The aim of the paper is to provide an economically viable solution for the blade repair process. There is a continual increase in the repair market, which requires an increased level of specialised technology to reduce the repair cost and to increase productivity of the process.Design/methodology/approach – This paper introduces the aerospace component defects to be repaired. Current repair technologies including building‐up and machining technology are reviewed. Through the analysis of these available technologies, this paper proposes an integrated repair strategy through information integration and processes concentration.Findings – Provides detailed description and discussion for the repair system, including 3D digitising system, repair inspection, reverse engineering‐based polygonal modelling, and adaptive laser cladding and adaptive machining process.Originality/value – This paper describes a 3D non‐contact measurement‐based repair integration system, and provides a solution to create an individual blade‐oriented nominal model to achieve adaptive repair process (laser cladding/machining) and automated inspection.
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1 February 2005
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Research Article|
February 01 2005
Investigation of a 3D non‐contact measurement based blade repair integration system Available to Purchase
Jian Gao;
Jian Gao
School of Mechanical, Materials, Manufacturing Engineering and Management, The University of Nottingham, University Park, Nottingham, UK
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Janet Folkes;
Janet Folkes
School of Mechanical, Materials, Manufacturing Engineering and Management, The University of Nottingham, University Park, Nottingham, UK
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Oguzhan Yilmaz;
Oguzhan Yilmaz
School of Mechanical, Materials, Manufacturing Engineering and Management, The University of Nottingham, University Park, Nottingham, UK
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Nabil Gindy
Nabil Gindy
School of Mechanical, Materials, Manufacturing Engineering and Management, The University of Nottingham, University Park, Nottingham, UK
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Publisher: Emerald Publishing
Online ISSN: 1758-4213
Print ISSN: 1748-8842
© Emerald Group Publishing Limited
2005
Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (1): 34–41.
Citation
Gao J, Folkes J, Yilmaz O, Gindy N (2005), "Investigation of a 3D non‐contact measurement based blade repair integration system". Aircraft Engineering and Aerospace Technology: An International Journal, Vol. 77 No. 1 pp. 34–41, doi: https://doi.org/10.1108/00022660510576028
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