A Virtual Inspection Technique for Assessing the Dimensional Accuracy of Forged Compressor Blades Using FE Modeling and CMM Inspection

Jonathan Makem; Hengan Ou; Cecil Armstrong; A. Rennie; S.  Nikov

doi:10.1007/s12289-008-0073-5

A Virtual Inspection Technique for Assessing the Dimensional Accuracy of Forged Compressor Blades Using FE Modeling and CMM Inspection

Jonathan Makem, Hengan Ou, Cecil Armstrong, A. Rennie, S. Nikov

Research output: Contribution to journal › Article › peer-review

5 Citations (Scopus)

490 Downloads (Pure)

Abstract

This paper presents research for developing a virtual inspection system that evaluates the dimensional tolerance of forged aerofoil blades formed using the finite element (FE) method. Conventional algorithms adopted by modern coordinate measurement processes have been incorporated with the latest free-form surface evaluation techniques to provide a robust framework for the dimensional inspection of FE aerofoil models. The accuracy of the approach had been verified with a strong correlation obtained between the virtual inspection data and coordinate measurement data from corresponding aerofoil components.

Original language	English
Pages (from-to)	375-378
Number of pages	4
Journal	International Journal of Material Forming
Volume	1
Issue number	1
DOIs	https://doi.org/10.1007/s12289-008-0073-5
Publication status	Published - Dec 2008

ASJC Scopus subject areas

Materials Science(all)

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10.1007/s12289-008-0073-5

A Virtual Inspection Technique for Assessing the Dimensional Accuracy of Forged Compressor Blades Using FE Modeling and CMM InspectionAccepted author manuscript, 268 KB

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abstract = "This paper presents research for developing a virtual inspection system that evaluates the dimensional tolerance of forged aerofoil blades formed using the finite element (FE) method. Conventional algorithms adopted by modern coordinate measurement processes have been incorporated with the latest free-form surface evaluation techniques to provide a robust framework for the dimensional inspection of FE aerofoil models. The accuracy of the approach had been verified with a strong correlation obtained between the virtual inspection data and coordinate measurement data from corresponding aerofoil components.",

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