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

Author:

Krieglsteiner Joscha,Horst Peter,Schmidt Carsten

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.

Publisher

Emerald

Subject

Aerospace Engineering

Reference47 articles.

1. Formation of voids in composite laminates: coupled effect of moisture content and processing pressure;Polymer Composites,2015

2. Arnold, P. and Rudolph, S. (2012), “Bridging the gap between product design and product manufacturing by means of graph-based design languages”, Paper Presented at 9th International Symposium on Tools and Methods of Competitive Engineering, 7-11 May, Karlsruhe.

3. Beilstein, L.T. (2012), “Eine Methodik zur analytischen Gewichtsabschätzung und Bewertung von Strukturverbindungen im Flugzeugvorentwurf”, Dissertation, Institute of Aircraft Design, Universität Stuttgart, Stuttgart.

4. Bieling, U. (2014), “Reference structure design principles: the basis for A350XWB design”, available at: www.cfk-convention.com/fileadmin/Convention_2014/Referenten/Vortraege/CFK_Conv2014_Bieling.pdf (accessed 23 August 2017).

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3