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Process-scheme-driven automatic construction of NC machining cell for aircraft structural parts

查看参考文献28篇

文摘 In order to enhance the NC programming efficiency and quality of aircraft structural parts (ASPs), an intelligent NC programming pattern driven by process schemes is presented. In this pattern, the NC machining cell is the minimal organizational structure in the technological process, consisting of an operation machining volume cell, and the type and parameters of the machining operation. After the machining cell construction, the final NC program can be easily obtained in a CAD/CAM system by instantiating the machining operation for each machining cell. Accordingly, how to automatically establish the machining cells is a key issue in intelligent NC programming. On the basis of the NC machining craft of ASP, the paper aims to make an in-depth research on this issue. Firstly, some new terms about the residual volume and the machinable volume are defined, and then, the technological process is modeled with a process scheme. Secondly, the approach to building the machining cells is introduced, in which real-time complement machining is mainly considered to avoid interference and overcutting. Thirdly, the implementing algorithm is designed and applied to the Intelligent NC Programming System of ASP. Finally, the developed algorithm is validated through two case studies.
来源 Chinese Journal of Aeronautics ,2013,26(5):1324-1335 【核心库】
DOI 10.1016/j.cja.2013.07.035
关键词 Aircraft structural part (ASP) ; Automatic programming ; Machining cell ; Process planning ; Process scheme ; Residual volume
地址

1. School of Mechanical Engineering and Automation, Beihang University, Beijing, 100191  

2. Shenyang Aircraft Industry (Group) Corporation Ltd., Shenyang, 110034

语种 英文
文献类型 研究性论文
ISSN 1000-9361
学科 航空
基金 supported by National Science and Technology Major Project
文献收藏号 CSCD:4957390

参考文献 共 28 共2页

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引证文献 4

1 李春晖 飞机结构件加工域单元分层识别及构造方法 图学学报,2014,35(6):847-853
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2 王泓晖 基于加工特征的车间可重构式自动编程系统设计与实现 计算机集成制造系统,2016,22(10):2396-2407
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