Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures

HAI Yu; ZHOU Laishui; AN Luling

doi:10.16080/j.issn1671-833x.2023.01/02.084

您当前的位置：

首页 >

文章列表页 >

Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures

更新时间：2025-10-30

- Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures
- Aeronautical Manufacturing Technology Vol. 66, Issue 1/2, (2023)
- 作者机构：
  
  南京航空航天大学,南京,210016
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2023.01/02.084
  CLC：
- Published：2023
- 稿件说明：
移动端阅览
海宇，周来水，安鲁陵. 复合材料热压罐固化框架式成型模具的参数化设计[J]. 航空制造技术, 2023, 66(1/2): 84-91. HAI Yu, ZHOU Laishui, AN Luling. Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2): 84-91.

HAI Yu, ZHOU Laishui, AN Luling. Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2).
海宇，周来水，安鲁陵. 复合材料热压罐固化框架式成型模具的参数化设计[J]. 航空制造技术, 2023, 66(1/2): 84-91. HAI Yu, ZHOU Laishui, AN Luling. Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2): 84-91. DOI： 10.16080/j.issn1671-833x.2023.01/02.084.

HAI Yu, ZHOU Laishui, AN Luling. Parametric Design of Framed-Mold in Autoclave Processing for Composite Structures[J]. Aeronautical Manufacturing Technology, 2023, 66(1/2). DOI： 10.16080/j.issn1671-833x.2023.01/02.084.

摘要

为解决复合材料热压罐固化框架式成型模具设计过程中重复性工作较多、设计效率较低、后续修改困难等问题，将参数化设计技术分为尺寸和拓扑结构的参数化设计两个方面，并运用于模具设计中。模具尺寸的参数化设计在分析模具结构特点的基础上，提取出模具的主要设计参数，利用自顶向下的设计思路规划了模具的参数化设计流程；引入参数追溯概念，提出对主要设计参数进行追溯的方法，以便通过参数驱动模具尺寸的快速修改。模具拓扑结构的参数化设计结合CATIA 的知识工程模块与面向对象的技术，实现参数化变更模具的拓扑结构。基于CATIACAA 二次开发平台，开发了复合材料固化框架式成型模具参数化设计系统，并给出实例验证。

Abstract

In order to solve the problems of repetitive work

low design efficiency and difficulty in subsequent modification in the design procedure of framed-mold in autoclave processing for composites structures

the parametric design technology which is applied to the design of the mold

is divided into two aspects: the parametric design of dimensions and the parametric design of topological structures. In terms of parametric design of dimensions

based on the analysis of structural characteristics of the mold

the main design parameters of the mold are extracted

and the parametric design process is planned using the top-down design method. The concept of parameters tracing and the method of tracing main design parameters are proposed so as to modify the dimensions of the mold rapidly through parameters. In aspect of parametric design of topological structures

some topological structures of the mold can be modified parametrically by combining the knowledge engineering module of CATIA with object-oriented technology. Based on CATIA CAA secondary development platform

a parametric design system of mold in autoclave processing for composites structures is developed and verified with examples.

关键词

Keywords

references

Views

191

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Research on Influence of Tightening Sequence and Assembly Gap on Preloading Force of Composites/Aluminum Alloy Laminated Multi-Bolt Structure

Research on Ultrasonic C-Scan Images Denoising and Super-Resolution Reconstruction for Composite Components

Contact Stress Simulation and Defect Study of Contour-Following Layups for Heat Protective Structures

A General Braiding Simulation Method for Special-Shaped Braiding Structural Parts Based on Model Reconstruction Algorithm

A Review of Preparation and Performance of High-Strength and High-Modulus Casting Mg–Li Alloy

Related Author

LIU Zhitong

AN Luling

ZHAO Cong

QU Zhengtao

XU Zhenye

LIU Zhenhao

QIAN Hengkui

JIN Shijie

Related Institution

Nanjing University of Aeromautics and Astronautics

NDT & E Laboratory, Dalian University of Technology

Key Lab of High Performance Electromagnetic Window for Aviation Science and Technology, AVIC Research Institute for Special Structures of Aeronautical Composites

College of Mechanical Engineering, Donghua University

AVIC Chengdu Aircraft Industrial (Group) Co., Ltd.

The platform construction and operation are provided by Beijing Founder electronics co., LTD 京ICP备09064830号-19 京公网安备11010802024621
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.
Total Visits：34462 Visits Today：409

⁰