DocumentCode :
538738
Title :
Digitally Adjustable Tooling Technology for Manufacturing of Aircraft Panels
Author :
Chunguo, Liu ; Mingzhe, Li ; Zhongyi, Cai ; Aimin, Yan ; Shizhong, Su
Author_Institution :
Roll-Forging Res. Inst., Jilin Univ., Changchun, China
Volume :
1
fYear :
2010
fDate :
18-20 Dec. 2010
Firstpage :
556
Lastpage :
559
Abstract :
Digitally adjustable tooling using multi-point forming methodology is a flexible manufacturing technology for aircraft panels. It includes multi-point press forming and multi-point stretch forming which are used in the forming of three dimensional aluminum alloy panels and multi-point positioning tool which is used in subsequent assembly operation. The deformation mechanism of the multi-point die less forming and positioning technology were analyzed with commercial FEM codes. The forming defects such as dimpling and spring back in forming were investigated and the preventing measures were proposed. The factors which affect the performance of multi-point positioning tool were given. Based the simulation results, three types of prototypes were developed under the supporting of EC 6th programme project DATAFORM.
Keywords :
aerospace components; aluminium alloys; assembling; deformation; dies (machine tools); finite element analysis; flexible manufacturing systems; pressing; prototypes; sheet metal processing; DATAFORM; FEM; aircraft panel manufacturing; assembly; deformation mechanism; digitally adjustable tooling technology; flexible manufacturing technology; multipoint dieless forming; multipoint positioning tool; multipoint press forming; multipoint stretch forming; prototypes; three dimensional aluminum alloy panels; Multi-point forming methodology; aircraft panel; digitally adjustable tooling; prototype; simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Manufacturing and Automation (ICDMA), 2010 International Conference on
Conference_Location :
ChangSha
Print_ISBN :
978-0-7695-4286-7
Type :
conf
DOI :
10.1109/ICDMA.2010.92
Filename :
5701220
Link To Document :
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