The paper is devoted to the simulation of A320 wing assembly on the base of numerical experiments carried out with the help of ASRP software. The main goal is to find fasteners’ configuration with minimal number of fastening elements that provides closing of admissible initial gaps.However, for considered junction type initial gap field is not known a priori though it should be provided as input data for computations. In order to resolve this problem the methodology of random initial gap generation based on available results of gap measurements is developed along with algorithms for optimization of fasteners' configuration on generated initial gaps.Presented paper illustrates how this methodology allows optimizing assembly process for A320 wing.
Combination of Experimental and Computational Approaches to A320 Wing Assembly
Sae Technical Papers
AeroTech Congress & Exhibition ; 2017
2017-09-19
Aufsatz (Konferenz)
Englisch
Combination of Experimental and Computational Approaches to A320 Wing Assembly
British Library Conference Proceedings | 2017
|Wing-strike raises A320 limit doubts
Online Contents | 2010
Wing Assembly System for British Aerospace Airbus for the A320
British Library Conference Proceedings | 1998
|Wing Assembly System for British Aerospace Airbus for the A320
SAE Technical Papers | 1998
|Programme Airbus A320 (A320 Airbus Program)
NTIS | 1987
|