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等强度三维空心叶片的内部拓扑结构
引用本文:李琳,薛铮.等强度三维空心叶片的内部拓扑结构[J].航空动力学报,2012,27(10):2329-2335.
作者姓名:李琳  薛铮
作者单位:北京航空航天大学能源与动力工程学院,北京,100191
摘    要:以ANSYS软件为平台基于双向渐进结构优化法对所提出的等强度风扇叶片的内部结构形式进行探索性研究,在对叶片内部结构进行拓扑优化的过程中提出了中面应力基准法,简化了优化模型,同时有针对性的解决了双向渐进结构优化法在应用中的一些技术问题,实现了等强度风扇叶片内部结构的优化获得了内部结构的拓扑形式.所得结果可为发动机轻量化设计提供参考.

关 键 词:航空发动机风扇叶片  等强度  轻量化设计  拓扑优化  双向渐进结构优化法
收稿时间:2011/11/29 0:00:00

Internal structure of three-dimensional hollow blade with equal strength
LI Lin and XUE Zheng.Internal structure of three-dimensional hollow blade with equal strength[J].Journal of Aerospace Power,2012,27(10):2329-2335.
Authors:LI Lin and XUE Zheng
Institution:School of Jet Propulsion, Beijing University of Aeronautics and Astronautics,Beijing 100191,China;School of Jet Propulsion, Beijing University of Aeronautics and Astronautics,Beijing 100191,China
Abstract:A research on the internal structure of the blade with equal strength was pressented.The research was based on bi-directional evolutionary structural optimization (BESO) method and ANSYS platform.In the topology optimization process of the internal structure of the blade,a method of stress reference on middle face was proposed to simplify the optimization model.Some special technical problems in the application of BESO were also solved.Finally,an optimized topological form of internal structure of the fan blade with equal strength was obtained.The results can provide a reference for the lightweight design of the aero-engine.
Keywords:aero-engine fan blades  equal strength  light weight design  topology optimization  BESO (bi-directional evolutionary structural optimization) method
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