A flexible development system for automated aircraft assembly

被引:0
|
作者
Inman, J
Carbrey, B
Calawa, R
Hartmann, J
Hempstead, B
Assadi, M
机构
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
McDonnell Douglas Aircraft in St. Louis, MO manufacturers various transport and fighter military aircraft such as the C-17 and the F/A-18. With shrinking military budgets and increased competition, market forces demand high quality parts at lower cost and shorter lead times. Currently, a large number of different fastener types which include both solid rivets and interference bolts are used to fasten these assemblies. The majority of these fasteners are installed by hand or by using manually operated C-Frame riveters. MDA engineers recognized that in order to reach their goals they would be required to rethink all phases of the assembly system, which includes fastener selection, part fixturing and fastener installation methods. Phase 1 of this program is to identify and to develop fastener installation processes which will provide the required flexibility. The EMR fastening process provides this flexibility. While EMR is currently used in production on a number of aircraft programs around the world, it has only been qualified for limited use within MDA. In conjunction with MDA engineers, Electroimpact designed and built an automated EMR development system. The test bench system has complete automated riveting and Lockbolt insertion capability. The test bench platform provides the means to optimize, validate and prequalify the fastener installation process prior to delivery of the full production system. After production implementation, the test bench can be utilized for the development of new processes or for investigating production problems off-line.
引用
收藏
页码:49 / 58
页数:10
相关论文
共 50 条
  • [21] The design of a flexible fixture & workcell for aircraft assembly
    Li, YJ
    Bahr, B
    Chen, XB
    CAD/CAM ROBOTICS AND FACTORIES OF THE FUTURE, 1996, : 248 - 255
  • [22] Flexible automated assembly of laminar products
    Feldmann, K
    Licha, A
    ROBOTIK 2002, 2002, 1679 : 27 - 32
  • [23] Flexible automated assembly of laminar products
    Feldmann, K.
    Licha, A.
    VDI Berichte, 2002, (1679): : 27 - 32
  • [24] Automated aircraft rework system
    Aerosp Eng (Warrendale PA), 1-2 (19):
  • [25] Automated aircraft - Rework system
    不详
    AEROSPACE ENGINEERING, 1996, 16 (1-2) : 19 - 23
  • [26] Development of a Flexible Assembly System for the World Robot Summit 2020 Assembly Challenge
    Xu, Lizhou
    Heravi, Farshad Nozad
    Lahoud, Marcel Gabriel
    Marchello, Gabriele
    D'Imperio, Mariapaola
    Abidi, Syed Haider Jawad
    Farajtabar, Mohammad
    Martini, Michele
    Cocuzza, Silvio
    Scaccia, Massimiliano
    Cannella, Ferdinando
    JOURNAL OF ROBOTICS AND MECHATRONICS, 2023, 35 (01) : 51 - 64
  • [27] Study on the Measurement Adied Assembly Technology of Aircraft Flexible Assembly Tool
    Qu Ligang
    Dong Zhiliang
    Zhou Haijun
    2014 IEEE INTERNATIONAL CONFERENCE ON CONTROL SCIENCE AND SYSTEMS ENGINEERING, 2014, : 66 - 69
  • [28] The development of specifications for an automated monitoring system interface associated with aircraft condition
    Deaton, JE
    Glenn, FA
    INTERNATIONAL JOURNAL OF AVIATION PSYCHOLOGY, 1999, 9 (02): : 175 - 187
  • [29] Development of Visualization System for Aircraft Assembling Process Oriented Assembly Field
    Qu, Ligang
    Zheng, Shuang
    Guo, Hongjie
    MANUFACTURING PROCESS TECHNOLOGY, PTS 1-5, 2011, 189-193 : 296 - +
  • [30] A FLEXIBLE ASSEMBLY SYSTEM
    SCHRODER, M
    WERKSTATTSTECHNIK ZEITSCHRIFT FUR INDUSTRIELLE FERTIGUNG, 1981, 71 (01): : 33 - 38