Current issue
Online first
Archive
About the Journal
Aims and scope
Publisher and Editorial
Advertising policy
For Authors
Paper review procedures
Procedures protecting authentic authorship of papers
Paper preparation manual
Plagiarism check
Publication ethics
Reviewers
APC
Editorial and Scientific Board
Contact
Reviewers
3E – A new paradigm for the development of civil aviation
1
Faculty of Mechanical Engineering and Aeronautics, Rzeszow University of Technology.
Submission date: 2020-01-25
Final revision date: 2020-04-06
Acceptance date: 2020-04-10
Publication date: 2020-05-20
Combustion Engines 2020,181(2), 3-10
KEYWORDS
airplaneelectric propulsionhybrid propulsiondistributed propulsionreduction of emission exhaustreduction of noisedecrease of fuel consumption
ABSTRACT
Introduction:
Nowadays, in civil aviation, issues related to improving efficiency, reducing the costs of air operations as well as the negative impact of air transport on the environment are of increasing importance. These ideas allow the formulation of the paradigm relating to the development of air transport – ‘more Efficiently, more Economically, more Eco-friendly – 3E’. The article presents in a cross-sectional and synthetic way research conducted by leading scientific centres around the world as well as prototype aviation constructions designed by companies from the aviation industry. Benefits and disadvantages of future propulsions, such as purely electric, hybrid and distributed propulsions, were presented. Conclusions were formulated regarding further possible directions of civil aviation development, taking into account the improvement of its efficiency as well as economic and ecological indicators.
Nowadays, in civil aviation, issues related to improving efficiency, reducing the costs of air operations as well as the negative impact of air transport on the environment are of increasing importance. These ideas allow the formulation of the paradigm relating to the development of air transport – ‘more Efficiently, more Economically, more Eco-friendly – 3E’. The article presents in a cross-sectional and synthetic way research conducted by leading scientific centres around the world as well as prototype aviation constructions designed by companies from the aviation industry. Benefits and disadvantages of future propulsions, such as purely electric, hybrid and distributed propulsions, were presented. Conclusions were formulated regarding further possible directions of civil aviation development, taking into account the improvement of its efficiency as well as economic and ecological indicators.
REFERENCES (37)
1.
AYAR, M., GULEREN, K.M, KARAKOC, T. Motor selection process with ahp on mini electric UAV. International Symposium on Electric Aviation and Autonomous Systems (ISEAS), 2018.
2.
BREJLE, B., MARTINS, J. Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches. Aerospace Sciences: article in progress; https://doi.org/10.1016/j.paer....
3.
DE VRIES, R. Preliminary sizing of a hybrid-electric passenger aircraft featuring over-the-wing distributed-propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019....
4.
DONATEO, T., SPEDICANTO, L. Fuel economy of hybrid electric flight. Applied Energy. 2017, 206, 723-738.
5.
FERMANN, Y. et al. Hybrid-electric motive power systems for commuter transport applications. ICAS 2016.
7.
FINGER, F.D. et al. A review of configuration design for distributed propulsion transitioning VTOL aircraft. 2017 Asia-Pacific International Symposium on Aerospace Technology (APISAT2018).
8.
FINGER, F.D. et al. On aircraft design under the consideration of hybrid-electric propulsion systems. 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT2018).
9.
FINGER, F.D., BRAUN, C. Case studies in initial sizing for hybrid-electric general aviation aircraft. 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. https://doi.org/10.2514/6.2018....
10.
FINGER, F.D., BRAUN, C. Impact of engine failure con-straints on the initial sizing of hybrid-electric GA aircraft. AI-AA Scitech 2019 Forum, San Diego. https://doi.org/10.2514/6.2019....
11.
FINGER, F.D., BRAUN, C., CEES, B. Impact of electric propulsion technology and mission requirements on the performance of VTOL UAVs. CEAS Aeronautical Journal. 2019, 10, 827-843.
12.
GEISS, I., STROHMAYER, A., et al. Optimized operation strategies for serial hybrid-electric aircraft aviation technolo-gy. Integration, and Operations Conference 2018. https://doi.org/10.2514/6.2018....
13.
FINGER, F.D., CEES, B.,BRAUN, C., Initial sizing methodology for hybrid-electric general aviation aircraft. Journal of Aircraft. 2019 (published online). https://doi.org/10.2514/1.C035....
14.
GOTTEN, F., FINGER, F.D., BRAUN, C. Empirical correlations for geometry build-up of fixed wing unmanned air. 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT2018).
15.
HOELZEN, J. et al. Conceptual design of operation strategies for hybrid electric aircraft. Energies. 2018, 11/217. https://doi.org/10.3390/en1101....
16.
HOELZEN, J. et al. Hybrid electric aircraft propulsion case study for skydiving mission. Aerospace. 2017, 4/45. https://doi.org/10.3390/aerosp....
17.
ISIKVEREN, A. The method of quadrant based algorithmic nomographs for hybrid/electric aircraft pre-design. Journal of Aircraft. 2017. https://doi.org/10.2514/1.C034....
18.
KAI, N. et al. Electrical and electronic technologies in more- electric aircraft: a review. IEEE Access. 2019. https://doi.org/10.1109/ACCESS....
19.
KIRNER, R. et al. An assessment of distributed propulsion: Part B – Advanced propulsion system architectures for blended wing body aircraft configurations. Aerospace Science and Technology. 2016, 50, 212-219.
20.
KUŹNIAR, M., ORKISZ, M. Analysis of the application of distributed propulsion to the AOS H2 motor glider. Journal of Kones. 2019, 26(2), 85-92.
21.
LIU, C., DOULGERIS, G., PANAGIOTIS, L. et al. Turboelectric distributed propulsion system modelling for hybrid-wing-body aircraft. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2012
22.
LIU, C., XIAYI, S. Method to explore the design space of a turbo-electric distributed propulsion system. Journal Aerospace Engineering. 2016. https://doi.org/10.1061/(ASCE)....
23.
ŁUKASIK, B. Analysis of the possibility of using full-electric, hybrid and turbo-electric technologies for future aircraft propulsion systems, in terms of mission energy con-sumption, NOx/CO2 emission and noise reduction. Doctoral Thesis. Instytut Lotnictwa 2018.
24.
PAWLAK, M., KUŹNIAR, M. Analysis of the wind dependent duration of the cruise phase on jet engine exhaust emissions. Journal of Kones. 2018, 25(3), 371-376.
25.
PAWLAK, M., MAJKA, A., KUŹNIAR, M. et al. Emission of selected exhaust compounds in jet engines of a jet aircraft in cruise phase. Combustion Engines. 2018, 173(2), 67-72.
26.
PAWLAK, M., KUŹNIAR, M. Determination of CO2 emis-sions for selected flight parameters of a business jet aircraft. Journal of Kones. 2019, 26(3), 155-163.
27.
PAWLAK, M., KUŹNIAR, M. Problematyka emisji toksycznych składników spalin silników lotniczych. Autobusy. 2017, 12, 338-344.
28.
PAWLAK, M., MAJKA, A., KUŹNIAR, M. et al. Analysis of wind impact on emission of selected exhaust compounds in jet engines of a business jet aircraft in cruise phase. Combustion Engines. 2018, 173(2), 55-60.
29.
PAWLAK, M. Metoda modelowania emisji związków szkodliwych w spalinach silników odrzutowych samolotów pasażerskich w warunkach przelotowych. Uniwersytet Morski w Gdyni 2019.
30.
RINGS, R, FLINGER, F.D. et al. Sizing studies of light aircraft with parallel hybrid propulsion systems. 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT2018).
31.
STOLL, A.M., BEVIRT, J., MOORE, M. et al. Drag reduc-tion through distributed electric aviation technology. Integration, and Operations Conference. 2014.
32.
VRATNY, P., HORNUNG, M. Sizing considerations of an electric ducted fan for hybrid energy aircraft. Transportation Research Procedia. 2018. https://doi.org/10.1016/j.trpr....
CITATIONS (8):
1.
Numerical Analysis of the Influence of Distributed Propulsion System on the Increase of the Lift Force Coefficient
Michal Kuzniar, Arkadiusz Bednarz, Marek Orkisz
AIAA Propulsion and Energy 2020 Forum
Michal Kuzniar, Arkadiusz Bednarz, Marek Orkisz
AIAA Propulsion and Energy 2020 Forum
2.
Effect of Energy Consumption Reduction on the Decrease of CO2 Emissions during the Aircraft’s Flight
Małgorzata Pawlak
Energies
Małgorzata Pawlak
Energies
3.
A rotating piston engine with electric generator in serial hybrid propulsion system
for use in light aircraft
Maciej KALWARA, Michał KUŹNIAR, Marek ORKISZ
Combustion Engines
Maciej KALWARA, Michał KUŹNIAR, Marek ORKISZ
Combustion Engines
4.
An assessment of the transient effect on helicopter main rotor stability and power demand
Radosław Raczyński, Ksenia Siadkowska, Karol Ścisłowski, Mirosław Wendeker
Combustion Engines
Radosław Raczyński, Ksenia Siadkowska, Karol Ścisłowski, Mirosław Wendeker
Combustion Engines
5.
The Effects of the Use of Algae and Jatropha Biofuels on Aircraft Engine Exhaust Emissions in Cruise Phase
Małgorzata Pawlak, Michał Kuźniar
Sustainability
Małgorzata Pawlak, Michał Kuźniar
Sustainability
6.
Comparison of Pollutants Emission for Hybrid Aircraft with Traditional and Multi-Propeller Distributed Propulsion
Michał Kuźniar, Małgorzata Pawlak, Marek Orkisz
Sustainability
Michał Kuźniar, Małgorzata Pawlak, Marek Orkisz
Sustainability
7.
Review of the hybrid gas - electric aircraft propulsion systems versus alternative systems
Agata Kuśmierek, Cezary Galiński, Wieńczysław Stalewski
Progress in Aerospace Sciences
Agata Kuśmierek, Cezary Galiński, Wieńczysław Stalewski
Progress in Aerospace Sciences
8.
Aerodynamic optimisation of flat-upper-surface wing
Wienczyslaw Stalewski, Pamela Bugała, Cezary Galinski
Aircraft Engineering and Aerospace Technology
Wienczyslaw Stalewski, Pamela Bugała, Cezary Galinski
Aircraft Engineering and Aerospace Technology
Share
RELATED ARTICLE
| eISSN: | 2658-1442 |
| ISSN: | 2300-9896 |
The scientific journal is financed under the Agreement 185/WCN/2019/1 from the funds of the Minister of Science and Higher Education
© 2006-2024 Journal hosting platform by Bentus
We process personal data collected when visiting the website. The function of obtaining information about users and their behavior is carried out by voluntarily entered information in forms and saving cookies in end devices. Data, including cookies, are used to provide services, improve the user experience and to analyze the traffic in accordance with the Privacy policy. Data are also collected and processed by Google Analytics tool (more).
You can change cookies settings in your browser. Restricted use of cookies in the browser configuration may affect some functionalities of the website.
You can change cookies settings in your browser. Restricted use of cookies in the browser configuration may affect some functionalities of the website.
