基于TRIZ理论的飞机蜂窝芯零件数控加工固持方法研究
2018-12-20
作者：刘元吉，刘适，姜振喜
单位：航空工业成都飞机工业（集团）有限责任公司数控加工厂
摘要：针对蜂窝芯零件数控加工装夹固持出现的效率低、稳定性差、成本高等问题，应用TRIZ理论及相应工具，对其工艺流程进行了系统功能分析，运用矛盾矩阵及创新原理，提出了一种新型的、更为经济的真空吸附装夹方式，并得到了成功的应用。
关键词：TRIZ理论；蜂窝芯圊持；系统功能分析；矛盾矩阵；创新原理
中图分类号：TG659；TH161文献标志码：A
Research of Aircraft Honeycomb Core Component Clamping Method for
NC Machining Based on TRIZ Theory
Liu Yuanji，Liu Shi，Jiang Zhenxi
Abstract:As technical issues，such as low efficiency，unsteadiness and high cost，of honeycomb clamping exist，this article uses TRIZ theory and related tools，applies system functional analysis on the engineering procedure and finds out a new and more economical clamping method using vacuum adsorbing by innovation tools of contradiction matrix and innovation principles，and this improvement has been successfully implemented in honeycomb core clamping.
Keywords:TRIZ theory；honeycomb core clamping；system functional analysis；contradiction matrix；innovation principles