郑州轻工业学院学报（自然科学版）Issue(5)：94-97,4.DOI:10.3969/j.issn.2095-476X.2014.05.021
基于 UG 的涡扇发动机风扇叶片变形分析方法研究
Study on simulation analysis method of turbafan engine fan blade on UG
赖晓琪 1郝艳华 1黄致建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
By the UG secondary development tools UG/OPEN API and NX OPEN C ++,and the integrated use of the C programming language,fan blade model,finite element model,simulation were created model parameterization on VS2008 platform.The measure of acguiring the information about the fan blade thick-ness information was also studied.The shell thickness of unit was loaded to mak it a solid shell element with physical properties.Solid shell element was used to mesh the fan blade in simulation analysis.Under the same calculation model,compared solid element and solid shell element analysis results,the solid shell element could effectively reduce computing scale(24.65%)and calculation time(45.97%)so it improved the computing efficiency,and reduced the computing time.关键词
UG 二次开发/参数化建模/涡扇发动机风扇叶片/中弧面模型/实体壳模型Key words
UG secondary development/parametric modeling/turbafan engine fan blade/central arced sur-face model/solid model分类
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赖晓琪,郝艳华,黄致建..基于 UG 的涡扇发动机风扇叶片变形分析方法研究[J].郑州轻工业学院学报（自然科学版）,2014,(5):94-97,4.
