Optimization of fastener pattern in airframe assembly. Issue 5 (24th June 2020)
- Record Type:
- Journal Article
- Title:
- Optimization of fastener pattern in airframe assembly. Issue 5 (24th June 2020)
- Main Title:
- Optimization of fastener pattern in airframe assembly
- Authors:
- Lupuleac, Sergey
Pogarskaia, Tatiana
Churilova, Maria
Kokkolaras, Michael
Bonhomme, Elodie - Abstract:
- Abstract : Purpose: The authors consider the problem of optimizing temporary fastener patterns in aircraft assembly. Minimizing the number of fasteners while maintaining final product quality is one of the key enablers for intensifying production in the aerospace industry. The purpose of this study is to formulate the fastener pattern optimization problem and compare different solving approaches on both test benchmarks and rear wing-to-fuselage assembly of an Airbus A350-900. Design/methodology/approach: The first considered algorithm is based on a local exhaustive search. It is proved to be efficient and reliable but requires much computational effort. Secondly, the Mesh Adaptive Direct Search (MADS) implemented in NOMAD software (Nonlinear Optimization by Mesh Adaptive Direct Search) is used to apply the powerful mathematical machinery of surrogate modeling and associated optimization strategy. In addition, another popular optimization algorithm called simulated annealing (SA) was implemented. Since a single fastener pattern must be used for the entire aircraft series, cross-validation of obtained results was applied. The available measured initial gaps from 340 different aircraft of the A350-900 series were used. Findings: The results indicated that SA cannot be applicable as its random character does not provide repeatable results and requires tens of runs for any optimization analysis. Both local variations (LV) method and MADS have proved to be appropriate as theyAbstract : Purpose: The authors consider the problem of optimizing temporary fastener patterns in aircraft assembly. Minimizing the number of fasteners while maintaining final product quality is one of the key enablers for intensifying production in the aerospace industry. The purpose of this study is to formulate the fastener pattern optimization problem and compare different solving approaches on both test benchmarks and rear wing-to-fuselage assembly of an Airbus A350-900. Design/methodology/approach: The first considered algorithm is based on a local exhaustive search. It is proved to be efficient and reliable but requires much computational effort. Secondly, the Mesh Adaptive Direct Search (MADS) implemented in NOMAD software (Nonlinear Optimization by Mesh Adaptive Direct Search) is used to apply the powerful mathematical machinery of surrogate modeling and associated optimization strategy. In addition, another popular optimization algorithm called simulated annealing (SA) was implemented. Since a single fastener pattern must be used for the entire aircraft series, cross-validation of obtained results was applied. The available measured initial gaps from 340 different aircraft of the A350-900 series were used. Findings: The results indicated that SA cannot be applicable as its random character does not provide repeatable results and requires tens of runs for any optimization analysis. Both local variations (LV) method and MADS have proved to be appropriate as they improved the existing fastener pattern for all available gaps. The modification of the MADS' search step was performed to exploit all the information the authors have about the problem. Originality/value: The paper presents deterministic and probabilistic optimization problem formulations and considers three different approaches for their solution. The existing fastener pattern was improved. … (more)
- Is Part Of:
- Assembly automation. Volume 40:Issue 5(2020)
- Journal:
- Assembly automation
- Issue:
- Volume 40:Issue 5(2020)
- Issue Display:
- Volume 40, Issue 5 (2020)
- Year:
- 2020
- Volume:
- 40
- Issue:
- 5
- Issue Sort Value:
- 2020-0040-0005-0000
- Page Start:
- 723
- Page End:
- 733
- Publication Date:
- 2020-06-24
- Subjects:
- Optimization -- Assembly process -- Simulated annealing -- Mesh adaptive direct search -- Temporary fastening element
Automation -- Periodicals
Automatic machinery -- Periodicals
Assembly-line methods -- Periodicals
Industrial engineering -- Periodicals
670.42705 - Journal URLs:
- http://www.emerald-library.com/0144-5154.htm ↗
http://www.emeraldinsight.com/journals.htm?issn=0144-5154 ↗
http://www.emeraldinsight.com/ ↗
http://firstsearch.oclc.org ↗ - DOI:
- 10.1108/AA-03-2019-0040 ↗
- Languages:
- English
- ISSNs:
- 0144-5154
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 1746.606200
British Library DSC - BLDSS-3PM
British Library STI - ELD Digital store - Ingest File:
- 22218.xml