Principle of modernization of the aircraft An-148, An-158, and An-178 for improving their fuel efficiency and increasing competitiveness
DOI:
https://doi.org/10.15587/1729-4061.2020.204780Keywords:
aircraft family, aircraft engine, aerodynamic performance, altitude and speed characteristics, operating costsAbstract
In order to create new competitive advantages for the medium-haul aircraft An-148 and An-158, the application of the D-436-148FM engine for these aircraft has been considered. This would expand the operational range of aircraft flights, reduce noise on the ground, and harmful emissions from the engine.
A distinctive feature is the achieved thrust of the engine D-436-148FM undera maximum emergency mode, 19.4 % higher than the thrust of the engine D-436-148D. That was made possible by optimizing the fan, improving the combustion chamber, and turbine cascade.
The required amount of bench and flight tests has been performed. The engine certification is currently being completed. Specialists at the Antonov State Enterprise and Ivchenko-Progress State Enterprise studied the issue of installing the D-436-148FM engine on the An-148 and An-158 aircraft family. No changes to the design of the engine and aircraft are required. The engine is mounted on the same pylons without changes to the nacelle and engine bonnets.
Energy-dependent systems associated with the engine have been investigated. There is no need for the fundamental changes in related systems for the engine’s operational modes according to the Aircraft Flight Manual.
An engineering analysis of the comparison of flight-technical and flight-landing characteristics of the An-158 aircraft equipped with the engines D-436-148D and D-436-148FM has been performed. The data were obtained from the flight tests of the An-158 certified aircraft, taking into consideration the wind tunnel studies, flight tests of the An-178 aircraft, data from the An-158 Flight Manual, and the altitude and speed performance of the D-436-148D and D-436-148FM engines. The altitude and speed characteristics of the D-436-148FM engine, which have been calculated, were confirmed by the flight tests of the An-178 aircraft.
A feasibility study of engine replacement has been carried out, based on the comparison of the technical and economic characteristics of the An-158 aircraft equipped with the D-436-148D engine and D-436-148FM operated in various atmospheric conditions.
The principle of creating a family of aircraft of transport category of different configurations and purposes, based on a single engine, has been proposedReferences
- Eger, S. M., Mishin, V. F., Liseytsev, N. K. et. al.; Eger, S. M. (Ed.) (1983). Proektirovanie samoletov. Moscow: Mashinostroenie, 616.
- Loginov, V. V. (2009). Kompleksniy podhod po formirovaniyu tehnicheskogo oblika silovoy ustanovki, integriruemoy v planer, pri sinteze letatel'nogo apparata. Intehrovani tekhnolohiyi ta enerhozberezhennia, 2, 88–99.
- Palkin, V. A.; Skibin, V. A., Solonin, V. I. (Eds.) (2010). Raboty vedushchih aviadvigatelestroitel'nyh kompaniy v obespechenie sozdaniya perspektivnyh aviatsionnyh dvigateley (analiticheskiy obzor). Moscow: TSIAM, 678.
- Palkin, V. A. (2019). Review of works in the USA and Europe on aero engines for civil aircraft of 2020...2040’s. Aviatsionnye dvigateli, 3 (4), 63–83.
- Annex 16 to the Convention on International Civil Aviation - Environmental Protection (2014). Vol. 2, 3rd Edition, Amendment 8 - Aircraft Engine Emissions. ICAO.
- International Air Transport Association IATA (2013). IATA Technology Roadmap.
- Benzakein, M. J. (2014). What does the future bring? A look at technologies for commercial aircraft in the years 2035–2050. Propulsion and Power Research, 3 (4), 165–174. doi: https://doi.org/10.1016/j.jppr.2014.11.004
- Abbas, A., de Vicente, J., Valero, E. (2013). Aerodynamic technologies to improve aircraft performance. Aerospace Science and Technology, 28 (1), 100–132. doi: https://doi.org/10.1016/j.ast.2012.10.008
- European Aviation in 2040 - Challenges of growth. Annex 1 - Flight Forecast to 2040 (2017).
- European Aviation Environmental Report 2016. Available at: https://ec.europa.eu/transport/sites/transport/files/european-aviation-environmental-report-2016-72dpi.pdf
- Aviation Strategy for Europe. Available at: https://ec.europa.eu/transport/modes/air/aviation-strategy_en#package_detail
- FLYING IN 2050. Available at: http://www.academie-air-espace.com/upload/doc/ressources/CP-2050-VOLUME2.pdf
- Haselbach, F. (2019). Key Technologies for the next Generation of Civil Aircraft Engines. ISABE-2019-24044_44. ISABE.
- Whurr, J., Hepperle, M., Donus, F., Tantot, N. (2019). An Overview of the ENOVAL Project: Definition and analysis of advanced low specific thrust propulsion systems and technologies for year 2025-30 civil aircraft. ISABE-2019-24260. ISABE.
- Sieber, J., Merkl, E. (2017). ENOVAL Low Pressure System Technologies for Ultra High Bypass Ratio Engines. ISABE-2017-21392. ISABE.
- ENOVAL Technology Brochure – Providing the Next Steps in Engine Technologies (2018). ENOVAL consortium.
- Commercial Engines 2018. Turbofan Focus (2018). FlightGlobal.
- Samolet An-158. Letnye harakteristiki. IA No. RIO 11 24-10 (2010). Kyiv.
- Samolet An-158. Letnoe rukovodstvo (2010).
- Yugov, O. K., Selivanov, O. D. (1989). Osnovy integratsii samoleta i dvigatelya. Moscow: Mashinostroenie, 304.
- Borgest, N. M., Aleev, R. H., Aksanjan, P. A., Gromov, A. A. (2012). Automated construction of a 3D plane model at the stage of technical proposals. Vestnik of the Samara State Aerospace University, 4 (35), 139–148.
- Kwon, E.-Y., Leblanc, R., Garem, J.-H. (2001). Experimental investigation of sonic jet flows for wing/nacelle integration. KSME International Journal, 15 (4), 522–530. doi: https://doi.org/10.1007/bf03185113
- Myalitsa, A. K., Malashenko, L. A., Grebenikov, A. G. et. al. (2010). Razrabotka avanproekta samoleta. Kharkiv: Nats. aerokosmicheskiy un-t “KhAI”, 233.
- Lukovnikov, A. V. (2008). Kontseptual'noe proektirovanie silovyh ustanovok letatel'nyh apparatov v mnogodistsiplinarnoy postanovke. Vestnik MAI, 15 (3), 34–43.
- Hughes, C., Van Zante, D., Heidmann, J. (2011). Aircraft Engine Technology for Green Aviation to Reduce Fuel Burn. 3rd AIAA Atmospheric Space Environments Conference. doi: https://doi.org/10.2514/6.2011-3531
- Antonov. Available at: https://www.antonov.com/en
- D-436-148FM Turbofan. Available at: http://ivchenko-progress.com/?portfolio=турбореактивный-двухконтурный-двига&lang=ua
- Raspolagaemye vysotno-skorostnye harakteristiki dvigatel'noy ustanovki samoleta An-158 s dvigatelyami D-436-148. T/O No. 158.01.6463.268 (2009). Kyiv.
- Raspolagaemye vysotno-skorostnye harakteristiki dvigatel'noy ustanovki samoleta An-158 s dvigatelyami D-436-148FM s soplom 6800 sm2, s/z No. 4/738 ot 09.10.2019 g.
- Levickiy, S. V., Levickaya, E. V. (2014). The methods of assessment of transportation efficiency of a passenger aircraft. Civil Aviation High Technologies, 205, 99–106. Available at: https://avia.mstuca.ru/jour/article/view/636/554
- Tinyakov, D. V. (2013). Vliyanie chastnyh kriteriev effektivnosti nesushchih poverhnostey samoletov transportnoy kategorii na velichinu kreyserskogo aerodinamicheskogo kachestva. Voprosy proektirovaniya i proizvodstva konstruktsiy letatel'nyh apparatov, 2, 18–24. Available at: http://nbuv.gov.ua/UJRN/Pptvk_2013_2_4
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2020 Volodymyr Shmyrov, Vyacheslav Merkulov, Vasyl Loginov
This work is licensed under a Creative Commons Attribution 4.0 International License.
The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.
A license agreement is a document in which the author warrants that he/she owns all copyright for the work (manuscript, article, etc.).
The authors, signing the License Agreement with TECHNOLOGY CENTER PC, have all rights to the further use of their work, provided that they link to our edition in which the work was published.
According to the terms of the License Agreement, the Publisher TECHNOLOGY CENTER PC does not take away your copyrights and receives permission from the authors to use and dissemination of the publication through the world's scientific resources (own electronic resources, scientometric databases, repositories, libraries, etc.).
In the absence of a signed License Agreement or in the absence of this agreement of identifiers allowing to identify the identity of the author, the editors have no right to work with the manuscript.
It is important to remember that there is another type of agreement between authors and publishers – when copyright is transferred from the authors to the publisher. In this case, the authors lose ownership of their work and may not use it in any way.