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Application of a knowledge based design methodology to support fuselage panel design

Published online by Cambridge University Press:  03 February 2016

S. W. G. van der Elst ,
M. J. L. van Tooren ,
B. Vermeulen ,
C. L. Emberey  and
N. R. Milton
S. W. G. van der Elst
Affiliation:
S.W.G.vanderElst@tudelft.nl, Delft University of Technology, Delft, The Netherlands
M. J. L. van Tooren
Affiliation:
S.W.G.vanderElst@tudelft.nl, Delft University of Technology, Delft, The Netherlands
B. Vermeulen
Affiliation:
Fokker Aerostructures, Papendrecht, The Netherlands
C. L. Emberey
Affiliation:
Tacit Connexions, Wokingham, UK
N. R. Milton
Affiliation:
Tacit Connexions, Wokingham, UK
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Abstract

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Knowledge is a vital component of engineering design. Computer systems enriched with logic and engineering knowledge can support engineering design by automating repetitive and time-consuming processes. This automation is enabled using knowledge based engineering (KBE) techniques and can be obtained using dedicated KBE systems or augmented CAD systems, already pervasive throughout engineering industry. The development of these KBE applications is supported by a six-phase development process ranging from engineering process analysis to software development to business implementation. Distinctions and similarities exploiting alternative KBE platforms are addressed for each phase of the development process. An example KBE application is discussed, supporting the design of laminate aircraft fuselage panels. The implementation of the application is emphasised and five key-aspects required for a successful implementation are defined.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 114 , Issue 1159 , September 2010 , pp. 589 - 597
Copyright
Copyright © Royal Aeronautical Society 2010 

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