Integration of Conceptual Design and MOKA into CATIA v5: A Knowledge-Based Application for an Aircraft Y-Bolt Component

Pai Zheng; Víctor Hugo Torres; José Ríos; Gang Zhao

doi:10.4028/www.scientific.net/AMM.271-272.974

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 271-272Integration of Conceptual Design and MOKA into...

Integration of Conceptual Design and MOKA into CATIA v5: A Knowledge-Based Application for an Aircraft Y-Bolt Component

Abstract:

The design process comprises the Conceptual Phase, the Embodiment Phase and the Detail Design Phase in which commercial PLM/CAD systems mainly support the latter ones. This situation causes the discontinuity in the overall design information flow: Customer Needs (CNs) - Functional Requirements (FRs) – Design Parameters (DPs) – Key Characteristics (KCs) – Geometric Parameters (GPs). There is also a lack of knowledge reuse in routine design process, resulting in large cost-waste of the overall design process. Aiming to enhance the continuity of the design information flow and facilitate the knowledge reuse, this paper makes use of a knowledge-based framework to integrate conceptual design tools: Quality Function Deployment (QFD), Axiomatic Design (AD), Failure Mode and Effects Analysis (FMEA) and the MOKA methodology into CATIA v5 system. A knowledge-based application (KBA) on the large aircraft y-bolt component design is presented as a case study to validate the proposed framework. The result shows how this novel integrated framework and KBA system could benefit designers in a practical way.

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Periodical:

Applied Mechanics and Materials (Volumes 271-272)

Pages:

974-980

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.271-272.974

Citation:

Cite this paper

Online since:

December 2012

Authors:

Pai Zheng, Víctor Hugo Torres, José Ríos, Gang Zhao

Keywords:

AD, Catia V5, Failure Mode Effect Analysis (FMEA), KBA, MOKA, QFD

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