共查询到18条相似文献,搜索用时 234 毫秒
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随着对螺旋桨性能要求的不断提高,螺旋桨设计面临着多目标、多学科综合提高的难题.在iSIGHT多学科优化设计平台上,采用试验设计方法和与基于响应面模型的逼近方法相结合的优化方法而建立的设计工程,不但完成设计过程的自动化和智能的设计探索,而且确定最佳设计参数使螺旋桨效率和最小压力系数都有提高,实现了优化设计的目的. 相似文献
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基于网格实现的汽轮机基础优化设计 总被引:1,自引:0,他引:1
工程优化设计往往需要进行大规模的数值计算,拥有大量闲置资源的网格环境为建立这种高性能计算平台提供了可能.但是网格资源的动态性、异构性和分布性的本质特征,阻碍了网格技术在工程应用上的普及.为了利用网格环境中大量的闲置资源来协同解决实际工程中复杂的优化设计问题,建立了一个4层结构的高性能网格计算平台,并利用Kriging近似模型,在该平台上开发了以减轻基础重量和降低基础振幅为目的的多目标汽轮机优化设计的网格算法.使用该算法,在网格平台上对两个汽轮机基础进行了优化设计,与序列线性规划方法的结果比较表明所开发的优化算法有较高的计算精度.还分析了当使用不同数量的计算节点时网格的加速情况,说明所发展的优化方法能够在网格环境中高效地运行,搭建的网格平台也适合于工程优化设计. 相似文献
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提出微位移传感器测控系统动态性能优化设计方法,建立系统数学模型和校正模型,借助Matlab控制系统工具箱、优化设计工具箱完成校正模型的参数寻优,实现测控系统动态性能的优化设计。仿真结果显示,该方法优化效果明显,拓展了工作频带,改善了系统的动态性能。 相似文献
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基于遗传算法的多目标空间区域内的探索性全局优化技术,将阻力系数、丰满度与最大减压系数发生位置作为综合判定指标,在解决UUV线型优化的过程中,引入集成优化框架,对UUV外形进行多目标优化设计;建立了UUV外形优化的一体化模型,针对UUV外形优化设计的要求,对外形设计进行参数化,提出设计变量的选取原则,并针对具体算例进行仿真优化设计,优化计算结果表明:该优化设计方法有效地改善了UUV的阻力性能和压力分布,阻力减小大约4%,在工程应用中是可行的,为目前UUV外形优化设计提供了一个完整的方法. 相似文献
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针对传统单材料热固耦合拓扑优化设计难以实现结构材料与性能综合最优的问题,提出一种基于变密度理论有序材料属性有理近似模型的多材料拓扑优化方法.该方法通过搭建比例系数与平移系数,将多种材料属性采用[0,1]连续分布的单设计变量进行描述,并研究和比较与有序固体各向同行惩罚微结构模型的优缺点;其次借助归一化加权方法定义以结构柔度最小化和散热弱度最小化为目标函数的数学模型.结合设计变量敏度分析,详细推导多材料、多目标条件下热固耦合结构拓扑优化的迭代公式.通过数值算例分析对比了不同权系数以及不同材料属性组合对优化结果的影响;结果表明,所提出的优化方法在热固耦合结构多材料多目标拓扑优化设计中具有可行性和有效性. 相似文献
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多学科优化设计也是在传统设计优化基础上重要的质的发展。它是设计方法、传统机械设计知识、过程设计知识、现代信息技术交叉集成的大系统方法。多学科设计优化技术 以提高产品性能、缩短设计周期和降低研制成本为目的。本文将多学科优化设计与传统优化设计进行对比,并以实例分别进行多学科设计优化和传统优化设计,证明了多学 科优化设计的可行性和高效性. 相似文献
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波音、空客等公司飞机设计中采用的先进设计手段之一是基于高性能计算的多学科、大规模设计变量优化的应用。目前我国的高性能计算在硬件方面已处于世界领先水平,但在工程应用系统方面还无法满足需求。文章介绍了以工程实际需求为导向,以高性能计算资源为辅助手段,基于飞机设计需求而开发的多学科、大变量的并行计算软件系统及计算平台,以及利用该平台实现的航空应用算例。 相似文献
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优化设计可以改善结构的应力分布,合理布置材料,从而提高材料的利用率.通过对全机结构逐层分解,确定优化设计变量、优化区域以及响应约束,并应用MSC Nastran中的可行方向法和敏度分析方法,对MA700飞机的机翼进行优化设计方法研究,考虑稳定性因素,初步解决长桁尺寸确定的问题,为后续优化设计工作积累经验. 相似文献
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Meta-heuristic algorithms are of considerable importance in solving optimization problems. This importance is more highlighted when the problems to be optimized are too complicated to achieve a solution using conventional methods or, the traditional methods are somehow not applicable for solving them. Imperial Competitive Algorithm has been proved to be an efficient and effective meta-heuristic optimization algorithm and it has been successfully applied in many scientific and engineering problems. By introducing the concept of explorers and retention policy, the original algorithm is enhanced with a dynamic population mechanism in this paper and hence, the performance of the Imperial Competitive Algorithm is improved. Performance of the proposed modification is tested with experiments of optimizing real-values functions and results are compared with results obtained with the original Imperialistic Competitive Algorithm, Genetic Algorithm, Particle Swarm Optimization and Simulated Annealing. Also, the applicability of the proposed improvement is verified by optimizing a ship propeller design problem. 相似文献
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Modern engineering design problems often involve computation-intensive analysis and simulation processes. Design optimization based on such processes is desired to be efficient, informative and transparent. This work proposes a rough set based approach that can identify multiple sub-regions in a design space, within which all of the design points are expected to have a performance value equal to or less than a given level. The rough set method is applied iteratively on a growing sample set. A novel termination criterion is also developed to ensure a modest number of total expensive function evaluations to identify these sub-regions and search for the global optimum. The significance of the proposed method is twofold. First, it provides an intuitive method to establish the mapping from the performance space to the design space, i.e. given a performance level, its corresponding design region(s) can be identified. Such a mapping could be potentially used to explore and visualize the entire design space. Second, it can be naturally extended to a global optimization method. It also bears potential for more broad application to problems such as metamodeling-based design and robust design optimization. The proposed method was tested with a number of test problems and compared with a few well-known global optimization algorithms. 相似文献
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In this paper a general methodology is presented for determining theoptimum design of a planar parallel platform to be used in machining.The method, based on a mathematical optimization approach, is used tofind a platform design and placement such that firstly, the execution ofa prescribed task path is feasible, and secondly, the actuator forcesrequired to execute the prescribed task are minimized. The applicationof the method is illustrated for two prescribed tasks, five designvariables and a number of geometrical inequality constraints such asactuator length limits. The method succeeds in finding locally optimumand feasible platform designs for which the required task lies insidethe workspace. Two optimization algorithms are implemented and theirrespective results are compared. The first algorithm is a robust andreliable trajectory algorithm, LFOPC, which is however expensive interms of the number of required function evaluations. As the simulationsperformed here in evaluating the objective and constraint functions maybe computationally intensive, an approximation method, Dynamic-Q, isalso used to find the optimum design with greater efficiency. Theeffectiveness of this approximation approach is evaluated. 相似文献