Hostname: page-component-cd9895bd7-dk4vv Total loading time: 0 Render date: 2024-12-22T10:24:29.679Z Has data issue: false hasContentIssue false
  • English
  • Français

Turbo-electric propulsive fuselage aircraft BLI benefits: A design space exploration using an analytical method

Published online by Cambridge University Press:  16 April 2020

P. Giannakakis Open the ORCID record for P. Giannakakis [Opens in a new window] ,
C. Pornet  and
A. Turnbull
P. Giannakakis*
Affiliation:
Energy and Propulsion Safran Tech Châteaufort France
C. Pornet
Affiliation:
Energy and Propulsion Safran Tech Châteaufort France
A. Turnbull
Affiliation:
Energy and Propulsion Safran Tech Châteaufort France
*
[email protected]
Get access Rights & Permissions [Opens in a new window]

Abstract

Turbo-electric propulsive fuselage aircraft featuring Boundary-Layer Ingestion (BLI) are considered promising candidates to achieve the emissions reduction targets set for aviation. This paper presents an analytical method capable of estimating the BLI benefit at aircraft level, enabling a quick exploration of the propulsive fuselage design space. The design space exploration showed that the assumptions regarding the underwing turbofans and BLI fan mass estimation can have an important impact on the final fuel burn estimation. The same applies to the total efficiency assumed for the electric transmission, the range of the aircraft mission, and the propulsive efficiency of the engines used as benchmark. The regional jet and short- to medium-range aircraft classes seem to be the most promising as the ingested drag and power saving are among the largest, with long-range aircraft being just behind. The future introduction of advanced technologies, which target the reduction of vortex and wave dissipation at aircraft level, could increase the potential benefit of propulsive fuselage BLI. On the other hand, the potential benefit would be decreased if more efficient and lighter ultra high bypass ratio engines were used as benchmark.

Keywords

Boundary-layer ingestionPropulsionTurbo-electricPerformance evaluation
Type
Research Article
Information
The Aeronautical Journal , Volume 124 , Issue 1280 , October 2020 , pp. 1523 - 1544
Copyright
© The Author(s) 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

Advisory Council for Aviation Research and Innovation in Europe, Strategic Research & Innovation Agenda, Volume 1, 2017.Google Scholar
Isikveren, A.T., Seitz, A., Bijewitz, J., Mirzoyan, A., Isyanov, A., Grenon, R., Atinault, O., Godard, J.-L. and Stückl, S.Distributed propulsion and ultra-high by-pass rotor study at aircraft level, The Aeronautical Journal, 2015, 119, pp 1327–1376.CrossRefGoogle Scholar
Welstead, J. and Felder, J. Conceptual design of a single-aisle turboelectric commercial transport with fuselage boundary layer ingestion, 54th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, no. AIAA 2016-1027, 2016.CrossRefGoogle Scholar
Bowman, C.L., Felder, J.L. and Marien, T.V. Turbo- and hybrid-electrified aircraft propulsion for commercial transport, AIAA/IEEE Electric Aircraft Technologies Symposium, AIAA Propulsion and Energy Forum, 2018.CrossRefGoogle Scholar
Hall, D.K., Dowdle, A.P., Gonzalez, J.J., Trollinger, L. and Thalheimer, W. Assessment of a boundary layer ingesting turboelectric aircraft configuration using signomial programming, Aviation Technology, Integration, and Operations Conference, AIAA Aviation Forum, 2018.CrossRefGoogle Scholar
Giannakakis, P., Maldonado, Y.-B., Tantot, N., Frantz, C. and Belleville, M. Fuel burn evaluation of a turbo-electric propulsive fuselage aircraft, AIAA Propulsion and Energy Forum, Indianapolis, IN, August 2019.CrossRefGoogle Scholar
Drela, M.Power balance in aerodynamic flows, AIAA Journal, 2009, 47, (7), pp 1761–1771.CrossRefGoogle Scholar
Sato, S. The Power Balance Method for Aerodynamic Performance Assessment, PhD thesis, Massachusetts Institute of Technology, 2012.Google Scholar
Hall, D.K., Huang, A.C., Uranga, A., Greitzer, E.M., Drela, M. and Sato, S.Boundary layer ingestion propulsion benefit for transport aircraft, Journal of Propulsion and Power, 2017, 33, (5), pp 1118–1129.CrossRefGoogle Scholar
Uranga, A., Drela, M., Greitzer, E.M., Hall, D.K., Titchener, N.A., Lieu, M.K., Siu, N.M., Casses, C., Huang, A.C., Gatlin, G.M. and Hannon, J.A. Boundary layer ingestion benefit of the D8 transport aircraft, AIAA Journal, 2017, 55, (11), pp 3693–3708.CrossRefGoogle Scholar
Smith, L.H.Wake ingestion propulsion benefit, Journal of Propulsion and Power, 1993, 9, (1), pp 74–82.CrossRefGoogle Scholar
Steiner, H.-J., Seitz, A., Wieczorek, K., PlÖtner, K., Isikveren, A.T. and Hornung, M. Multidisciplinary design and feasibility study of distributed propulsion systems, 28th International Congress of the Aeronautical Sciencies, no. Paper ICAS 2012-1.7.5, September 2012.Google Scholar
Hall, D.K. Analysis of Civil Aircraft Propulsors with Boundary Layer Ingestion,. PhD thesis, Massachusetts Institute of Technology, 2015.Google Scholar
Felder, J., Kim, H., Brown, G. and Kummer, J. An examination of the effect of boundary layer ingestion on turboelectric distributed propulsion systems, 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Aerospace Sciences Meetings, AIAA, January 2011.CrossRefGoogle Scholar
Giannakakis, P., Laskaridis, P. and Pilidis, P.Effects of off-takes for aircraft secondary-power systems on jet engine efficiency, Journal of Propulsion and Power, 2011, 27, (5), pp 1024–1031.CrossRefGoogle Scholar
Guha, A., Boylan, D. and Gallagher, P.Determination of optimum specific thrust for civil aero gas turbine engines: a multidisciplinary design synthesis and optimisation, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2013, 227, (3), pp 502–527.CrossRefGoogle Scholar
Greitzer, E.M., Bonnefoy, P., DelaRosaBlanco, E., Dorbian, C., Drela, M., Hall, D., Hansman, R., Hileman, J., Liebeck, R., Lovegren, J., Mody, P., Pertuze, J., Sato, S., Spakovszky, Z., Tan, C., Hollman, J., Duda, J., Fitzgerald, N., Houghton, J., Kerrebrock, J., Kiwada, G., Kordonowy, D., Parrish, J., Tylko, J., Wen, andLord, W. N+ 3 aircraft concept designs and trade studies. volume 2: appendices-design methodologies for aerodynamics, structures, weight, and thermodynamic cycles, Tech Rep CR 2010-216794, NASA, 2010.Google Scholar
Coles, D.The law of the wake in the turbulent boundary layer, Journal of Fluid Mechanics, 1956, 1, (2), pp 191–226.CrossRefGoogle Scholar
Fefermann, Y., Maury, C., Level, C., Zarati, K., Salanne, J.-P., Pornet, C., Thoraval, B. and Isikveren, A. T. Hybrid-electric motive power systems for commuter transport applications, 30th Congress of the International Council of the Aeronautical Sciences (ICAS), No. ICAS-2016-0438, Daejeon, Korea, 2016.Google Scholar
Bijewitz, J., Seitz, A., Isikveren, A.T. and Hornung, M.Multi-disciplinary design investigation of propulsive fuselage aircraft concepts, Aircraft Eng & Aerospace Tech, 2016, 88, pp 257–267.10.1108/AEAT-02-2015-0053CrossRefGoogle Scholar
Schmidt, M., PlÖtner, K.O., Pornet, C., Isikveren, A.T. and Hornung, M. Contributions of cabin related and ground operation technologies towards flightpath 2050, Deutscher Luft- und Raumfahrtkongress 2013 (DGLR), No. Paper 301299, Stuttgart, Germany, September 2013.Google Scholar