摘要
通过分析飞行器结构装配的特点和难点,在分析虚拟装配的特征和关键的基础上,引入虚拟装配方法,对复杂飞行器结构设计中的虚拟装配实施方案进行探讨和应用,并作出与装配相关的工程决策,可以有效地提高产品装配质量和速度,能够有效地减少设计过程中由于装配而导致的设计反复。
By analyzing the characteristics and difficulties of assembly of aircraft structure, and analyzing the characteristics and the key of virtual assembly, the method of virtual assembly is introduced. The implementation plan of virtual assembly for complex missile structure is focused on, and engineering decision related to virtual assembly is made , which can effectively improve reduce design error by assembly in product design.
出处
《机械研究与应用》
2014年第4期125-127,共3页
Mechanical Research & Application
关键词
飞行器
虚拟装配
结构设计
aircraft
virtual assembly
structure design