A virtual inspection framework for precision manufacturing of aerofoil components

• Published in: Computer aided design 2012-09, Vol.44 (9), p.858-874
• Main Authors: Makem, Jonathan E., Ou, Hengan, Armstrong, Cecil G.
• Format: Article
• Language: English
• Subjects: Aeroengine blades; Blades; Computer simulation; Coordinate measurement; Design engineering; Error analysis; Finite element modelling; Forging; Hot-forging; Inspection; Mathematical analysis; Mathematical models; Virtual inspection
• ISSN: 0010-4485; 1879-2685
• DOI: 10.1016/j.cad.2012.04.002

The finite element method plays an extremely important role in forging process design as it provides a valid means to quantify forging errors and thereby govern die shape modification to improve the dimensional accuracy of the component. However, this dependency on process simulation could raise significant problems and present a major drawback if the finite element simulation results were inaccurate. This paper presents a novel approach to assess the dimensional accuracy and shape quality of aeroengine blades formed from finite element hot-forging simulation. The proposed virtual inspection system uses conventional algorithms adopted by modern coordinate measurement processes as well as the latest free-form surface evaluation techniques to provide a robust framework for virtual forging error assessment. Established techniques for the physical registration of real components have been adapted to localise virtual models in relation to a nominal design model. Blades are then automatically analysed using a series of intelligent routines to generate measurement data and compute dimensional errors. The results of a comparison study indicate that the virtual inspection results and actual coordinate measurement data are highly comparable and the procedures for registration and virtual inspection are computationally efficient, validating the approach as an effective and accurate means to quantify forging error in a virtual environment. Consequently, this provides adequate justification for the implementation of the virtual inspection system in the virtual process design, modelling and validation of forged aeroengine blades in industry. ► The paper presents a virtual inspection framework to assess the accuracy of aero-engine. ► Both the 3–2–1 approach and the ICP method are developed for part registration. ► The ICP method achieves a better solution than the 3–2–1 approach in registration. ► A case study produces reveals a good correlation exists between the virtual inspection data and the actual measurement data.