened plates due to lateral collisions and this method is substantiated with the test results. Also proposed is a simple criterion with which the occurrence of crack damage can be judged. 相似文献
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Five specimens of wide stiffened panel with four stiffeners under axial compression until collapse are studied with a nonlinear finite element analysis and Common Structural Rules to compare with the experimental results. The stiffened panel models have two longitudinal bays to produce reasonable boundary condition at the end of edges. Tension tests have been conducted to obtain the material properties of the steel that are used in the finite element analysis. Three boundary condition configurations are adopted to investigate their influence on the collapse behaviour of the stiffened panels. A displacement transducer was used to measure the initial geometrical imperfections of the stiffened plates. The collapse behaviour of the stiffened panels is analysed in finite element analysis with the measured initial imperfections and with nominal imperfections. An equivalent initial imperfection is validated for the ultimate strength of stiffened panel under compressive load until collapse for the panels under consideration. With the same imperfection amplitude, the shape of the column-type initial deflection of stiffeners affects significantly the collapse shape, but only slightly the ultimate strength and the mode of collapse of the stiffened panels. The 1/2 + 1 + 1/2 bays model with restrained boundary condition BC3 gives an adequate FE modelling and is possible to be fabricated in experiment. 相似文献
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Five specimens are tested under axial compression until collapse to investigate the ultimate strength of wide stiffened panels with four stiffeners. To avoid the side bays collapse and reduce the influence of the clamped boundary condition on the collapse behaviour, the tests are made on panels with two half bays plus one full bay in the longitudinal direction with simply supported condition at the end edge of loading. Initial loading cycles are used to release the residual stresses of the stiffened panels and the gap between the stiffened panels and the supported steel block. Strain gauges are installed on the plates and the stiffeners to record the distribution of strain. This series of experiments is compared to a series of tests with narrow panels (two stiffeners), which allows analysing the effect of the width on the strength of stiffened panels. 相似文献
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A series of finite element analyses are conducted to investigate the influence of boundary conditions and geometry of the model on the predicted collapse behaviour of stiffened panels. Periodic and symmetric boundary conditions in the longitudinal direction are used to calculate the ultimate strength of stiffened panels under combined biaxial thrust and lateral pressure. The calculated ultimate strength of stiffened panels are compared with those by different FEM (finite element method) code and are assessed. The periodic boundary condition in the longitudinal direction for two spans or bays model provides an appropriate modelling to a continuous stiffened panel and can consider both odd and even number of half waves and thus, is considered to introduce the smaller model uncertainty for the analysis of a continuous stiffened panel. 相似文献
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研究铝合金加筋板结构的极限强度,有利于充分发挥铝合金材料的强度潜力和结构的后屈曲承载能力。本文将广义切线模量理论应用于铝合金加筋板结构的轴压极限强度计算,并推导了适用于加筋板的协调参数、极限弯矩系数及结构系数等相关参数的解析算式,建立了铝合金加筋板结构的强度利用率函数,从而得到结构的极限强度,进一步完善了广义切线模量理论在加筋板结构极限强度研究领域的应用。通过将广义切线模量法计算结果与经验公式、有限元计算结果进行比较,验证了其适用性与可靠性,可用于工程分析计算。 相似文献
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文章给出了基于弹性大挠度理论和刚塑性分析的加筋板格高级屈曲分析方法(EPM),该方法包括五种失效模式,即正交加筋板格整体屈曲、纵向加筋子板格整体屈曲、纵向加筋和带板的局部屈曲或屈服、纵向加筋的侧倾以及全部屈服,可以考虑初始挠度和残余应力的影响以及双向压缩和侧向载荷的联合作用。以EPM方法为核心开发了加筋板格高级屈曲分析软件系统,包括任务管理、数据输入、屈曲分析、结果查看、能力曲线和文件分析等六个模块。为验证EPM方法的精度进行了系列纵向加筋和正交加筋板格试验模型的比较计算,并计算了四种典型加筋板格的双向应力能力曲线,与板格极限状态分析(PULS)软件和协调共同结构规范(HCSR)方法进行了比较分析。结果表明EPM方法可以分析联合载荷等因素对加筋板格极限强度的影响,文中开发的软件系统可用于加筋板格高级屈曲分析。 相似文献