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Clean Sky research and demonstration programmes for next-generation aircraft engines

Published online by Cambridge University Press:  09 July 2018

Jean-François Brouckaert*
Affiliation:
Clean Sky Joint Undertaking, Brussels, Belgium
François Mirville
Affiliation:
Safran Aircraft Engines, Moissy-Cramayel, France
Kevin Phuah
Affiliation:
Rolls-Royce plc, Derby, UK
Peter Taferner
Affiliation:
MTU Aero Engines AG, Munich, Germany

Abstract

The Clean Sky Joint Undertaking is currently managing two large-scale research and innovation programmes under FP7 and Horizon 2020 to contribute to the strengthening of the European aeronautical sector ensuring global leadership and competitiveness. This paper describes the research and demonstration programmes in Clean Sky (2008–2017) and Clean Sky 2 (2014–2024) related to propulsion technologies for the next-generation aircraft. The bulk of this work is addressed in Clean Sky 1 under the “Sustainable And Green Engines” (SAGE) programme and under the “ENGINES” programme in Clean Sky 2. The High-Level Objectives are described for each engine architecture as well as the targets in terms of CO2 and noise reduction versus a year 2000 reference unless stated otherwise. An overview of the new engine concepts that would satisfy the ACARE objectives is presented, including the main technologies which are to be developed to ensure the successful demonstration of each of those new engine concepts.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 2018 

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References

REFERENCES

1.Tantot, N. and Julliard, J. From turbojet to innovative architectures: Open rotor and contra rotative fan engines, Von Karman Institute Lecture Series, Aero-engine design: From state-of-the-art turbofans towards innovative architectures, 3–7 March 2008, Dénos, R. and Paniagua, G. (Eds).Google Scholar
2.Bittar, B., Bocquet, D., Desaulty, M. and Doussinault, M. Project Sage2: Enabling Open Rotor Technologies, ISABE 2011, 12–16 September 2011, Gothenburg, Sweden.Google Scholar
3.Bouty, E., Cheftel-Py, B. and Paty, G. SAGE5 Cleansky's approach to greener helicopter turboshafts, Proceedings of the XX International Symposium on Air Breathing Engines, 12–16 September 2011, Gothenburg, Sweden, pp 736-741.Google Scholar
4.Cortes, J., Iturriza, I., Aristizabal, M., Attallah, M. and Loretto, M. Effect of HIP temperature and post-HIP heat treatments on coincidence site lattices and twin boundaries in IN718, Powder Metallurgy World Congress, 9–13 September 2016, Hamburg, Germany.Google Scholar
5.Segurado, J., Cruzado, A., Llorca, J., Lucarini, S., Ostolaza, K. and Linaza, A. Microstructure dependent material models: Application to wrought 718 alloy, XXIII International Symposium on Air Breathing Engines, 3–8 September 2017, Manchester, UK.Google Scholar
6.Pacey, M. N. and Peace, A. Project SAGE3: Towards cleaner quieter turbofans, Proceedings of the XX International Symposium on Air Breathing Engines, 12–16 September 2011, Gothenburg, Sweden, pp 717-726.Google Scholar
7.Stegmaier, K., Carpintero Rogero, E. and Wackers, P. Y. SAGE 4 geared turbofan demonstrator, Proceedings of the XX International Symposium on Air Breathing Engines, 12–16 September 2011, Gothenburg, Sweden, pp 727-735.Google Scholar
8.Fuss, U. and Parry, A. B. SAGE1 demonstrator: Enabling open rotor technologies, Proceedings of the XX International Symposium on Air Breathing Engines, 12–16 September 2011, Gothenburg, Sweden, pp 752-763.Google Scholar