Aircraft wing box rapid modeling based on skeleton model  

作　　者：Zhang Chao Xi Ping 

机构地区：[1]School of Mechanical Engineering and Automation,Beihang University

出　　处：《Computer Aided Drafting,Design and Manufacturing》2016年第4期30-36,共7页计算机辅助绘图设计与制造（英文版）

摘　　要：In the process of traditional aircraft structure design, repetitive manual modeling of aircraft wing box parts is time consuming. Meanwhile, it＇s difficult to update associated models when product design changes. Aiming at solving these problems, a method for rapid modeling and updating associated models was put forward. Based on skeleton model, combining with the technology of template re-use, it makes aircraft wing box rapid modeling and correct updating possible. The detailed implementation process of the method was given, and a certain aircraft wing box was taken as an instance to verify the feasibility and effectiveness of this method.In the process of traditional aircraft structure design, repetitive manual modeling of aircraft wing box parts is time consuming. Meanwhile, it＇s difficult to update associated models when product design changes. Aiming at solving these problems, a method for rapid modeling and updating associated models was put forward. Based on skeleton model, combining with the technology of template re-use, it makes aircraft wing box rapid modeling and correct updating possible. The detailed implementation process of the method was given, and a certain aircraft wing box was taken as an instance to verify the feasibility and effectiveness of this method.

关 键 词：skeleton model parametric template template re-use rapid modeling 

分 类 号：V224[航空宇航科学与技术—飞行器设计]