Optimization of Automated Airframe Assembly Process on Example of A350 S19 Splice Joint 2019-01-1882
The paper presents the numerical approach to simulation and optimization of A350 S19 splice assembly process. The main goal is to reduce the number of installed temporary fasteners while preventing the gap between parts from opening during drilling stage. The numerical approach includes computation of residual gaps between parts, optimization of fastener pattern and validation of obtained solution on input data generated on the base of available measurements. The problem is solved with ASRP (Assembly Simulation of Riveting Process) software. The described methodology is applied to the optimization of the robotized assembly process for A350 S19 section.
Citation: Lupuleac, S., Shinder, J., Churilova, M., Zaitseva, N. et al., "Optimization of Automated Airframe Assembly Process on Example of A350 S19 Splice Joint," SAE Technical Paper 2019-01-1882, 2019, https://doi.org/10.4271/2019-01-1882. Download Citation
Author(s):
Sergey Lupuleac, Julia Shinder, Maria Churilova, Nadezhda Zaitseva, Valeriia Khashba, Elodie Bonhomme, Pedro Montero-Sanjuan
Affiliated:
Peter the Great St. Petersburg Polytechnic University, Airbus
Pages: 5
Event:
AeroTech Europe
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Assembling
Fastening
Fasteners
Automation
Optimization
Simulation and modeling
Parts
Drilling
Airframes
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