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Flexible Assembly System Implementation
ISSN: 0148-7191, e-ISSN: 2688-3627
Published October 06, 1999 by SAE International in United States
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This paper covers issues related to the installation, testing, and production implementation of a large-scale automated wing drilling/fastener installation system. Emphasis is placed on describing the production process, foundation requirements, axes alignment, calibration, testing and implementation. Description will include key hardware features such as the multi-function end effector and spindle end effector. The objective is to convey the complexity of implementing this system as well as reviewing the lessons learned from this experience.
CitationSalour, A. and Cunov, J., "Flexible Assembly System Implementation," SAE Technical Paper 1999-01-3447, 1999, https://doi.org/10.4271/1999-01-3447.
- Ali Salour, James Cunov, Philippe Prat, Flexible Assembly System SAE 1998 Aerofast Conference, paper 982150
- Cunov, J.R. LaValle, D.R. Marrinan, T.E. Optimum Machine Configurations for Automated Wing Assembly SAE 1997 Aerofast Conference, paper 972813
- DaCosta, S.J. Carpentier, J.P. LeCann, R.P. PEGASUS, A New Programming Method SAE 1997 Aerofast Conference, paper 972814