A parametric lightweight turbine disk structure CAD/CAE integration method

LUO Bin; DING Shui-ting; LI Guo

Chinese

您当前的位置：

首页 >

文章列表页 >

A parametric lightweight turbine disk structure CAD/CAE integration method

更新时间：2026-07-07

- A parametric lightweight turbine disk structure CAD/CAE integration method
- Vol. 28, Issue 9, (2013)
- 作者机构：
  
  北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室适航技术研究中心,北京,100191
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2013
- 稿件说明：
移动端阅览
LUO Bin, DING Shui-ting, LI Guo. A parametric lightweight turbine disk structure CAD/CAE integration method[J]. 2013, 28(9).
DOI：

LUO Bin, DING Shui-ting, LI Guo. A parametric lightweight turbine disk structure CAD/CAE integration method[J]. 2013, 28(9). DOI：

摘要

针对一种轻量化涡轮盘结构的特点

分析了参数化CAD/CAE集成过程的文件与输入参数的关联性.编写C/C++程序

利用UG/OPEN API实现参数化建模

通过修改脚本并基于单向流固耦合算法有序调用CAE软件执行脚本的方式实现关联文件与输入参数关联

从而实现参数化涡轮盘CAD/CAE过程自动集成.程序运行效果显示

相比人工执行同样的一次CAD/CAE流程

该方法至少要快54min

说明了该方法有效提高了轻量化涡轮盘的设计分析效率.

Abstract

The relevance between input parameters and the files of parametric computer aided design(CAD)/computer aided engineering(CAE) integration was analyzed based on the lightweight turbine disk structure's characteristics.C/C++ program was compiled

and software UG/OPEN API was used to accomplish parametric modeling.CAE softwares were called sequentially to run the scripts modified based on one-way fluid structure interaction method to insure the relevance between input parameters and relevant files.Thus

the automated integration of parametric lightweight turbine disk CAD/CAE process was achieved.The program running results show that compared with the manual work which is the same with CAD/CAE process

this method costs less than 54 min

proving that the design and analysis efficiency is improved effectively.

关键词

Keywords

references

Views

897

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

High⁃efficiency DSMC implement method based on combination of dual spatial grids

Fault diagnosis of helicopter rolling bearing based on improved SqueezeNet

Simulation method of short crack propagation in turbine disks based on crystal plasticity

Fatigue life prediction method based on the features of surface defects

Fatigue life evaluation procedure and its application for turbine disk

Related Author

Songwei DU

Xuede WANG

Zhifeng YU

Bangshu XIONG

Xinmin LI

Qiaofeng OU

Ping ZHANG

Shan LU

Related Institution

School of Energy and Power Engineering，Nanjing University of Science and Technology

Provincial Key Laboratory of Image Processing and Pattern Recognition，Nanchang Hangkong University

Science and Technology on Rotorcraft Aeromechanics Laboratory，China Helicopter Research and Development Institute，Aviation Industry Corporation of China，Limited

Nondestructive Testing and Evaluation Laboratory， Dalian University of Technology

College of Civil Engineering， Hefei University of Technology

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰