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基于CATIA的飞机结构件参数化设计
引用本文:梁振刚,程学朋.基于CATIA的飞机结构件参数化设计[J].成组技术与生产现代化,2012,29(2):55-57.
作者姓名:梁振刚  程学朋
作者单位:沈阳理工大学,辽宁沈阳,110168
摘    要:以CAA作为CAITA的二次开发工具,采用面向对象和可视化界面编程技术,针对飞机结构件开发出参数化设计系统,对特征模板进行交互式参数化设计,提高了对已有设计资源的利用率,实现飞机结构件的快速响应设计.

关 键 词:CATIA  飞机结构件  参数化设计

The Parametric Design of Aircraft Structural Parts based on CATIA
LIANG Zhen-gang , CHENG Xue-peng.The Parametric Design of Aircraft Structural Parts based on CATIA[J].Group Technology & Production Modernization,2012,29(2):55-57.
Authors:LIANG Zhen-gang  CHENG Xue-peng
Affiliation:(Shenyang Ligong University,Shenyang 110168,China)
Abstract:aircraft structural parts are the important parts of the plane,and also the important basis of the the design,manufacture and obtaining higher efficiency and good performance.Using CAA CAITA for parametric design system is developed,which can improve the efficiency of designing aircraft structure parts and the utilization rate of the existing resource.
Keywords:CATIA  aircraft structural parts  parametric design
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