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考虑到夹层结构玻纤增强塑料船舶的结构强度数值仿真分析方法与一般钢质海船不同,采用层合板单元模拟玻璃钢复合材料和复合材料夹层结构,并参照中国船级社《海上高速船入级与建造规范》2015的最新要求,对某玻璃钢夹层结构双体游艇进行总强度有限元计算分析及评估,并对不满足规范要求复合材料构件提出改善夹层纤维增强建议。文中采用的分析方法和提出的建议,可为复合材料船舶的结构设计提供参考。 相似文献
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利用MSC/PATRAN、MSC/NASTRAN对38In双体甲板货船总体结构强度进行了有限元强度计算。给出了外载荷的计算方法和边界条件的施加方法,并在11种工况下对38m双体甲板货船进行了总体结构强度有限元分析。通过有限元分析得到的结论可用于双体甲板货船设计与优化。计算结果表明结构强度满足强度要求。 相似文献
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本文述及了法国玻璃双体风帆游艇的设计和建造的概况,通过分析该船型的特点和承载形式,提出了一种适合小长这经双体船型的合理结构形式,以及介绍了新型玻绗材料的应用和夹层板施工的新工艺技术。 相似文献
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结构的轻量化设计直接关系到水下潜器总体性能的优劣,是深海水下潜器结构设计的重要目标。以全海深无人潜水器本体浮力构件的安装防护结构为研究对象,选取典型浮力构件,采用3种设计方案,使用ANSYS Workbench软件在假设的碰撞载荷和浮力载荷作用下对设计的安装防护结构的应力和变形进行计算分析和比较。结果表明,基于Inspire软件拓扑优化方法的结构设计,显著提高了设计效率,满足强度和功能设计需求,能充分发挥材料性能,实现了轻量化的设计目标,并通过了水池测试和海试应用验证。 相似文献
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玻璃钢双体快艇艇体结构设计 总被引:1,自引:1,他引:0
对玻璃双体快艇艇体结构形式的选择及复合材料设计进行了论证,列出了单,双体双艇船型主要参数及其区别,叙述了艇体的受冲击力特点和纵,横向的分布情况,并介绍了双体快的适用范围及结构设计中需引起重视的问题。 相似文献
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双体船在横浪与斜浪中会遭受比较严重的横向弯矩和扭转力矩作用,此时双体船的强度对其安全性至关重要。本文采用波浪直接计算方法对本船在航行海区进行波浪载荷长期预报,得到各强度工况计算设计波。采用直接计算方法对双体船进行了总纵强度、横向强度和扭转强度的整船有限元分析,对计算结果分析该船在各工况下的应力分布,结果表明该船结构强度满足要求,但高盈利区域出现在抗扭箱与片体连接处,针对该危险区域提出修改方案,为其他类似船舶设计提出参考意见。 相似文献
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11.9m双体交通艇总强度有限元分析 总被引:2,自引:2,他引:0
双体船因其甲板面积大、稳性好等优点在近几年备受关注。双体船的两个片体由中间的连接桥连接而成,连接桥在航行环境中要遭受比较大的横向弯矩和扭转力矩的作用,其自身的强度对双体船的安全性来说至关重要。本文在有限元理论的基础上,采用直接计算方法对某双体船进行了横向强度和扭转强度的最上层主甲板以下全船结构有限元分析。对其总横强度及扭转强度进行了校核,并根据应力云图提出了双体船在设计时应注意的几点建议。 相似文献
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舰船的砰击载荷与结构响应的研究一直备受关注.对于双体船来说,砰击按部位可分为底部砰击、外飘砰击和甲板上浪,和连接相邻船体的甲板下侧,即湿甲板砰击.目前对于双体船的砰击计算还不完善,因此对于该船型的砰击研究十分必要.本文分别利用规范计算和直接计算的方式,对砰击载荷作用下双体船强度影响进行研究.规范计算主要基于中国船级社规范计算砰击载荷,直接计算则是通过线性势流理论预报船波相对速度,借助相关规范确定砰击压力系数,实现砰击载荷的直接计算.通过有限元软件加载计算,分析比较2种载荷计算方法对双体船强度的影响,以指导砰击载荷作用下双体船局部结构的设计实践. 相似文献
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Catamaran vessels operating at high-speed can be exposed to deck diving and bow damage and one resolution of this problem is the wave-piercer design of INCAT Tasmania. Owing to the complexity of the unsteady non-linear flow in the bow area during large wave encounter model testing has been undertaken to identify the peak dynamic slam loads on the ship structure. This paper provides experimental benchmark information relating to the wave slam loads on wave-piercing catamaran ferries. Since the time frames of transient slam loadings and whipping vibration of the entire hull in its first bending mode are similar it is important that the test model replicates the whipping response and therefore needs to be a hydro-elastic model. A 2.5 m hydro-elastic segmented catamaran model has been developed based on the 112 m INCAT Tasmania wave-piercer catamaran to establish the peak wave slamming loads acting on the full-scale vessel. Towing tank tests were performed in regular seas at a maximum full-scale operating speed of 38 knots. The model was instrumented to measure the dynamic slam loads acting on the centre bow and vertical bending moments acting in the demihulls of the catamaran model as a function of wave frequency and wave height. Peak slam loads measured on the centre bow were found to approach the total weight of the model, this being a broadly similar result to the peak loads measured at full-scale. It was found that global dimensionless heave and pitch accelerations peaked in the same range of encounter frequency as did the peak slam load. 相似文献
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双体车客渡船作为一种对安全性要求较高的船舶 ,动力装置的设计不仅要满足规范要求 ,而且还要考虑船东对所配置动力设备的熟悉程度及机务管理习惯 ,以提高设备操作维护的准确性和船舶运营的安全性 相似文献
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The offshore wind industry experienced a boost during the last decade in terms of size of wind farms and rated capacity of the wind turbines: towers are getting taller and blades are getting longer, constantly facing new and complex challenges. Because of the relative immaturity of the wind industry, and the fact that the offshore design standards stemmed from the oil and gas industry, it is generally acknowledged that the reliability levels achieved, although not very well understood, might result in partial safety factors not optimal for OWT. This paper addresses this situation by studying the reliability levels delivered by the current standards and assessing the validity of the safety factors through a reliability-based code calibration. The combination of the low probability of failure imposed on the design of OWTs and the computational cost of the aero-elastic time-domain simulations brings out the need to develop new approaches for reliability analyses. In this paper, the reliability analysis is performed using a Kriging surrogate model to approximate the load-effect from the aero-elastic simulations converting expensive-to-evaluate limit state functions to explicit functions. Subsequently, a calibration of the safety factors is carried out using the probabilistic models from literature. The approach is applied to an industry-reference turbine and support structure. The results showed very low probabilities of failure for the most severe design cases and confirm that the safety factors from the IEC are mostly adequate. 相似文献