首页> 外文会议>AIAA/ISSMO multidisciplinary analysis and optimization conference;AIAA aviation technology, integration and operations conference >A Multi-Objective Design Optimization Approach for the Preliminary Design of High Speed Low Pressure Turbine Disks for Green Engine Architectures
【24h】

A Multi-Objective Design Optimization Approach for the Preliminary Design of High Speed Low Pressure Turbine Disks for Green Engine Architectures

机译:用于绿色发动机架构的高速低压涡轮盘初步设计的多目标设计优化方法

获取原文

摘要

The so-called Green Engine architectures are deeply investigated by the scientific community with the aim of reducing fuel consumption and noise emissions by 50%, and pollutants by 80%, environmental targets established by the Advisory Council for Aeronautical Research in Europe to be achieved by 2020. Low pressure turbine improvements will be important to increase the efficiency of the two most innovative propulsive architectures, the Geared Turbofan and the Geared Open Rotor. The low pressure turbine is released from the fan and can rotate at higher speed values, implying a reduction in fuel consumption. Due to a higher rotational speed, low pressure turbine disks design needs careful considerations due to their higher stress level and reduced burst limit. The presented study falls within the preliminary design phase of an engine, thus a code based on finite differences was used to perform disks analyses and optimization studies were set up. This paper presents two multi-objective hybrid optimization methodologies designed to study high speed low pressure turbine disks. The objective functions of both the constrained multi-objective optimizations were the minimization of disks weight and the maximization of their burst speed, and a hybrid approach was pursued to better investigate the design space and find the optimum. The code-based methodology provides an innovative approach to design such critical components by reducing disks weight by 15% and computational time by 30%, if compared to reference corporate design methodologies. The second study was conducted by considering a surrogate-model-based optimization to further reduce computational time while ensuring the analysis accuracy. A trade-off of most common approximation strategies was conducted and main results are shown in the paper. Distributed computing was used in both the considered optimization strategies, by involving three national research centers, and parallel computing was adopted to spread the calculation tasks on local workstations. Numeric and Finite-Element-Methodology-based validations followed to ensure the goodness of the achievements. Finally a good match between the predicted optimal solutions was found, thus justifying a surrogate-model-based-approach that led to further gains in computational time.
机译:科学界对所谓的“绿色发动机”架构进行了深入研究,旨在将燃料消耗和噪音排放减少50%,将污染物减少80%,这是欧洲航空研究咨询委员会确定的环境目标, 2020年。低压涡轮机的改进对于提高两个最具创新性的推进式结构,即齿轮涡轮风扇和齿轮开放转子的效率至关重要。低压涡轮从风扇中释放出来,并可以更高的转速旋转,这意味着减少了燃油消耗。由于转速较高,低压涡轮盘的设计因其较高的应力水平和降低的爆破极限而需要仔细考虑。提出的研究属于发动机的初步设计阶段,因此使用基于有限差分的代码进行了磁盘分析,并建立了优化研究。本文提出了两种多目标混合优化方法,旨在研究高速低压涡轮盘。两种受约束的多目标优化的目标函数是磁盘重量的最小化和它们的爆发速度的最大化,并且寻求一种混合方法来更好地研究设计空间并找到最优方法。与参考公司设计方法相比,基于代码的方法通过减少磁盘重量15%和计算时间30%,提供了一种设计此类关键组件的创新方法。第二项研究是通过考虑基于替代模型的优化来进一步减少计算时间,同时又确保了分析准确性。进行了最常见的近似策略的权衡,并在本文中显示了主要结果。在涉及三个国家研究中心的情况下,已考虑的优化策略均使用了分布式计算,并采用并行计算将计算任务分散在本地工作站上。随后进行了基于数字和有限元方法论的验证,以确保成就的良好性。最后,在预测的最佳解决方案之间找到了良好的匹配,从而证明了基于代理模型的方法的合理性,该方法导致了计算时间的进一步增加。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号