摘要
飞机装配中的自动制孔工艺设计包括基准设计、夹紧孔设计和自动制孔设计,为了在保证自动制孔要求的前提下快速自动实现夹紧孔设计,提出了保证夹紧孔最大间距和自动制孔基本要求的夹紧孔设计算法,给出了具体的实施方法,开发了夹紧孔设计的原型模块,并进行了验证。该方法对于提高夹紧孔设计的效率、保证自动制孔的准确性和稳定性具有重要意义。
Automatic hole-making in the assembly of aircraft includes the design of reference holes,clamping holes and automatic making holes. And the quick and automatic design of clamping holes is a key problem. In this paper,an algorithm for the clamping holes design w as proposed to ensure the maximum spacing betw een any tw o clamping holes and satisfy the basic requirements of automatic hole-making. Details of the design w ere provided and the prototype module w as developed and verified. This algorithm is significant to improve the efficiency of the clamping holes design and to ensure accuracy and stability of the automatic hole-making.
出处
《沈阳航空航天大学学报》
2017年第5期21-25,共5页
Journal of Shenyang Aerospace University
基金
国防重点实验室开放基金(项目编号:SHSYS2015001)
