Development of Bolted Flange Design Tool Based on Artificial Neural Network

Abstract

Finite element analysis (FEA) of bolted flange connections is the common methodology for the analysis of bolted flange connections. However, it requires high computational power for model preparation and nonlinear analysis due to contact definitions used between the mating parts. Design of an optimum bolted flange connection requires many costly finite element analyses to be performed to decide on the optimum bolt configuration and minimum flange and casing thicknesses. In this study, very fast responding and accurate artificial neural network-based bolted flange design tool is developed. Artificial neural network is established using the database which is generated by the results of more than 10,000 nonlinear finite element analyses of the bolted flange connection of a typical aircraft engine. The FEA database is created by taking permutations of the parametric geometric design variables of the bolted flange connection and input load parameters. In order to decrease the number of FEA points, the significance of each design variable is evaluated by performing a parameter correlation study beforehand, and the number of design points between the lower and upper and bounds of the design variables is decided accordingly. The prediction of the artificial neural network based design tool is then compared with the FEA results. The results show excellent agreement between the artificial neural network-based design tool and the nonlinear FEA results within the training limits of the artificial neural network.

Conceptual design modeling by the novel aircraft conceptual design and analysis system (ACDAS)

“…At recent years, the software usage for (conceptual) design processes has been increasing dramatically depending on the importance of cost reduction at aviation (Park et al , 2009; Brelje and Martins, 2019; Yıldırım et al , 2019; Xie et al , 2021). Comprehensive and important projects were initiated like Simulating Aircraft Stability and Control Characteristics (SimSAC), which was supported by the European Commission (Rizzi, 2011) (“Simulating Aircraft Stability and Control Characteristics for use in Conceptual Design,” available at: https://trimis.ec.europa.eu/project/simulating-aircraft-stability-and-control-characteristics-use-conceptual-design [accessed 10 February 2021]).…”