飞机部件级的数字化柔性工装设计  

Design of Digital Flexible Assembly Tooling on Aircraft Component

作　　者：王仲奇[1] 康永刚[1] 王辉坪[1] 杨勃[1] 

机构地区：[1]西北工业大学机电学院

出　　处：《航空制造技术》2011年第22期101-104,共4页Aeronautical Manufacturing Technology

基　　金：国防基础科研项目(B062006034)资助

摘　　要：基于对数字化柔性装配技术的深入分析,结合数字化测量和误差补偿方法、工装模块化设计等,针对某型号飞机前襟翼装配,设计一套数字化柔性装配系统,该系统可以实现内外前襟及其左右对称件4个部件的数字化装配,为提高飞机前襟翼的装配质量稳定性和装配效率,缩短生产准备周期提供了保障,同时为飞机部件级数字化柔性工装设计提供了一个范例。According to the analysis of assembly techniques and methods on the existing front aircraft flaps, a digital flexible assembly method on certain front aircraft flaps is proposed, and a set of flexible assembly tooling is designed. This solves the status that it can not be reconciled and only assembly a single product on rigid tooling, as the flexible one changes its structure and the locating of products. This digital flexible tooling can assembly four types front flaps on aircraft, improve assembly quality and effi ciency effectively, and shorten production cycle.

关 键 词：数字化 柔性 工装 定位 

分 类 号：V262.42[航空宇航科学与技术—航空宇航制造工程]