A knowledge‐based engineering tool to estimate cost and weight of composite aerospace structures at the conceptual stage of the design process

Author:

Choi Jin‐Woo,Kelly Don,Raju John

Abstract

PurposeThis paper seeks to address issues related to the development of a knowledge‐based engineering system for estimating manufacturing cost and weight of a composite structure at the conceptual stage of a design.Design/methodology/approachThe system has been developed in the CATIA V5 knowledge environment and is applied to structures made of composite materials. At the conceptual stage of the design process, a structure is often represented by simple surfaces. The system adds the details necessary to accurately estimate weight and manufacturing cost using geometry and process‐based techniques. Knowledge captured from an expert was used to construct the knowledge base in the system.FindingsIt has been found that the system can provide continuous tracking of the weight and cost as the design evolves. Structural FEA and optimisation using MSC.NASTRAN have been integrated into the design process to enables the designer to conduct “what‐if” analyses to explore different design options involving geometry parameters such as the internal configuration of the structure.Originality/valueThe paper demonstrates that tools embedded in CAD systems can be expected to be able to facilitate the task of estimation of weight and manufacturing cost at the conceptual stage of the design process.

Publisher

Emerald

Reference21 articles.

1. Bader, M.G. (2002), “Selection of composite materials and manufacturing routes for cost‐ effective performance”, Composites Part A, Vol. 33 No. 7, pp. 913‐34.

2. Baker, A., Dutton, S. and Kelly, D. (Eds) (2004), Composite Materials for Aircraft Structures, 2nd ed., AIAA, New York, NY.

3. Bao, H.P. (2000), “In‐depth survey of cost/time estimating models”, paper presented at Seminar, Multidisciplinary Optimization Branch, NASA Langley Research Center, July.

4. Bruhn, E.F. (1965), Analysis and Design of Flight Vehicle Structures, Tri‐State Offset Company, Cincinnati, OH, Ch. A‐17.

5. CATIA V5 R12 (2003), HTML Online Documentation, Dassault Systems, Cedex.

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