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Definition and representation of stiffened shell structures in the context of an integrated development process

Joscha Krieglsteiner (Institute of Aircraft Design and Lightweight Structures, Technische Universität Braunschweig, Braunschweig, Germany)
Peter Horst (Institute of Aircraft Design and Lightweight Structures, Technische Universität Braunschweig, Braunschweig, Germany)
Carsten Schmidt (Institute of Production Engineering and Machine Tools, Leibniz Universitat Hannover, Hannover, Germany)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 4 March 2019

Issue publication date: 17 May 2019

170

Abstract

Purpose

A novel development process aims at finding solutions for lightweight stiffened shell structures and their efficient production. To respect the strong interdependency of structural design and production planning, particularly observed for composite structures, it is of high interest to start considering production effects in early development phases. This integrated approach requires an integrated representation of structure and production. The purpose of this study is to investigate the scope of relevant data and to find a structure for its representation.

Design/methodology/approach

The development task is analyzed and a system of so-called solution dimensions is presented, which covers all important aspects of stiffened shell structures and their production. An integrated product data model is developed to cover all of the solution dimensions.

Findings

The product data model consists of five coherent partial models. It is explained how these models are defined and how they are connected to each other. An academic example of an aircraft fuselage panel is used to demonstrate the definition process. It is shown how even complex structural concepts are defined systematically.

Practical implications

It is explained how this integrated product data model is used in a software project for the development of aircraft fuselage structures.

Originality/value

The presented approach for the definition and representation of stiffened shell structures enables the developer, e.g. of aircraft fuselage, to respect the crucial criterion of manufacturability from early development phases on. Further, new design approaches, e.g. as inspired by topology optimization, can be considered.

Keywords

Acknowledgements

The authors would like to thank the German Research Foundation for the support of the project Integrated method for process planning and structural design of composite structures (ProDesign, HO 2122/26-1) and the federal state of Lower Saxony and the European Regional Development Fund (ERDF) for financial and organizational support of the project: High-Performance Production of CFRP Structures (HP CFK).

Citation

Krieglsteiner, J., Horst, P. and Schmidt, C. (2019), "Definition and representation of stiffened shell structures in the context of an integrated development process", Aircraft Engineering and Aerospace Technology, Vol. 91 No. 4, pp. 607-619. https://doi.org/10.1108/AEAT-07-2018-0205

Publisher

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Emerald Publishing Limited

Copyright © 2019, Emerald Publishing Limited

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