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Process-scheme-driven automatic construction of NC machining cell for aircraft structural parts
Alternative TitleProcess-scheme-driven automatic construction of NC machining cell for aircraft structural parts
Chen Shulin1; Zheng Guolei1; Zhou Min1; Du Baorui2; Chu Hongzhen2
2013
Source PublicationCHINESE JOURNAL OF AERONAUTICS
ISSN1000-9361
Volume26Issue:5Pages:1324-1335
AbstractIn 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. (C) 2013 Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA.
Other AbstractIn 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.
KeywordTOOL-PATH GENERATION OPERATIONS SELECTION SYSTEM SURFACES FEATURES Aircraft structural part (ASP) Automatic programming Machining cell Process planning Process scheme Residual volume
Indexed ByCSCD
Language英语
Funding Project[National Science and Technology Major Project]
CSCD IDCSCD:4957390
Citation statistics
Cited Times:3[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://ir.imr.ac.cn/handle/321006/151057
Collection中国科学院金属研究所
Affiliation1.北京航空航天大学
2.中国科学院金属研究所
Recommended Citation
GB/T 7714
Chen Shulin,Zheng Guolei,Zhou Min,et al. Process-scheme-driven automatic construction of NC machining cell for aircraft structural parts[J]. CHINESE JOURNAL OF AERONAUTICS,2013,26(5):1324-1335.
APA Chen Shulin,Zheng Guolei,Zhou Min,Du Baorui,&Chu Hongzhen.(2013).Process-scheme-driven automatic construction of NC machining cell for aircraft structural parts.CHINESE JOURNAL OF AERONAUTICS,26(5),1324-1335.
MLA Chen Shulin,et al."Process-scheme-driven automatic construction of NC machining cell for aircraft structural parts".CHINESE JOURNAL OF AERONAUTICS 26.5(2013):1324-1335.
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