An Optimization Method Selecting the Location Points for Drilling and Riveting of Aircraft’s Wing Panel

Kai Fu Zhang; Feng Gang Liu; Zhen Xing Liu; Yuan Li

doi:10.4028/www.scientific.net/AMM.80-81.1103

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 80-81An Optimization Method Selecting the Location...

An Optimization Method Selecting the Location Points for Drilling and Riveting of Aircraft’s Wing Panel

Abstract:

In order to select the optimal location points for automated drilling and riveting process, an optimization method selecting the location points of Aircraft’s Wing Panel in Automatic Drilling and Riveting System is presented. This method includes three steps: 1) building the matching model based on the multiplicity; 2) presenting the matching method based on scatter search algorithm; 3) selecting the optimal location points according to the minimal deviation based on linear programming method. This method was applied in a panel to match the mathematical surface and the fitting one of this panel perfectly and select the optimal location points. The efficacy and quality during the process of drilling and riveting of this panel was improved greatly.

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Periodical:

Applied Mechanics and Materials (Volumes 80-81)

Pages:

1103-1108

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.80-81.1103

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Online since:

July 2011

Authors:

Kai Fu Zhang, Feng Gang Liu, Zhen Xing Liu, Yuan Li

Keywords:

Location Point, Optimization, Scatter Search Algorithm (SSA), Surface Matching

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