共查询到18条相似文献,搜索用时 859 毫秒
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《舰船科学技术》2016,(13)
聚氨酯弹性体钢夹层板结构(SPS)因其优异的力学性能和可设计性,近年来在船舶制造等领域得到广泛应用。本文通过理论与数值仿真,研究了SPS夹层板结构自由振动以及脱层对振动特性的影响。首先,对SPS夹层结构,提出一种等效模型,采用简化一阶剪切变形理论,建立了夹层板横向自由振动控制方程,并结合边界条件给出了SPS夹层结构的振动频率表达式。通过与文献和数值仿真结果的对比分析,验证了本模型与方法的有效性与准确性。考虑结构易脱层的特点,研究了面/芯脱层对结构振动特性的影响,对比分析脱层范围、脱层位置以及脱层形状对结构低阶频率的影响,给出了各脱层参数与结构低阶振动频率的关系,为SPS结构的设计与应用提供指导。 相似文献
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聚氨酯弹性体钢夹层板结构(SPS)因其优异的力学性能和可设计性,近年来在船舶制造等领域得到广泛应用。本文通过理论与数值仿真,研究了 SPS夹层板结构自由振动以及脱层对振动特性的影响。首先,对 SPS夹层结构,提出一种等效模型,采用简化一阶剪切变形理论,建立了夹层板横向自由振动控制方程,并结合边界条件给出了 SPS夹层结构的振动频率表达式。通过与文献和数值仿真结果的对比分析,验证了本模型与方法的有效性与准确性。考虑结构易脱层的特点,研究了面/芯脱层对结构振动特性的影响,对比分析脱层范围、脱层位置以及脱层形状对结构低阶频率的影响,给出了各脱层参数与结构低阶振动频率的关系,为 SPS结构的设计与应用提供指导。 相似文献
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本文基于有限元软件Abaqus,采用三维内聚力单元模拟蒙皮与芯层界面,建立静水压力载荷下复合材料夹层圆柱壳极限承载能力预报方法,数值计算与试验结果吻合较好,验证数值模型和计算方法的准确可行性。进而,研究了浮体/吸声混合芯材夹层复合材料圆柱壳芯层模量对承载特性的影响,并基于Isight与Abaqus集成运算,以提高临界失稳载荷为优化目标,对深水静压作用下的复合材料夹层圆柱壳表层缠绕方式进行优化设计,得到最优表层缠绕角度。研究结果对复合材料夹层圆柱壳的水下应用与研究有一定参考价值和指导作用。 相似文献
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舰船桅杆在风载、船舶横摇惯性载荷以及由螺旋桨引起的桅杆基础加速度激励等载荷作用下,其顶部雷达处会产生较大的转角振动,严重影响雷达追踪的分辨率.文中以磁流变液阻尼器(Magneto-Rheological Damper)为作动器,采用神经网络模拟该阻尼器的逆向动特性,并运用独立模态空间控制算法设计了半主动控制系统.研究了基于ANSYS平台的振动半主动控制实现方法,并最终在ANSYS中实现了基于磁流变阻尼器的舰船桅杆振动半主动控制.数值计算结果表明,文中设计的控制系统能有效地减小桅杆顶部雷达的转角振动,基于ANSYS实现结构振动控制仿真是可行的. 相似文献
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对舰船RCS基本统计量进行归类和分析,以桁架式和封闭式桅杆缩比模型为研究对象,基于快速多极子方法,对其在各种极化组合下的单站RCS进行计算和统计分析.结果显示:桅杆的RCS随雷达波入射姿态角有较多的起伏,且幅值较大,RCS序列密度峰值偏向低于平均值方向.封闭式桅杆比桁架式桅杆的整体的隐身效果更好,但在当舰船处于最不利角度时封闭式桅杆的隐身效果并不一定占优.RCS分布在不同极化方式下均存在差异,在进行桅杆隐身设计或分类识别时应不建议考评单个极化方式,但可忽略交叉极化工况. 相似文献
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Wei Zhang Chao Wu Wenshan Yang Shanshan Xu Shaofei Ren . China Ship Development Design Center Wuhan China . College of Shipbuilding Engineering Harbin Engineering University Harbin China 《船舶与海洋工程学报》2011,(3)
Due to the unique structural mode and material property of a composite sandwich plate, related research such as fragment impact resistance of a composite mast is short of publication and urgent in this field. In this paper, the commonly accepted sandwich core board theory was modified. Damage caused by a fragment attack was simulated onto a sandwich plate model built with solid and shell elements. It was shown that shear failure and vast matrix cracking are the main reasons for outer coat damage, and tensio... 相似文献
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Due to the unique structural mode and material property of a composite sandwich plate, related research such as fragment impact resistance of a composite mast is short of publication and urgent in this field. In this paper, the commonly accepted sandwich core board theory was modified. Damage caused by a fragment attack was simulated onto a sandwich plate model built with solid and shell elements. It was shown that shear failure and vast matrix cracking are the main reasons for outer coat damage, and tension failure and partial matrix cracking are the cause for inner coat damage. Additionally, according to complexities in actual sea battles, different work conditions of missile attacks were set. Ballistic limit values of different fragment sizes were also obtained, which provides references for enhancing the fragment impact resistance of a composite mast. 相似文献
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The panel and core materials of sandwich composite usually have the characteristics of unequal elastic modulus in tension and compression. However, in the numerical calculation of sandwich composite, it is usually considered as the material with the same tensile modulus or compression modulus, which often leads to larger calculation errors. The test results show that when the elastic modulus of tension and compression is about 10 times different, the maximum calculated stress and maximum deflection will be more than twice different. In view of the complexity of sandwich composite structure, based on the bi-modulus model of laminated plates, a simplified theoretical formula and numerical calculation method are proposed for bi-modulus sandwich composite structures in this paper. Furthermore, the accuracy of the proposed numerical calculation method of bi-module is verified by the experimental study of composite single-layer plate structure and sandwich composite cabin structure. The results show that the error between the improved numerical calculation method and the experimental measurement results is basically within 6%. Meanwhile, the numerical method based on field variables has wide application range and high convergence, and can be used to calculate complex marine composite structures. 相似文献
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舱室内战斗部爆炸产生的冲击波是舱室结构板架承受的主要载荷之一,舱室内爆冲击波在舱室内部将发生多次反射,并在舱室内部形成持续时间较长的准静态压力,在此过程中舱室板架承受多次冲击波反射载荷。本文以舱室典型加筋板为对象进行夹层板概念设计,选取面板厚度、背板厚度、夹芯壁厚及夹芯间距4个参数作为试验参数,以抗爆综合评价指标最小为目标,采用正交试验优化设计方法得到该加筋板结构在舱室内爆冲击波载荷作用下最优抗爆性能的夹层板结构,并对比最优夹层板与普通加筋板在舱室内爆载荷作用下的响应特征。研究表明,经过优化设计后的夹层板具有更好抵抗冲击波载荷的能力,正交试验设计能较好适用于夹层板结构优化设计。 相似文献
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通过对桥梁防护装置研究,提出四棱柱式与双折叠式夹层板桥梁防护装置,采用ANSYS/LS-DYNA非线性有限元对其耐撞性能进行数值仿真,探讨两种夹层板防护装置的尺寸参数对其性能的影响.研究结果表明:经结构优化后四棱柱式夹层板的耐撞性能优于双折叠式;分别用两种夹层板替换传统钢质箱式防护装置的外围板,两种夹层板式防护装置的耐撞性能均优于传统钢质防护装置,而四棱柱式防护装置的性能最佳. 相似文献