首页> 外文会议>ASME turbo expo >DEVELOPMENT OF AN OPTIMIZATION DESIGN METHOD FOR TURBOMACHINERY BY INCORPORATING THE COOPERATIVE COEVOLUTION GENETIC ALGORITHM AND ADAPTIVE APPROXIMATE MODEL
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DEVELOPMENT OF AN OPTIMIZATION DESIGN METHOD FOR TURBOMACHINERY BY INCORPORATING THE COOPERATIVE COEVOLUTION GENETIC ALGORITHM AND ADAPTIVE APPROXIMATE MODEL

机译:结合合作协作遗传算法和自适应近似模型的涡轮机械优化设计方法

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An optimization design method is developed, which is motivated by the optimal design of a cryogenic liquid turbine (including an asymmetric volute, variable stager vane nozzles, shroud impeller and diffuser) for replacement of the Joule-Thompson throttling valve in the internal compression air-separation unit. The method involves mainly three elements: geometric parameterization, prediction of objective function, and mathematical optimization algorithm. Traditional parameterization approach is used for the geometry representation, while some novel work in the latter two aspects (i.e. objective function evaluation and optimization algorithm) is done to reduce the computing time and improve the optimization solution. A modified Cooperative Coevolution Genetic Algorithms (CCGA) is developed by incorporating a modified variable classification algorithm and some new self-adapted GA operators, which help to enhance the global search ability with an excessive number of optimization variables. Design of Experiment (DOE) is carried out to initialize the kriging approximation model, which is used to approximate the time-costly objective function. Then the CCGA is started, and once a potential superior individual is found, a decision will be made by the in-house code on whether or not it needs a updating. If required, the true objective function prediction based on the real model will be conducted and the obtained value of objective function will be used to update the kriging model. In such a way, the CCGA can complete its optimal searching with a limited number of real evaluations for objective function. All the above features are integrated into the optimization framework and encoded for the optimal turbine design. In addition, CFD software ANSYS CFX is used for the real objective function evaluations, and a well-organized batch code is developed by the authors for calling the CFD simulation which helps to promote this automation of the optimization process. For validation, the optimization method is used to solve some classical mathematical optimization problems and its effectiveness is demonstrated. The method is then used in the optimal design of the cryogenic liquid turbine stage, it is demonstrated that the optimal design method can help to reduce significantly the searching time for the optimal design and improve the design solution to the liquid turbine.
机译:开发了一种优化设计方法,其由低温液体涡轮机(包括不对称蜗壳,可变台阶叶片喷嘴,护罩叶轮和扩散器)的最佳设计,用于在内部压缩空气中更换joule-thompson节流阀 - 分离单位。该方法主要涉及三个要素:几何参数化,客观函数预测和数学优化算法。传统的参数化方法用于几何表示,而在后两方面的一些新颖的工作(即客观函数评估和优化算法)是为了减少计算时间并改善优化解决方案。通过结合修改的可变分类算法和一些新的自适应GA运算符来开发修改的协作共同遗传遗传算法(CCGA),这有助于通过过多的优化变量来增强全球搜索能力。实验(DOE)的设计进行了初始化Kriging近似模型,用于近似时间昂贵的客观函数。然后,CCGA开始,一旦发现潜在的优势,就会通过内部代码进行决定是否需要更新。如果需要,将进行基于真实模型的真实目标函数预测,并且可以使用所获得的目标函数的值来更新Kriging模型。以这样的方式,CCGA可以通过有限数量的目标函数来完成其最佳搜索。所有上述功能都集成到优化框架中,并为最佳涡轮设计编码。此外,CFD软件ANSYS CFX用于真正的客观函数评估,并且由作者开发了一个有组织的批处理代码,用于调用CFD仿真,有助于促进优化过程的这种自动化。为了验证,优化方法用于解决一些经典数学优化问题,并且证明其有效性。然后将该方法用于低温液体涡轮级的最佳设计中,证明了最佳设计方法可以帮助显着减少最佳设计的搜索时间,并改善液体涡轮机的设计解决方案。

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