Author:
Yilmaz Oguzhan,Noble Dominic,Gindy Nabil N.Z.,Gao Jian
Abstract
PurposeThis paper discusses research on machining and repairing of turbomachinery components which are generally complex geometries and made up of difficult to machine materials (nickel super alloys or titanium alloys).Design/methodology/approachThe approaches, methods and methodologies used for machining and repairing of blades are reviewed as well as the comparisons between them are made.FindingsParticularly, the most recent blade machining and repair techniques using high flexible machine tools and industrial robots, are mentioned.Practical implicationsThe limitation of the approaches, methods and methodologies are given and supported by real practical application examples.Originality/valueThis paper presents a state of the art review of research in machining and repairing of turbomachinery components, which have been mainly done in the last decade. The paper act as a reference, gathering the works about turbomachinery components from a manufacturing point of view.
Reference75 articles.
1. Albert, M. (2003), “Rapid traverse: on the cusp – faster machining or finer surfaces”, MMS online, available at: www.mmsonline.com/articles/0403rt1.html.
2. Bariani, P.F., Bruschi, S., Masiero, S., Maurizio, A. and Zuttion, F. (2002), “Optimisation of the hot forging process of ST70AH turbine blades”, Advanced Technology of Plasticity, Proceedings of Seventh ICTP, Vol. 1, pp. 217‐22.
3. Bariani, P.F., Bruschi, S. and Dal Negro, T. (2004), “Integrating physical and numerical simulation techniques to design the hot forging process of stainless steel turbine blades”, International Journal of Machine Tools & Manufacture, Vol. 44 No. 9, pp. 945‐51.
4. Bohez, E.L.J. (2002), “Five‐axis milling machine tool kinematic chain design and analysis”, International Journal of Machine Tools & Manufacture, Vol. 42, pp. 505‐20.
5. Bremer, C. (2000), “Adaptive strategies for manufacturing and repair of blades and blisks”, Proceedings of ASME Turbo Expo 2000: 45th ASME International Gas Turbine & Aeroengine Technical Congress, Munich.
Cited by
23 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献