涡轮叶片的多学科设计优化系统

王婧超; 李立州; 岳珠峰

涡轮叶片的多学科设计优化系统

1.
西北工业大学力学与土木建筑学院, 陕西西安 710072
2.
西北工业大学, 航空学院陕西西安, 710072

基金项目: 国家自然科学基金(50375124,10472094);航空科学基金(02C53011,03B53003)

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- 被引次数: 0
出版历程
- 收稿日期: 2005-12-15
- 刊出日期: 2007-01-28

Multidisciplinary optimization design system for turbine blade

1.
School of Mechanics Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, China
2.
School of Aviation, Northwestern Polytechnical University, Xi'an 710072, China

摘要

摘要: 建立了一个全三维涡轮叶片的一体化多学科设计优化系统, 并对某叶片进行涉及五学科的设计优化分析.在此优化系统中, 采用5次多项式方法进行三维涡轮叶片的参数化建模, 单元线性插值法完成学科间载荷信息的传递, 多岛遗传算法及二次序列规划法联合进行整个优化问题的寻优.实例分析结果表明, 一体化优化使涡轮叶片性能得到明显提高, 所建系统稳定、高效, 具有应用于工程实践的可行性及可靠性.
- 航空、航天推进系统 /
- 涡轮叶片 /
- 多学科设计优化 /
- 一体化优化 /
- 单元线性插值
Abstract: An integrated,three-dimensional,multi-disciplinary optimization design system for turbine blades has been set up,which enables the design and analysis of certain blades optimized involving five disciplines.In this system,quintic polynomial is used for parameter modeling of three-dimensional turbine blades,and unit linear interpolation method used for transfer of interdisciplinary load information,while MIGA(Multi-island Genetic Algorithm) and SQP(Sequential Quadratic Programming) are used for overall optimization.The case study shows that, optimization efforts could improve greatly the performance of turbine blades,and the system exhibits higher stability,feasibility and efficiency for engineering applications.
- aerospace propulsion system /
- turbine blade /
- multidisciplinary design optimization(MDO) /
- all-at-once(AAO) /
- elemental linear interpolation(ELI

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参考文献(11)

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