郑州轻工业学院学报（自然科学版）Issue(5)：89-93,5.DOI:10.3969/j.issn.2095-476X.2014.05.020
基于 UG NX 二次开发的压气机叶片结构优化设计
Structure optimization design of compressor blade based on UG NX secondary development
邹驰宇 1黄致建 1郝艳华1
作者信息
- 1. 华侨大学 机电及自动化学院，福建 厦门 361021
- 折叠
摘要
Abstract
Taking a compressor blade as subject,the mathematical model of a compressor blade was estab-lished to ensure that it would not distort when it was modeled.With the UG NX secondary development and C ++,the compressor blade was optimized to obtain the lightest structure that can satisfy the strength and vibration,based on the finite element analysis.The results showed that the compressor blade was modeled without error in the iterative process.And the optimal volume (mass)of the axial compressor blade was re-duced by 6.680% than origin which could satisfied the work requirement that the original structure didn’ t.The total method of the structural optimization was effective and feasible and could be used in the design process of other mechanical products.关键词
压气机叶片/UG NX 二次开发/参数化/结构优化设计Key words
compressor blade/UG NX secondary development/parameterization/structure optimization design分类
航空航天引用本文复制引用
邹驰宇,黄致建,郝艳华..基于 UG NX 二次开发的压气机叶片结构优化设计[J].郑州轻工业学院学报（自然科学版）,2014,(5):89-93,5.
